GB735866A - Improvements in or relating to fuel pumps and systems - Google Patents
Improvements in or relating to fuel pumps and systemsInfo
- Publication number
- GB735866A GB735866A GB4150/52A GB415052A GB735866A GB 735866 A GB735866 A GB 735866A GB 4150/52 A GB4150/52 A GB 4150/52A GB 415052 A GB415052 A GB 415052A GB 735866 A GB735866 A GB 735866A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- pipe
- nozzle
- venturi
- air
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D9/00—Priming; Preventing vapour lock
- F04D9/001—Preventing vapour lock
- F04D9/002—Preventing vapour lock by means in the very pump
- F04D9/003—Preventing vapour lock by means in the very pump separating and removing the vapour
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D31/00—Pumping liquids and elastic fluids at the same time
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Jet Pumps And Other Pumps (AREA)
Abstract
735,866. Centrifugal and screw pumps. ROLLS-ROYCE, Ltd. May 15, 1953 [Feb. 15, 1952], No. 4150/52. Class 110 (1). [Also in Group XXVIII] In a fuel pump, a pipe or conduit is provided, with an inlet at or near a location at which free air or vapour collects, and a stream of fluid is produced in the pipe or conduit to withdraw the air or vapour and entrain it in the fluid stream. Fig. 1 shows a fuel pump submerged in a fuel tank 10 and driven by an electric motor 15. Fuel under pressure is tapped off from the volute 12a and passes through a pipe 20, gland 19 and bores 18a and 18 in the driving shaft 14 to a nozzle 21. The nozzle discharges into a venturi 22 leading to a drain pipe 23 which preferably discharges to the tank 10. The nozzle and venturi form an injector which withdraws air or vapour accumulating in the central space 16 and entrains it in the jet of fuel issuing from the nozzle. In the fuel pump shown in Fig. 3, air or vapour liberated at the periphery of the impeller 35 passes through an annular gap 38a to a manifold 38, from which it is withdrawn by an injector comprising a nozzle 41 and venturi 39 and discharged through a pipe 40. The entraining fluid comprises fuel under pressure supplied to the nozzle 41 from the volute 36. The manifold 38 may have more than one outlet. The impeller 35 may be of the helical or helicocentrifugal types. Fig. 2 shows a modification of Fig. 1, but a similar modification may be applied to Fig. 3. The venturi 22 is replaced by a plain pipe 24 leading to a discharge pipe 25 having a venturi portion 25b. Entraining fuel is fed from the volute 12a through a pipe 27 to a nozzle 26. An additional nozzle 28 may be provided, fed with an inert gas such as nitrogen. The inert gas, mixed with fuel and air, passes through the pipe 25 to the fuel tank and forms a non-explosive atmosphere above the free surface of the fuel. In any of these embodiments, the fuel used for operating the injector may be derived from the exhaust of a hydraulic motor which drives the pump and is fed with motive fluid from a main fuel pump which is connected in series with the pump, as described in Specification 735,874.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4150/52A GB735866A (en) | 1952-02-15 | 1952-02-15 | Improvements in or relating to fuel pumps and systems |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4150/52A GB735866A (en) | 1952-02-15 | 1952-02-15 | Improvements in or relating to fuel pumps and systems |
Publications (1)
Publication Number | Publication Date |
---|---|
GB735866A true GB735866A (en) | 1955-08-31 |
Family
ID=9771682
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4150/52A Expired GB735866A (en) | 1952-02-15 | 1952-02-15 | Improvements in or relating to fuel pumps and systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB735866A (en) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1183376B (en) * | 1958-06-06 | 1964-12-10 | Dr Ernst Lange | Device for venting centrifugal pumps during their operation with a venting pipe arranged near the hub of the impeller |
US3323465A (en) * | 1964-04-17 | 1967-06-06 | Shell Oil Co | Inlet piece for a centrifugal pump |
DE1274446B (en) * | 1960-07-22 | 1968-08-01 | Hans Ley | Venting device for self-priming centrifugal pumps |
US3438330A (en) * | 1965-10-20 | 1969-04-15 | Waterous Co | Noise suppression means |
US3660127A (en) * | 1969-08-11 | 1972-05-02 | Lake Chemical Co | Flux for use in soldering of stainless steels |
FR2175847A1 (en) * | 1972-03-10 | 1973-10-26 | Lucas Aerospace Ltd | |
US4183722A (en) * | 1977-06-06 | 1980-01-15 | Roeder George K | Downhole jet pumps |
FR2564744A1 (en) * | 1984-05-24 | 1985-11-29 | Spiro Research Bv | METHOD AND DEVICE FOR DECREASING THE GAS CONTENT OF A LIQUID |
DE3810950A1 (en) * | 1988-03-31 | 1989-10-12 | Klein Schanzlin & Becker Ag | Degassing device |
WO1995018337A1 (en) * | 1993-12-31 | 1995-07-06 | J. Eberspächer | Vehicle heating appliance with water pump venting |
EP3045734A1 (en) * | 2015-01-15 | 2016-07-20 | Honeywell International Inc. | Centrifugal fuel pump with an auxiliary inlet for the injection of inert gas and with a valve regulating the gas flow |
US9656187B2 (en) | 2014-11-12 | 2017-05-23 | Honeywell International Inc. | Fuel deoxygenation system contactor-separator |
US9687773B2 (en) | 2014-04-30 | 2017-06-27 | Honeywell International Inc. | Fuel deoxygenation and fuel tank inerting system and method |
US9834315B2 (en) | 2014-12-15 | 2017-12-05 | Honeywell International Inc. | Aircraft fuel deoxygenation system |
EP3434904A1 (en) * | 2017-07-24 | 2019-01-30 | Hamilton Sundstrand Corporation | Hydrocarbon fuel system |
-
1952
- 1952-02-15 GB GB4150/52A patent/GB735866A/en not_active Expired
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1183376B (en) * | 1958-06-06 | 1964-12-10 | Dr Ernst Lange | Device for venting centrifugal pumps during their operation with a venting pipe arranged near the hub of the impeller |
DE1274446B (en) * | 1960-07-22 | 1968-08-01 | Hans Ley | Venting device for self-priming centrifugal pumps |
US3323465A (en) * | 1964-04-17 | 1967-06-06 | Shell Oil Co | Inlet piece for a centrifugal pump |
US3438330A (en) * | 1965-10-20 | 1969-04-15 | Waterous Co | Noise suppression means |
US3660127A (en) * | 1969-08-11 | 1972-05-02 | Lake Chemical Co | Flux for use in soldering of stainless steels |
FR2175847A1 (en) * | 1972-03-10 | 1973-10-26 | Lucas Aerospace Ltd | |
US4183722A (en) * | 1977-06-06 | 1980-01-15 | Roeder George K | Downhole jet pumps |
AT399291B (en) * | 1984-05-24 | 1995-04-25 | Spiro Research Bv | METHOD AND DEVICE FOR REDUCING THE GAS CONTENT OF A LIQUID |
FR2564744A1 (en) * | 1984-05-24 | 1985-11-29 | Spiro Research Bv | METHOD AND DEVICE FOR DECREASING THE GAS CONTENT OF A LIQUID |
DE3810950A1 (en) * | 1988-03-31 | 1989-10-12 | Klein Schanzlin & Becker Ag | Degassing device |
WO1995018337A1 (en) * | 1993-12-31 | 1995-07-06 | J. Eberspächer | Vehicle heating appliance with water pump venting |
US5660329A (en) * | 1993-12-31 | 1997-08-26 | J. Eberspacher Gmbh & Co. | Vehicle heater with water pump venting |
US9687773B2 (en) | 2014-04-30 | 2017-06-27 | Honeywell International Inc. | Fuel deoxygenation and fuel tank inerting system and method |
US9656187B2 (en) | 2014-11-12 | 2017-05-23 | Honeywell International Inc. | Fuel deoxygenation system contactor-separator |
US9834315B2 (en) | 2014-12-15 | 2017-12-05 | Honeywell International Inc. | Aircraft fuel deoxygenation system |
EP3045734A1 (en) * | 2015-01-15 | 2016-07-20 | Honeywell International Inc. | Centrifugal fuel pump with an auxiliary inlet for the injection of inert gas and with a valve regulating the gas flow |
US9897054B2 (en) | 2015-01-15 | 2018-02-20 | Honeywell International Inc. | Centrifugal fuel pump with variable pressure control |
EP3434904A1 (en) * | 2017-07-24 | 2019-01-30 | Hamilton Sundstrand Corporation | Hydrocarbon fuel system |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB735866A (en) | Improvements in or relating to fuel pumps and systems | |
US4037991A (en) | Fluid-flow assisting devices | |
US2000741A (en) | Fluid jet pump | |
US2439273A (en) | Turbo-jet engine for aircraft | |
GB583022A (en) | Improvements relating to internal combustion turbines and the like | |
GB1332072A (en) | Aircraft engine fuel system | |
US2693674A (en) | Driving device for turbojet boosting auxiliaries | |
GB1125251A (en) | Improved gas turbine engine | |
GB574140A (en) | Improvements in or relating to pumping systems | |
SE8503224D0 (en) | centrifugal | |
GB1116549A (en) | Internal combustion engine fuel systems | |
ES435536A1 (en) | Liquid ring compressor | |
GB709002A (en) | Improvements relating to fuel systems for internal combustion engines | |
GB636712A (en) | Pump assembly | |
GB735874A (en) | Improvements relating to gas-turbine engine fuel systems | |
US2791968A (en) | Self-priming centrifugal pump | |
US1326652A (en) | Inghouse electric | |
GB743859A (en) | Improvements in or relating to fuel systems for gas-turbine engines | |
GB654854A (en) | Liquid pumping unit | |
GB709868A (en) | Improvements in and relating to self-priming centrifugal pumps | |
GB684230A (en) | Improvements relating to a liquified gas system of a rocket motor | |
GB635270A (en) | Improvements in or relating to centrifugal pumps and compressors | |
GB914077A (en) | Centrifugal boost pumps for aircraft fuel systems | |
GB684428A (en) | Improvements in or relating to a power plant | |
GB191029357A (en) | Improvements in Rotary Pumps, Condensers or Compressors. |