DE2344240A1 - Treibstoff-verteilungssystem - Google Patents

Treibstoff-verteilungssystem

Info

Publication number
DE2344240A1
DE2344240A1 DE19732344240 DE2344240A DE2344240A1 DE 2344240 A1 DE2344240 A1 DE 2344240A1 DE 19732344240 DE19732344240 DE 19732344240 DE 2344240 A DE2344240 A DE 2344240A DE 2344240 A1 DE2344240 A1 DE 2344240A1
Authority
DE
Germany
Prior art keywords
fuel
distribution system
housing
fuel distribution
engine
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.)
Pending
Application number
DE19732344240
Other languages
German (de)
English (en)
Inventor
John Mac Richey
Richard Edward Stenger
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of DE2344240A1 publication Critical patent/DE2344240A1/de
Pending 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
    • 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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Fuel-Injection Apparatus (AREA)
DE19732344240 1972-09-05 1973-09-01 Treibstoff-verteilungssystem Pending DE2344240A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US28643372A 1972-09-05 1972-09-05

Publications (1)

Publication Number Publication Date
DE2344240A1 true DE2344240A1 (de) 1974-03-21

Family

ID=23098585

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19732344240 Pending DE2344240A1 (de) 1972-09-05 1973-09-01 Treibstoff-verteilungssystem

Country Status (8)

Country Link
US (1) US3775975A (cg-RX-API-DMAC10.html)
JP (1) JPS4964707A (cg-RX-API-DMAC10.html)
BE (1) BE804376A (cg-RX-API-DMAC10.html)
CA (1) CA980583A (cg-RX-API-DMAC10.html)
DE (1) DE2344240A1 (cg-RX-API-DMAC10.html)
FR (1) FR2198055A1 (cg-RX-API-DMAC10.html)
GB (1) GB1437397A (cg-RX-API-DMAC10.html)
IT (1) IT993052B (cg-RX-API-DMAC10.html)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3879940A (en) * 1973-07-30 1975-04-29 Gen Electric Gas turbine engine fuel delivery tube assembly
US4387559A (en) * 1981-05-13 1983-06-14 Curtiss-Wright Corporation Fuel burner and combustor assembly for a gas turbine engine
GB2168755B (en) * 1984-12-08 1988-05-05 Rolls Royce Improvements in or relating to gas turbine engines
US4918925A (en) * 1987-09-30 1990-04-24 General Electric Company Laminar flow fuel distribution system
US5181377A (en) * 1991-04-16 1993-01-26 General Electric Company Damped combustor cowl structure
US5321949A (en) * 1991-07-12 1994-06-21 General Electric Company Staged fuel delivery system with secondary distribution valve
US5257502A (en) * 1991-08-12 1993-11-02 General Electric Company Fuel delivery system for dual annular combustor
US5273249A (en) * 1992-11-12 1993-12-28 General Electric Company Slide joint bracket
US5390498A (en) * 1994-02-15 1995-02-21 General Electric Company Fuel distribution assembly
US5924288A (en) * 1994-12-22 1999-07-20 General Electric Company One-piece combustor cowl
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.
DE19815914B4 (de) * 1998-04-09 2005-05-04 Alstom Verteiler
US6691519B2 (en) * 2000-02-18 2004-02-17 Siemens Westinghouse Power Corporation Adaptable modular gas turbine power plant
FR2825780B1 (fr) * 2001-06-06 2003-08-29 Snecma Moteurs Architecure de chambre de combustion de turbomachine en materiau a matrice ceramique
US20060156733A1 (en) * 2005-01-14 2006-07-20 Pratt & Whitney Canada Corp. Integral heater for fuel conveying member
FR2884868B1 (fr) * 2005-04-26 2007-06-22 Snecma Moteurs Sa Dispositif d'alimentation en carburant d'une chambre de combustion dans une turbomachine
US7856825B2 (en) * 2007-05-16 2010-12-28 Pratt & Whitney Canada Corp. Redundant mounting system for an internal fuel manifold
US8549859B2 (en) * 2008-07-28 2013-10-08 Siemens Energy, Inc. Combustor apparatus in a gas turbine engine
US20100071377A1 (en) * 2008-09-19 2010-03-25 Fox Timothy A Combustor Apparatus for Use in a Gas Turbine Engine
CN102128719B (zh) * 2010-12-13 2012-10-24 中国航空动力机械研究所 扇形回流燃烧室及其对开式燃烧室机匣
US9732960B2 (en) 2014-02-19 2017-08-15 United Technologies Corporation Fuel manifold for a gas turbine engine
US10533502B2 (en) * 2017-04-03 2020-01-14 United Technologies Corporation Combustor fuel manifold
US10746101B2 (en) 2017-06-13 2020-08-18 General Electric Company Annular fuel manifold with a deflector
CN115949505A (zh) * 2021-10-07 2023-04-11 通用电气公司 火焰检测器镜头维护系统
US11939922B2 (en) * 2022-08-19 2024-03-26 Pratt & Whitney Canada Corp. Fuel assembly for a gas turbine engine
US20250154877A1 (en) * 2023-11-15 2025-05-15 Rtx Corporation Slider seal of gas turbine engine

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2969925A (en) * 1958-02-03 1961-01-31 Delavan Mfg Company Multiple variable area orifice injector
FR1406603A (fr) * 1964-06-09 1965-07-23 Snecma Dispositif de brûleur et son montage dans une chambre de combustion
US3335567A (en) * 1965-11-19 1967-08-15 Gen Electric Multi-nozzle fuel delivery system
US3516252A (en) * 1969-02-26 1970-06-23 United Aircraft Corp Fuel manifold system
US3528250A (en) * 1969-04-16 1970-09-15 Gen Motors Corp Bypass engine with afterburning and compressor bleed air heat exchanger in bypass duct

Also Published As

Publication number Publication date
US3775975A (en) 1973-12-04
FR2198055A1 (cg-RX-API-DMAC10.html) 1974-03-29
CA980583A (en) 1975-12-30
GB1437397A (en) 1976-05-26
BE804376A (fr) 1974-01-02
JPS4964707A (cg-RX-API-DMAC10.html) 1974-06-22
IT993052B (it) 1975-09-30

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