BE804376A - Systeme de distribution du carburant d'un moteur a turbine a gaz - Google Patents
Systeme de distribution du carburant d'un moteur a turbine a gazInfo
- Publication number
- BE804376A BE804376A BE135246A BE135246A BE804376A BE 804376 A BE804376 A BE 804376A BE 135246 A BE135246 A BE 135246A BE 135246 A BE135246 A BE 135246A BE 804376 A BE804376 A BE 804376A
- Authority
- BE
- Belgium
- Prior art keywords
- gas turbine
- distribution system
- turbine engine
- fuel distribution
- fuel
- Prior art date
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)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US28643372A | 1972-09-05 | 1972-09-05 |
Publications (1)
Publication Number | Publication Date |
---|---|
BE804376A true BE804376A (fr) | 1974-01-02 |
Family
ID=23098585
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE135246A BE804376A (fr) | 1972-09-05 | 1973-09-03 | Systeme de distribution du carburant d'un moteur a turbine a gaz |
Country Status (8)
Country | Link |
---|---|
US (1) | US3775975A (fr) |
JP (1) | JPS4964707A (fr) |
BE (1) | BE804376A (fr) |
CA (1) | CA980583A (fr) |
DE (1) | DE2344240A1 (fr) |
FR (1) | FR2198055A1 (fr) |
GB (1) | GB1437397A (fr) |
IT (1) | IT993052B (fr) |
Families Citing this family (24)
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 |
JP2015155698A (ja) * | 2014-02-19 | 2015-08-27 | ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation | ガスタービンエンジン用の燃料マニホールド |
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 |
US11939922B2 (en) * | 2022-08-19 | 2024-03-26 | Pratt & Whitney Canada Corp. | Fuel assembly for a gas turbine engine |
Family Cites Families (5)
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 |
-
1972
- 1972-09-05 US US00286433A patent/US3775975A/en not_active Expired - Lifetime
-
1973
- 1973-07-30 CA CA177,567A patent/CA980583A/en not_active Expired
- 1973-08-10 GB GB3797173A patent/GB1437397A/en not_active Expired
- 1973-08-24 IT IT28183/73A patent/IT993052B/it active
- 1973-09-01 DE DE19732344240 patent/DE2344240A1/de active Pending
- 1973-09-03 BE BE135246A patent/BE804376A/fr unknown
- 1973-09-03 FR FR7331750A patent/FR2198055A1/fr not_active Withdrawn
- 1973-09-05 JP JP48099382A patent/JPS4964707A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
JPS4964707A (fr) | 1974-06-22 |
DE2344240A1 (de) | 1974-03-21 |
US3775975A (en) | 1973-12-04 |
CA980583A (en) | 1975-12-30 |
IT993052B (it) | 1975-09-30 |
FR2198055A1 (fr) | 1974-03-29 |
GB1437397A (en) | 1976-05-26 |
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