GB9510164D0 - Fuel supply arrangement for turbojet engines with afterburner - Google Patents
Fuel supply arrangement for turbojet engines with afterburnerInfo
- Publication number
- GB9510164D0 GB9510164D0 GBGB9510164.8A GB9510164A GB9510164D0 GB 9510164 D0 GB9510164 D0 GB 9510164D0 GB 9510164 A GB9510164 A GB 9510164A GB 9510164 D0 GB9510164 D0 GB 9510164D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- afterburner
- fuel supply
- supply arrangement
- turbojet engines
- turbojet
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F02C7/236—Fuel delivery systems comprising two or more pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F02C7/228—Dividing fuel between various burners
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19944418680 DE4418680C2 (en) | 1994-05-28 | 1994-05-28 | Fuel supply device for a turbo jet engine with afterburner |
Publications (3)
Publication Number | Publication Date |
---|---|
GB9510164D0 true GB9510164D0 (en) | 1995-08-02 |
GB2289722A GB2289722A (en) | 1995-11-29 |
GB2289722B GB2289722B (en) | 1997-09-10 |
Family
ID=6519207
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9510164A Expired - Fee Related GB2289722B (en) | 1994-05-28 | 1995-05-19 | Fuel supply arrangement for turbojet engines with afterburner |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE4418680C2 (en) |
FR (1) | FR2720442B1 (en) |
GB (1) | GB2289722B (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9900115D0 (en) * | 1999-01-06 | 1999-02-24 | Lucas Ind Plc | Fuel system |
GB0206222D0 (en) * | 2002-03-15 | 2002-05-01 | Lucas Industries Ltd | Control system |
DE102005048019A1 (en) * | 2005-10-06 | 2007-04-12 | Rolls-Royce Deutschland Ltd & Co Kg | Aircraft engine e.g. gas turbine, oil supplying method, involves leading oil into oil cooler, where oil cooler controls oil supply temperature to respective storage chamber such that same oil outlet temperature results for storage chambers |
DE102005048017A1 (en) * | 2005-10-06 | 2007-04-12 | Rolls-Royce Deutschland Ltd & Co Kg | Fuel and oil system for gas turbine, has oil pump with outlet pipeline connected with heat exchanger, and another heat exchanger arranged in fuel rear guiding pipeline for guiding high pressure fuel pump from pump outlet to pump inlet |
US9657643B2 (en) * | 2013-10-16 | 2017-05-23 | Hamilton Sundstrand Corporation | Energy efficient pump system |
GB2521508B (en) * | 2013-10-16 | 2020-06-03 | Hamilton Sundstrand Corp | Energy efficient pump system |
US20210079848A1 (en) | 2019-03-20 | 2021-03-18 | United Technologies Corporation | Secondary fuel flow demand fuel pumping system |
US11725585B2 (en) * | 2021-11-30 | 2023-08-15 | Hamilton Sundstrand Corporation (HSC) | Fuel delivery pump selection |
GB2616286A (en) * | 2022-03-03 | 2023-09-06 | Rolls Royce Plc | Fuel management system |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB724004A (en) * | 1952-04-29 | 1955-02-16 | Rolls Royce | Improvements in or relating to fuel supply arrangements for gas-turbine engines |
US2782595A (en) * | 1952-08-29 | 1957-02-26 | Westinghouse Electric Corp | Fuel system for a gas turbine engine |
BE542467A (en) * | 1953-11-19 | |||
GB758679A (en) * | 1954-01-06 | 1956-10-10 | George Raymond Shepherd | Improvements in or relating to fuel systems for aviation gas turbine power plants |
FR1098147A (en) * | 1954-01-08 | 1955-07-18 | Snecma | Post-combustion nozzle reactor feed device |
GB831670A (en) * | 1957-11-18 | 1960-03-30 | George Raymond Shepherd | Improvements in or relating to aviation turbojet engines having exhaust reheaters |
GB1079293A (en) * | 1964-05-07 | 1967-08-16 | Rolls Royce | A fuel system for gas turbine engines |
GB1194041A (en) * | 1967-01-06 | 1970-06-10 | Dowty Fuel Syst Ltd | Centrifugal Pumping Apparatus |
US3658440A (en) * | 1970-01-28 | 1972-04-25 | Bendix Corp | Dual-element centrifugal pump pressure responsive flow regulator means |
US4038817A (en) * | 1975-06-02 | 1977-08-02 | General Electric Company | Fuel jettison system |
GB2227795A (en) * | 1989-02-07 | 1990-08-08 | Rolls Royce Plc | Gas turbine engine fuel system |
-
1994
- 1994-05-28 DE DE19944418680 patent/DE4418680C2/en not_active Expired - Lifetime
-
1995
- 1995-05-19 FR FR9505977A patent/FR2720442B1/en not_active Expired - Fee Related
- 1995-05-19 GB GB9510164A patent/GB2289722B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2720442B1 (en) | 1999-08-27 |
GB2289722B (en) | 1997-09-10 |
DE4418680A1 (en) | 1995-11-30 |
GB2289722A (en) | 1995-11-29 |
DE4418680C2 (en) | 1998-04-09 |
FR2720442A1 (en) | 1995-12-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
AU695675B2 (en) | Gas fuel supply mechanism for gas combustion engine | |
EP0678708A3 (en) | Gas turbine engine fuel injector. | |
EP0718484A3 (en) | Arrangement for operating an internal combustion engine with different fuels | |
GB2229806B (en) | Flameholder for gas turbine engine afterburner | |
DE59404243D1 (en) | Fuel supply system for combustion chamber | |
GB8817774D0 (en) | Fuel injectors for i c engines | |
EP0606106A3 (en) | Fuel supply system for internal combustion engines. | |
GB2297151B (en) | Fuel injector arrangement for gas-or liquid-fuelled turbine | |
EP0746677A4 (en) | Fuel supply system for internal combustion engines | |
EP0350795A3 (en) | Gas engine including fuel supply system | |
GB2247720B (en) | Fuel supply system for an internal combustion engine | |
GB2244514B (en) | Fuel supply control system for an internal combustion engine | |
GB2289722B (en) | Fuel supply arrangement for turbojet engines with afterburner | |
GB2248882B (en) | Fuel supply apparatus for internal combustion engines | |
GB9714645D0 (en) | Fuel metering arrangement for a gas turbine engine | |
ZA944664B (en) | Fuel for internal combustion engines and turbines | |
GB9410760D0 (en) | Gas turbine engine fuel control system | |
GB9714471D0 (en) | Fuel regulator for turbo jet engines | |
GB2266923B (en) | Internal combustion engine fuel supply | |
GB9713335D0 (en) | Fuel injection systems for diesel engines | |
EP0822330A3 (en) | Fuel supply system for internal combustion engines | |
GB9407820D0 (en) | Gas turbine engine fuel injector | |
GB9424364D0 (en) | Gas turbine fuel injector | |
GB9418406D0 (en) | Fuel supply apparatus for an internal combustion engine | |
GB9006841D0 (en) | Internal combustion engine modified fuel supply |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20140519 |