GB2086482B - Priming device for burner manifolds of gas turbine engines - Google Patents

Priming device for burner manifolds of gas turbine engines

Info

Publication number
GB2086482B
GB2086482B GB8128583A GB8128583A GB2086482B GB 2086482 B GB2086482 B GB 2086482B GB 8128583 A GB8128583 A GB 8128583A GB 8128583 A GB8128583 A GB 8128583A GB 2086482 B GB2086482 B GB 2086482B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engines
priming device
burner manifolds
manifolds
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
Application number
GB8128583A
Other versions
GB2086482A (en
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.)
Rolls Royce PLC
Original Assignee
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB8128583A priority Critical patent/GB2086482B/en
Publication of GB2086482A publication Critical patent/GB2086482A/en
Application granted granted Critical
Publication of GB2086482B publication Critical patent/GB2086482B/en
Expired 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
    • F02C7/232—Fuel valves; Draining valves or systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)
GB8128583A 1980-10-30 1981-09-22 Priming device for burner manifolds of gas turbine engines Expired GB2086482B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8128583A GB2086482B (en) 1980-10-30 1981-09-22 Priming device for burner manifolds of gas turbine engines

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8034940 1980-10-30
GB8128583A GB2086482B (en) 1980-10-30 1981-09-22 Priming device for burner manifolds of gas turbine engines

Publications (2)

Publication Number Publication Date
GB2086482A GB2086482A (en) 1982-05-12
GB2086482B true GB2086482B (en) 1984-02-08

Family

ID=26277372

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8128583A Expired GB2086482B (en) 1980-10-30 1981-09-22 Priming device for burner manifolds of gas turbine engines

Country Status (1)

Country Link
GB (1) GB2086482B (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8527146D0 (en) * 1985-11-04 1985-12-11 Normalair Garrett Ltd Fuel flow control valve
US4928491A (en) * 1988-06-29 1990-05-29 United States Of America As Represented By The Secretary Of Air Force Fuel supply device for supplying fuel to an engine combustor
US5184457A (en) * 1991-04-11 1993-02-09 Eaton Corporation Valve assembly and method
GB2320063B (en) * 1993-12-09 1998-07-15 United Technologies Corp Fuel staging system
US5442922A (en) * 1993-12-09 1995-08-22 United Technologies Corporation Fuel staging system
GB2312250A (en) * 1996-04-18 1997-10-22 Rolls Royce Plc Staged gas turbine fuel system with a single supply manifold, to which the main burners are connected through valves.
JP4785973B2 (en) * 2010-02-02 2011-10-05 川崎重工業株式会社 Gas turbine engine fuel supply system
JP4815537B1 (en) * 2010-04-23 2011-11-16 川崎重工業株式会社 Gas turbine engine fuel supply system
CN111765004B (en) * 2020-05-22 2023-01-03 中国航发贵州红林航空动力控制科技有限公司 Conversion valve mechanism of fuel pump regulator

Also Published As

Publication number Publication date
GB2086482A (en) 1982-05-12

Similar Documents

Publication Publication Date Title
GB2098719B (en) Gas turbine engine combustion apparatus
JPS57124005A (en) Turbine of gas turbine engine
JPS5720539A (en) Exhaust nozzle for gas turbine engine
JPS56168040A (en) Circular combustor for gas turbine engine
JPS5793636A (en) Duplex fuel passage stem for gas turbine engine
JPS55165413A (en) Fuel burner for gas turbine engine
GB2072268B (en) Fuel efficiency of a gas turbine engine
JPS55131626A (en) Combustion chamber for gas turbine engine
GB2087536B (en) Gas turbine engine ceramic combustor mounting
JPS57122130A (en) Fuel feeder for gas turbine engine
GB2102936B (en) Fuel injector for gas turbine engines
JPS55102836A (en) Combustion chamber for gas turbine engine
DE3061595D1 (en) Combustion apparatus for gas turbine engines
JPS5392022A (en) Combustion apparatus of gas turbine engine
GB2086482B (en) Priming device for burner manifolds of gas turbine engines
GB2107448B (en) Gas turbine engine combustion chambers
GB2045421B (en) Gas turbine combustion chamber
JPS55134213A (en) Gas turbine engine fuel burner
DE3360470D1 (en) Gas turbine combustion chamber
GB2062839B (en) Gas turbine engine fuel burner
JPS56168037A (en) Fuel injector for gas turbine engine
JPS5792609A (en) Fuel nozzle for gas turbine engine
GB2020371B (en) Gas turbine combustion chamber
GB2018971B (en) Gas turbine combustion chamber
GB2086031B (en) Gas turbine combustion system

Legal Events

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

Effective date: 19960922