DE60044733D1 - Raketenmotor - Google Patents

Raketenmotor

Info

Publication number
DE60044733D1
DE60044733D1 DE60044733T DE60044733T DE60044733D1 DE 60044733 D1 DE60044733 D1 DE 60044733D1 DE 60044733 T DE60044733 T DE 60044733T DE 60044733 T DE60044733 T DE 60044733T DE 60044733 D1 DE60044733 D1 DE 60044733D1
Authority
DE
Germany
Prior art keywords
combustion chamber
annular passages
effusion cooling
combustion
respective annular
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
Application number
DE60044733T
Other languages
English (en)
Inventor
Richard D Stephens
Robert S Thompson Jr
Guido J Defever
John F Jones
Dean S Musgrave
Gregg G Williams
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.)
Williams International Corp
Original Assignee
Williams International Corp
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 Williams International Corp filed Critical Williams International Corp
Application granted granted Critical
Publication of DE60044733D1 publication Critical patent/DE60044733D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/52—Injectors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/46—Feeding propellants using pumps
    • F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/66—Combustion or thrust chambers of the rotary type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/72—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/40—Use of a multiplicity of similar components

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Testing Of Engines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Telescopes (AREA)
DE60044733T 1999-03-10 2000-03-10 Raketenmotor Expired - Lifetime DE60044733D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12362199P 1999-03-10 1999-03-10

Publications (1)

Publication Number Publication Date
DE60044733D1 true DE60044733D1 (de) 2010-09-02

Family

ID=22409771

Family Applications (2)

Application Number Title Priority Date Filing Date
DE60038012T Expired - Lifetime DE60038012T2 (de) 1999-03-10 2000-03-10 Raketenmotor
DE60044733T Expired - Lifetime DE60044733D1 (de) 1999-03-10 2000-03-10 Raketenmotor

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE60038012T Expired - Lifetime DE60038012T2 (de) 1999-03-10 2000-03-10 Raketenmotor

Country Status (11)

Country Link
US (3) US6220016B1 (de)
EP (1) EP1171705B1 (de)
JP (3) JP4386589B2 (de)
CN (2) CN100417801C (de)
AT (1) ATE386203T1 (de)
AU (1) AU6045800A (de)
CA (1) CA2364284C (de)
DE (2) DE60038012T2 (de)
IL (4) IL164183A0 (de)
RU (1) RU2243403C2 (de)
WO (1) WO2000057048A2 (de)

Families Citing this family (56)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10054333B4 (de) * 2000-11-02 2006-11-30 Eads Space Transportation Gmbh Brennkammer mit erhöhtem Wärmeeintrag in eine Kühleinrichtung
US6591603B2 (en) * 2001-03-08 2003-07-15 Trw Inc. Pintle injector rocket with expansion-deflection nozzle
US7007475B2 (en) * 2003-03-11 2006-03-07 Honeywell International, Inc. Conical helical of spiral combustor scroll device in gas turbine engine
US6964154B1 (en) 2003-03-11 2005-11-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Axisymmetric, throttleable non-gimballed rocket engine
RU2333869C2 (ru) * 2003-03-28 2008-09-20 Моуджейв Аэроспейс Венчерз, Ллс Унифицированная комбинированная ракетная система
US7007480B2 (en) * 2003-04-09 2006-03-07 Honeywell International, Inc. Multi-axial pivoting combustor liner in gas turbine engine
US6925812B2 (en) * 2003-05-22 2005-08-09 Williams International Co., L.L.C. Rotary injector
DE10358953A1 (de) 2003-12-15 2005-07-28 Man Turbo Ag Lagerung des Rotors einer Gasturbine
US6988367B2 (en) 2004-04-20 2006-01-24 Williams International Co. L.L.C. Gas turbine engine cooling system and method
EP1875058A4 (de) * 2005-04-25 2011-03-30 Williams Int Co Llc System und verfahren zum kühlen einer gasturbine
US7685822B1 (en) 2005-11-09 2010-03-30 Florida Turbine Technologies, Inc. Rotary cup fuel injector
US7926403B1 (en) 2006-06-29 2011-04-19 Utron Inc. Transient, high rate, closed system cryogenic injection
US7621119B2 (en) * 2006-06-30 2009-11-24 United Technologies Corporation Heat exchange injector for use in a rocket engine
US7762072B2 (en) 2007-01-16 2010-07-27 Honeywell International Inc. Combustion systems with rotary fuel slingers
US7942006B2 (en) 2007-03-26 2011-05-17 Honeywell International Inc. Combustors and combustion systems for gas turbine engines
US20080264035A1 (en) * 2007-04-25 2008-10-30 Ricciardo Mark J Coolant flow swirler for a rocket engine
EP2238020A2 (de) * 2008-01-07 2010-10-13 Aerojet-General Corporation Antriebssystem mit beweglicher wärmedrossel
WO2009126847A1 (en) * 2008-04-09 2009-10-15 Williams International Co., L.L.C. Gas turbine engine cooling system and method
US8763405B2 (en) * 2008-04-09 2014-07-01 Williams International Co., L.L.C. Gas turbine engine rotary injection system and method
KR100925858B1 (ko) 2008-08-22 2009-11-06 (주)씨앤스페이스 로켓 추진용 메탄엔진의 터보펌프
CN102029981B (zh) * 2009-09-29 2014-12-10 李开超 四种机动车用火箭及制动系统
JP5113230B2 (ja) * 2010-01-04 2013-01-09 貴之 伊東 ロケット発電エンジン及びロケット発電ファンエンジン
CN101915182B (zh) * 2010-06-09 2013-05-22 北京航空航天大学 一种固体燃料火箭发动机
CN101956981B (zh) * 2010-07-08 2012-05-23 中国航天科技集团公司第六研究院第十一研究所 一种气液组元高室压大范围变工况燃烧器
CN102619642B (zh) * 2010-10-19 2014-03-19 靳北彪 高效涡轮喷气发动机
CN101984240B (zh) * 2010-11-11 2013-04-24 西北工业大学 一种提高脉冲爆震火箭发动机工作频率的方法及装置
JP5666353B2 (ja) * 2011-03-11 2015-02-12 株式会社Ｉｈｉエアロスペース 液体ロケットエンジン用ノズル
JP2012189014A (ja) * 2011-03-11 2012-10-04 Ihi Aerospace Co Ltd ガス発生器
US9127622B2 (en) * 2011-11-21 2015-09-08 United Technologies Corporation Reversible flow discharge orifice
US9394803B2 (en) * 2012-03-14 2016-07-19 United Technologies Corporation Bypass air-pump system within the core engine to provide air for an environmental control system in a gas turbine engine
US9163562B2 (en) * 2012-03-14 2015-10-20 United Technologies Corporation Constant speed pump system for engine ECS loss elimination
US9151224B2 (en) * 2012-03-14 2015-10-06 United Technologies Corporation Constant-speed pump system for engine thermal management system AOC reduction and environmental control system loss elimination
RU2539064C2 (ru) * 2013-03-12 2015-01-10 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Двигательная установка космического летательного аппарата
US10920714B2 (en) * 2013-03-15 2021-02-16 Exquadrum, Inc. Stable hybrid rocket technology
TWI504538B (zh) * 2013-05-31 2015-10-21 Nat Applied Res Laboratories 雙旋流混合火箭引擎
CN103437914B (zh) * 2013-08-23 2015-12-09 中国航天科技集团公司第六研究院第十一研究所 一种变循环空气涡轮火箭组合发动机
GB2519155B (en) 2013-10-11 2016-10-12 Reaction Engines Ltd Engine
GB2519152B (en) * 2013-10-11 2016-09-07 Reaction Engines Ltd Engine
CN103742296B (zh) * 2013-12-23 2017-03-01 中国航天科技集团公司第六研究院第十一研究所 一种气膜冷却喷管
US9759161B2 (en) * 2014-03-28 2017-09-12 The Boeing Company Propulsion system and launch vehicle
CN103953463A (zh) * 2014-05-06 2014-07-30 中国航天科技集团公司第六研究院第十一研究所 一种低流阻锥阀
RU2551713C1 (ru) * 2014-06-26 2015-05-27 Открытое акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель
CN104309562A (zh) * 2014-10-25 2015-01-28 陈恒兰 车用准固液推进剂火箭防护系统
CN105630002B (zh) * 2014-10-30 2018-11-02 北京精密机电控制设备研究所 一种液体火箭发动机变推力调节机电伺服机构
CN106050475A (zh) * 2016-08-03 2016-10-26 杨斯涵 一种液固耦合式火箭发动机
CN106438104B (zh) * 2016-09-18 2018-05-22 中国科学院工程热物理研究所 一种富燃预燃涡扇发动机
CN107829844B (zh) * 2017-09-28 2019-07-16 西安航天动力试验技术研究所 一种四角切圆式的注气装置
CN108131205B (zh) * 2017-11-20 2019-06-18 北京动力机械研究所 一种涡扇发动机燃烧室启动方法
CN110541758B (zh) * 2019-08-14 2024-04-12 张繁荣 一种含氧燃料用涡轮喷气发动机
AU2021211979A1 (en) * 2020-08-06 2022-02-24 Dawn Aerospace Limited Rocket motor and components thereof
CN113266492B (zh) * 2021-04-16 2022-03-15 北京星际荣耀空间科技股份有限公司 发动机推力室、火箭发动机、液体火箭
JP7039095B1 (ja) * 2021-06-17 2022-03-22 基輝 三森 ロケットエンジン用水素噴射装置
CN113882971B (zh) * 2021-09-15 2023-02-03 浙江理工大学 一种火箭发动机涡轮泵的定子导叶结构
CN114991997B (zh) * 2022-06-01 2024-09-13 西安航天动力研究所 一种身部和推力室
CN115726905B (zh) * 2022-11-16 2024-06-11 青岛星辰航线科技有限公司 一种液氧、煤油火炬式点火器
GB2624129A (en) * 2024-02-09 2024-05-08 Wirth Res Limited Rocket engine

Family Cites Families (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2479777A (en) 1943-05-22 1949-08-23 Lockheed Aircraft Corp Fuel injection means for gas turbine power plants for aircraft
US2479776A (en) 1944-04-15 1949-08-23 Lockheed Aircraft Corp Turbo-jet power plant with fuel vaporizer for afterburners
US2518881A (en) * 1947-06-25 1950-08-15 Daniel And Florence Guggenheim Fuel feeding and cooling construction for rotating combustion chambers
US2508420A (en) 1948-09-21 1950-05-23 Westinghouse Electric Corp Combustion apparatus
US2637973A (en) * 1949-04-01 1953-05-12 Reaction Motors Inc Rocket engine having turbine located in nozzle for driving auxiliaries
US2866313A (en) 1950-04-14 1958-12-30 Power Jets Res & Dev Ltd Means for cooling turbine-blades by liquid jets
US2775864A (en) 1951-04-10 1957-01-01 Gen Motors Corp Jet propulsion engine with afterburner
FR1104644A (fr) 1954-02-15 1955-11-22 Thomson Houston Comp Francaise Perfectionnements aux systèmes de commande de l'écoulement d'un fluide
US2914912A (en) 1955-10-24 1959-12-01 Gen Electric Combustion system for thermal powerplant
US3002340A (en) 1957-04-05 1961-10-03 United Aircraft Corp Rocket gas generator for turbofan engine
DE1164753B (de) * 1959-12-12 1964-03-05 Boelkow Entwicklungen Kg Raketentriebwerk fuer fluessige Treibstoffe
US3307359A (en) * 1963-06-26 1967-03-07 North American Aviation Inc Turbopump assembly
US3286473A (en) 1963-06-26 1966-11-22 North American Aviation Inc Fixed injector and turbopump assembly
DE977815C (de) * 1963-12-21 1970-12-03 Messerschmitt Boelkow Blohm Fluessigkeitsraketentriebwerk
US3440821A (en) * 1964-10-15 1969-04-29 Bolkow Gmbh Fuel component feed system for a liquid fuel thrust engine and liquid fuel rocket engine construction
US3318574A (en) 1964-11-30 1967-05-09 Canadian Patents Dev Gas turbine
DE1257489B (de) 1965-05-15 1967-12-28 Boelkow Gmbh Raketentriebwerk fuer fluessige Treibstoffe mit einer Hauptbrennkammer und einer Vorbrennkammer
DE1264870B (de) * 1965-10-21 1968-03-28 Boelkow Gmbh Fluessigkeitsraketentriebwerk
DE1278182B (de) 1966-11-11 1968-09-19 Boelkow Gmbh Ausbildung und Halterung des Hitzeschildes bei Fluessigkeitsraketentriebwerken in Hauptstrombauart
DE1626055B1 (de) 1967-04-05 1970-07-30 Messerschmitt Boelkow Blohm Aus mehreren Flüssigkeitsraketen bestehendes Antriebsaggregat
US3772885A (en) 1968-09-23 1973-11-20 Bolkow Gmbh Method for separation of a fluid monergol for running a rocket motor
US3577735A (en) * 1969-11-05 1971-05-04 Bolkow Ges Mit Beschrankter Liquid fuel rocket engine construction
DE2117219A1 (de) 1970-04-14 1971-11-04 Cav Ltd Heißgasgenerator
DE2144819C3 (de) 1971-09-08 1978-06-22 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Steuereinrichtung für ein Flüssigkeitsraketentriebwerk der sogenannten Hauptstrombauart
DE2155786A1 (de) 1971-11-10 1973-05-17 Messerschmitt Boelkow Blohm Startverfahren fuer ein fluessigkeitsraketentriebwerk
US3882676A (en) 1972-11-01 1975-05-13 Messerschmitt Boelkow Blohm Main stream liquid-fuel rocket engine construction
DE2300983A1 (de) 1973-01-10 1974-07-11 Messerschmitt Boelkow Blohm Zuendsystem fuer mit nichthypergolen treibstoffkomponenten betriebene brennkammern von raketentriebwerken
DE2949522C2 (de) * 1979-12-08 1982-01-28 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Gekühlte Schubdüse für ein Raketentriebwerk
US4589253A (en) * 1984-04-16 1986-05-20 Rockwell International Corporation Pre-regenerated staged-combustion rocket engine
USH1234H (en) 1985-02-06 1993-10-05 The United States Of America As Represented By The Secretary Of The Navy Solid propellant air-turborocket
JPS62261652A (ja) 1986-05-07 1987-11-13 Natl Space Dev Agency Japan<Nasda> 液体ロケツトエンジン
US4769996A (en) 1987-01-27 1988-09-13 Teledyne Industries, Inc. Fuel transfer system for multiple concentric shaft gas turbine engines
US5010730A (en) 1988-02-24 1991-04-30 Acurex Corporation Gas-fed hybrid propulsion system
US4901525A (en) 1988-03-09 1990-02-20 Acurex Corporation Booster-sustainer rocket engine and method
FR2628790A1 (fr) 1988-03-16 1989-09-22 Snecma Propulseur combine turbofusee aerobie
US4870825A (en) 1988-06-09 1989-10-03 Williams International Corporation Rotary fuel injection system
FR2665223B1 (fr) * 1990-07-26 1994-07-08 Snecma Procede pour entrainer simultanement deux pompes a regimes differents et turbopompe pour comprimer simultanement deux fluides.
US5267437A (en) 1991-05-23 1993-12-07 United Technologies Corporation Dual mode rocket engine
US5224713A (en) 1991-08-28 1993-07-06 General Electric Company Labyrinth seal with recirculating means for reducing or eliminating parasitic leakage through the seal
US5261223A (en) * 1992-10-07 1993-11-16 General Electric Company Multi-hole film cooled combustor liner with rectangular film restarting holes
US5323602A (en) 1993-05-06 1994-06-28 Williams International Corporation Fuel/air distribution and effusion cooling system for a turbine engine combustor burner
US5758504A (en) * 1996-08-05 1998-06-02 Solar Turbines Incorporated Impingement/effusion cooled combustor liner
US5765361A (en) 1996-08-23 1998-06-16 Jones; Herbert Stephen Hybrid-LO2-LH2 low cost launch vehicle
US5842665A (en) 1996-09-09 1998-12-01 Hmx, Inc. Launch vehicle with engine mounted on a rotor

Also Published As

Publication number Publication date
EP1171705A4 (de) 2005-01-12
US6220016B1 (en) 2001-04-24
US6269647B1 (en) 2001-08-07
JP2009150402A (ja) 2009-07-09
WO2000057048A2 (en) 2000-09-28
IL145349A (en) 2007-06-17
JP4386589B2 (ja) 2009-12-16
JP2009150401A (ja) 2009-07-09
CN1670353A (zh) 2005-09-21
CN100417801C (zh) 2008-09-10
IL164184A0 (en) 2005-12-18
JP2002540340A (ja) 2002-11-26
WO2000057048A3 (en) 2001-01-18
CA2364284C (en) 2008-05-06
ATE386203T1 (de) 2008-03-15
DE60038012T2 (de) 2009-02-12
EP1171705A2 (de) 2002-01-16
US6205770B1 (en) 2001-03-27
CN1201076C (zh) 2005-05-11
DE60038012D1 (de) 2008-03-27
CN1343282A (zh) 2002-04-03
AU6045800A (en) 2000-10-09
IL145349A0 (en) 2002-06-30
IL164183A0 (en) 2005-12-18
RU2243403C2 (ru) 2004-12-27
CA2364284A1 (en) 2000-09-28
EP1171705B1 (de) 2008-02-13

Similar Documents

Publication Publication Date Title
DE60044733D1 (de) Raketenmotor
SE8505707L (sv) Gasturbinmotorforsterkare
WO2008091307A3 (en) Core burning for scramjet engines
EP1363075A3 (de) Hitzeschildplatten für eine Gasturbinenbrennkammer
WO2008097320A3 (en) Premixing injector for gas turbine engines
GB1468508A (en) Engine cooling system
EP0957311A3 (de) Gasturbinenbrennkammer
CN1114732A (zh) 自燃燃烧室的冷却方法
SG142117A1 (en) Counter swirl annular combustor
WO2004072465A3 (en) Diversion of combustion gas within a rocket engine to preheat fuel
EP1126152A3 (de) Zylinderkopf und Brennkraftmaschine
WO2005003542A8 (en) Recuperator and combustor for use in external combustion engines and system for generating power employing same
GB1108705A (en) Improvements in cooling structure or combustion chamber
TR201909258T4 (tr) Brülör düzeneği ve yanma yöntemi.
JPS5455221A (en) Internal combustion engine with plurality of intake ports
AU2003246555A1 (en) Cooled cylinder head for a reciprocating engine
CA2394694A1 (en) Pilot nozzle of gas turbine combustor
WO2005028960A3 (en) Pilot combustor for stabilizing combustion in gas turbine engines
GB1037923A (en) Combustion chamber for a gas turbine
IT1317775B1 (it) Dispositivo passafiamma per camere di combustione di turbine a gas nonanulari
US20170321623A1 (en) Multistage throttling and expansion method for saving energy and reducing emissions of an engine
AU2003238144A1 (en) Ramjet engine combustion chamber and ramjet engine equipped with same
ATE178388T1 (de) Abgastemperatursteuerung
KR960024003A (ko) 층류식 버너
CA2246218A1 (en) Gas turbine combustor