EP0124512A1 - Turbo jet pump - Google Patents
Turbo jet pumpInfo
- Publication number
- EP0124512A1 EP0124512A1 EP19820903226 EP82903226A EP0124512A1 EP 0124512 A1 EP0124512 A1 EP 0124512A1 EP 19820903226 EP19820903226 EP 19820903226 EP 82903226 A EP82903226 A EP 82903226A EP 0124512 A1 EP0124512 A1 EP 0124512A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- diverter
- jet pump
- turbo jet
- direct
- reactor
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H11/00—Marine propulsion by water jets
- B63H11/02—Marine propulsion by water jets the propulsive medium being ambient water
- B63H11/04—Marine propulsion by water jets the propulsive medium being ambient water by means of pumps
- B63H11/08—Marine propulsion by water jets the propulsive medium being ambient water by means of pumps of rotary type
Definitions
- Sheet 1/4 - 4/4 shows invention of the Turbo Jet Pump, invented, designed and constructed by George Branko Skrinjar for heavy liquids.
- FIG. 1 - 2 is a longitudinal section of the Turbo Jet Pump showing the main elements.
- FIG. 1A- 2A is a cross section A - A, through the Suction stage of the Turbo Jet Pump, showing the Front of the Action Impeller.
- FIG. 1B- 2B is a cross section B - B, through the Diverter stage I showing the Front of the Diverter
- FIG. 1C- 2C is a cross section C -C, through the Reactor stage showing the Front of the Reactor Turbine wheel.
- FIG. 1D- 2D is a cross section C - C, through the Diverter stage II, showing the Front of the Diverter
- the Diverter Core 15, is connected with Diverter Ribs 14, to the Diverter Body 16.
- the Reactor Blades 17, are fixed to the Reactor Wheel 18, which freely rotates in the slide Bearing 19, on the Shaft 20, casted in the Diverter Core 22, connected with Diverter Ribs 21, to the Diverter Body 23, which is bolted together with first Diverter stage Body 16, sheet 1/4, FIG.
- FIG. 1E - 1L and 2E - 2L show elevation, plan and contuor line of the Blades and Ribs.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Une pompe de turbo réacteur comprend un arbre entraîné (6) avec des lames de turbine fixées (13), des lames de rotor (17) pouvant tourner librement sur l'arbre (20), le liquide pompé étant forcé de passer par des nervures de dérivation (14 et 21) à une vitesse s'accroissant.A turbojet pump comprises a driven shaft (6) with fixed turbine blades (13), rotor blades (17) which can rotate freely on the shaft (20), the pumped liquid being forced to pass through ribs bypass (14 and 21) at an increasing speed.
Description
Turbo Jet Pump
D E S C R I P T I O N
Sheet 1/4 - 4/4 shows invention of the Turbo Jet Pump, invented, designed and constructed by George Branko Skrinjar for heavy liquids.
Sheet 1/4 - 4/4 shows invention of the Turbo Jet Pump, invented, designed and constructed by George Branko Skrinjar for light liquids. FIG. 1 - 2 is a longitudinal section of the Turbo Jet Pump showing the main elements. FIG. 1A- 2A is a cross section A - A, through the Suction stage of the Turbo Jet Pump, showing the Front of the Action Impeller. FIG. 1B- 2B is a cross section B - B, through the Diverter stage I showing the Front of the Diverter
Passages. FIG. 1C- 2C is a cross section C -C, through the Reactor stage showing the Front of the Reactor Turbine wheel. FIG. 1D- 2D is a cross section C - C, through the Diverter stage II, showing the Front of the Diverter
Passages.
Through the Turbo Jet Pump Body 1 , passes vertical drive shaft 2, which rotates in the Bearings 3 and 4., the Vertical drive Shaft 2, through helical Gears 5, in the gear Box 9, and horizontal Shaft 6, which is rotating in its Bearings 7 and 8 and 12, rotates the Impeller 10, assembled on the shaft with Keys 11., the Impeller 10, has blades 13.
The Diverter Core 15, is connected with Diverter Ribs 14, to the Diverter Body 16., the Reactor Blades 17, are fixed to the Reactor Wheel 18, which freely rotates in the slide Bearing 19, on the Shaft 20, casted in the Diverter Core 22, connected with Diverter Ribs 21, to the Diverter Body 23, which is bolted together with first Diverter stage Body 16, sheet 1/4, FIG. 1, to the Body 1, with Bolts 24.,
The Cap 25, is fixed with bolts to the gear box Body 9., the Flange 26, holds the Bearing 3, in position, and is bolted to the Turbo Jet Pump Body 1., the seal Ring 27, is positioned in the groove between Impeller Body 10, and first stage Diverter Core 15., the Desmophrene packers 28, are pressed into the gear Box 9., the Diverter Body 23, and the Diverter Eody 16, are fixed with Bolts 29,and 24, to each other, and together to the Turbo Jet Pump Body 1., the Thrust Bearing 30, is situated in the Flange 26, bolted to the Turbo Jet Pump Body 1.
FIG. 1E - 1L and 2E - 2L, show elevation, plan and contuor line of the Blades and Ribs.
Claims
C L A I M S
CLAIM 1 Principle of Operation
Suction of the Media direct from the Front into the
Turbo Jet Pump. Divertisation of molecules of the
Media streams flow, and transfer of Media flow by rotation of the Reactor turbine, through Diverters out to the back through jet nozzle.
CLAIM 2 The Contour line, outside and inside of the operation Stages elements of the Turbo Jet Pump. CLAIM 3 Stages of Operation
Action Impeller, Diverter I, Reactor, Diverter II. CLAIM 4 Driven direct or through transmission with flexible or solid vertical or horizontal shaft by combustion engines or electric motors.
CLAIM 5 Assembly of the Turbo Jet Pump direct into pipe line or in any degree elbow.
CLAIM 6 As a water bore Pump, direct into the casing. CLAIM 7 For Pumping the gases and light and heavy liquids. CLAIM 8 Impeller Blades from 55 -- 3311 Diverter I Ribs from 66 -- 3322 Reactor Blades from 33 -- 2299
Diverter II Ribs from 44 -- 3300
Inlet ϕ S from 50 mm -- 17 000 mm
Outlet ϕ O from 10 mm -- 10 000 mm
Length 0 from 100 mm -- 30000 mm
CLAIM 9 Operation in Reverse. CLAIM 10 The Turbo Jet Pump, is a Pump System Skrinjar.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/AU1982/000177 WO1984001758A1 (en) | 1982-10-27 | 1982-10-27 | Turbo jet pump |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP0124512A1 true EP0124512A1 (en) | 1984-11-14 |
Family
ID=3760626
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP19820903226 Withdrawn EP0124512A1 (en) | 1982-10-27 | 1982-10-27 | Turbo jet pump |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP0124512A1 (en) |
| AU (1) | AU9052682A (en) |
| WO (1) | WO1984001758A1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN212550093U (en) * | 2020-04-30 | 2021-02-19 | 南京韬恒工业科技有限公司 | Pulverized coal injection device |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2965065A (en) * | 1955-06-15 | 1960-12-20 | Walter H Tinker | Hydraulic jet propulsion units for boats |
| US3328961A (en) * | 1965-10-13 | 1967-07-04 | Twin Disc Clutch Co | Multiple stage, hydraulic jet propulsion apparatus for water craft |
| AU412103B2 (en) * | 1966-11-18 | 1968-05-23 | The Buehler Corporation | Jetboat pump |
| US3405526A (en) * | 1967-03-01 | 1968-10-15 | Twin Disc Inc | Multiple stage, hydraulic jet propulsion apparatus for water craft |
-
1982
- 1982-10-27 EP EP19820903226 patent/EP0124512A1/en not_active Withdrawn
- 1982-10-27 AU AU90526/82A patent/AU9052682A/en not_active Abandoned
- 1982-10-27 WO PCT/AU1982/000177 patent/WO1984001758A1/en unknown
Non-Patent Citations (1)
| Title |
|---|
| See references of WO8401758A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| AU9052682A (en) | 1984-05-22 |
| WO1984001758A1 (en) | 1984-05-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): CH DE FR GB LI NL SE |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
| 18D | Application deemed to be withdrawn |
Effective date: 19840928 |