DE68901357D1 - Kombinationstriebwerk, rakete mit luftatmendem turbinenstrahltriebwerk. - Google Patents

Kombinationstriebwerk, rakete mit luftatmendem turbinenstrahltriebwerk.

Info

Publication number
DE68901357D1
DE68901357D1 DE8989400714T DE68901357T DE68901357D1 DE 68901357 D1 DE68901357 D1 DE 68901357D1 DE 8989400714 T DE8989400714 T DE 8989400714T DE 68901357 T DE68901357 T DE 68901357T DE 68901357 D1 DE68901357 D1 DE 68901357D1
Authority
DE
Germany
Prior art keywords
engine
rocket
air
turbine jet
combination
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
DE8989400714T
Other languages
English (en)
Inventor
Francois Jean-Pierre Mirville
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of DE68901357D1 publication Critical patent/DE68901357D1/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
    • F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/78—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with an air-breathing jet-propulsion plant
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/073—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric

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)
DE8989400714T 1988-03-16 1989-03-15 Kombinationstriebwerk, rakete mit luftatmendem turbinenstrahltriebwerk. Expired - Lifetime DE68901357D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8803367A FR2628790A1 (fr) 1988-03-16 1988-03-16 Propulseur combine turbofusee aerobie

Publications (1)

Publication Number Publication Date
DE68901357D1 true DE68901357D1 (de) 1992-06-04

Family

ID=9364293

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8989400714T Expired - Lifetime DE68901357D1 (de) 1988-03-16 1989-03-15 Kombinationstriebwerk, rakete mit luftatmendem turbinenstrahltriebwerk.

Country Status (5)

Country Link
US (1) US5012640A (de)
EP (1) EP0333585B1 (de)
JP (1) JPH0660602B2 (de)
DE (1) DE68901357D1 (de)
FR (1) FR2628790A1 (de)

Families Citing this family (70)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3909050C1 (de) * 1989-03-18 1990-08-16 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
JP2654577B2 (ja) * 1991-05-23 1997-09-17 宇宙科学研究所長 航空機エンジン用超音速プリクーラ
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
DE19617916B4 (de) * 1996-05-03 2007-02-01 Airbus Deutschland Gmbh Verdampfer zum Verdampfen eines tiefkalten flüssigen Mediums
US5938975A (en) * 1996-12-23 1999-08-17 Ennis; Bernard Method and apparatus for total energy fuel conversion systems
CA2364284C (en) 1999-03-10 2008-05-06 Williams International Co., L.L.C. Rocket engine
EP1175332A4 (de) 1999-04-28 2003-10-22 Anthony I Provitola Luftschiff/raumfahrzeug
US6119983A (en) * 1999-04-28 2000-09-19 Provitola; Anthony Italo Airship/spacecraft
US6148609A (en) * 1999-05-27 2000-11-21 Provitola; Anthony Italo Turbo-rocket thruster
US6227486B1 (en) * 1999-05-28 2001-05-08 Mse Technology Applications, Inc. Propulsion system for earth to orbit vehicle
AU2001284386A1 (en) * 2000-09-11 2002-03-22 Petur Thordarson Hydrogen motor
US6691504B1 (en) * 2000-11-01 2004-02-17 Anthony Italo Provitola Gaseous-fuel breathing rocket engine
US7117663B2 (en) * 2004-05-25 2006-10-10 Jonathan Cleaveland Knapp Air breathing, hydrogen fueled jet engine for high speed aircraft
US8024931B2 (en) 2004-12-01 2011-09-27 United Technologies Corporation Combustor for turbine engine
US8807936B2 (en) 2004-12-01 2014-08-19 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
US8083030B2 (en) 2004-12-01 2011-12-27 United Technologies Corporation Gearbox lubrication supply system for a tip engine
EP1831530B1 (de) 2004-12-01 2009-02-25 United Technologies Corporation Fernbetätigung für eine verstellbare stufe eines verdichters für einen turbinenmotor
EP1825111B1 (de) 2004-12-01 2011-08-31 United Technologies Corporation Gegenläufiges kompressorgehäuse für ein tip-turbinentriebwerk
EP1825128B1 (de) 2004-12-01 2011-03-02 United Technologies Corporation Regenerative Kühlung einer Leit- und Laufschaufel für ein Tipturbinentriebwerk
EP1825114B1 (de) * 2004-12-01 2008-08-20 United Technologies Corporation Tip-turbinentriebwerk mit wärmetauscher
US7845157B2 (en) 2004-12-01 2010-12-07 United Technologies Corporation Axial compressor for tip turbine engine
WO2006060013A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
WO2006060012A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine comprising turbine blade clusters and method of assembly
US8033092B2 (en) 2004-12-01 2011-10-11 United Technologies Corporation Tip turbine engine integral fan, combustor, and turbine case
WO2006110122A2 (en) 2004-12-01 2006-10-19 United Technologies Corporation Inflatable bleed valve for a turbine engine and a method of operating therefore
US7959532B2 (en) 2004-12-01 2011-06-14 United Technologies Corporation Hydraulic seal for a gearbox of a tip turbine engine
WO2006059999A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method
US7980054B2 (en) * 2004-12-01 2011-07-19 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
US9845727B2 (en) 2004-12-01 2017-12-19 United Technologies Corporation Tip turbine engine composite tailcone
WO2006059988A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Modular tip turbine engine
WO2006059987A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Particle separator for tip turbine engine
EP1831521B1 (de) 2004-12-01 2008-08-20 United Technologies Corporation Variable gebläseeinlassleitschaufelanordnung, turbinenmotor mit solch einer anordnung und entsprechendes steuerverfahren
WO2006059980A2 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Diffuser aspiration for a tip turbine engine
WO2006059979A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine integral case, vane, mount, and mixer
EP1831519B1 (de) * 2004-12-01 2010-08-04 United Technologies Corporation Tip-Turbinentriebwerk mit mehreren Gebläse- und Turbinenstufen
WO2006059975A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Peripheral combustor for tip turbine engine
WO2006060009A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Turbine blade engine comprising turbine clusters and radial attachment lock arrangement therefor
EP1825113B1 (de) * 2004-12-01 2012-10-24 United Technologies Corporation Gegenläufiges getriebe für ein tip-turbinen-triebwerk
WO2006060011A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
WO2006112807A2 (en) 2004-12-01 2006-10-26 United Technologies Corporation Turbine engine and method for starting a turbine engine
WO2006060003A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
US8087885B2 (en) * 2004-12-01 2012-01-03 United Technologies Corporation Stacked annular components for turbine engines
EP1828545A2 (de) 2004-12-01 2007-09-05 United Technologies Corporation Ringförmiger turbinenringrotor
EP1828574B1 (de) 2004-12-01 2010-11-03 United Technologies Corporation Enggekoppelte getriebeanordnung für einen spitzenturbinenmotor
DE602004019709D1 (de) * 2004-12-01 2009-04-09 United Technologies Corp Tip-turbinentriebwerk und entsprechendes betriebsverfahren
WO2006060001A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Fan rotor assembly for a tip turbine engine
WO2006059986A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
US7976273B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Tip turbine engine support structure
WO2006060010A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Compressor inlet guide vane for tip turbine engine and corresponding control method
WO2006060014A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Starter generator system for a tip turbine engine
EP1825117B1 (de) 2004-12-01 2012-06-13 United Technologies Corporation Turbinentriebwerk mit von einem differentialgetriebe angetriebenem fan und verdichter
EP1825126B1 (de) * 2004-12-01 2011-02-16 United Technologies Corporation Übergangskanal mit mitteln zur strömungsvektorbeeinflussung bei einer gasturbine
US7883314B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan-turbine rotor of a tip turbine engine
WO2006059978A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Cantilevered tip turbine engine
WO2006062497A1 (en) 2004-12-04 2006-06-15 United Technologies Corporation Tip turbine engine mount
US20070205330A1 (en) * 2006-01-11 2007-09-06 Hubbard Aerospace, Llc Flight/launch vehicle and method using internally stored air for air-breathing engines
US20080264035A1 (en) * 2007-04-25 2008-10-30 Ricciardo Mark J Coolant flow swirler for a rocket engine
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
JP4672747B2 (ja) * 2008-03-18 2011-04-20 三菱重工業株式会社 ロケットノズル及びロケットエンジン燃焼ガス流れの制御方法
US8522521B2 (en) * 2010-11-09 2013-09-03 Hamilton Sundstrand Corporation Combined air turbine starter, air-oil cooler, and fan
US9403600B2 (en) * 2012-05-01 2016-08-02 Lockheed Martin Corporation Integrated thermal protection and leakage reduction in a supersonic air intake system
US9650997B2 (en) 2013-03-05 2017-05-16 John Bossard Rotary turbo rocket
JP6417167B2 (ja) * 2014-09-29 2018-10-31 川崎重工業株式会社 ガスタービン
US10590786B2 (en) * 2016-05-03 2020-03-17 General Electric Company System and method for cooling components of a gas turbine engine
JP6743776B2 (ja) * 2017-07-06 2020-08-19 トヨタ自動車株式会社 燃料電池モジュール
CN108759146A (zh) * 2018-05-28 2018-11-06 张家港富瑞氢能装备有限公司 一种氢透平膨胀装置
CN113217463A (zh) * 2021-06-19 2021-08-06 西北工业大学太仓长三角研究院 单级轴流式涡轮增压机构
CN113339844B (zh) * 2021-06-22 2022-11-18 西安航天动力研究所 一种空气氢气喷注单元及其燃烧组织方法
US11578871B1 (en) 2022-01-28 2023-02-14 General Electric Company Gas turbine engine combustor with primary and secondary fuel injectors
US11885498B2 (en) 2022-01-31 2024-01-30 General Electric Company Turbine engine with fuel system including a catalytic reformer

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3253406A (en) * 1966-05-31 Turbine propulsion unit
US2883828A (en) * 1954-11-10 1959-04-28 Alun R Howell Power plant incorporating a dynamic compressor
FR1136237A (fr) * 1954-11-30 1957-05-10 Power Jets Res & Dev Ltd Perfectionnements apportés aux aubages pour des installations avec turbine à gaz
US3237400A (en) * 1957-04-05 1966-03-01 United Aircraft Corp Turborocket engine
US3241311A (en) * 1957-04-05 1966-03-22 United Aircraft Corp Turbofan engine
US3002340A (en) * 1957-04-05 1961-10-03 United Aircraft Corp Rocket gas generator for turbofan engine
US3241310A (en) * 1957-04-05 1966-03-22 United Aricraft Corp Lightweight power plant
US2941790A (en) * 1957-05-01 1960-06-21 Thompson Ramo Wooldridge Inc Gas turbine engine actuated starter and dryer
US3237401A (en) * 1958-01-17 1966-03-01 United Aircraft Corp Regenerative expander engine
US2994785A (en) * 1958-04-09 1961-08-01 Snecma Starting method and apparatus for aircraft equipped with alternators
US3145532A (en) * 1961-07-27 1964-08-25 Plessey Co Ltd Gas-turbine operated engine starters
US3747339A (en) * 1961-11-13 1973-07-24 Texaco Inc Reaction propulsion engine and method of operation
US3705496A (en) * 1963-11-20 1972-12-12 Texaco Experiment Inc Reaction propulsion engine and method of operation
US3279192A (en) * 1963-12-30 1966-10-18 Gen Electric Variable area exhaust nozzle
US3355890A (en) * 1965-06-09 1967-12-05 Gen Electric Cruise fan powerplant
DE2146793B2 (de) * 1971-09-18 1974-08-15 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Raketen-Turbinen-Luftstrahltriebwerk
US3812672A (en) * 1972-02-10 1974-05-28 Cci Aerospace Corp Supercharged ejector ramjet aircraft engine
FR2215538B1 (de) * 1973-01-26 1976-11-05 Texaco Development Corp
AT358335B (de) * 1975-10-03 1980-09-10 Gilli Paul Viktor Dipl Ing Dr Einrichtung zum schnellanfahren und/oder zum kurzzeitigen ueberlasten eines gasturbinen- satzes mit offener prozessfuehrung

Also Published As

Publication number Publication date
EP0333585B1 (de) 1992-04-29
FR2628790A1 (fr) 1989-09-22
US5012640A (en) 1991-05-07
EP0333585A1 (de) 1989-09-20
JPH0660602B2 (ja) 1994-08-10
JPH01273860A (ja) 1989-11-01

Similar Documents

Publication Publication Date Title
DE68901357D1 (de) Kombinationstriebwerk, rakete mit luftatmendem turbinenstrahltriebwerk.
DE68924202T2 (de) Überschall-Kraftstoff-Einspritzdüse.
DE58900152D1 (de) Propfan-turbotriebwerk.
DE3772253D1 (de) Gasturbinenmotorbeschalung mit reduziertem widerstand.
DE68919829D1 (de) Generator mit gasturbine.
DE3768156D1 (de) Fluessigtreibstoffraketenmotor.
DE68900273D1 (de) Zweistoffraketenmotor.
GB2226995B (en) Gas turbine jet engine having a thrust reverser.
DE68912214D1 (de) Motorregler.
DE68908321T2 (de) Mantelgebläse-Turbinentriebwerk.
DE69107148T2 (de) Gasturbine mit gekühlten Schaufeln.
DE69008429T2 (de) Turbostrahl- und Raketenkombinationstriebwerk.
DE69018338T2 (de) Gasturbine.
DE3761916D1 (de) Raketentriebwerke.
DE69100339T2 (de) Raketensteuerungsanlage mit seitlichem Gasstrahl.
DE68901360D1 (de) Turbine mit variabler statorgeometrie.
DE68903324T2 (de) Brennstoffeinspritzduese.
DE69111526T2 (de) Schubumkehrsteuerung bei Gasturbinen.
DE68923602D1 (de) Rakentendüse mit ringförmiger Zusatzdüse.
DE69002283D1 (de) Gasturbinen-triebwerkseinheit.
DE68904172T2 (de) Kraftstoffeinspritzduese.
DE68903944D1 (de) Raketenwerfer.
DE68901330D1 (de) Kraftstoffeinspritzduese.
DE59000866D1 (de) Integriertes turbo-staustrahltriebwerk.
DE59000390D1 (de) Turbinen-staustrahltriebwerk.

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee