EP0686763B1 - Fuel injection valve for internal combustion engines - Google Patents

Fuel injection valve for internal combustion engines Download PDF

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Publication number
EP0686763B1
EP0686763B1 EP95107718A EP95107718A EP0686763B1 EP 0686763 B1 EP0686763 B1 EP 0686763B1 EP 95107718 A EP95107718 A EP 95107718A EP 95107718 A EP95107718 A EP 95107718A EP 0686763 B1 EP0686763 B1 EP 0686763B1
Authority
EP
European Patent Office
Prior art keywords
control
piston
injection valve
pressure
control chamber
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP95107718A
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German (de)
French (fr)
Other versions
EP0686763A1 (en
Inventor
Marco A. Ganser
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Ganser Hydromag AG
Original Assignee
Ganser Hydromag AG
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Filing date
Publication date
Application filed by Ganser Hydromag AG filed Critical Ganser Hydromag AG
Priority to EP97112502A priority Critical patent/EP0807757A1/en
Publication of EP0686763A1 publication Critical patent/EP0686763A1/en
Application granted granted Critical
Publication of EP0686763B1 publication Critical patent/EP0686763B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M47/00Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure
    • F02M47/02Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure of accumulator-injector type, i.e. having fuel pressure of accumulator tending to open, and fuel pressure in other chamber tending to close, injection valves and having means for periodically releasing that closing pressure
    • F02M47/027Electrically actuated valves draining the chamber to release the closing pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M45/00Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/20Closing valves mechanically, e.g. arrangements of springs or weights or permanent magnets; Damping of valve lift
    • F02M61/205Means specially adapted for varying the spring tension or assisting the spring force to close the injection-valve, e.g. with damping of valve lift
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/30Fuel-injection apparatus having mechanical parts, the movement of which is damped
    • F02M2200/304Fuel-injection apparatus having mechanical parts, the movement of which is damped using hydraulic means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2547/00Special features for fuel-injection valves actuated by fluid pressure
    • F02M2547/001Control chambers formed by movable sleeves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/0012Valves
    • F02M63/0031Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
    • F02M63/0054Check valves
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/8593Systems
    • Y10T137/86389Programmer or timer
    • Y10T137/86405Repeating cycle

Definitions

  • the invention relates to a fuel injection valve for intermittent fuel injection into the combustion chamber an internal combustion engine according to the preamble of Claim 1.
  • Injectors of this type are for example from the Patents EP 0 228 578 or EP 0 426 205 are known.
  • the invention as characterized in the claims solves the task of creating a fuel injector, that ensures improved operating behavior and also extremely easy to manufacture and assemble is.
  • Fig.1 is a fuel injector 1 in one Position shown between two injection processes.
  • the Fuel injector 1 is over a High-pressure fuel connection 10 and via a Fuel return connection 12 with a high-pressure delivery device for the fuel and over electrical Connections 14 connected to an electronic control.
  • the high pressure conveyor and the electronic Controls are not shown in the drawing.
  • the housing of the fuel injection valve 1 is 15 designated. At the lower end is the housing 15 with a Union nut trained holding part 16, with at the upper end a corresponding retaining nut 17 screwed.
  • a nozzle body 18 is inserted, the Nozzle tip 19 protrudes from the holding part 16.
  • the Nozzle tip 19 is provided with a nozzle needle seat 20 and has a plurality of injection openings 21 in this area.
  • in the Nozzle body 18 is an injection valve member, axially adjustable nozzle needle 24 in one Needle guide bore 23 slidably.
  • the Injection openings 21 of the nozzle tip 19 are through a lower end 25 of the nozzle needle 24 can be locked.
  • the housing 15 has a central guide bore 29 provided, in which a control device 3 for control the adjustment movement of the injection valve member or Nozzle needle 24 is arranged.
  • the control device 3 is described in detail below with reference to FIG. 2.
  • the fuel is fed through the high pressure delivery device via the high-pressure fuel connection and a first short Fuel supply bore 31 in two in the housing 15 parallel to Guide bore 29 arranged high pressure supply lines 32.33 promoted.
  • the upper high pressure supply line 33 leads to the control device 3.
  • the lower high pressure supply line 32 is arranged obliquely in an intermediate plate 36 Connecting bore 35 to a nozzle body bore 26 connected in an annular space 27 in the nozzle body 18th flows.
  • the fuel does not pass from the annular space 27 Passages shown in more detail to the nozzle needle seat 20 and the injection openings 21.
  • the nozzle needle 24 is provided with a shoulder 28.
  • the intermediate plate 36 is opposite the housing 15 via a Pin 37 (there could also be two pins 37) positioned and sealing between the housing 15 and the nozzle body 18 arranged.
  • a Pin 37 (there could also be two pins 37) positioned and sealing between the housing 15 and the nozzle body 18 arranged.
  • One in a central bore 38 of the Intermediate plate 36 protruding upper part 39 of the nozzle needle 24 is operatively connected to an intermediate needle element 40 which on the other hand via a connecting rod 44 with a Control piston 50 of the control device 3 is connected.
  • a connecting rod 44 surrounding nozzle needle spring 47 arranged biased.
  • the control device 3 has one in the guide bore 29 control body 52 used in a stationary manner.
  • the control piston 50 is with an upper, stepped in diameter Piston part 51 provided.
  • the upper piston part 51 protrudes into one in the Guide bore 29 axially displaceable and tightly sliding arranged sleeve 64 into it.
  • Also between the piston part 51 and the inner diameter of the sleeve 64 are narrow Sliding fits provided.
  • the sleeve 64 is supported with a narrow annular sealing surface 66 on a lower End face 55 of the control body 52, on the other hand by a lock nut 54 screwed to the housing 15 in the guide bore 29 is axially fixed.
  • control body 52 In the lower area of the control body 52 is in the Housing 15 is an annular space 69, which has a transverse bore 68 the upper high pressure supply line 33 is connected. Of the Control body 52 has an annular space 69 corresponding Circumferential ring groove 67. The control body 52 is also included one opening into a first control room 70 Provided connecting bore 60, which via a Inlet throttle bore 58 with the circumferential ring groove 67 or with the annular space 69 and thus also with the high pressure supply line 33 is connected. The connection bore 60 narrows at the top into an outlet opening 59.
  • the first control space 70 is radial through the inner surface of FIG Sleeve 64, axially through the lower end face 55 of the Control body 52 and an upper end face 56 of the Piston part 51 limited.
  • the control body 52 is in the guide bore 29 of the Housing 15 installed in such a way that no significant leakage can take place. This will e.g. with a press fit or reached a tight sliding seat, but could also through other fuel-tight connections, for example realized using suitable sealing rings become.
  • the control device 3 also has an electromagnetic actuatable pilot valve 80, of which only in Fig.2 an armature 82 firmly connected to a pilot valve stem 81 can be seen.
  • an armature 82 firmly connected to a pilot valve stem 81 can be seen.
  • the exhaust throttle bore 59 via a flat valve seat 85 held in the closed position.
  • Electromagnet 86 of the pilot valve stem 81 by the force a compression spring 87 down into the valve flat seat 85 closing position pressed. This force is through a Adjustment screw 88 adjustable in size.
  • For Actuation of the pilot valve 80 or to raise the Pilot valve stem 81 from valve flat seat 85 receives one excitation coil 83 of the electromagnet assigned to armature 82 86 via the electrical connections 14 control pulses from the electronic control.
  • the high pressure part of the Fuel injector 1 i.e. in the Fuel feed hole 31, in both High pressure supply lines 32.33, in the annular spaces 27.69 and the same high pressure or in both control rooms 70, 74 Injection pressure, which can be up to over 1000 bar.
  • the end of the injection process is known to be done as quickly as possible.
  • the pilot valve 80 into its via the electromagnet 86 Brought to the closed position. Since the outlet opening 59 is closed again, increases in the first control room 70 Pressure on, and the control piston 50 is by the on the force acting on the upper end face 56 of the piston part 51 moved down.
  • the volume of the second control room 74 the fuel pressure in the second control room is increased 74 falls.
  • the sleeve 64 initially remains on the control body 52 pressed. At certain decrease in fuel pressure in the second control chamber 74, the sleeve 64 follows Piston movement; it should be noted that the spring 63 is relatively weakly biased, so that the pressure effect of the Spring 63 is negligible compared to Fuel pressure forces.
  • a Control device 4 is the sleeve 64 known from FIGS. 1 and 2 replaced by a sleeve 94.
  • the sleeve 94 has on the circumference several axially arranged ribs 95, whose Outside diameter a precisely defined radial annular gap 93 forms opposite the guide bore 29.
  • the ring groove 67 in Control body 52 and the annular space 69 in the housing 15 omitted.
  • Above the top rib 95 opens into the Guide bore 29 that supplying the high pressure fuel Cross bore 68 into it.
  • the sleeve is on the upper face 94 with a narrow, annular sealing surface 96.
  • the sealing surface 96 has a plurality of radial circumferentially distributed Wells 97 of shallow depth (approx. 0.02 - 0.03 mm), through which the fuel throttled from the pilot hole 29 and consequently from the transverse bore 68 to the first control chamber 70 arrives and the inlet throttle bore 58 of the from Fig.2 replace known control device 3.
  • the ribs 95 on the other hand, replace the one known from FIG second control room 74 and the high pressure supply line 33 built-in throttle 77.
  • the ribs 95 have sharp edges on to a regardless of the toughness of the fuel to achieve turbulent flow. By arranging several Ribs 95 in a row, the fuel pressure gradually reduced or the flow rate reduced. Thereby the annular gap can be dimensioned more generously.
  • the position of the sealing surface 96 in relation to the outside or Inner diameter of sleeve 94 may be necessary Contact pressure can be selected.
  • the same sealing surface 96 and / or the radial recesses 97 could also in the Sleeve 64 of Fig.2 can be used.
  • control device 4 is technically simpler than that in Fig. 1 and 2 illustrated embodiment. Otherwise it works same as already described.
  • a sleeve 98 guided closely sliding, the same as the sleeve 94 known from FIG. 3 with the Recesses 97 provided narrow sealing surface 96 Is provided.
  • the spring 63 is between the lower End face 65 of sleeve 98 and a housing shoulder 100 biased.
  • Ball check valve 103 Parallel to the guide bore 29 is in the housing 15 Housing bore 102 made in the one Ball check valve 103 is installed.
  • a lower one Valve seat element 104 of the ball check valve 103 has a bore 105 on the holes 106, 107 with the second control room 74 is connected.
  • One of the Ball 108 assigned to valve seat element 104 is moved over a second valve element 109 by the force of a spring 110 the valve seat member 104 is pressed.
  • the ball check valve 103 is by means of a locking pin 111, over which also the spring preload can be selected in the Housing bore 102 axially fixed. The connection of the second Control room 74 with the high pressure zone is thus over Ball check valve 103 manufactured.
  • a quick closing movement is the same as for Control device 3 reached in which the sleeve 98 at Downward movement of the control piston 50 and when the Fuel pressure in the second control room 74 under one certain size the connection of the high pressure system to the first control room 70 releases.
  • FIG. 5 shows a further alternative embodiment of the Control device shown and designated 6.
  • a bore seat valve 113 is installed in the housing bore 102.
  • the valve body 114 is with a Cross bore 116 and one perpendicular to cross bore 116 arranged throttle bore 117 provided.
  • the second Control room 74 is through the bores 107, 106, the Throttle bore 117 and the transverse bore 116 with the High pressure region connected.
  • Fig. 6 shows an alternative form of training in partial section of the fuel injector, designated 2 and a further control device 7 is equipped. From 1 to 5 already known, identical and parts with the same effect are again given the same reference numbers designated. Part of the control device 7 is for the better Understanding enlarged in Fig.7.
  • the fuel injector 2 has Housing 120 on that with a central guide bore 121st is provided for the control device 7.
  • Guide bore 121 is a spool 122 closely sliding axially displaceable.
  • the control piston points at the top 122 a piston part 123 with a reduced diameter.
  • the corresponding sales area is designated 126.
  • a piston shoulder 129 is formed to the connecting rod 124.
  • existing room 125 opens directly into the relatively short, first fuel supply bore 31 from High-pressure fuel connection 10.
  • the housing 120 itself has no more high pressure supply lines on the Designation shown in Fig.1 designated 32.33 were; there are also no further ring spaces or Cross bores made in the housing 120, which makes an extreme simple and technically advantageous housing 120 is realized.
  • the upper piston part 123 is on its upper face a recess 128 provided in the one in the control piston 122 made central connection bore 130 opens.
  • the connecting bore 130 is in the control piston 122 made cross bore 131 to the high-pressure fuel filled room 125 connected.
  • a control body 135 is stationary in the guide bore 121 used (pressed in, for example) by the already known lock nut 54 is axially fixed.
  • the Control body 135 is on its lower end face with a Recess 136 equipped into which the upper piston part 123th protrudes tightly.
  • a stepped diameter Part 137 of the recess 136 has a spring 138 arranged in it, via which a valve seat washer 140 to the upper one, with 127 designated annular end face of the upper piston part 123 is pressed.
  • the valve seat disk 140 has a central disc hole 141 on.
  • valve seat plate 140 and the plate hole 141 closing valve bodies 143 form a first flat valve seat 151.
  • the end face 127 of the piston part 123 and the valve seat plate 140 form a second valve flat seat 152 (see Fig. 7).
  • first control chamber 155 which passes radially through the upper piston part 123 on the one hand and the guide bore 121 is limited on the other hand.
  • an inlet throttle 133 is made, which in the Connecting bore 130 opens radially and a connection of the forms first control chamber 155 to the high-pressure fuel zone.
  • a second control chamber 156 is in the recess 136 of the Control body 135 formed above the piston part 123 and through the two valve flat seats 151, 152 from the system or High-pressure fuel zone in the illustrated Starting position separated between two injection processes held.
  • the mode of operation of the fuel injection valve 2 or of the control device 7 is as follows: When the pilot valve stem 81 is raised and electronically controlled in the same way as described above, the outlet opening 159 is opened. The fuel pressure in the first control room 155 drops. The control piston 122 is moved upward by the high fuel pressure acting on the piston shoulder 129 and prevailing in the space 125. The injection valve member opens the injection openings to the combustion chamber of the internal combustion engine in the manner already described. When the control piston 122 together with the valve seat disk 140 is raised, the volume of the second control chamber 156 is reduced, the pressure increases with this pumping action and counteracts the opening movement in the desired manner. This results in a slow opening process.
  • valve body 143 is pressed down against the system pressure prevailing in the recess 128 and the force of the spring 144 via the disk hole 141 and the first flat valve seat 151 is opened, as a result of which the opening process of the control piston 122 and consequently the injection valve member is accelerated.
  • Exhaust port 159 becomes through the pilot valve stem closed again, so the pressure in the first control room rises 155 again.
  • the pressure in the second control room 156 is adjusted again to the system high pressure.
  • the spring 144 presses the valve body 143 against the valve seat plate 140 which on the other hand is loaded by the force of the spring 138.
  • Of the first valve flat seat 151 is closed.
  • the control piston 122 is moved down.
  • the volume of the second control chamber 156 is increased, the Pressure drops.
  • the pressure in the second control room 156 is one falls below a certain value at which insufficient Pressure force exerted on the valve seat plate 140 from above the second valve flat seat 152 is opened.
  • the fuel over the control piston 122 the end face 127 is additionally accelerated downwards. In in this way a quick closing of the Injector member performed.
  • the fuel injector 2 according to the invention brings in addition to the simplification of construction and assembly technology also has the advantage of minimal leakage occur.
  • the one from the exhaust throttle bore 159 escaping fuel is in turn through the drain hole 90 fed to the fuel return port.
  • valve body 143 with the throttle bore 142 and the Omit spring 144 and valve seat disk 140 directly with provided as a throttle disc hole 141 so would the operation of the control device 7 of those correspond to the control device 3 from FIG. That as Throttle-formed disc hole 141 would then become the throttle 77 corresponding to FIG. 2, which correspond to the second control space 156 (in Fig. 2 control room 74) connects to the high pressure zone.
  • control device 7 of the second alternative variant to the control device 3 according to FIG. 2 With additional omission of the valve seat plate 140 and the Spring 138 would control device 7 of the second alternative variant to the control device 3 according to FIG. 2 (with large or missing throttle 77) correspond, since in this If the second control room 156 also directly with the High pressure zone would be connected.
  • FIG Control device 8 shown for the Fuel injector 2 can be used. From Fig. 6 and 7 known parts are again the same Designated reference numbers.
  • control piston 122 has no in this case Diameter of the piston part, but it is with an upper end face 161 is completed.
  • a Intermediate piston 162 arranged in the recess 136 of the Control body 135 protrudes closely sliding.
  • a first annular control chamber 160 is radial through the Intermediate piston 162 and the guide bore 121, axially through the upper end face 161 of the control piston 122 and the lower end face 139 of the control body 135 limited.
  • a second control chamber 165 is located in recess 136 above the intermediate piston 162 or above an upper one End face 163 of the intermediate piston 162.
  • the intermediate piston 162 is provided with a shoulder 166.
  • a spring 167 surrounding the intermediate piston 162 is on the shoulder 166 on the one hand and on the lower end face 139 of the Control body 135 supported on the other.
  • the intermediate piston 162 has a narrow, annular sealing surface 168 at the bottom that of the upper end face 161 of the control piston 122 assigned.
  • the diameter of the sealing surface is 168 smaller than the diameter of the recess 136 or than that Diameter of the upper end face 163 of the intermediate piston 162.
  • the intermediate piston 162 is from the bottom with a central one Provide recess 170. Between the recess 170 and the second control chamber 165 is one in the intermediate piston Connection hole 174 made, the one in the recess arranged ball valve 171 is assigned.
  • a valve spring 173 is in the recess 170 by means of a in a bore 180 of the intermediate piston 162 pressed or screwed securing element 172 biased.
  • the Securing element 172 has a central connecting bore 182 over which the space of the recess 170 with the Connection bore arranged centrally in the control piston 122 130 and thus in connection with the high-pressure fuel zone stands.
  • the intermediate piston 162 is also with a Throttle bore 175 provided, through which the second Control chamber 165 parallel to that via ball valve 171 lockable connecting hole 174 with the recess 170 and is thus connected to the high-pressure fuel zone.
  • the intermediate piston 162 has an inlet throttle 184, which the first control chamber 160 with the bore 180 and thus with connects the high pressure fuel zone.
  • the structure of the control device 8 has the following operation: When the pilot valve stem 81 is raised, the pressure in the first control chamber 160 is reduced via the outlet opening 159, the transverse bore 158 and the connecting groove 157. The control piston 122 is moved upwards in the manner already described, the injection valve member opening the injection openings to the combustion chamber of the internal combustion engine. The intermediate piston 162 pressed against the end face 161 with the sealing surface 168 is also moved upward. Due to the pumping action of the intermediate piston 162, the pressure in the second control chamber 165 increases. At a certain excess pressure, the ball valve 171; thus the opening movement of the control piston 122 is accelerated.
  • the control device 8 means an essential one constructive simplification. It is known that the narrow Fits of individual parts the exact concentricity, i.e. precise processing important. In this embodiment points none of the parts two such to be coordinated Sliding surfaces.
  • the control piston 122 has an extreme here simple shape on. The assembly of individual parts of the Control device 8 in the fuel injection valve 2 is no problem. Furthermore, the essential ones are the function determining controls (the throttle bores 175 and 184 and the ball valve 171) in the intermediate piston 162 made or installed. This throttle bores 175,184 and the ball valve 171 can before assembling the Fuel injector 2 for their correct function being checked.
  • the ball valve 171st with valve spring 173, the device would correspond to the control device 2 known from FIG. 2; also the second control room 165 would then only be via the Throttle 175 (corresponding to throttle 77 according to FIG. 2) with the High pressure zone connected.
  • control device 8 could also correspond to the described, not shown in the drawing second alternative variant to the control device 2 is formed be by the second control chamber 165 does not have the throttle 175, which together with the securing element 172, the Ball valve 171 and valve spring 173 would be eliminated, but via a large through hole in the intermediate piston 162 would be connected directly to the high pressure zone.
  • Control device 9 shows a further embodiment of a Control device 9 shown in its design and Operation essentially from the control device 8 Fig.8 corresponds, but for example for the Fuel injector 1 according to Fig.1 is suitable at which, in contrast to fuel injector 2 6 shows the high-pressure fuel supply to the control device of done above. Analogous to control device 8, the Control device 9 the above-mentioned manufacturing and advantages in terms of assembly.
  • the Indian Guide bore 29 is axially displaceable control piston 50 provided with a central recess 176 above.
  • the intermediate piston 179 corresponds essentially to that Intermediate piston 162 according to Figure 8, however, is opposite this arranged vertically reversed by 180 °.
  • a spring 183 surrounding the intermediate piston 179 is on the one hand on a shoulder 185 of the intermediate piston 179, on the other hand on an upper end face 186 of the control piston 50 supported.
  • a first, annular control space 201 is radially through the intermediate piston 179 and the guide bore 29, axially through the upper end face 186 of the control piston 50 and the lower end face 178 of the control body 177 limited.
  • the first control room 201 is analogous to that Control devices 7 and 8 according to Fig.
  • the transverse bore 158 is via a throttle 198 and via a passage 199 to the upper one High-pressure supply line 33 (see FIG. 1) leading transverse bore 68 connected.
  • a second control chamber 202 is located below the intermediate piston 179 formed in the recess 176 of the control piston 50. Of the second control room 202 is temporarily over the by the Ball valve 171 lockable connecting hole 174 and constantly on the throttle 175 as well as on the Connection bore 182 in the securing element 172 and over a passage 200 made in the control body 177 with the transverse bore 68 in connected to the high pressure zone Connection.
  • control device 9 corresponds to that described mode of operation of the control device 8 according to Fig. 8 and is therefore not repeated.
  • This control device too 9 could be omitted analogously to the control device 8 individual parts are alternatively formed, then the Control device 2 according to Figure 2 or the described second alternative variant of this control device 2 correspond.
  • FIG. 10 shows a further embodiment of a Control device 11 shown, provided for the Fuel injector 1 according to Fig. 1.
  • This form of training is particularly suitable for small fuel injectors, where there is no space for arranging valves and springs is available.
  • a control body 205 is used in a fixed position (for example pressed) and by the here as a union nut trained lock nut 54 axially fixed.
  • the Control body 205 has one with a reduced diameter Part 206 with which it fits into a central recess 207 of the axially displaceable in the guide bore 29 Control piston 50 protrudes.
  • a first, ring-shaped Control room 211 is radial through part 206 of the Control body 205 and through the guide bore 29, axially through a shoulder surface 209 of the control body 205 and a upper end face 208 of the control piston 50 limited.
  • the Cross bore 158 is the same as in control device 9 via the throttle 198 and via the passage 199 to the upper high pressure supply line 33 (see Fig.1) leading Cross bore 68 connected, which is arranged obliquely here, and the one radial recess 213 of the control body 205 assigned.
  • the recess 213 is via a throttle 214 and a central bore 215 in the control body 205 with a connected second control room 212, which is below the Control body 205 in the central recess 207 of the Control piston 50 is located.
  • the opening process takes place similar to the control device 2 of Figure 2 in a Step; the throttle 214 corresponds here to the throttle 77 Fig. 2.
  • this variant takes place at Closing no additional acceleration instead of how this was the case with the control device 2.
  • the Control device 11 is manufacturing and assembly technology simple and as already mentioned especially for small ones Suitable for fuel injectors.
  • FIG. 11 shows another one for the fuel injector 2 applicable embodiment of a Control device 13.
  • the one with the central one, to the High pressure zone connected connection bore 130 provided in the guide bore 121 of the valve housing 120 axially displaceable control piston 122 has a central top Recess 218 on.
  • a second control body part 221 projects into the recess 218 and is arranged in the recess 218 by one Spring 222 on top of a lower end face 223 of the first Control body part 220 pressed.
  • the first control body part 220 has a bore 260 provided, which in one of the pilot valve stem 81 lockable outlet opening 259 tapers, and the over at least one made in the lower end face 223 radial groove 224 connected to a first control chamber 226 is.
  • the groove 224 could also be in the end face of the second Control body part 221 may be formed.
  • the first, annular control chamber 226 is radial through the Guide bore 121 and the second control body part 221, axially through the lower end face 223 of the first Control body part 220 and an upper end face 225 of the Spool 122 limited.
  • a second, about that Connection bore 130 directly to the high pressure zone connected control room 227 is in the Recess 218 below the second control body part 221.
  • the second control body part 221 has a central one Provide hole 257, which is in a top Inlet throttle bore 258 tapers. About the Inlet throttle bore 258 is (similar to that over the Inlet throttle bore 58 according to FIG. 2) the first control chamber 226 connected to the high pressure zone.
  • the spring 222 can possibly omitted since the one prevailing in the second control room 227 System high pressure for the constant pressing of the second Control body part 221 to the first control body part 220 worries.
  • the control device 13 corresponds in its mode of operation the mentioned, but not shown in the drawing second alternative variant to the control device 2 Fig. 2.
  • This variant also prevails in the second Control room 227 constantly the system fuel high pressure by the pumping action of the control piston 122 practically remains unaffected.
  • the opening and closing movement of the Control piston 122 and thus also the nozzle needle 24 is over the annular upper end face 225 of the control piston 122 by the control pressure prevailing in the first control chamber 226 controlled, this control pressure from the design and spatial arrangement of the inlet throttle bore 258 and Exhaust opening 259 is dependent.
  • FIG. 12 Another embodiment of a control device 22 for the fuel injection valve 2 according to FIG. 6 is in FIG. 12 shown and described below. For those already known parts are again the same reference numerals used.
  • This form of training is similar to the control device 11 according to Fig. 10 especially for small ones Fuel injectors suitable where there is no space for Arranging valves and springs is present.
  • the first control chamber 155 of the control device 22 is the same as in the control device 7 according to Figures 6 and 7 radially through the guide bore 121 and the stepped in diameter Piston part 123, axially through a piston shoulder 126 and the lower end face 139 of the control body 135 limited.
  • Piston part 123 is here with an additional offset Part 190 provided.
  • a second control room 195 is above of the piston part 123 in the recess 136 of the control body 135 formed.
  • One in the offset part 190 radially Made throttle 191 connects the second control room 195 with the connecting bore 130 and thus with the High pressure fuel zone.
  • the throttle 191 could also on the Longitudinal axis of the control piston 122 or the Fuel injector 2 (similar to that Throttle bores 197 and 159) are attached.
  • in the Control body 135 is one in the second control chamber 195 opening, central bore 196 available, which over a Throttle 197 is connected to the transverse bore 158.
  • the first Control room 155 is here in contrast to the control device 7 not connected to the high pressure system according to FIG. 7 (cf. Throttle bore 133 in Fig.7), but it receives over the Throttle 197, the transverse bore 158 and the connecting groove 157 Pressure from the second control room 195.
  • the pressure in the two Control rooms 155, 195 or the pumping action of the control piston 122 hangs both when opening and when closing the design of the chokes 191, 197.
  • the throttle 191 replaces the first valve flat seat 151 or the Throttle bore 142 according to Fig. 7. In this embodiment finds no additional acceleration during the closing process instead of.
  • the form of training as well as assembly is extreme simple.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
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  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

There is a longitudinally displaceable injection valve member (24) is provided for closing and opening the injection apertures (21). The injection valve member is activated in the opening direction with fuel pressure from a fuel high pressure feed conduit (32). A control device (3) controls the adjustment movement of the injection valve member and incorporates a longitudinally displaceable control piston (50), which on the one first side is activated by the fuel control pressure in a control chamber, which via at least one inlet aperture is connected with the fuel high pressure feed conduit (32).

Description

Die Erfindung betrifft ein Brennstoffeispritzventil zur intermittirenden Brennstoffeinspritzung in den Brennraum einer Verbrennungskraftmaschine gemäss dem Oberbegriff des Anspruches 1.The invention relates to a fuel injection valve for intermittent fuel injection into the combustion chamber an internal combustion engine according to the preamble of Claim 1.

Einspritzventile dieser Art sind beispielsweise aus den Patentschriften EP 0 228 578 oder EP 0 426 205 bekannt.Injectors of this type are for example from the Patents EP 0 228 578 or EP 0 426 205 are known.

Die Erfindung, wie sie in den Ansprüchen gekennzeichnet ist, löst die Aufgabe, ein Brennstoffeinspritzventil zu schaffen, das ein verbessertes Betriebsverhalten gewährleistet und zudem herstellungs- und montagetechnisch äusserst einfach ist.The invention as characterized in the claims solves the task of creating a fuel injector, that ensures improved operating behavior and also extremely easy to manufacture and assemble is.

Die Erfindung wird im folgenden anhand der in der Zeichnung gezeigten Ausführungsbeispiele näher beschrieben.The invention is described below with reference to the drawing The exemplary embodiments shown are described in more detail.

Es zeigen:

Fig.1
eine erste Ausbildungsform eines Brennstoffeinspritzventils im Längsschnitt;
Fig.2
im vergrössertem Massstab und im Längsschnitt eine der Fig.1 entsprechende erste Ausführungsform einer Steuervorrichtung des Brennstoffeinspritzventils;
Fig.3
eine zweite Ausführungsform der Steuervorrichtung;
Fig.4
eine dritte Ausführungsform der Steuervorrichtung;
Fig.5
eine vierte Ausführungsform der Steuervorrichtung;
Fig.6
im partiellen Längsschnitt eine zweite Ausbildungsform des Brennstoffeinspritzventils mit einer fünften Ausführungsform der Steuervorrichtung;
Fig.7
in vergrössertem Massstab einen Teil der Steuervorrichtung gemäss Fig.6;
Fig.8
eine sechste Ausführungsform der Steuervorrichtung für das Brennstoffeinspritzventil nach Fig.6;
Fig.9
eine siebte Ausführungsform der Steuervorrichtung für das Brennstoffeinspritzventil nach Fig.1;
Fig.10
eine achte Ausführungsform der Steuervorrichtung für das Brennstoffeinspritzventil nach Fig.1;
Fig.11
eine neunte Ausführungsform der Steuervorrichtung für das Brennstoffeinspritzventil nach Fig.6;
Fig.12
eine zehnte Ausführungsform der Steuervorrichtung für das Brennstoffeinspritzventil nach Fig.6.
Show it:
Fig. 1
a first embodiment of a fuel injector in longitudinal section;
Fig. 2
on an enlarged scale and in longitudinal section, a first embodiment of a control device of the fuel injector corresponding to FIG. 1;
Fig. 3
a second embodiment of the control device;
Fig. 4
a third embodiment of the control device;
Fig. 5
a fourth embodiment of the control device;
Fig. 6
in partial longitudinal section, a second embodiment of the fuel injector with a fifth embodiment of the control device;
Fig. 7
on an enlarged scale, part of the control device according to Figure 6;
Fig. 8
a sixth embodiment of the control device for the fuel injector according to Figure 6;
Fig. 9
a seventh embodiment of the control device for the fuel injector of Figure 1;
Fig. 10
an eighth embodiment of the control device for the fuel injector according to Figure 1;
Fig. 11
a ninth embodiment of the control device for the fuel injector according to Figure 6;
Fig. 12
a tenth embodiment of the control device for the fuel injector according to Figure 6.

In Fig.1 ist ein Brennstoffeinspritzventil 1 in einer Stellung zwischen zwei Einspritzvorgängen dargestellt. Das Brennstoffeinspritzventil 1 ist über einen Brennstoffhochdruckanschluss 10 und über einen Brennstoffrücklaufanschluss 12 mit einer Hochdruck-Fördereinrichtung für den Brennstoff und über elektrische Anschlüsse 14 mit einer elektronischen Steuerung verbunden. Die Hochdruck-Fördereinrichtung und die elektronische Steuerung sind in der Zeichnung nicht dargestellt.In Fig.1 is a fuel injector 1 in one Position shown between two injection processes. The Fuel injector 1 is over a High-pressure fuel connection 10 and via a Fuel return connection 12 with a high-pressure delivery device for the fuel and over electrical Connections 14 connected to an electronic control. The high pressure conveyor and the electronic Controls are not shown in the drawing.

Das Gehäuse des Brennstoffeinspritzventils 1 ist mit 15 bezeichnet. Am unteren Ende ist das Gehäuse 15 mit einem als Überwurfmutter ausgebildeten Halteteil 16, am oberen Ende mit einer entsprechenden Haltemutter 17 festgeschraubt. The housing of the fuel injection valve 1 is 15 designated. At the lower end is the housing 15 with a Union nut trained holding part 16, with at the upper end a corresponding retaining nut 17 screwed.

Im Halteteil 16 ist ein Düsenkörper 18 eingesetzt, dessen Düsenspitze 19 aus dem Halteteil 16 hinausragt. Die Düsenspitze 19 ist mit einem Düsennadelsitz 20 versehen und weist in diesem Bereich mehrere Einspritzöffnungen 21 auf. Im Düsenkörper 18 ist eine ein Einspritzventilglied bildende, axial verstellbare Düsennadel 24 in einer Nadelführungsbohrung 23 gleitend geführt. Die Einspritzöffnungen 21 der Düsenspitze 19 sind durch ein unteres Ende 25 der Düsennadel 24 abschliessbar.In the holding part 16, a nozzle body 18 is inserted, the Nozzle tip 19 protrudes from the holding part 16. The Nozzle tip 19 is provided with a nozzle needle seat 20 and has a plurality of injection openings 21 in this area. in the Nozzle body 18 is an injection valve member, axially adjustable nozzle needle 24 in one Needle guide bore 23 slidably. The Injection openings 21 of the nozzle tip 19 are through a lower end 25 of the nozzle needle 24 can be locked.

Das Gehäuse 15 ist mit einer zentralen Führungsbohrung 29 versehen, in welcher eine Steuervorrichtung 3 zur Steuerung der Verstellbewegung des Einspritzventilgliedes bzw.der Düsennadel 24 angeordnet ist. Die Steuervorrichtung 3 wird weiter unten anhand der Fig.2 ausführlich beschrieben.The housing 15 has a central guide bore 29 provided, in which a control device 3 for control the adjustment movement of the injection valve member or Nozzle needle 24 is arranged. The control device 3 is described in detail below with reference to FIG. 2.

Der Brennstoff wird durch die Hochdruck-Fördereinrichtung über den Brennstoffhochdruckanschluss und eine erste kurze Brennstoffzufuhrbohrung 31 in zwei im Gehäuse 15 parallel zur Führungsbohrung 29 angeordneten Hochdruckzufuhrleitungen 32,33 gefördert. Die obere Hochdruckzufuhrleitung 33 führt zur Steuervorrichtung 3. Die untere Hochdruckzufuhrleitung 32 ist über eine schräg in einer Zwischenplatte 36 angeordnete Verbindungsbohrung 35 an eine Düsenkörperbohrung 26 angeschlossen, die in einen Ringraum 27 im Düsenkörper 18 mündet. Vom Ringraum 27 gelangt der Brennstoff über nicht näher dargestellte Durchgänge zum Düsennadelsitz 20 bzw. zu den Einspritzöffnungen 21. Im Bereich des Ringraumes 27 ist die Düsennadel 24 mit einem Absatz 28 versehen.The fuel is fed through the high pressure delivery device via the high-pressure fuel connection and a first short Fuel supply bore 31 in two in the housing 15 parallel to Guide bore 29 arranged high pressure supply lines 32.33 promoted. The upper high pressure supply line 33 leads to the control device 3. The lower high pressure supply line 32 is arranged obliquely in an intermediate plate 36 Connecting bore 35 to a nozzle body bore 26 connected in an annular space 27 in the nozzle body 18th flows. The fuel does not pass from the annular space 27 Passages shown in more detail to the nozzle needle seat 20 and the injection openings 21. In the area of the annular space 27 the nozzle needle 24 is provided with a shoulder 28.

Die Zwischenplatte 36 ist gegenüber dem Gehäuse 15 über einen Stift 37 (es könnten auch zwei Stifte 37 sein) positioniert und dichtend zwischen dem Gehäuse 15 und dem Düsenkörper 18 angeordnet. Ein in eine zentrale Bohrung 38 der Zwischenplatte 36 hineinragende obere Teil 39 der Düsennadel 24 ist mit einem Nadel-Zwischenelement 40 wirkverbunden, der anderseits über eine Verbindungsstange 44 mit einem Steuerkolben 50 der Steuervorrichtung 3 verbunden ist. Zwischen einer sich an einem Absatz 45 des Gehäuses 15 abstützenden Federspannscheibe 46 und dem Nadel-Zwischenelement 40 ist eine die Verbindungsstange 44 umgebende Düsennadelfeder 47 vorgespannt angeordnet.The intermediate plate 36 is opposite the housing 15 via a Pin 37 (there could also be two pins 37) positioned and sealing between the housing 15 and the nozzle body 18 arranged. One in a central bore 38 of the Intermediate plate 36 protruding upper part 39 of the nozzle needle 24 is operatively connected to an intermediate needle element 40 which on the other hand via a connecting rod 44 with a Control piston 50 of the control device 3 is connected. Between one on a shoulder 45 of the housing 15 supporting spring washer 46 and the needle intermediate element 40 is a connecting rod 44 surrounding nozzle needle spring 47 arranged biased.

Die Steuervorrichtung 3 weist einen in die Führungsbohrung 29 ortsfest eingesetzten Steuerkörper 52 auf. Der Steuerkolben 50 ist mit einem oberen, im Durchmesser abgesetzten Kolbenteil 51 versehen. Wie besonders aus Fig.2 ersichtlich ist, ragt das obere Kolbenteil 51 in eine in der Führungsborung 29 axial verschiebbar und eng gleitend angeordnete Hülse 64 hinein. Auch zwischen dem Kolbenteil 51 und dem Innendurchmesser der Hülse 64 sind enge Gleitpassungen vorgesehen. Zwischen einer unteren Stirnfläche 65 der Hülse 64 und einer Kolbenabsatzfläche 53 ist eine Feder 63 angeordnet. Die Hülse 64 stützt sich mit einer schmalen ringförmigen Dichtfläche 66 an einer unteren Stirnfläche 55 des Steuerkörpers 52 ab, der anderseits durch eine mit dem Gehäuse 15 verschraubte Sicherungsmutter 54 in der Führungsbohrung 29 axial fixiert ist.The control device 3 has one in the guide bore 29 control body 52 used in a stationary manner. The control piston 50 is with an upper, stepped in diameter Piston part 51 provided. As can be seen particularly in Fig. 2 is, the upper piston part 51 protrudes into one in the Guide bore 29 axially displaceable and tightly sliding arranged sleeve 64 into it. Also between the piston part 51 and the inner diameter of the sleeve 64 are narrow Sliding fits provided. Between a lower face 65 of the sleeve 64 and a piston shoulder surface 53 is one Spring 63 arranged. The sleeve 64 is supported with a narrow annular sealing surface 66 on a lower End face 55 of the control body 52, on the other hand by a lock nut 54 screwed to the housing 15 in the guide bore 29 is axially fixed.

Im unteren Bereich des Steuerkörpers 52 befindet sich im Gehäuse 15 ein Ringraum 69, der über eine Querbohrung 68 an die obere Hochdruckzufuhrleitung 33 angeschlossen ist. Der Steuerkörper 52 weist eine dem Ringraum 69 entsprechende Umfangsringnut 67 auf. Ferner ist der Steuerkörper 52 mit einer in einen ersten Steuerraum 70 mündenden Verbindungsbohrung 60 versehen, die über eine Einlassdrosselbohrung 58 mit der Umfangsringnut 67 bzw. mit dem Ringraum 69 und somit auch mit der Hochdruckzufuhrleitung 33 verbunden ist. Oben verengt sich die Verbindungsbohrung 60 in eine Auslassöffnung 59.In the lower area of the control body 52 is in the Housing 15 is an annular space 69, which has a transverse bore 68 the upper high pressure supply line 33 is connected. Of the Control body 52 has an annular space 69 corresponding Circumferential ring groove 67. The control body 52 is also included one opening into a first control room 70 Provided connecting bore 60, which via a Inlet throttle bore 58 with the circumferential ring groove 67 or with the annular space 69 and thus also with the high pressure supply line 33 is connected. The connection bore 60 narrows at the top into an outlet opening 59.

Der erste Steuerraum 70 ist radial durch die Innenfläche der Hülse 64 , axial durch die untere Stirnfläche 55 des Steuerkörpers 52 und eine obere Stirnfläche 56 des Kolbenteils 51 begrenzt.The first control space 70 is radial through the inner surface of FIG Sleeve 64, axially through the lower end face 55 of the Control body 52 and an upper end face 56 of the Piston part 51 limited.

Zwischen dem Kolbenteil 51 und der Führungsbohrung 29 befindet sich unterhalb der Hülse 64 ein ringförmiger, zweiter Steuerraum 74, in dem auch die Feder 63 angeordnet ist, und der über eine Verbindungsbohrung 75 an die Hochdruckzufuhrleitung 33 angeschlossen ist. In die Verbindungsbohrung 75 ist eine Blende 76 mit einer Drossel 77 eingesetzt.Between the piston part 51 and the guide bore 29 there is an annular, underneath the sleeve 64, second control chamber 74, in which the spring 63 is also arranged is, and the via a connecting bore 75 to the High pressure supply line 33 is connected. In the The connecting bore 75 is an orifice 76 with a throttle 77 used.

Der Steuerkörper 52 ist in die Führungsbohrung 29 des Gehäuses 15 derart eingebaut, dass keine nennenswerte Leckage stattfinden kann. Dies wird z.B. mit einem Pressitz oder einem engen Schiebesitz erreicht, könnte allerdings auch durch andere brennstoffdichte Verbindungen, beispielsweise unter Verwendung von geeigneten Dichtungsringen realisiert werden.The control body 52 is in the guide bore 29 of the Housing 15 installed in such a way that no significant leakage can take place. This will e.g. with a press fit or reached a tight sliding seat, but could also through other fuel-tight connections, for example realized using suitable sealing rings become.

Die Steuervorrichtung 3 weist ferner ein elektromagnetisch betätigbares Pilotventil 80 auf, von dem in Fig.2 lediglich ein mit einem Pilotventilschaft 81 fest verbundener Anker 82 ersichtlich ist. In der in Fig.2 dargestellten Stellung wird die Auslassdrosselbohrung 59 über einen Ventil-Flachsitz 85 in der geschlossener Stellung gehalten. Wie aus Fig.1 zu sehen ist, wird dabei im stromlosen Zustand eines Elektromagnets 86 der Pilotventilschaft 81 durch die Kraft einer Druckfeder 87 nach unten in die den Ventil-Flachsitz 85 schliessende Stellung gedrückt. Diese Kraft ist mittels einer Einstellschraube 88 in ihrer Grösse einstellbar. Zur Betätigung des Pilotventils 80 bzw. zur Anhebung des Pilotventilschaftes 81 vom Ventil-Flachsitz 85 erhält eine dem Anker 82 zugeordnete Erregerspule 83 des Elektromagnets 86 über die elektrischen Anschlüsse 14 Steuerimpulse von der elektronischen Steuerung. The control device 3 also has an electromagnetic actuatable pilot valve 80, of which only in Fig.2 an armature 82 firmly connected to a pilot valve stem 81 can be seen. In the position shown in Fig.2 the exhaust throttle bore 59 via a flat valve seat 85 held in the closed position. As shown in Fig.1 can be seen in the currentless state Electromagnet 86 of the pilot valve stem 81 by the force a compression spring 87 down into the valve flat seat 85 closing position pressed. This force is through a Adjustment screw 88 adjustable in size. For Actuation of the pilot valve 80 or to raise the Pilot valve stem 81 from valve flat seat 85 receives one excitation coil 83 of the electromagnet assigned to armature 82 86 via the electrical connections 14 control pulses from the electronic control.

Der beim Anheben des Pilotventilschaftes 81 aus der Auslassöffnung 59 austretende Brennstoff wird gemäss Fig.1 in einem Abflussraum 89 gesammelt und über eine Abflussbohrung 90 dem Brennstoffrücklaufanschluss 12 zugeführt, der zusammen mit dem Elektromagneten 86 in der Haltemutter 17 eingebaut ist. In den Abflussraum 89 fliesst auch über eine Entlastungsbohrung 92 der durch Leckagen in einem Raum 91 unterhalb des Steuerkolbens 50 angesammelte Brennstoff. Somit wird ein Teil des Brennstoffes praktisch drucklos der Hochdruck-Fördereinrichtung zurückgeführt. Der Raum 91, die Entlastungsbohrung 92, der Abflussraum 89 und die Abflussbohrung 90 bilden einen sogenannten Niederdruckteil des Brennstoffeinspritzventils 1.When lifting the pilot valve stem 81 from the Outlet opening 59 is in accordance with Fig.1 in a drain space 89 collected and via a drain hole 90 fed to the fuel return port 12, which together installed with the electromagnet 86 in the holding nut 17 is. A flow also flows into the discharge space 89 Relief bore 92 of leakage in a space 91st fuel accumulated below the control piston 50. Consequently part of the fuel becomes practically depressurized High-pressure conveyor returned. The room 91, the Relief bore 92, the drain chamber 89 and the Drain hole 90 form a so-called low-pressure part the fuel injector 1.

Aus dem beschriebenen Aufbau ergibt sich folgende Wirkungsweise des Brennstoffeinspritzventils 1:The following results from the structure described Mode of operation of fuel injector 1:

Vor dem Einspritzvorgang herrscht im Hochdruckteil des Brennstoffeinspritzventils 1, d.h. in der Brennstoffzufuhrbohrung 31, in beiden Hochdruckzufuhrleitungen 32,33, in den Ringräumen 27,69 und in beiden Steuerräumen 70,74 der gleiche Hochdruck bzw. Einspritzdruck, der bis über 1000 bar betragen kann.Before the injection process, the high pressure part of the Fuel injector 1, i.e. in the Fuel feed hole 31, in both High pressure supply lines 32.33, in the annular spaces 27.69 and the same high pressure or in both control rooms 70, 74 Injection pressure, which can be up to over 1000 bar.

Sobald über die elektronische Steuerung ein Impuls von gewählter Dauer dem Elektromagnet 86 erteilt wird, wird der Anker 82 entgegen der Kraft der Feder 87 angezogen, wodurch das Pilotventil 80 geöffnet wird. Somit wird die Auslassöffnung 59 des Steuerkörpers 52 geöffnet. Der Druck im ersten Steuerraum 70 sinkt. Die Düsennadel 24 wird durch den im Ringraum 27 herrschenden und auf den Absatz 28 wirkenden Brennstoffdruck vom Düsennadelsitz 20 angehoben. Die Einspritzöffnungen 21 werden freigegeben, und der Brennstoff wird in an sich bekannter Weise in den Brennraum der Verbrennungskraftmaschine eingespritzt. As soon as a pulse of selected duration is given to the electromagnet 86, the Armature 82 attracted against the force of the spring 87, whereby the pilot valve 80 is opened. Thus the Outlet opening 59 of the control body 52 opened. The pressure in first control room 70 sinks. The nozzle needle 24 is by the prevailing in the annular space 27 and acting on the paragraph 28 Fuel pressure raised from the nozzle needle seat 20. The Injection ports 21 are released and the fuel is in a manner known per se in the combustion chamber Internal combustion engine injected.

Beim Anheben der Düsennadel 24 wird auch über das Nadel-Zwischenelement 40 und die Verbindungsstange 44 der Steuerkolben 50 nach oben bewegt. Das Volumen des zweiten Steuerraumes 74 wird kleiner, der Druck im Steuerraum 74 steigt unter dieser Pumpwirkung. Die Hülse 64 wird noch stärker in die dichtende Stellung gegenüber dem Steuerkörper 52 gedrückt. Über die Verbindungsbohrung 75 und die Drossel 77, die zur Hochdruckzufuhrleitung 33 führen, wird der der Öffnungsbewegung des Einspritzventilgliedes bzw. der Düsennadel 24 entgegenwirkende Druck im zweiten Steuerraum 74 in gewünschter, kontrollierter Weise definiert. Dadurch wird ein angestrebtes, kontrolliertes Öffnen des Einspritzventils erreicht.When the nozzle needle 24 is raised, the needle intermediate element is also used 40 and the connecting rod 44 of the Control piston 50 moves upward. The volume of the second Control room 74 becomes smaller, the pressure in control room 74 increases under this pumping action. The sleeve 64 is still more in the sealing position with respect to the control body 52 pressed. Via the connection bore 75 and the throttle 77, which lead to the high pressure supply line 33, the Opening movement of the injection valve member or Nozzle needle 24 counteracting pressure in the second control chamber 74 defined in the desired, controlled manner. This will a desired, controlled opening of the injection valve reached.

Die Beendigung des Einspritzvorgangs soll bekanntlich möglichst rasch erfolgen. Wiederum elektronisch gesteuert wird über den Elektromagnet 86 das Pilotventil 80 in seine Schliessstellung gebracht. Da nun die Auslassöffnung 59 wieder geschlossen ist, steigt im ersten Steuerraum 70 der Druck an, und der Steuerkolben 50 wird durch die auf die obere Stirnfläche 56 des Kolbenteils 51 einwirkende Kraft nach unten bewegt. Das Volumen des zweiten Steuerraumes 74 wird vergrössert, der Brennstoffdruck im zweiten Steuerraum 74 fällt. Die Hülse 64 bleibt anfänglich an den Steuerkörper 52 angedrückt. Beim bestimmten Absinken des Brennstoffdruckes im zweiten Steuerraum 74 folgt die Hülse 64 der Kolbenbewegung; dazu ist zu erwähnen, dass die Feder 63 relativ schwach vorgespannt ist, so dass die Druckwirkung der Feder 63 vernachlässigbar ist gegenüber den Brennstoffdruckkräften. Sobald sich die Hülse 64 mit der Dichtfläche 66 vom Steuerkörper 52 abhebt, gelangt schlagartig über diese neue Verbindung Brennstoff vom Ringraum 69 bzw. aus der Hochdruckzufuhrleitung 33 in den ersten Steuerraum 70. Der Steuerkolben 50 sowie auch die Hülse 64 werden nach unten beschleunigt; über die Verbindungsstange 44 und das Nadel-Zwischenelement 40 wird die Düsennadel 24 in die die Einspritzöffnungen 21 schliessende Stellung gedrückt. In dieser Weise wird beim erfindungsgemässen Brennstoffeinspritzventil 1 ein rascher Einspritzschliessvorgang realisiert.The end of the injection process is known to be done as quickly as possible. Again electronically controlled the pilot valve 80 into its via the electromagnet 86 Brought to the closed position. Since the outlet opening 59 is closed again, increases in the first control room 70 Pressure on, and the control piston 50 is by the on the force acting on the upper end face 56 of the piston part 51 moved down. The volume of the second control room 74 the fuel pressure in the second control room is increased 74 falls. The sleeve 64 initially remains on the control body 52 pressed. At certain decrease in fuel pressure in the second control chamber 74, the sleeve 64 follows Piston movement; it should be noted that the spring 63 is relatively weakly biased, so that the pressure effect of the Spring 63 is negligible compared to Fuel pressure forces. Once the sleeve 64 with the Seals sealing surface 66 from the control body 52, arrives abruptly about this new fuel connection from Annulus 69 or from the high pressure supply line 33 in the first control chamber 70. The control piston 50 and also the Sleeve 64 are accelerated downward; about the Connecting rod 44 and the needle intermediate element 40 is the nozzle needle 24 into which the injection openings 21 closing position pressed. In this way the Fuel injector 1 according to the invention is a faster one Injection closing process realized.

Sobald der Druck im zweiten Steuerraum 74 über die Drossel 77 und die Verbindungsbohrung 75 wieder dem Systembrennstoffhochdruck angeglichen wird, drückt die Feder 63 die Hülse 64 mit der Dichtfläche 66 in die den ersten Steuerraum 70 radial begrenzende Stellung.As soon as the pressure in the second control chamber 74 via the throttle 77 and the connecting bore 75 again System fuel high pressure is adjusted, pushes the spring 63 the sleeve 64 with the sealing surface 66 in the first Control chamber 70 radially limiting position.

In einer ersten, in der Zeichnung nicht dargestellten alternativen Variante zur Steuervorrichtung 3 nach Fig.2 wird entweder in der Querbohrung 68 oder in der oberen Hochdruckzufuhrleitung 33 eine als eine Drossel ausgebildete Verengung angebracht, die eine schwache Drosselung bewirkt und dadurch beim Schliessvorgang die Beschleunigung des Steuerkolbens 50 leicht dämpft. Damit wird das Aufprallen der Düsennadel 24 auf den Düsennadelsitz 20 am Ende des Schliessvorganges vermindert. Wird die erwähnte Verengung in der oberen Hochdruckzufuhrleitung 33 vorgesehen, so kann sich diese entweder im Bereich unterhalb der Drossel 77 oder oberhalb derselben befinden. Diese erste Variante zur Steuervorrichtung 3 ist besonders dann zu bevorzugen, wenn (aus konstruktiven Gründen) die Gefahr besteht, dass der Düsennadelsitz 20 durch einen zu starken Aufprall der Düsennadel 24 beschädigt werden könnte.In a first, not shown in the drawing alternative variant to the control device 3 according to FIG. 2 either in the transverse bore 68 or in the upper one High-pressure supply line 33 designed as a throttle Narrowing applied, which causes a weak throttling and thereby the acceleration of the Control piston 50 dampens slightly. This will make the bounce Nozzle needle 24 on the nozzle needle seat 20 at the end of Closing process reduced. Will the mentioned narrowing in the upper high pressure supply line 33 is provided, so this either in the area below the throttle 77 or are above it. This first variant of Control device 3 is particularly preferred if (for design reasons) there is a risk that the Nozzle needle seat 20 due to an excessive impact Nozzle needle 24 could be damaged.

In einer zweiten, in der Zeichnung ebenfalls nicht dargestellten alternativen Variante zur Steuervorrichtung 3 wird die Drossel 77 gross ausgebildet, oder es wird auf die Drossel 77 ganz verzichtet, so dass die Verbindungsbohrung 75 direkt mit der oberen Hochdruckzufuhrleitung 33 verbunden ist. Somit herrscht bei dieser Variante im zweiten Steuerraum 74 immer der Systembrennstoffhochdruck, der infolge der Pumpwirkung des Steuerkolbens 50 während der Öffnungsbewegung der Düsennadel 24 praktisch oder gar nicht ansteigt; während des Schliessvorganges fällt der Druck im zweiten Steuerraum 74 auch nicht ab. Die Hülse 64 verliert in diesem Fall während der Schliessbewegung der Düsennadel 24 nicht den Kontakt mit der unteren Stirnfläche 55 des Steuerkörpers 52, was durch geeignete Dimensionierung der Feder 63 gewährleistet ist. Der Vorteil dieser Variante liegt in einer gegenüber bekannten Lösungen verminderten Steuerfläche, welche durch die beiden Drosselbohrungen 59 und 58 gesteuert werden muss. Über die der Stirnfläche 56 des oberen Kolbenteils 51 entsprechende Steuerfläche wird die Bewegung des wesentlich grösseren Steuerkolbens 50 gesteuert.In a second one, neither in the drawing Alternative variant to the control device 3 shown the throttle 77 is formed large, or it is on the Throttle 77 is completely dispensed with, so that the connecting bore 75 directly connected to the upper high pressure supply line 33 is. Thus, in this variant, there is a second control room 74 always the system fuel high pressure, which as a result of Pumping action of the control piston 50 during the opening movement the nozzle needle 24 rises practically or not at all; while during the closing process, the pressure in the second control room drops 74 either. The sleeve 64 loses in this case not during the closing movement of the nozzle needle 24 Contact with the lower end face 55 of the control body 52, what by appropriate dimensioning of the spring 63rd is guaranteed. The advantage of this variant is one control surface reduced compared to known solutions, which is controlled by the two throttle bores 59 and 58 must become. Over that of the front surface 56 of the upper Piston part 51 corresponding control surface, the movement of the much larger control piston 50 controlled.

In den Figuren 3, 4, und 5 werden weitere Ausführungsformen der Steuervorrichtung für das Brennstoffeinspritzventil dargestellt und im folgenden näher beschrieben. Die aus Fig.1 und 2 bekannten und gleichwirkenden Teile sind weiterhin mit gleichen Bezugsziffern bezeichnet.3, 4 and 5 show further embodiments the control device for the fuel injector shown and described in more detail below. The from Fig.1 and 2 known and equivalent parts are still with the same reference numerals.

Bei der in Fig.3 dargestellten Ausführungsform einer Steuervorrichtung 4 ist die aus Fig.1 und 2 bekannte Hülse 64 durch eine Hülse 94 ersetzt. Die Hülse 94 weist am Umfang mehrere axial hintereinander angeordnete Rippen 95 auf, deren Aussendurchmesser einen exakt definierten radialen Ringspalt 93 gegenüber der Führungsbohrung 29 bildet. Die Ringnut 67 im Steuerkörper 52 sowie der Ringraum 69 im Gehäuse 15 entfallen. Oberhalb der obersten Rippe 95 mündet in die Führungsbohrung 29 die den Hochdruckbrennstoff zuführende Querbohrung 68 hinein. An der oberen Stirnseite ist die Hülse 94 mit einer schmalen, ringförmigen Dichtfläche 96 versehen. Die Dichtfläche 96 weist mehrere am Umfang verteilte radiale Vertiefungen 97 von geringer Tiefe ( ca 0,02 - 0,03 mm ) auf, über welche der Brennstoff gedrosselt von der Führungsbohrung 29 und folglich von der Querbohrung 68 zum ersten Steuerraum 70 gelangt und die die Einlassdrosselbohrung 58 der aus Fig.2 bekannten Steuervorrichtung 3 ersetzen. Die Rippen 95 hingegen ersetzen die aus Fig.2 bekannte, zwischen den zweiten Steuerraum 74 und die Hochdruckzufuhrleitung 33 eingebaute Drossel 77. Die Rippen 95 weisen scharfe Kanten auf, um unabhängig von der Zähigkeit des Brennstoffes eine turbulente Strömung zu erzielen. Durch die Anordnung mehrerer Rippen 95 hintereinander wird der Brennstoffdruck stufenweise abgebaut bzw. die Strömungsgeschwindigkeit reduziert. Dadurch kann der Ringspalt grosszügiger dimensioniert werden.In the embodiment shown in Figure 3 a Control device 4 is the sleeve 64 known from FIGS. 1 and 2 replaced by a sleeve 94. The sleeve 94 has on the circumference several axially arranged ribs 95, whose Outside diameter a precisely defined radial annular gap 93 forms opposite the guide bore 29. The ring groove 67 in Control body 52 and the annular space 69 in the housing 15 omitted. Above the top rib 95 opens into the Guide bore 29 that supplying the high pressure fuel Cross bore 68 into it. The sleeve is on the upper face 94 with a narrow, annular sealing surface 96. The sealing surface 96 has a plurality of radial circumferentially distributed Wells 97 of shallow depth (approx. 0.02 - 0.03 mm), through which the fuel throttled from the pilot hole 29 and consequently from the transverse bore 68 to the first control chamber 70 arrives and the inlet throttle bore 58 of the from Fig.2 replace known control device 3. The ribs 95 on the other hand, replace the one known from FIG second control room 74 and the high pressure supply line 33 built-in throttle 77. The ribs 95 have sharp edges on to a regardless of the toughness of the fuel to achieve turbulent flow. By arranging several Ribs 95 in a row, the fuel pressure gradually reduced or the flow rate reduced. Thereby the annular gap can be dimensioned more generously.

Die Lage der Dichtfläche 96 gegenüber dem Aussen- bzw. Innendurchmesser der Hülse 94 kann je nach notwendiger Anpressungskraft gewählt werden. Die gleiche Dichtfläche 96 und/oder die radialen Vertiefungen 97 könnten auch bei der Hülse 64 von Fig.2 verwendet werden.The position of the sealing surface 96 in relation to the outside or Inner diameter of sleeve 94 may be necessary Contact pressure can be selected. The same sealing surface 96 and / or the radial recesses 97 could also in the Sleeve 64 of Fig.2 can be used.

Diese Ausführungsform der Steuervorrichtung 4 ist herstellungstechnisch einfacher als die in Fig.1 und 2 dargestellte Ausführungsform. Ansonsten ist die Wirkungsweise gleich wie bereits beschrieben.This embodiment of the control device 4 is technically simpler than that in Fig. 1 and 2 illustrated embodiment. Otherwise it works same as already described.

Ähnlich wie die Steuervorrichtung 3 nach Fig.2 kann auch die Steuervorrichtung 4 nach Fig.3 entsprechend der beschriebenen ersten sowie auch der zweiten alternativen Variante ausgebildet sein. Um die zweite Variante zu realisieren, bei welcher der zweite Steuerraum 74 in direkter Verbindung mit der Hochdruckzone steht, kann ein breiter Ringspalt 93 zwischen der Hülse 94 und der Führungsbohrung 29 vorgesehen werden, oder es können die Rippen 95 ganz weggelassen werden.Similar to the control device 3 according to FIG Control device 4 according to Figure 3 corresponding to that described first and also the second alternative variant be trained. To implement the second variant, at which the second control room 74 is in direct communication with is in the high pressure zone, a wide annular gap 93 provided between the sleeve 94 and the guide bore 29 or the ribs 95 can be omitted entirely.

In Fig.4 ist eine weitere Ausführungsform der Steuervorrichtung dargestellt und mit 5 bezeichnet.4 shows a further embodiment of the Control device shown and designated 5.

In einem im Durchmesser erweiterten Teil 99 der Führungsbohrung 29 ist eine Hülse 98 eng gleitend geführt, die gleich wie die aus Fig. 3 bekannte Hülse 94 mit der mit Vertiefungen 97 versehenen schmalen Dichtfläche 96 ausgestattet ist. Die Feder 63 ist zwischen der unteren Stirnfläche 65 der Hülse 98 und einem Gehäuseabsatz 100 vorgespannt. In a part 99 of enlarged diameter Guide bore 29 is a sleeve 98 guided closely sliding, the same as the sleeve 94 known from FIG. 3 with the Recesses 97 provided narrow sealing surface 96 Is provided. The spring 63 is between the lower End face 65 of sleeve 98 and a housing shoulder 100 biased.

Parallel zur Führungsbohrung 29 ist im Gehäuse 15 eine Gehäusebohrung 102 angefertigt, in die ein Kugelrückschlagventil 103 eingebaut ist. Ein unteres Ventilsitzelement 104 des Kugelrückschlagventils 103 weist eine Bohrung 105 auf, die über Bohrungen 106, 107 mit dem zweiten Steuerraum 74 verbunden ist. Eine dem Ventilsitzelement 104 zugeordnete Kugel 108 wird über ein zweites Ventilelement 109 durch die Kraft einer Feder 110 an das Ventilsitzelement 104 gedrückt. Das Kugelrückschlagventil 103 ist mittels eines Verschlusszapfens 111, über welchen auch die Federvorspannung gewählt werden kann, in der Gehäusebohrung 102 axial fixiert. Die Verbindung des zweiten Steuerraumes 74 mit der Hochdruckzone wird somit über das Kugelrückschlagventil 103 hergestellt.Parallel to the guide bore 29 is in the housing 15 Housing bore 102 made in the one Ball check valve 103 is installed. A lower one Valve seat element 104 of the ball check valve 103 has a bore 105 on the holes 106, 107 with the second control room 74 is connected. One of the Ball 108 assigned to valve seat element 104 is moved over a second valve element 109 by the force of a spring 110 the valve seat member 104 is pressed. The ball check valve 103 is by means of a locking pin 111, over which also the spring preload can be selected in the Housing bore 102 axially fixed. The connection of the second Control room 74 with the high pressure zone is thus over Ball check valve 103 manufactured.

Steigt im zweiten Steuerraum 74 bei Aufwärtsbewegung der Düsennadel 24 und des Steuerkolbens 50 der Brennstoffdruck durch die Pumpwirkung des Steuerkolbens 50 auf eine bestimmte Grösse, wird die Kugel 108 des Kugelrückschlagventils 103 angehoben und der Druck plötzlich an den Systemhochdruck angeglichen, wodurch die Gegenwirkung gegnüber der Öffnungsbewegung der Düsennadel 24 plötzlich aufgehoben wird (Die Drossel 77 gemäss Fig.2 hat eine kontinuierliche Druckangleichung bewirkt.). Mittels der Steuervorrichtung 5 wird die Öffnungsbewegung der Düsennadel 24 in eine Phase mit kleiner ( vor dem Öffnen des Kugelrückschlagventils 103 ) und eine Phase mit grosser Öffnungsgeschwindigkeit unterteilt. Ein solcher Verlauf der Öffnungsbewegung der Düsennadel 24 bewirkt eine günstige Motorverbrennung.Increases in the second control chamber 74 when the Nozzle needle 24 and the control piston 50 the fuel pressure by the pumping action of the control piston 50 to a specific one Size, the ball 108 of the ball check valve 103 raised and the pressure suddenly reached the system high pressure adjusted, whereby the counteraction against the Opening movement of the nozzle needle 24 is suddenly canceled (The choke 77 according to FIG. 2 has a continuous one Pressure equalization causes.). By means of the control device 5 is the opening movement of the nozzle needle 24 in one phase smaller (before opening the ball check valve 103) and divided a phase with high opening speed. Such a course of the opening movement of the nozzle needle 24 causes a favorable engine combustion.

Eine rasche Schliessbewegung wird in gleicher Weise wie bei Steuervorrichtung 3 erreicht, in dem die Hülse 98 bei Abwärtsbewegung des Steuerkolbens 50 und beim Absinken des Brennstoffdruckes im zweiten Steuerraum 74 unter eine bestimmte Grösse die Verbindung des Hochdrucksystems zum ersten Steuerraum 70 frei gibt. A quick closing movement is the same as for Control device 3 reached in which the sleeve 98 at Downward movement of the control piston 50 and when the Fuel pressure in the second control room 74 under one certain size the connection of the high pressure system to the first control room 70 releases.

In Fig.5 ist eine weitere alternative Ausführungsform der Steuervorrichtung dargestellt und mit 6 bezeichnet. Anstelle des aus Fig.4 bekannten Kugelrückschlagsventils 103 ist in der Gehäusebohrung 102 ein Kegelsitzventil 113 eingebaut. Der Kegelsitz zwischen einem Ventilkörper 114 und dem Gehäuse 15 ist mit 115 bezeichnet. Der Ventilkörper 114 ist mit einer Querbohrung 116 und einer senkrecht zur Querbohrung 116 angeordneten Drosselbohrung 117 versehen. Der zweite Steuerraum 74 ist über die Bohrungen 107, 106, die Drosselbohrung 117 und die Querbohrung 116 mit der Hochdruckregion verbunden.5 shows a further alternative embodiment of the Control device shown and designated 6. Instead of of the ball check valve 103 known from FIG a bore seat valve 113 is installed in the housing bore 102. Of the Taper seat between a valve body 114 and the housing 15 is designated 115. The valve body 114 is with a Cross bore 116 and one perpendicular to cross bore 116 arranged throttle bore 117 provided. The second Control room 74 is through the bores 107, 106, the Throttle bore 117 and the transverse bore 116 with the High pressure region connected.

Bei dieser Variante kann der Brennstoffdruck im zweiten Steuerraum 74 bei Aufwärtsbewegung des Steuerkolbens 50 sowohl allmählich bei geschlossenem Kegelsitzventil 113 über die Drosselbohrung 117 ausgeglichen werden, als auch bei grossem Überdruck schlagartig durch Anheben des Ventilkörpers 114 vom Kegelsitz 115 dem Systemdruck angeglichen werden. Bei kleinem Systemdruck spricht das Kegelsitzventil 113 nicht an.In this variant, the fuel pressure in the second Control chamber 74 when control piston 50 moves upward both gradually over with the cone seat valve 113 closed the throttle bore 117 are balanced, as well large overpressure suddenly by lifting the valve body 114 from the conical seat 115 to be adjusted to the system pressure. At low cone seat valve 113 does not respond.

Fig.6 zeigt im Teilschnitt eine alternative Ausbildungsform des Brennstoffeinspritzventils, der mit 2 bezeichnet und mit einer weiteren Steuervorrichtung 7 ausgestattet ist. Die aus Fig.1 bis 5 bereits bekannten, identischen und gleichwirkenden Teile sind wieder mit gleichen Bezugsziffern bezeichnet. Ein Teil der Steuervorrichtung 7 ist zum besseren Verständnis in Fig.7 vergrössert dargestellt.Fig. 6 shows an alternative form of training in partial section of the fuel injector, designated 2 and a further control device 7 is equipped. From 1 to 5 already known, identical and parts with the same effect are again given the same reference numbers designated. Part of the control device 7 is for the better Understanding enlarged in Fig.7.

Gemäss Fig.6 weist das Brennstoffeinspritzventil 2 ein Gehäuse 120 auf, das mit einer zentralen Führungsbohrung 121 für die Steuervorrichtung 7 versehen ist. In der Führungsbohrung 121 ist ein Steuerkolben 122 eng gleitend axial verschiebbar angeordnet. Oben weist der Steuerkolben 122 ein im Durchmesser abgesetztes Kolbenteil 123 auf. Die entsprechende Absatzfläche ist mit 126 bezeichnet. Unten geht der Steuerkolben 122 in eine Verbindungsstange 124 über, über die er kraftschlüssig mit dem in Fig.6 nicht dargestellten Einspritzventilglied (Düsennadel) verbunden ist. Gegebenenfalls könnte sogar die Verbindungsstange 124 mit dem Einspritzventilglied einstückig ausgebildet sein. Am Übergang zur Verbindungsstange 124 wird ein Kolbenabsatz 129 gebildet.According to Figure 6, the fuel injector 2 has Housing 120 on that with a central guide bore 121st is provided for the control device 7. In the Guide bore 121 is a spool 122 closely sliding axially displaceable. The control piston points at the top 122 a piston part 123 with a reduced diameter. The corresponding sales area is designated 126. Goes down the control piston 122 in a connecting rod 124 over, over which he non-positively with that not shown in Fig.6 Injection valve member (nozzle needle) is connected. If necessary, even the connecting rod 124 could with the Injection valve member be integrally formed. At the transition a piston shoulder 129 is formed to the connecting rod 124.

In einen zwischen der Verbindungsstange 124 und der Führungsbohrung 121 vorhandenen Raum 125 mündet direkt die relativ kurze, erste Brennstoffzufuhrbohrung 31 vom Brennstoffhochdruckanschluss 10. Das Gehäuse 120 selber weist keine weiteren Hochdruckzufuhrleitungen mehr auf, die bei der in Fig.1 gezeigten Ausbildungsform mit 32,33 bezeichnet waren; es sind auch keine weiteren Ringräume oder Querbohrungen im Gehäuse 120 angefertigt, wodurch ein extrem einfaches und herstellungstechnisch vorteilhaftes Gehäuse 120 realisiert wird.In one between the connecting rod 124 and the Guide hole 121 existing room 125 opens directly into the relatively short, first fuel supply bore 31 from High-pressure fuel connection 10. The housing 120 itself has no more high pressure supply lines on the Designation shown in Fig.1 designated 32.33 were; there are also no further ring spaces or Cross bores made in the housing 120, which makes an extreme simple and technically advantageous housing 120 is realized.

Das obere Kolbenteil 123 ist auf seiner oberen Stirnseite mit einer Ausnehmung 128 versehen, in die eine im Steuerkolben 122 angefertigte zentrale Verbindungsbohrung 130 mündet. Die Verbindungsbohrung 130 ist über eine im Steuerkolben 122 angefertigte Querbohrung 131 an den mit Hochdruckbrennstoff gefüllten Raum 125 angeschlossen.The upper piston part 123 is on its upper face a recess 128 provided in the one in the control piston 122 made central connection bore 130 opens. The The connecting bore 130 is in the control piston 122 made cross bore 131 to the high-pressure fuel filled room 125 connected.

In die Führungsbohrung 121 ist ein Steuerkörper 135 ortsfest eingesetzt (beispielsweise eingepresst), der durch die bereits bekannte Sicherungsmutter 54 axial fixiert ist. Der Steuerkörper 135 ist auf seiner unteren Stirnseite mit einer Ausnehmung 136 ausgestattet, in die das obere Kolbenteil 123 eng gleitend hineinragt. In einem im Durchmesser abgesetzten Teil 137 der Ausnehmung 136 ist eine Feder 138 angeordnet, über welche eine Ventilsitzscheibe 140 an die obere, mit 127 bezeichnete ringförmige Stirnfläche des oberen Kolbenteils 123 angedrückt wird. Die Ventilsitzscheibe 140 weist ein zentrales Scheibenloch 141 auf.A control body 135 is stationary in the guide bore 121 used (pressed in, for example) by the already known lock nut 54 is axially fixed. Of the Control body 135 is on its lower end face with a Recess 136 equipped into which the upper piston part 123th protrudes tightly. In a stepped diameter Part 137 of the recess 136 has a spring 138 arranged in it, via which a valve seat washer 140 to the upper one, with 127 designated annular end face of the upper piston part 123 is pressed. The valve seat disk 140 has a central disc hole 141 on.

In der Ausnehmung 128 des Steuerkolbens 122 ist ein in der dargestellten Stellung das Scheibenloch 141 unter Wirkung einer Feder 144 bis auf eine Drosselbohrung 142 abschliessender Ventilkörper 143 angeordnet.In the recess 128 of the control piston 122 is in the position shown the disc hole 141 under effect a spring 144 except for a throttle bore 142 final valve body 143 arranged.

Die Ventilsitzscheibe 140 und der das Scheibenloch 141 verschliessende Ventilkörper 143 bilden einen ersten Ventil-Flachsitz 151. Die Stirnfläche 127 des Kolbenteils 123 und die Ventilsitzscheibe 140 bilden einen zweiten Ventil-Flachsitz 152 (siehe Fig.7).The valve seat plate 140 and the plate hole 141 closing valve bodies 143 form a first flat valve seat 151. The end face 127 of the piston part 123 and the valve seat plate 140 form a second valve flat seat 152 (see Fig. 7).

Zwischen einer ringförmigen, unteren Stirnfläche 139 des Steuerkörpers 135 und der Absatzfläche 126 des Steuerkolbens 122 ist ein erster Steuerraum 155 vorhanden, der radial durch das obere Kolbenteil 123 einerseits und die Führungsbohrung 121 anderseits begrenzt ist. Am Umfang des oberen Kolbenteils 123 ist eine Einlassdrossel 133 angefertigt, welche in die Verbindungsbohrung 130 radial mündet und eine Verbindung des ersten Steuerraums 155 zur Brennstoffhochdruckzone bildet.Between an annular, lower end face 139 of the Control body 135 and the shoulder surface 126 of the control piston 122 there is a first control chamber 155 which passes radially through the upper piston part 123 on the one hand and the guide bore 121 is limited on the other hand. On the circumference of the upper part of the piston 123 an inlet throttle 133 is made, which in the Connecting bore 130 opens radially and a connection of the forms first control chamber 155 to the high-pressure fuel zone.

Am Umfang des Steuerkörpers 135 ist mindestens eine Verbindungsnut 157 angefertigt, die den ersten Steuerraum 155 mit einer Querbohrung 158 im Steuerkörper 135 verbindet. Eine in die Querbohrung 158 mündende Auslassöffnung 159 des Steuerkörpers 135 ist in der dargestellten Stellung durch den Pilotventilschaft 81 geschlossen gehalten, wodurch der erste Steuerraum 155 von dem Niederdruckteil des Brennstoffeinspritzventils 2 getrennt ist.At least one is on the circumference of the control body 135 Connection groove 157 made the first control room 155 connects with a transverse bore 158 in the control body 135. A in the transverse bore 158 opening 159 of the Control body 135 is in the position shown by the Pilot valve stem 81 kept closed, making the first Control room 155 from the low pressure part of the Fuel injector 2 is separated.

Ein zweiter Steuerraum 156 ist in der Ausnehmung 136 des Steuerkörpers 135 oberhalb des Kolbenteils 123 gebildet und durch die beiden Ventil-Flachsitze 151, 152 von der System- bzw. Brennstoffhochdruckzone in der dargestellten Ausgangsstellung zwischen zwei Einspritzvorgängen getrennt gehalten.A second control chamber 156 is in the recess 136 of the Control body 135 formed above the piston part 123 and through the two valve flat seats 151, 152 from the system or High-pressure fuel zone in the illustrated Starting position separated between two injection processes held.

Die Wirkungsweise des Brennstoffeinspritzventils 2 bzw. der Steuervorrichtng 7 ist wie folgt:
Bei einer in gleicher Weise wie bereits beschrieben eingeleiteten, elektronisch gesteuerten Anhebung des Pilotventilschaftes 81 wird die Auslassöffnung 159 geöffnet. Der Brennstoffdruck im ersten Steuerraum 155 sinkt. Durch den auf den Kolbenabsatz 129 einwirkenden, im Raum 125 herrschenden Brennstoffhochdruck wird der Steuerkolben 122 nach oben bewegt. Dabei gibt das Einspritzventilglied in bereits beschriebener Weise die Einspritzöffnungen zum Brennraum der Verbrennungskraftmaschine frei. Beim Anheben des Steuerkolbens 122 samt der Ventilsitzscheibe 140 wird das Volumen des zweiten Steuerraums 156 verkleinert, der Druck steigt bei dieser Pumpwirkung an und wirkt der Öffnungsbewegung in gewünschter Weise entgegen. Dadurch wird ein langsamer Öffnungsvorgang realisiert. Sobald der Druck im zweiten Steuerraum 156 eine gewisse Höhe erreicht, wird über das Scheibenloch 141 der Ventilkörper 143 entgegen dem in der Ausnehmung 128 herrschenden Systemdruck und der Kraft der Feder 144 nach unten gedrückt und der erste Ventil-Flachsitz 151 wird geöffnet, wodurch der Öffnungsvorgang des Steuerkolbens 122 und folglich des Einspritzventilgliedes beschleunigt wird.
The mode of operation of the fuel injection valve 2 or of the control device 7 is as follows:
When the pilot valve stem 81 is raised and electronically controlled in the same way as described above, the outlet opening 159 is opened. The fuel pressure in the first control room 155 drops. The control piston 122 is moved upward by the high fuel pressure acting on the piston shoulder 129 and prevailing in the space 125. The injection valve member opens the injection openings to the combustion chamber of the internal combustion engine in the manner already described. When the control piston 122 together with the valve seat disk 140 is raised, the volume of the second control chamber 156 is reduced, the pressure increases with this pumping action and counteracts the opening movement in the desired manner. This results in a slow opening process. As soon as the pressure in the second control chamber 156 reaches a certain level, the valve body 143 is pressed down against the system pressure prevailing in the recess 128 and the force of the spring 144 via the disk hole 141 and the first flat valve seat 151 is opened, as a result of which the opening process of the control piston 122 and consequently the injection valve member is accelerated.

Wird die Auslassöffnung 159 durch den Pilotventilschaft wieder geschlossen, so steigt der Druck im ersten Steuerraum 155 erneut an. Der Druck im zweiten Steuerraum 156 wird wieder an den Systemhochdruck angeglichen. Die Feder 144 drückt den Ventilkörper 143 an die Ventilsitzscheibe 140, die anderseits durch die Kraft der Feder 138 belastet ist. Der erste Ventil-Flachsitz 151 wird geschlossen. Über die Absatzfläche 126 wird der Steuerkolben 122 nach unten bewegt. Das Volumen des zweiten Steuerraums 156 wird vergrössert, der Druck sinkt. Sobald der Druck im zweiten Steuerraum 156 einen gewissen Wert unterschreitet, bei dem keine ausreichende Anpresskraft von oben auf die Ventilsitzscheibe 140 ausgeübt wird, wird der zweite Ventil-Flachsitz 152 geöffnet. In diesem Augenblick wird eine Verbindung des zweiten Steuerraums 156 mit der Hochdruckbrennstoffzufuhr hergestellt, wobei der Brennstoff den Steuerkolben 122 über die Stirnfläche 127 zusätzlich nach unten beschleunigt. In dieser Weise wird ein rascher Schliessvorgang des Einspritzventilgliedes durchgeführt.Exhaust port 159 becomes through the pilot valve stem closed again, so the pressure in the first control room rises 155 again. The pressure in the second control room 156 is adjusted again to the system high pressure. The spring 144 presses the valve body 143 against the valve seat plate 140 which on the other hand is loaded by the force of the spring 138. Of the first valve flat seat 151 is closed. About the Sales surface 126, the control piston 122 is moved down. The volume of the second control chamber 156 is increased, the Pressure drops. As soon as the pressure in the second control room 156 is one falls below a certain value at which insufficient Pressure force exerted on the valve seat plate 140 from above the second valve flat seat 152 is opened. In at that moment a connection of the second Control room 156 with the high pressure fuel supply made, the fuel over the control piston 122 the end face 127 is additionally accelerated downwards. In in this way a quick closing of the Injector member performed.

Der erfindungsgemässe Brennstoffeinspritzventil 2 bringt neben der konstruktiven und montagetechnischen Vereinfachung auch noch den Vorteil mit sich, dass minimale Leckagen stattfinden. Der aus der Auslassdrosselbohrung 159 austretende Brennstoff wird wiederum über die Abflussbohrung 90 dem Brennstoffrücklaufanschluss zugeführt.The fuel injector 2 according to the invention brings in addition to the simplification of construction and assembly technology also has the advantage of minimal leakage occur. The one from the exhaust throttle bore 159 escaping fuel is in turn through the drain hole 90 fed to the fuel return port.

Würde man bei der Steuervorrichtung 7 nach den Figuren 6 bzw. 7 den Ventilkörper 143 mit der Drosselbohrung 142 sowie die Feder 144 weglassen und die Ventilsitzscheibe 140 direkt mit einem als Drossel ausgebildeten Scheibenloch 141 versehen, so würde die Wirkungsweise der Steuervorrichtung 7 derjenigen der Steuervorrichtung 3 aus Fig.2 entsprechen. Das als Drossel ausgebildete Scheibenloch 141 würde dann der Drossel 77 aus Fig.2 entsprechen, die den zweiten Steuerraum 156 (in Fig.2 Steuerraum 74) mit der Hochdruckzone verbindet.Would the control device 7 according to FIGS. 7 the valve body 143 with the throttle bore 142 and the Omit spring 144 and valve seat disk 140 directly with provided as a throttle disc hole 141, so would the operation of the control device 7 of those correspond to the control device 3 from FIG. That as Throttle-formed disc hole 141 would then become the throttle 77 corresponding to FIG. 2, which correspond to the second control space 156 (in Fig. 2 control room 74) connects to the high pressure zone.

Bei zusätzlichem Weglassen der Ventilsitzscheibe 140 und der Feder 138 würde die Steuervorrichtung 7 der zweiten alternativen Variante zur Steuervorrichtung 3 nach Fig.2 (mit grosser oder fehlender Drossel 77) entsprechen, da in diesem Fall auch der zweite Steuerraum 156 direkt mit der Hochdruckzone verbunden wäre.With additional omission of the valve seat plate 140 and the Spring 138 would control device 7 of the second alternative variant to the control device 3 according to FIG. 2 (with large or missing throttle 77) correspond, since in this If the second control room 156 also directly with the High pressure zone would be connected.

In Fig.8 ist eine weitere alternative Ausführungsform einer Steuervorrichtung 8 dargestellt, die für das Brennstoffeinspritzventil 2 verwendet werden kann. Die aus Fig.6 und 7 bekannten Teile sind erneut mit gleichen Bezugsziffern bezeichnet.Another alternative embodiment is shown in FIG Control device 8 shown for the Fuel injector 2 can be used. From Fig. 6 and 7 known parts are again the same Designated reference numbers.

Der in der Führungsbohrung 121 des Gehäuses 120 verschiebbar angeordnete Steuerkolben 122 weist in diesem Fall kein im Durchmesser abgesetztes Kolbenteil auf, sonder er ist mit einer oberen Stirnfläche 161 abgeschlossen. Zwischen dem Steuerkolben 122 und dem Steuerkörper 135 ist ein Zwischenkolben 162 angeordnet, der in die Ausnehmung 136 des Steuerkörpers 135 eng gleitend hineinragt. Ein erster, ringförmiger Steuerraum 160 ist radial durch den Zwischenkolben 162 und die Führungsbohrung 121, axial durch die obere Stirnfläche 161 des Steuerkolbens 122 und die untere Stirnfläche 139 des Steuerkörpers 135 begrenzt. Ein zweiter Steuerraum 165 befindet sich in der Ausnehmung 136 oberhalb des Zwischenkolbens 162 bzw. oberhalb einer oberen Stirnfläche 163 des Zwischenkolbens 162.That is slidable in the guide bore 121 of the housing 120 arranged control piston 122 has no in this case Diameter of the piston part, but it is with an upper end face 161 is completed. Between the Control piston 122 and the control body 135 is a Intermediate piston 162 arranged in the recess 136 of the Control body 135 protrudes closely sliding. A first annular control chamber 160 is radial through the Intermediate piston 162 and the guide bore 121, axially through the upper end face 161 of the control piston 122 and the lower end face 139 of the control body 135 limited. A second control chamber 165 is located in recess 136 above the intermediate piston 162 or above an upper one End face 163 of the intermediate piston 162.

Der Zwischenkolben 162 ist mit einem Absatz 166 versehen. Eine den Zwischenkolben 162 umgebende Feder 167 ist am Absatz 166 einerseits und an der unteren Stirnfläche 139 des Steuerkörpers 135 anderseits abgestützt. Der Zwischenkolben 162 weist unten eine schmale, ringförmige Dichtfläche 168 auf, die der oberen Stirnfläche 161 des Steuerkolbens 122 zugeordnet ist. Der Durchmesser der Dichtfläche 168 ist kleiner als der Durchmesser der Ausnehmung 136 bzw. als der Durchmesser der oberen Stirnfläche 163 des Zwischenkolbens 162.The intermediate piston 162 is provided with a shoulder 166. A spring 167 surrounding the intermediate piston 162 is on the shoulder 166 on the one hand and on the lower end face 139 of the Control body 135 supported on the other. The intermediate piston 162 has a narrow, annular sealing surface 168 at the bottom that of the upper end face 161 of the control piston 122 assigned. The diameter of the sealing surface is 168 smaller than the diameter of the recess 136 or than that Diameter of the upper end face 163 of the intermediate piston 162.

Der Zwischenkolben 162 ist von unten mit einer zentralen Aussparung 170 versehen. Zwischen der Aussparung 170 und dem zweiten Steuerraum 165 ist im Zwischenkolben eine Verbindungsbohrung 174 angefertigt, der ein in der Aussparung angeordnetes Kugelventil 171 zugeordnet ist. Eine Ventilfeder 173 ist in der Aussparung 170 mittels eines in eine Bohrung 180 des Zwischenkolbens 162 eingepressten oder eingeschraubten Sicherungselementes 172 vorgespannt. Das Sicherungselement 172 weist eine zentrale Verbindungsbohrung 182 auf, uber welche der Raum der Aussparung 170 mit der zentral im Steuerkolben 122 angeordneten Verbindungsbohrung 130 und somit mit der Brennstoffhochdruckzone in Verbindung steht. Der Zwischenkolben 162 ist zusätzlich mit einer Drosselbohrung 175 versehen, über welche der zweite Steuerraum 165 parallel zu der über das Kugelventil 171 abschliessbaren Verbindungsbohrung 174 mit der Aussparung 170 und somit mit der Brennstoffhochdruckzone verbunden ist.The intermediate piston 162 is from the bottom with a central one Provide recess 170. Between the recess 170 and the second control chamber 165 is one in the intermediate piston Connection hole 174 made, the one in the recess arranged ball valve 171 is assigned. A valve spring 173 is in the recess 170 by means of a in a bore 180 of the intermediate piston 162 pressed or screwed securing element 172 biased. The Securing element 172 has a central connecting bore 182 over which the space of the recess 170 with the Connection bore arranged centrally in the control piston 122 130 and thus in connection with the high-pressure fuel zone stands. The intermediate piston 162 is also with a Throttle bore 175 provided, through which the second Control chamber 165 parallel to that via ball valve 171 lockable connecting hole 174 with the recess 170 and is thus connected to the high-pressure fuel zone.

Der Zwischenkolben 162 weist eine Einlassdrossel 184 auf, die den ersten Steuerraum 160 mit der Bohrung 180 und somit mit der Brennstoffhochdruckzone verbindet.The intermediate piston 162 has an inlet throttle 184, which the first control chamber 160 with the bore 180 and thus with connects the high pressure fuel zone.

Es wäre durchaus möglich, anstelle der Einlassdrossel 184 die Dichtfläche 168 des Zwischenkolbens 162 mit mehreren am Umfang verteilten, radialen Vertiefungen zu versehen - ähnlich wie es bei der Hülse 94 gemäss Fig.3 der Fall ist (vgl. Vertiefungen 97), um eine Einlassdrosselverbindung des ersten Steuerraumes 160 mit der Brennstoffhochdruckzone herzustellen.It would be entirely possible to replace the inlet throttle 184 Sealing surface 168 of the intermediate piston 162 with several To provide circumferentially distributed radial depressions - similar to the case with the sleeve 94 according to FIG. 3 (see. wells 97) to an inlet throttle connection of the first control room 160 with the high-pressure fuel zone to manufacture.

Aus dem beschriebenen Aufbau ergibt sich folgende Wirkungsweise der Steuervorrichtung 8:
Beim Anheben des Pilotventilschaftes 81 wird über die Auslassöffnung 159, die Querbohrung 158 und die Verbindungsnut 157 der Druck im ersten Steuerraum 160 gesenkt. Der Steuerkolben 122 wird in bereits beschriebener Weise nach oben bewegt, wobei das Einspritzventilglied die Einspritzöffnungen zum Brennraum der Verbrennungskraftmaschine freigibt. Der mit der Dichtfläche 168 an die Stirnfläche 161 gepresste Zwischenkolben 162 wird nach oben mitbewegt. Durch die Pumpwirkung des Zwischenkolbens 162 steigt der Druck im zweiten Steuerraum 165. Bei einem gewissen Überdruck öffnet das Kugelventil 171; somit wird die Öffnungsbewegung des Steuerkolbens 122 beschleunigt.
The structure of the control device 8 has the following operation:
When the pilot valve stem 81 is raised, the pressure in the first control chamber 160 is reduced via the outlet opening 159, the transverse bore 158 and the connecting groove 157. The control piston 122 is moved upwards in the manner already described, the injection valve member opening the injection openings to the combustion chamber of the internal combustion engine. The intermediate piston 162 pressed against the end face 161 with the sealing surface 168 is also moved upward. Due to the pumping action of the intermediate piston 162, the pressure in the second control chamber 165 increases. At a certain excess pressure, the ball valve 171; thus the opening movement of the control piston 122 is accelerated.

Wird die Ausslassöffnung 159 durch den Pilotventilschaft 81 wieder geschlossen, so steigt der Druck im ersten Steuerraum 160. Der Druck im zweiten Steuerraum 165 wird an den Systemhochdruck angeglichen. Das Kugelventil 171 schliesst. Mit dem steigenden Druck im ersten Steuerraum 160 wird der Steuerkolben 122 sowie auch der Zwischenkolben 162 nach unten bewegt. Das Volumen des zweiten Steuerraumes 165 wird grösser, der Druck sinkt. Bei einem bestimmten Druckabfall ist die Anpresskraft des Zwischenkolbens 162 an die Stirnfläche 161 des Steuerkolbens 122 nicht mehr gewährleistet. Der Zwischenkolben 162 bzw. seine Dichtfläche 168 trennt sich vom Steuerkolben 122, und der Steuerkolben 122 wird zusätzlich durch den auf seine Stirnfläche 161 einwirkenden Brennstoffhochdruck (über die Verbindungsbohrung 130 geliefert) nach unten beschleunigt. Das Einspritzventilglied wird schlagartig geschlossen. Im Gegensatz zu der aus Fig.7 bekannten Steuervorrichtung 7 wird hier die ganze Kolbenfläche - ähnlich wie bei der Steuervorrichtung 3 in Fig.2 - beaufschlagt.Is the outlet opening 159 through the pilot valve stem 81 closed again, so the pressure in the first control room rises 160. The pressure in the second control room 165 is applied to the System high pressure adjusted. The ball valve 171 closes. With the increasing pressure in the first control room 160, the Control piston 122 and the intermediate piston 162 down emotional. The volume of the second control room 165 becomes bigger, the pressure drops. With a certain pressure drop is the contact pressure of the intermediate piston 162 against the End face 161 of the control piston 122 no longer guaranteed. The intermediate piston 162 or its sealing surface 168 separates from the spool 122 and the spool 122 is additionally by the on its end face 161st acting high pressure fuel (via the connecting hole 130 delivered) accelerated downwards. The Injector member is closed suddenly. in the Contrary to the control device 7 known from FIG here the entire piston surface - similar to the Control device 3 in Figure 2 - acted upon.

Die Steuervorrichtung 8 bedeutet eine wesentliche konstruktive Vereinfachung. Bekanntlich ist bei den engen Passungen einzelner Teile die exakte Konzentrizität, d.h. genaue Bearbeitung wichtig. Bei dieser Ausführungsform weist keiner der Teile zwei solche aufeinander abzustimmende Gleitflächen auf. Der Steuerkolben 122 weist hier eine extrem einfache Form auf. Die Montage einzelner Teile der Steuervorrichtung 8 im Brennstoffeinspritzventil 2 ist problemlos. Ferner sind die wesentlichen, die Funktion bestimmenden Steuerelemente ( die Drosselbohrungen 175 und 184 sowie das Kugelventil 171 ) im Zwischenkolben 162 angefertigt bzw. eingebaut. Diese Drosselbohrungen 175,184 sowie das Kugelventil 171 können vor dem Zusammenbauen des Brennstoffeinspritzventils 2 auf ihre korrekte Funktion hin geprüft werden.The control device 8 means an essential one constructive simplification. It is known that the narrow Fits of individual parts the exact concentricity, i.e. precise processing important. In this embodiment points none of the parts two such to be coordinated Sliding surfaces. The control piston 122 has an extreme here simple shape on. The assembly of individual parts of the Control device 8 in the fuel injection valve 2 is no problem. Furthermore, the essential ones are the function determining controls (the throttle bores 175 and 184 and the ball valve 171) in the intermediate piston 162 made or installed. This throttle bores 175,184 and the ball valve 171 can before assembling the Fuel injector 2 for their correct function being checked.

Würde man bei dieser Steuervorrichtung 8 das Kugelventil 171 mit der Ventilfeder 173 weglassen, so würde die Vorrichtung der aus Fig.2 bekannten Steuervorrichtung 2 entsprechen; auch hier wäre dann der zweite Steuerraum 165 lediglich über die Drossel 175 (entsprechend der Drossel 77 nach Fig.2) mit der Hochdruckzone verbunden.Would one in this control device 8, the ball valve 171st with valve spring 173, the device would correspond to the control device 2 known from FIG. 2; also the second control room 165 would then only be via the Throttle 175 (corresponding to throttle 77 according to FIG. 2) with the High pressure zone connected.

Die Steuervorrichtung 8 könnte aber auch entsprechend der beschriebenen, in der Zeichnung nicht dargestellten zweiten alternativen Variante zur Steuervorrichtung 2 ausgebildet sein, indem der zweite Steuerraum 165 nicht über die Drossel 175, die zusammen mit dem Sicherungselement 172, dem Kugelventil 171 und der Ventilfeder 173 wegfallen würde, sondern über ein grosses Durchgangsloch im Zwischenkolben 162 direkt an die Hochdruckzone angeschlossen wäre.The control device 8 could also correspond to the described, not shown in the drawing second alternative variant to the control device 2 is formed be by the second control chamber 165 does not have the throttle 175, which together with the securing element 172, the Ball valve 171 and valve spring 173 would be eliminated, but via a large through hole in the intermediate piston 162 would be connected directly to the high pressure zone.

In Fig.9 ist eine weitere Ausführungsform einer Steuervorrichtung 9 dargestellt, die in ihrer Gestaltung und Funktionsweise im wesentlichen der Steuervorrichtung 8 aus Fig.8 entspricht, die jedoch beispielsweise für das Brennstoffeinspritzventil 1 nach Fig.1 geeignet ist, bei welchem im Gegensatz zum Brennstoffeinspritzventil 2 nach Fig.6 die Brennstoffhochdruckzufuhr zur Steuervorrichtung von oben erfolgt. Analog zu Steuervorrichtung 8 weist auch die Steuervorrichtung 9 die oben erwähnten herstellungs- und montagetechnischen Vorteile auf.9 shows a further embodiment of a Control device 9 shown in its design and Operation essentially from the control device 8 Fig.8 corresponds, but for example for the Fuel injector 1 according to Fig.1 is suitable at which, in contrast to fuel injector 2 6 shows the high-pressure fuel supply to the control device of done above. Analogous to control device 8, the Control device 9 the above-mentioned manufacturing and advantages in terms of assembly.

Bei dieser Variante ist in der Führungsbohrung 29 des Ventilgehäuses 15 ein mit einer unteren Stirnfläche 178 versehener Steuerkörper 177 ortsfest angeordnet. Der in der Führungsbohrung 29 axial verschiebbare Steuerkolben 50 ist oben mit einer zentralen Ausnehmung 176 versehen. Ein sich an der Stirnfläche 178 des Steuerkörpers 177 über eine schmale, ringförmige Dichtfläche 187 abstützender Zwischenkolben 179 ragt eng gleitend in die Ausnehmung 176 des Steuerkolbens 50 hinein. Der Zwischenkolben 179 entspricht im wesentlichen dem Zwischenkolben 162 nach Fig.8, ist jedoch diesem gegenüber vertikal um 180° gekehrt angeordnet. Da die innere Ausgestaltung des Zwischenkolbens 179 derjenigen des Zwischenkolbens 162 entspricht, sind die gleichwirkenden Teile mit gleichen Bezugsziffern bezeichnet (vgl. Aussparung 170, Kugelventil 171, Sicherungselement 172, Verbindungsbohrungen 174, 182, Drossel 175, Ventilfeder 170). Eine den Zwischenkolben 179 umgebende Feder 183 ist einerseits an einem Absatz 185 des Zwischenkolbens 179, anderseits an einer oberen Stirnfläche 186 des Steuerkolbens 50 abgestützt. Ein erster, ringförmiger Steuerraum 201 ist radial durch den Zwischenkolben 179 und die Führungsbohrung 29, axial durch die obere Stirnfläche 186 des Steuerkolbens 50 und die untere Stirnfläche 178 des Steuerkörpers 177 begrenzt. Der erste Steuerraum 201 ist analog zu den Steuervorrichtungen 7 bzw. 8 nach Fig.7 bzw. 8 über mindestens eine am Umfang des Steuerkörpers 177 angefertigte Verbindungsnut 157 und über die Querbohrung 158 mit der durch den Pilotventilschaft 81 abschliessbaren Auslassöffnung 159 verbunden. Die Querbohrung 158 ist über eine Drossel 198 und über einen Durchgang 199 an die zur oberen Hochdruckzufuhrleitung 33 (vgl. Fig.1) führende Querbohrung 68 angeschlossen.In this variant, the guide bore 29 of the Valve housing 15 a with a lower end face 178 provided control body 177 arranged stationary. The Indian Guide bore 29 is axially displaceable control piston 50 provided with a central recess 176 above. One yourself the end face 178 of the control body 177 over a narrow, annular sealing surface 187 supporting intermediate piston 179 protrudes tightly into the recess 176 of the control piston 50 inside. The intermediate piston 179 corresponds essentially to that Intermediate piston 162 according to Figure 8, however, is opposite this arranged vertically reversed by 180 °. Because the inner Design of the intermediate piston 179 that of the Corresponds to intermediate piston 162, are the same Parts labeled with the same reference numbers (see recess 170, ball valve 171, securing element 172, Connection bores 174, 182, throttle 175, valve spring 170). A spring 183 surrounding the intermediate piston 179 is on the one hand on a shoulder 185 of the intermediate piston 179, on the other hand on an upper end face 186 of the control piston 50 supported. A first, annular control space 201 is radially through the intermediate piston 179 and the guide bore 29, axially through the upper end face 186 of the control piston 50 and the lower end face 178 of the control body 177 limited. The first control room 201 is analogous to that Control devices 7 and 8 according to Fig. 7 and 8 over at least one made on the circumference of the control body 177 Connection groove 157 and through the transverse bore 158 with the through the outlet valve 159 which can be closed off the pilot valve stem 81 connected. The transverse bore 158 is via a throttle 198 and via a passage 199 to the upper one High-pressure supply line 33 (see FIG. 1) leading transverse bore 68 connected.

Ein zweiter Steuerraum 202 wird unterhalb des Zwischenkolbens 179 in der Ausnehmung 176 des Steuerkolbens 50 gebildet. Der zweite Steuerraum 202 steht zeitweise über die durch den Kugelventil 171 abschliessbare Verbindungsbohrung 174 und ständig über die Drossel 175 sowie über die Verbindungsbohrung 182 im Sicherungselement 172 und über einen im Steuerkörper 177 angefertigten Durchgang 200 mit der an die Hochdruckzone angeschlossenen Querbohrung 68 in Verbindung.A second control chamber 202 is located below the intermediate piston 179 formed in the recess 176 of the control piston 50. Of the second control room 202 is temporarily over the by the Ball valve 171 lockable connecting hole 174 and constantly on the throttle 175 as well as on the Connection bore 182 in the securing element 172 and over a passage 200 made in the control body 177 with the transverse bore 68 in connected to the high pressure zone Connection.

Die Wirkungsweise der Steuervorrichtung 9 entspricht der beschriebenen Wirkunsweise der Steuervorrichtung 8 nach Fig.8 und wird daher nicht wiederholt. Auch diese Steuervorrichtung 9 könnte analog zur Steuervorrichtung 8 durch weglassen einzelner Teile alternativ ausgebildet werden, um dann der Steuervorrichtung 2 nach Fig.2 bzw. der beschriebenen zweiten alternativen Variante dieser Steuervorrichtung 2 zu entsprechen. The operation of the control device 9 corresponds to that described mode of operation of the control device 8 according to Fig. 8 and is therefore not repeated. This control device too 9 could be omitted analogously to the control device 8 individual parts are alternatively formed, then the Control device 2 according to Figure 2 or the described second alternative variant of this control device 2 correspond.

In Fig.10 ist eine weitere Ausführungsform einer Steuervorrichtung 11 dargestellt, vorgesehen für das Brennstoffeinspritzventil 1 nach Fig.1. Diese Ausbildungsform ist besonders für kleine Brennstoffeinspritzventile geeignet, bei denen kein Platz zum Anordnen von Ventilen und Federn vorhanden ist.10 shows a further embodiment of a Control device 11 shown, provided for the Fuel injector 1 according to Fig. 1. This form of training is particularly suitable for small fuel injectors, where there is no space for arranging valves and springs is available.

In der zentralen Führungsbohrung 29 des Ventilgehäuses 15 ist ein Steuerkörper 205 ortsfest eigesetzt (beispielsweise eingepresst) und durch die hier als Überwurfmutter ausgebildete Sicherungsmutter 54 axial fixiert. Der Steuerkörper 205 weist unten einen im Durchmesser abgesetzten Teil 206 auf, mit welchem er in eine zentrale Ausnehmung 207 des in der Führungsbohrung 29 axial verschiebbaren Steuerkolbens 50 hineinragt. Ein erster, ringförmiger Steuerraum 211 ist radial durch den Teil 206 des Steuerkörpers 205 und durch die Führungsbohrung 29, axial durch eine Absatzfläche 209 des Steuerkörpers 205 und eine obere Stirnfläche 208 des Steuerkolbens 50 begrenzt. Der erste Steuerraum 211 ist wiederum gleich wie bei Steuervorrichtungen 7, 8 und 9 über mindestens eine am Umfang des Steuerkörpers 205 angefertigte Verbindungsnut 157 und über die Querbohrung 158 mit der durch den Pilotventilschaft 81 abschliessbaren Auslassöffnung 159 verbunden. Die Querbohrung 158 ist gleich wie bei der Steuervorrichtung 9 über die Drossel 198 und über den Durchgang 199 an die zur oberen Hochdruckzufuhrleitung 33 (vgl. Fig.1) führende Querbohrung 68 angeschlossen, die hier schräg angeordnet ist, und der eine radiale Ausnehmung 213 des Steuerkörpers 205 zugeordnet ist. Die Ausnehmung 213 ist über eine Drossel 214 und eine zentrale Bohrung 215 im Steuerkörper 205 mit einem zweiten Steuerraum 212 verbunden, der sich unterhalb des Steuerkörpers 205 in der zentralen Ausnehmung 207 des Steuerkolbens 50 befindet.In the central guide bore 29 of the valve housing 15 a control body 205 is used in a fixed position (for example pressed) and by the here as a union nut trained lock nut 54 axially fixed. Of the Control body 205 has one with a reduced diameter Part 206 with which it fits into a central recess 207 of the axially displaceable in the guide bore 29 Control piston 50 protrudes. A first, ring-shaped Control room 211 is radial through part 206 of the Control body 205 and through the guide bore 29, axially through a shoulder surface 209 of the control body 205 and a upper end face 208 of the control piston 50 limited. Of the first control room 211 is again the same as in Control devices 7, 8 and 9 via at least one on the circumference of the control body 205 made connecting groove 157 and via the transverse bore 158 with that through the pilot valve stem 81 lockable outlet opening 159. The Cross bore 158 is the same as in control device 9 via the throttle 198 and via the passage 199 to the upper high pressure supply line 33 (see Fig.1) leading Cross bore 68 connected, which is arranged obliquely here, and the one radial recess 213 of the control body 205 assigned. The recess 213 is via a throttle 214 and a central bore 215 in the control body 205 with a connected second control room 212, which is below the Control body 205 in the central recess 207 of the Control piston 50 is located.

Bei dieser Ausführungsform erfolgt der Öffnungsvorgang ähnlich wie bei der Steuervorrichtung 2 nach Fig.2 in einer Stufe; die Drossel 214 entspricht hier der Drossel 77 aus Fig.2. Allerdings findet bei dieser Variante beim Schliessvorgang keine zusätzliche Beschleunigung statt, wie dies bei der Steuervorrichtung 2 der Fall war. Die Steuervorrichtung 11 ist herstellungs- und montagetechnisch einfach und wie bereits erwähnt vor allem für kleine Brennstoffeinspritzventile geeignet.In this embodiment, the opening process takes place similar to the control device 2 of Figure 2 in a Step; the throttle 214 corresponds here to the throttle 77 Fig. 2. However, this variant takes place at Closing no additional acceleration instead of how this was the case with the control device 2. The Control device 11 is manufacturing and assembly technology simple and as already mentioned especially for small ones Suitable for fuel injectors.

Fig.11 zeigt eine weitere, für das Brennstoffeinspritzventil 2 nach Fig.6 anwendbare Ausführungsform einer Steuervorrichtung 13. Der mit der zentralen, an die Hochdruckzone angeschlossenen Verbindungsbohrung 130 versehene, in der Führungsbohrung 121 des Ventilgehäuses 120 axial verschiebbare Steuerkolben 122 weist oben eine zentrale Ausnehmung 218 auf. In der Führungsbohrung 121 ist ein erster Steuerkörperteil 220 ortsfest angeordnet (beispielsweise eingepresst) und durch die Sicherungsmutter 54 axial fixiert. Ein zweiter Steuerkörperteil 221 ragt in die Ausnehmung 218 hinein und wird von einer in der Ausnehmung 218 angeordneten Feder 222 oben an eine untere Stirnfläche 223 des ersten Steuerkörperteiles 220 gedrückt.11 shows another one for the fuel injector 2 applicable embodiment of a Control device 13. The one with the central one, to the High pressure zone connected connection bore 130 provided in the guide bore 121 of the valve housing 120 axially displaceable control piston 122 has a central top Recess 218 on. There is a first one in the guide bore 121 Control body part 220 arranged stationary (for example pressed in) and axially fixed by the lock nut 54. A second control body part 221 projects into the recess 218 and is arranged in the recess 218 by one Spring 222 on top of a lower end face 223 of the first Control body part 220 pressed.

Der erste Steuerkörperteil 220 ist mit einer Bohrung 260 versehen, die sich in eine vom Pilotventilschaft 81 abschliessbare Auslassöffnung 259 verjüngt, und die über mindestens eine in der unteren Stirnfläche 223 angefertigte radiale Nut 224 mit einem ersten Steuerraum 226 verbunden ist. Die Nut 224 könnte auch in der Stirnfläche des zweiten Steuerkörperteiles 221 ausgebildet sein. Der erste, ringförmige Steuerraum 226 ist radial durch die Führungsbohrung 121 und den zweiten Steuerkörperteil 221, axial durch die untere Stirnfläche 223 des ersten Steuerkörperteiles 220 und eine obere Stirnfläche 225 des Steuerkolbens 122 begrenzt. Ein zweiter, über die Verbindungsbohrung 130 direkt an die Hochdruckzone angeschlossener Steuerraum 227 befindet sich in der Ausnehmung 218 unterhalb des zweiten Steuerkörperteiles 221. The first control body part 220 has a bore 260 provided, which in one of the pilot valve stem 81 lockable outlet opening 259 tapers, and the over at least one made in the lower end face 223 radial groove 224 connected to a first control chamber 226 is. The groove 224 could also be in the end face of the second Control body part 221 may be formed. The first, annular control chamber 226 is radial through the Guide bore 121 and the second control body part 221, axially through the lower end face 223 of the first Control body part 220 and an upper end face 225 of the Spool 122 limited. A second, about that Connection bore 130 directly to the high pressure zone connected control room 227 is in the Recess 218 below the second control body part 221.

Der zweite Steuerkörperteil 221 ist mit einer zentralen Bohrung 257 versehen, die sich oben in eine Einlassdrosselbohrung 258 verjüngt. Über die Einlassdrosselbohrung 258 ist (ähnlich wie über die Einlassdrosselbohrung 58 nach Fig.2) der erste Steuerraum 226 mit der Hochdruckzone verbunden. Die Feder 222 kann eventuell entfallen, da der im zweiten Steuerraum 227 herrschende Systemhochdruck für das ständige Andrücken des zweiten Steuerkörperteiles 221 an den ersten Steuerkörperteil 220 sorgt.The second control body part 221 has a central one Provide hole 257, which is in a top Inlet throttle bore 258 tapers. About the Inlet throttle bore 258 is (similar to that over the Inlet throttle bore 58 according to FIG. 2) the first control chamber 226 connected to the high pressure zone. The spring 222 can possibly omitted since the one prevailing in the second control room 227 System high pressure for the constant pressing of the second Control body part 221 to the first control body part 220 worries.

Die Steuervorrichtung 13 entspricht in ihrer Wirkungsweise der erwähnten, in der Zeichnung jedoch nicht dargestellten zweiten alternativen Variante zur Steuervorrichtung 2 nach Fig.2. Auch bei dieser Variante herrscht im zweiten Steuerraum 227 ständig der Systembrennstoffhochdruck, der durch die Pumpwirkung des Steuerkolbens 122 praktisch unbeeinflusst bleibt. Die Öffnungs- und Schliessbewegung des Steuerkolbens 122 und somit auch der Düsennadel 24 wird über die ringförmige obere Stirnfläche 225 des Steuerkolbens 122 durch den im ersten Steuerraum 226 herrschenden Steuerdruck gesteuert, wobei dieser Steuerdruck von der Auslegung und räumlichen Anordnung der Einlassdrosselbohrung 258 und der Auslassöffnung 259 abhängig ist.The control device 13 corresponds in its mode of operation the mentioned, but not shown in the drawing second alternative variant to the control device 2 Fig. 2. This variant also prevails in the second Control room 227 constantly the system fuel high pressure by the pumping action of the control piston 122 practically remains unaffected. The opening and closing movement of the Control piston 122 and thus also the nozzle needle 24 is over the annular upper end face 225 of the control piston 122 by the control pressure prevailing in the first control chamber 226 controlled, this control pressure from the design and spatial arrangement of the inlet throttle bore 258 and Exhaust opening 259 is dependent.

Die Teilung eines einzigen Steuerkörpers in zwei Steuerkörperteile 220,221 bringt eine besonders einfache Herstellung und Montage der Steuervorrichtung 13 mit sich.The division of a single control body into two Control body parts 220.221 brings a particularly simple Manufacture and assembly of the control device 13 with itself.

Eine weitere Ausführungsform einer Steuervorrichtung 22 für das Brennstoffeinspritzventil 2 nach Fig.6 ist in Fig.12 dargestellt und im folgenden beschrieben. Für die bereits bekannten Teile werden wieder gleiche Bezugsziffern verwendet.Another embodiment of a control device 22 for the fuel injection valve 2 according to FIG. 6 is in FIG. 12 shown and described below. For those already known parts are again the same reference numerals used.

Diese Ausbildungsform ist ähnlich wie die Steuervorrichtung 11 nach Fig.10 besonders für kleine Brennstoffeinspritzventile geeignet, bei denen kein Platz zum Anordnen von Ventilen und Federn vorhanden ist.This form of training is similar to the control device 11 according to Fig. 10 especially for small ones Fuel injectors suitable where there is no space for Arranging valves and springs is present.

Der erste Steuerraum 155 der Steuervorrichtung 22 ist gleich wie bei der Steuervorrichtung 7 nach Fig.6 und 7 radial durch die Führungsbohrung 121 und den im Durchmesser abgesetzten Kolbenteil 123, axial durch einen Kolbenabsatz 126 und die untere Stirnfläche 139 des Steuerkörpers 135 begrenzt. Der Kolbenteil 123 ist hier noch mit einem zusätzlich abgesetzten Teil 190 versehen. Ein zweiter Steuerraum 195 ist oberhalb des Kolbenteils 123 in der Ausnehmung 136 des Steuerkörpers 135 gebildet. Eine im abgesetzten Teil 190 radial angefertigte Drossel 191 verbindet den zweiten Steuerraum 195 mit der Verbindungsbohrung 130 und somit mit der Brennstoffhochdruckzone. Die Drossel 191 könnte auch auf der Längsachse des Steuerkolbens 122 bzw. des Brennstoffeinspritzventils 2 ( ähnlich wie die Drosselbohrungen 197 und 159 ) angebracht werden. Im Steuerkörper 135 ist eine in den zweiten Steuerraum 195 mündende, zentrale Bohrung 196 vorhanden, die über eine Drossel 197 mit der Querbohrung 158 verbunden ist. Der erste Steuerraum 155 ist hier im Gegensatz zu der Steuervorrichtung 7 nach Fig.7 nicht mit dem Hochdrucksystem verbunden ( vgl. Drosselbohrung 133 in Fig.7 ), sondern er erhält über die Drossel 197, die Querbohrung 158 und die Verbindungsnut 157 Druck vom zweiten Steuerraum 195. Der Druck in den beiden Steuerräumen 155, 195 bzw. die Pumpwirkung des Steuerkolbens 122 hängt sowohl beim Öffnen, als auch beim Schliessen von der Auslegung der Drosseln 191, 197 ab. Die Drossel 191 ersetzt den ersten Ventilflachsitz 151 bzw. die Drosselbohrung 142 nach Fig.7. Bei dieser Ausführungsform findet beim Schliessvorgang keine zusätzliche Beschleunigung statt. Die Ausbildungsform sowie auch Montage ist extrem einfach.The first control chamber 155 of the control device 22 is the same as in the control device 7 according to Figures 6 and 7 radially through the guide bore 121 and the stepped in diameter Piston part 123, axially through a piston shoulder 126 and the lower end face 139 of the control body 135 limited. Of the Piston part 123 is here with an additional offset Part 190 provided. A second control room 195 is above of the piston part 123 in the recess 136 of the control body 135 formed. One in the offset part 190 radially Made throttle 191 connects the second control room 195 with the connecting bore 130 and thus with the High pressure fuel zone. The throttle 191 could also on the Longitudinal axis of the control piston 122 or the Fuel injector 2 (similar to that Throttle bores 197 and 159) are attached. in the Control body 135 is one in the second control chamber 195 opening, central bore 196 available, which over a Throttle 197 is connected to the transverse bore 158. The first Control room 155 is here in contrast to the control device 7 not connected to the high pressure system according to FIG. 7 (cf. Throttle bore 133 in Fig.7), but it receives over the Throttle 197, the transverse bore 158 and the connecting groove 157 Pressure from the second control room 195. The pressure in the two Control rooms 155, 195 or the pumping action of the control piston 122 hangs both when opening and when closing the design of the chokes 191, 197. The throttle 191 replaces the first valve flat seat 151 or the Throttle bore 142 according to Fig. 7. In this embodiment finds no additional acceleration during the closing process instead of. The form of training as well as assembly is extreme simple.

Claims (26)

  1. Fuel injection valve for the intermittent injection of fuel into the combustion space of an internal combustion engine, having a housing (15; 120), having a valve seat element (19) provided with injection openings (21), having a longitudinally displaceable injection valve member mounted in the housing (15; 120) for closing or opening the injection openings (21), having a control device (3; 4; 5; 6; 7; 8; 9; 11; 13; 22) for controlling the displacement movement of the injection valve member, the control device (3; 4; 5; 6; 7; 8; 9; 11; 13; 22) having a control piston (50; 122) guided so as to be longitudinally displaceable in a guide hole (29; 121) and being connected to the injection valve member and being subjected on one side to the system fuel pressure from a high-pressure fuel supply conduit (32; 31) and on the other side to the fuel control pressure in a first control chamber (70; 155; 160; 201; 211; 226), the first control chamber (70; 155; 160; 201; 211; 226) being in connection with the high-pressure fuel supply conduit (31) by means of at least one inlet throttle (58; 97; 133; 184; 197; 198; 258), and the control pressure in the first control chamber (70; 155; 160; 201; 211; 226) being controllable by opening or closing at least one outlet opening (59; 159; 259), whereto the control device (3; 4; 5; 6; 7; 8; 9; 11; 13; 22) is provided with a controllable pilot valve (80), characterized in that the control device (3; 4; 5; 6; 7; 8; 9; 11; 13; 22) has a second control chamber (74; 156; 165; 195; 202; 212; 227) which is connected continuously or at times to the high-pressure supply conduit (31), whose volume is changed by the displacement movement of the control piston (50; 122), whereby the pressure in the second control chamber (74; 156; 165; 195; 202; 212; 227) acts in opposition to the opening movement of the injection valve member and respectively of the control piston (50; 122).
  2. Fuel injection valve according to Claim 1, characterized in that the pressure in the second control chamber (74; 156; 165; 202; 227) is kept practically constant by means of a direct connection (130) of the second control chamber (74; 156; 165; 202; 227) with the high-pressure supply conduit (31).
  3. Fuel injection valve according to Claim 1, characterized in that during the opening movement of the injection valve member and respectively of the control piston (50; 122) an increase in pressure acting against this opening movement is generated in the second control chamber (74; 156; 165; 195; 212), the control device (3; 4; 5; 6; 7; 8; 9; 11; 13; 22) having relief elements (75, 77; 95; 103; 113, 117; 142, 151; 171, 175; 191; 214) for connecting the second control chamber (74; 156; 165; 195; 212) to the high-pressure supply conduit (31).
  4. Fuel injection valve according to Claim 3, characterized in that means (64; 94; 98; 152; 162) are provided by means of which a rapid closing movement of the injection valve member and respectively of the control piston (50; 122) can take place.
  5. Fuel injection valve according to Claim 4, characterized in that by the means (64; 94; 98; 152; 162) when the fuel pressure in the second control chamber (74; 156; 165) drops, a direct connection is freed from the high pressure conduit (33, 31) to one of the two control chambers (70; 156; 160) in order to effect a further acceleration of the control piston (50; 122).
  6. Fuel injection valve according to one of the Claims 3 to 5, in which the first control chamber (70) is arranged between an upper end surface (56) of the control piston (50) and a fixed control body (52) provided with the outlet opening (59), characterized in that the control piston (50) has a reduced diameter piston part (51) and a corresponding piston shoulder surface (53), in that a displaceable sleeve (64; 94; 98) is arranged with a close sliding fit on the one side on the piston part (51) and on the other side in the guide hole (29), in that the second, annular control chamber (74) is bounded radially by the piston part (51) and the guide hole (29) and axially at least by the piston shoulder surface (53) and a lower end surface (65) of the sleeve (64; 94; 98), and in that the sleeve (64; 94; 98), which is in contact by means of a sealing surface (66; 96) on the control body (52) when the pressure in both control chambers (70; 74) is the same as well as during the opening movement of the control piston (50), during the closing movement of the control piston (50) at a given pressure drop in the second control chamber (74) frees a connection between the high-pressure fuel supply conduit (33) and the first control chamber (70).
  7. Fuel injection valve according to one of the Claims 3 to 6, characterized in that the relief elements are formed by a connecting bore (75) provided with a throttle (77) and connecting the second control chamber (74) with the high-pressure supply conduit (33).
  8. Fuel injection valve according to one of the Claims 3 to 6, characterized in that the relief elements are formed by a ball non-return valve (103).
  9. Fuel injection valve according to one of the Claims 3 to 6, characterized in that the relief elements are formed by valve (113), the valve body (114) of which is provided with a throttle hole (117) connecting the second control chamber (74) to the high-pressure supply conduit (33) when the seat (115) of the valve is closed.
  10. Fuel injection valve according to Claim 6, characterized in that the sleeve (94) has at the circumference a plurality of ribs (95) arranged axially in series, everyone of which is forming an annular gap (93) relative to the guide hole (29), the ribs (95) forming the relief elements in the connection of the second control chamber (74) with the high-pressure supply conduit which opens into the guide hole (29) above the uppermost rib (95).
  11. Fuel injection valve according to Claim 6, characterized in that the sealing surface (66; 96) of the sleeve (64; 94; 98) is provided with a plurality of depressions (97) which form the inlet throttle connection between the high pressure supply conduit (33) and the first control chamber (70).
  12. Fuel injection valve according to one of the Claims 1 to 3, having a fixed-location control body (135) provided with the outlet opening (159), characterized in that the control body (135) is provided with a recess (136) into which protrudes an upper, reduced diameter piston part (123) with a close sliding fit to permit displacement, and in that the first, annular control chamber (155) is radially bounded by the piston part (123) and by the guide hole (121) and is axially bounded by a piston shoulder (126) and a lower end surface (139) of the control body (135).
  13. Fuel injection valve according to one of the Claims 1 to 3, having a fixed-location control body (135) provided with the outlet opening (159), characterized in that the control body (135) is provided with a recess (136) into which an intermediate piston (162) protrudes with a close sliding fit, which is operatively connected by means of a sealing surface (168) to an upper end surface (161) of the control piston (122), and in that the first, annular control chamber (160) is radially bounded by the intermediate piston (162) and the guide hole (121) and is axially bounded by the upper end surface (161) of the control piston (122) and a lower end surface (139) of the control body (135).
  14. Fuel injection valve according to Claim 12, characterized in that the second control chamber (156; 195) is formed above a piston end surface (127) in the recess (136) and is connected by means of a throttle (142; 191) to a connecting hole (130), which is arranged centrally in the control piston (122), to the high-pressure supply conduit (31).
  15. Fuel injection valve according to Claim 13, characterized in that the second control chamber (165) is formed above an end surface (163) of the intermediate piston (162) in the recess (136) and is connected by means of a throttle (175) to a connecting hole (130), which is arranged centrally in the control piston (122), to the high-pressure supply conduit (31).
  16. Fuel injection valve according to Claim 5, Claim 12 and Claim 14, characterized in that the upper piston end surface (127) is associated with a valve seat disc (140) provided with the throttle (141) and separating the second control chamber (156) from the connecting hole (130), which valve seat disc (140) forms, together with the piston end surface (127), a valve flat seating (152) which, when there is a certain drop in pressure in the second control chamber (156) during the closing event, frees the direct connection between the second control chamber (156) and the connecting hole (130) and, by this means, permits the piston to be directly subjected to the high fuel pressure.
  17. Fuel injection valve according to Claim 16, characterized in that the piston part (123) is provided with a recess (128) in which is arranged an axially movable valve body (143) provided with the throttle (142), in that the valve seat disc (140) has a disc hole (141) which can be closed by the valve body (143) with the exception of the throttle (142), and in that the valve seat disc (140), together with the valve body (143), forms a further valve flat seating (151) for relieving the second control chamber (156) when there is a given pressure rise during the opening motion of the control piston (122).
  18. Fuel injection valve according to Claim 5, Claim 13 and Claim 15, characterized in that the intermediate piston (162), which is in contact by means of the sealing surface (168) with the end surface (161) of the control piston (122) when there is the same pressure in both control chambers (160, 165), frees the connection between the connecting hole (130) or the high-pressure supply conduit (31) and the first control chamber (160) when during the closing movement of the control piston (122) a given pressure drop in the second control chamber (165) takes place.
  19. Fuel injection valve according to Claim 3 and Claim 15, characterized in that the intermediate piston (162) is provided with a recess (170) which is connected to the connecting hole (130) and in which is arranged a valve (171) closing a connecting bore (174) between the recess (170) and the second control chamber (165) in order to relieve the second control chamber (165) at a given pressure rise during the opening movement of the control piston (122).
  20. Fuel injection valve according to Claim 15 and Claim 19, characterized in that the throttle (175) is manufactured parallel to the connecting hole (174) in the intermediate piston (162) and opens into the recess (170).
  21. Fuel injection valve according to Claim 3 and according to either of Claims 12 or 13, characterized in that the first control chamber (155; 160) is connected to the outlet opening (159) by means of a connecting groove (157) on the periphery of the control body (135) and by means of a transverse hole (158) in the control body (135).
  22. Fuel injection valve according to Claim 3 and Claim 12, characterized in that the first control chamber (155) is connected to the high-pressure supply conduit (31) by means of an inlet throttle (133) which is manufactured in the piston part (123) and which opens radially into a central connecting hole (130) of the control piston (122).
  23. Fuel injection valve according to Claim 3 and Claim 13, characterized in that the first control chamber (160) is in connection with the high-pressure supply conduit (31) by means of an inlet throttle (184) manufactured in the intermediate piston (162) and opening radially into a central hole (180) of the intermediate piston (162).
  24. Fuel injection valve according to Claim 3 and Claim 13, characterized in that the sealing surface (168) of the intermediate piston (162) is provided with a plurality of depressions which form the inlet throttle connection between the high-pressure supply conduit (31) and the first control chamber (160).
  25. Fuel injection valve according to Claim 12, Claim 14 and Claim 21, characterized in that the second control chamber (195) is connected onto the transverse hole (158) by means of a hole (196) manufactured in the control body (135) and provided with a throttle (197) and is therefore in connection with the first control chamber (155).
  26. Fuel injection valve for the intermittent injection of fuel into the combustion space of an internal combustion engine, particularly according to one of the Claims 1 to 25, having a housing (120), having a valve seat element (19) provided with injection openings (21), having a longitudinally displaceable injection valve member (24) mounted in the housing (120) for closing or opening the injection openings (21), having a control device (13) for controlling the displacement movement of the injection valve member (24), the control device (13) having a control piston (122) guided so as to be longitudinally displaceable in a guide hole (121) and being connected to the injection valve member (24) and being subjected on one side to the system fuel pressure from a high-pressure fuel supply conduit (31) and on the other side to the fuel control pressure in a control chamber (226), the control chamber (226) being in connection with the high-pressure fuel supply conduit (31) by means of at least one inlet opening (258), and the control pressure in the control chamber (226) being controllable by opening or closing at least one outlet opening (259), whereto the control device (13) is provided with a controllable pilot valve (80, 81, 82), characterized in that the control device (13) has a second chamber (227) which is connected continuously to the high-pressure supply conduit (31), which is foreseen in a recess (218) in the control piston (122) and which is closed by one end-side of a control element (221) arranged in the recess (218), the control element (221) being movable relative to the control piston (122), whereby the pressure in the second chamber (227) acts in opposition to the opening movement of the injection valve member (24) and respectively of the control piston (122) and presses the other end-side of the control element (221) against a housing-fixed stop (220), and whereby a displacement movement of the control piston (122) relative to the control element (221) supported against the housing-fixed stop (220) changes the volume of the second chamber (227).
EP95107718A 1994-06-06 1995-05-20 Fuel injection valve for internal combustion engines Expired - Lifetime EP0686763B1 (en)

Priority Applications (1)

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EP97112502A EP0807757A1 (en) 1994-06-06 1995-05-20 Fuel injection valve for internal combustion engines

Applications Claiming Priority (3)

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CH178294 1994-06-06
CH178294 1994-06-06
CH1782/94 1994-06-06

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EP0787900A2 (en) * 1996-01-30 1997-08-06 Wartsila Diesel International Ltd. OY Injection valve arrangement
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US5992767A (en) * 1997-01-11 1999-11-30 Lucas Industries Plc Injector
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EP0807757A1 (en) 1997-11-19
ATE184078T1 (en) 1999-09-15
DE59506715D1 (en) 1999-10-07
JPH07332193A (en) 1995-12-22
EP0686763A1 (en) 1995-12-13
US5685483A (en) 1997-11-11
US5842640A (en) 1998-12-01

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