ES2117402T3 - Procedimiento para la combustion de un combustible en aire comprimido. - Google Patents
Procedimiento para la combustion de un combustible en aire comprimido.Info
- Publication number
- ES2117402T3 ES2117402T3 ES95907593T ES95907593T ES2117402T3 ES 2117402 T3 ES2117402 T3 ES 2117402T3 ES 95907593 T ES95907593 T ES 95907593T ES 95907593 T ES95907593 T ES 95907593T ES 2117402 T3 ES2117402 T3 ES 2117402T3
- Authority
- ES
- Spain
- Prior art keywords
- current
- fuel
- combustion
- procedure
- compressed air
- 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 - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
- F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
- F23R3/22—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants movable, e.g. to an inoperative position; adjustable, e.g. self-adjusting
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
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)
- Combustion Of Fluid Fuel (AREA)
- Control Of Combustion (AREA)
Abstract
LA INVENCION SE REFIERE A UN PROCEDIMIENTO PARA COMBUSTION DE COMBUSTIBLE EN AIRE COMPRIMIDO QUE FLUYE EN UNA CORRIENTE (2) A LO LARGO DE UN EJE (1). VARIAS CORRIENTES (3) COMPONENTES ESTAN PRIMERO SEPARADAS CON RESPECTO A LA CORRIENTE (2) PRINCIPAL Y UNA PORCION DE COMBUSTIBLE SE INTRODUCE DE FORMA SEPARADA EN CADA UNA DE LAS CORRIENTE COMPONENTES Y SE QUEMA EN UNA LLAMA (25) PILOTO QUE SOBRESALE DENTRO DE LA CORRIENTE (2). CUALQUIER COMBUSTIBLE QUE PERMANECE SE DISIPA DENTRO DE LA CORRIENTE (2), ENTRA EN IGNICION MEDIANTE LA LLAMA (25) PILOTO Y SE QUEMA. LA DISTRIBUCION (28) DE COMBUSTIBLE EN LA CORRIENTE (2) NO ES HOMOGENEA Y DISPONE DE MAXIMOS (29) LOCALES EN CADA LLAMA (25) PILOTO. EL METODO ES ESPECIALMENTE ADECUADO PARA UTILIZACION EN TURBINAS DE GAS Y ASEGURA UNA COMBUSTION DEL COMBUSTIBLE RAPIDA Y COMPLETA.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP94100989 | 1994-01-24 | ||
EP94100988 | 1994-01-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2117402T3 true ES2117402T3 (es) | 1998-08-01 |
Family
ID=26135445
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES95907593T Expired - Lifetime ES2117402T3 (es) | 1994-01-24 | 1995-01-24 | Procedimiento para la combustion de un combustible en aire comprimido. |
ES95907594T Expired - Lifetime ES2126881T3 (es) | 1994-01-24 | 1995-01-24 | Camara de combustion para una turbina de gas. |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES95907594T Expired - Lifetime ES2126881T3 (es) | 1994-01-24 | 1995-01-24 | Camara de combustion para una turbina de gas. |
Country Status (10)
Country | Link |
---|---|
US (1) | US5735115A (es) |
EP (2) | EP0741849B1 (es) |
JP (2) | JPH09507703A (es) |
KR (2) | KR970700846A (es) |
CN (2) | CN1092777C (es) |
CZ (2) | CZ217396A3 (es) |
DE (2) | DE59504264D1 (es) |
ES (2) | ES2117402T3 (es) |
RU (2) | RU2142601C1 (es) |
WO (2) | WO1995020131A1 (es) |
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 (de) * | 2001-09-03 | 2003-03-05 | Siemens Aktiengesellschaft | Übergangsabschnitt einer Gasturbinenbrennkammer |
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 |
BRPI0413784A (pt) * | 2003-09-05 | 2006-11-07 | Delavan Inc | queimador para um combustor de turbina de gás |
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 | Burner compartment cover |
WO2015054136A1 (en) | 2013-10-07 | 2015-04-16 | 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 |
US10830150B2 (en) | 2016-01-28 | 2020-11-10 | Rolls-Royce Corporation | Fuel heat exchanger with leak management |
US11118784B2 (en) | 2016-01-28 | 2021-09-14 | Rolls-Royce North American Technologies Inc. | Heat exchanger integrated with fuel nozzle |
CA2955613A1 (en) * | 2016-01-28 | 2017-07-28 | Rolls-Royce North American Technologies, Inc. | Heat exchanger integrated with fuel nozzle |
JP7214332B2 (ja) * | 2017-01-18 | 2023-01-30 | ゼネラル・エレクトリック・カンパニイ | ガスタービンの燃焼システムにおける段階的な燃料および空気噴射 |
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 (zh) * | 2018-07-27 | 2018-11-16 | 清华大学 | 发动机的环形燃烧室 |
CN109632325B (zh) * | 2018-12-17 | 2021-05-25 | 中国航发沈阳发动机研究所 | 一种主燃烧室流量分配方法 |
RU2753203C1 (ru) * | 2020-10-09 | 2021-08-12 | Открытое акционерное общество "Всероссийский дважды ордена Трудового Красного Знамени теплотехнический научно-исследовательский институт" (ОАО "ВТИ") | Способ сжигания топлива в малоэмиссионной камере сгорания |
RU2753202C1 (ru) * | 2020-10-09 | 2021-08-12 | Открытое акционерное общество "Всероссийский дважды ордена Трудового Красного Знамени теплотехнический научно-исследовательский институт" (ОАО "ВТИ") | Малоэмиссионная камера сгорания с двумя зонами кинетического горения |
RU2761713C1 (ru) * | 2021-01-13 | 2021-12-13 | Иван Иванович Кутыш | Способ сжигания предварительно подготовленной "бедной" топливовоздушной смеси жидкого и (или) газообразного топлива и воздуха в трехконтурной малоэмиссионной горелке (варианты) |
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 (fr) * | 1956-01-23 | 1957-09-04 | Snecma | Perfectionnements aux dispositifs de combustion des machines à combustion interne à flux continu |
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 (es) * | 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 (de) * | 1985-03-04 | 1989-05-15 | Siemens Ag | Brenneranordnung fuer feuerungsanlagen, insbesondere fuer brennkammern von gasturbinenanlagen sowie verfahren zu ihrem betrieb. |
DE3664374D1 (en) * | 1985-12-02 | 1989-08-17 | Siemens Ag | 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 (es) * | 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 |
DE59010740D1 (de) * | 1990-12-05 | 1997-09-04 | Asea Brown Boveri | Gasturbinen-Brennkammer |
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 RU RU96117120A patent/RU2142601C1/ru not_active IP Right Cessation
- 1995-01-24 KR KR1019960703976A patent/KR970700846A/ko not_active Application Discontinuation
- 1995-01-24 EP EP95907594A patent/EP0741849B1/de not_active Expired - Lifetime
- 1995-01-24 WO PCT/EP1995/000244 patent/WO1995020131A1/de not_active Application Discontinuation
- 1995-01-24 CZ CZ962173A patent/CZ217396A3/cs unknown
- 1995-01-24 RU RU96117119A patent/RU2133916C1/ru not_active IP Right Cessation
- 1995-01-24 ES ES95907593T patent/ES2117402T3/es not_active Expired - Lifetime
- 1995-01-24 EP EP95907593A patent/EP0741850B1/de not_active Expired - Lifetime
- 1995-01-24 WO PCT/EP1995/000245 patent/WO1995020130A1/de active IP Right Grant
- 1995-01-24 KR KR1019960703975A patent/KR970700845A/ko not_active Application Discontinuation
- 1995-01-24 CZ CZ962174A patent/CZ217496A3/cs unknown
- 1995-01-24 ES ES95907594T patent/ES2126881T3/es not_active Expired - Lifetime
- 1995-01-24 JP JP7519353A patent/JPH09507703A/ja active Pending
- 1995-01-24 DE DE59504264T patent/DE59504264D1/de not_active Expired - Fee Related
- 1995-01-24 DE DE59502335T patent/DE59502335D1/de not_active Expired - Fee Related
- 1995-01-24 JP JP51935495A patent/JP3667757B2/ja not_active Expired - Fee Related
- 1995-01-24 CN CN95191343A patent/CN1092777C/zh not_active Expired - Fee Related
- 1995-01-24 CN CN95191592A patent/CN1140489A/zh active Pending
-
1996
- 1996-07-23 US US08/682,755 patent/US5735115A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US5735115A (en) | 1998-04-07 |
CN1140489A (zh) | 1997-01-15 |
EP0741849B1 (de) | 1998-11-18 |
JPH09507703A (ja) | 1997-08-05 |
EP0741849A1 (de) | 1996-11-13 |
EP0741850B1 (de) | 1998-05-27 |
CN1139476A (zh) | 1997-01-01 |
RU2133916C1 (ru) | 1999-07-27 |
KR970700846A (ko) | 1997-02-12 |
EP0741850A1 (de) | 1996-11-13 |
DE59504264D1 (de) | 1998-12-24 |
CZ217496A3 (en) | 1997-02-12 |
ES2126881T3 (es) | 1999-04-01 |
KR970700845A (ko) | 1997-02-12 |
RU2142601C1 (ru) | 1999-12-10 |
WO1995020131A1 (de) | 1995-07-27 |
WO1995020130A1 (de) | 1995-07-27 |
DE59502335D1 (de) | 1998-07-02 |
JP3667757B2 (ja) | 2005-07-06 |
JPH09507704A (ja) | 1997-08-05 |
CN1092777C (zh) | 2002-10-16 |
CZ217396A3 (en) | 1996-10-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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