RU96117120A - METHOD FOR COMBUSING FUEL IN COMPRESSED AIR - Google Patents
METHOD FOR COMBUSING FUEL IN COMPRESSED AIRInfo
- Publication number
- RU96117120A RU96117120A RU96117120/06A RU96117120A RU96117120A RU 96117120 A RU96117120 A RU 96117120A RU 96117120/06 A RU96117120/06 A RU 96117120/06A RU 96117120 A RU96117120 A RU 96117120A RU 96117120 A RU96117120 A RU 96117120A
- Authority
- RU
- Russia
- Prior art keywords
- stream
- fuel
- partial streams
- supplied
- compressed air
- Prior art date
Links
- 239000000446 fuel Substances 0.000 title claims 8
- 238000002485 combustion reaction Methods 0.000 claims 1
Claims (5)
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP94100988 | 1994-01-24 | ||
EP94100988.8 | 1994-01-24 | ||
EP94100989.6 | 1994-01-24 | ||
EP94100989 | 1994-01-24 | ||
PCT/EP1995/000244 WO1995020131A1 (en) | 1994-01-24 | 1995-01-24 | Method of burning fuel in compressed air |
Publications (2)
Publication Number | Publication Date |
---|---|
RU96117120A true RU96117120A (en) | 1998-11-27 |
RU2142601C1 RU2142601C1 (en) | 1999-12-10 |
Family
ID=26135445
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU96117119A RU2133916C1 (en) | 1994-01-24 | 1995-01-24 | Gas turbine combustion chamber |
RU96117120A RU2142601C1 (en) | 1994-01-24 | 1995-01-24 | Method for fuel combustion in compressed air |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU96117119A RU2133916C1 (en) | 1994-01-24 | 1995-01-24 | Gas turbine combustion chamber |
Country Status (10)
Country | Link |
---|---|
US (1) | US5735115A (en) |
EP (2) | EP0741849B1 (en) |
JP (2) | JP3667757B2 (en) |
KR (2) | KR970700846A (en) |
CN (2) | CN1140489A (en) |
CZ (2) | CZ217496A3 (en) |
DE (2) | DE59502335D1 (en) |
ES (2) | ES2126881T3 (en) |
RU (2) | RU2133916C1 (en) |
WO (2) | WO1995020130A1 (en) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5657632A (en) * | 1994-11-10 | 1997-08-19 | Westinghouse Electric Corporation | Dual fuel gas turbine combustor |
US6638424B2 (en) * | 2000-01-19 | 2003-10-28 | Jensen Enterprises | Stormwater treatment apparatus |
US6295801B1 (en) * | 1998-12-18 | 2001-10-02 | General Electric Company | Fuel injector bar for gas turbine engine combustor having trapped vortex cavity |
US6286298B1 (en) * | 1998-12-18 | 2001-09-11 | General Electric Company | Apparatus and method for rich-quench-lean (RQL) concept in a gas turbine engine combustor having trapped vortex cavity |
EP1288441A1 (en) * | 2001-09-03 | 2003-03-05 | Siemens Aktiengesellschaft | Transition piece for the combustion chamber of a gas turbine |
US6820424B2 (en) | 2001-09-12 | 2004-11-23 | Allison Advanced Development Company | Combustor module |
US7229029B2 (en) * | 2002-10-29 | 2007-06-12 | Phisser Technologies, Inc. | Propulsion system |
CA2537926C (en) * | 2003-09-05 | 2011-01-11 | Delavan Inc. | Pilot combustor for stabilizing combustion in gas turbine engines |
US20080196414A1 (en) * | 2005-03-22 | 2008-08-21 | Andreadis Dean E | Strut cavity pilot and fuel injector assembly |
US7500364B2 (en) | 2005-11-22 | 2009-03-10 | Honeywell International Inc. | System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines |
US8015815B2 (en) * | 2007-04-18 | 2011-09-13 | Parker-Hannifin Corporation | Fuel injector nozzles, with labyrinth grooves, for gas turbine engines |
US20080280238A1 (en) * | 2007-05-07 | 2008-11-13 | Caterpillar Inc. | Low swirl injector and method for low-nox combustor |
US7827795B2 (en) * | 2008-09-19 | 2010-11-09 | Woodward Governor Company | Active thermal protection for fuel injectors |
HUE027667T2 (en) * | 2011-02-09 | 2016-10-28 | Siemens Ag | Combustion chamber casing |
EP3055536B1 (en) * | 2013-10-07 | 2020-04-08 | United Technologies Corporation | Air cooled fuel injector for a turbine engine |
US10139111B2 (en) * | 2014-03-28 | 2018-11-27 | Siemens Energy, Inc. | Dual outlet nozzle for a secondary fuel stage of a combustor of a gas turbine engine |
US9932940B2 (en) * | 2015-03-30 | 2018-04-03 | Honeywell International Inc. | Gas turbine engine fuel cooled cooling air heat exchanger |
US11118784B2 (en) | 2016-01-28 | 2021-09-14 | Rolls-Royce North American Technologies Inc. | Heat exchanger integrated with fuel nozzle |
US10830150B2 (en) | 2016-01-28 | 2020-11-10 | Rolls-Royce Corporation | Fuel heat exchanger with leak management |
CA2955613A1 (en) * | 2016-01-28 | 2017-07-28 | Rolls-Royce North American Technologies, Inc. | Heat exchanger integrated with fuel nozzle |
JP7214332B2 (en) * | 2017-01-18 | 2023-01-30 | ゼネラル・エレクトリック・カンパニイ | Staged fuel and air injection in gas turbine combustion systems |
US10947902B2 (en) * | 2017-06-13 | 2021-03-16 | Haier Us Appliance Solutions, Inc. | Fuel nozzle, fuel supply assembly thereof, and method of assembling a fuel nozzle |
US10775046B2 (en) | 2017-10-18 | 2020-09-15 | Rolls-Royce North American Technologies Inc. | Fuel injection assembly for gas turbine engine |
CN108826357A (en) * | 2018-07-27 | 2018-11-16 | 清华大学 | The toroidal combustion chamber of engine |
CN109632325B (en) * | 2018-12-17 | 2021-05-25 | 中国航发沈阳发动机研究所 | Main combustion chamber flow distribution method |
RU2753203C1 (en) * | 2020-10-09 | 2021-08-12 | Открытое акционерное общество "Всероссийский дважды ордена Трудового Красного Знамени теплотехнический научно-исследовательский институт" (ОАО "ВТИ") | Method for burning fuel in a low-emission combustion chamber |
RU2753202C1 (en) * | 2020-10-09 | 2021-08-12 | Открытое акционерное общество "Всероссийский дважды ордена Трудового Красного Знамени теплотехнический научно-исследовательский институт" (ОАО "ВТИ") | Method for burning fuel in a low-emission combustion chamber |
RU2761713C1 (en) * | 2021-01-13 | 2021-12-13 | Иван Иванович Кутыш | Method for burning a preliminarily prepared "lean" fuel-air mixture of liquid and (or) gaseous fuel and air in a three-circuit low-emission burner (variants) |
US11555450B1 (en) * | 2021-08-19 | 2023-01-17 | Collins Engine Nozzles, Inc. | Fuel injectors with heat exchangers |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB816878A (en) * | 1956-04-18 | 1959-07-22 | Rolls Royce | Improvements in or relating to combustion equipment |
GB768370A (en) * | 1953-08-18 | 1957-02-13 | Snecma | Improvements in gas turbine engines, particularly for aircraft propulsion |
FR1141587A (en) * | 1956-01-23 | 1957-09-04 | Snecma | Improvements to the combustion devices of continuous flow internal combustion machines |
US3019606A (en) * | 1959-09-04 | 1962-02-06 | Avco Corp | Combustion section for a gas turbine engine |
US3433015A (en) * | 1965-06-23 | 1969-03-18 | Nasa | Gas turbine combustion apparatus |
US3460345A (en) * | 1967-12-28 | 1969-08-12 | Lucas Industries Ltd | Combustion apparatus for gas turbine engines |
JPS4829308B1 (en) * | 1969-07-31 | 1973-09-08 | ||
GB1283827A (en) * | 1970-09-26 | 1972-08-02 | Rolls Royce | Improvements in or relating to combustion apparatus |
US3701255A (en) * | 1970-10-26 | 1972-10-31 | United Aircraft Corp | Shortened afterburner construction for turbine engine |
US3736746A (en) * | 1971-08-13 | 1973-06-05 | Gen Electric | Recirculating annular slot fuel/air carbureting system for gas turbine combustors |
US3879939A (en) * | 1973-04-18 | 1975-04-29 | United Aircraft Corp | Combustion inlet diffuser employing boundary layer flow straightening vanes |
US3877221A (en) * | 1973-08-27 | 1975-04-15 | Gen Motors Corp | Combustion apparatus air supply |
US4052844A (en) * | 1975-06-02 | 1977-10-11 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Gas turbine combustion chambers |
GB1573926A (en) * | 1976-03-24 | 1980-08-28 | Rolls Royce | Fluid flow diffuser |
US4100732A (en) * | 1976-12-02 | 1978-07-18 | General Electric Company | Centrifugal compressor advanced dump diffuser |
US4194359A (en) * | 1977-12-12 | 1980-03-25 | United Technologies Corporation | Means for improving the performance of burner shroud diffusers |
ATE42821T1 (en) * | 1985-03-04 | 1989-05-15 | Siemens Ag | BURNER ARRANGEMENT FOR COMBUSTION PLANTS, IN PARTICULAR FOR COMBUSTION CHAMBERS OF GAS TURBINE PLANTS, AND METHOD FOR THEIR OPERATION. |
EP0224817B1 (en) * | 1985-12-02 | 1989-07-12 | Siemens Aktiengesellschaft | Heat shield arrangement, especially for the structural components of a gas turbine plant |
US5058375A (en) * | 1988-12-28 | 1991-10-22 | Sundstrand Corporation | Gas turbine annular combustor with radial dilution air injection |
CH682009A5 (en) * | 1990-11-02 | 1993-06-30 | Asea Brown Boveri | |
US5207064A (en) * | 1990-11-21 | 1993-05-04 | General Electric Company | Staged, mixed combustor assembly having low emissions |
EP0489193B1 (en) * | 1990-12-05 | 1997-07-23 | Asea Brown Boveri Ag | Combustion chamber for gas turbine |
US5211003A (en) * | 1992-02-05 | 1993-05-18 | General Electric Company | Diffuser clean air bleed assembly |
US5239818A (en) * | 1992-03-30 | 1993-08-31 | General Electric Company | Dilution pole combustor and method |
-
1995
- 1995-01-24 ES ES95907594T patent/ES2126881T3/en not_active Expired - Lifetime
- 1995-01-24 CN CN95191592A patent/CN1140489A/en active Pending
- 1995-01-24 CN CN95191343A patent/CN1092777C/en not_active Expired - Fee Related
- 1995-01-24 JP JP51935495A patent/JP3667757B2/en not_active Expired - Fee Related
- 1995-01-24 WO PCT/EP1995/000245 patent/WO1995020130A1/en active IP Right Grant
- 1995-01-24 JP JP7519353A patent/JPH09507703A/en active Pending
- 1995-01-24 CZ CZ962174A patent/CZ217496A3/en unknown
- 1995-01-24 ES ES95907593T patent/ES2117402T3/en not_active Expired - Lifetime
- 1995-01-24 CZ CZ962173A patent/CZ217396A3/en unknown
- 1995-01-24 WO PCT/EP1995/000244 patent/WO1995020131A1/en not_active Application Discontinuation
- 1995-01-24 EP EP95907594A patent/EP0741849B1/en not_active Expired - Lifetime
- 1995-01-24 EP EP95907593A patent/EP0741850B1/en not_active Expired - Lifetime
- 1995-01-24 DE DE59502335T patent/DE59502335D1/en not_active Expired - Fee Related
- 1995-01-24 RU RU96117119A patent/RU2133916C1/en not_active IP Right Cessation
- 1995-01-24 KR KR1019960703976A patent/KR970700846A/en not_active Application Discontinuation
- 1995-01-24 DE DE59504264T patent/DE59504264D1/en not_active Expired - Fee Related
- 1995-01-24 RU RU96117120A patent/RU2142601C1/en not_active IP Right Cessation
- 1995-01-24 KR KR1019960703975A patent/KR970700845A/en not_active Application Discontinuation
-
1996
- 1996-07-23 US US08/682,755 patent/US5735115A/en not_active Expired - Fee Related
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