GB2289722B - Fuel supply arrangement for turbojet engines with afterburner - Google Patents

Fuel supply arrangement for turbojet engines with afterburner

Info

Publication number
GB2289722B
GB2289722B GB9510164A GB9510164A GB2289722B GB 2289722 B GB2289722 B GB 2289722B GB 9510164 A GB9510164 A GB 9510164A GB 9510164 A GB9510164 A GB 9510164A GB 2289722 B GB2289722 B GB 2289722B
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.)
Expired - Fee Related
Application number
GB9510164A
Other versions
GB2289722A (en
GB9510164D0 (en
Inventor
Peter John Harding
Helmut Streifinger
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.)
MTU Aero Engines GmbH
Rolls Royce PLC
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
Rolls Royce PLC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by MTU Motoren und Turbinen Union Muenchen GmbH, Rolls Royce PLC filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of GB9510164D0 publication Critical patent/GB9510164D0/en
Publication of GB2289722A publication Critical patent/GB2289722A/en
Application granted granted Critical
Publication of GB2289722B publication Critical patent/GB2289722B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
GB9510164A 1994-05-28 1995-05-19 Fuel supply arrangement for turbojet engines with afterburner Expired - Fee Related GB2289722B (en)

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 GB9510164D0 (en) 1995-08-02
GB2289722A GB2289722A (en) 1995-11-29
GB2289722B true 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)

* Cited by examiner, † Cited by third party
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

Citations (6)

* Cited by examiner, † Cited by third party
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
GB758679A (en) * 1954-01-06 1956-10-10 George Raymond Shepherd Improvements in or relating to fuel systems for aviation gas turbine power plants
GB762328A (en) * 1953-11-19 1956-11-28 Thompson Prod Inc Improvements in or relating to fuel pumping systems for aero engines
GB831670A (en) * 1957-11-18 1960-03-30 George Raymond Shepherd Improvements in or relating to aviation turbojet engines having exhaust reheaters
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

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2782595A (en) * 1952-08-29 1957-02-26 Westinghouse Electric Corp Fuel system for a gas turbine engine
FR1098147A (en) * 1954-01-08 1955-07-18 Snecma Post-combustion nozzle reactor feed device
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

Patent Citations (6)

* Cited by examiner, † Cited by third party
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
GB762328A (en) * 1953-11-19 1956-11-28 Thompson Prod Inc Improvements in or relating to fuel pumping systems for aero engines
GB758679A (en) * 1954-01-06 1956-10-10 George Raymond Shepherd Improvements in or relating to fuel systems for aviation gas turbine power plants
GB831670A (en) * 1957-11-18 1960-03-30 George Raymond Shepherd Improvements in or relating to aviation turbojet engines having exhaust reheaters
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

Also Published As

Publication number Publication date
FR2720442B1 (en) 1999-08-27
DE4418680A1 (en) 1995-11-30
GB2289722A (en) 1995-11-29
DE4418680C2 (en) 1998-04-09
FR2720442A1 (en) 1995-12-01
GB9510164D0 (en) 1995-08-02

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20140519