JPH076455B2 - 組合せ式駆動装置 - Google Patents

組合せ式駆動装置

Info

Publication number
JPH076455B2
JPH076455B2 JP2064473A JP6447390A JPH076455B2 JP H076455 B2 JPH076455 B2 JP H076455B2 JP 2064473 A JP2064473 A JP 2064473A JP 6447390 A JP6447390 A JP 6447390A JP H076455 B2 JPH076455 B2 JP H076455B2
Authority
JP
Japan
Prior art keywords
engine
turbine
rocket
compressor
drive
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
JP2064473A
Other languages
English (en)
Japanese (ja)
Other versions
JPH02283846A (ja
Inventor
ハンス・リフカ
Original Assignee
メツセルシユミツト―ベルコウ―ブローム・ゲゼルシヤフト・ミト・ベシユレンクテル・ハフツング
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 メツセルシユミツト―ベルコウ―ブローム・ゲゼルシヤフト・ミト・ベシユレンクテル・ハフツング filed Critical メツセルシユミツト―ベルコウ―ブローム・ゲゼルシヤフト・ミト・ベシユレンクテル・ハフツング
Publication of JPH02283846A publication Critical patent/JPH02283846A/ja
Publication of JPH076455B2 publication Critical patent/JPH076455B2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/401—Liquid propellant rocket engines
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/4005—Air-breathing propulsion
    • 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
    • F02C3/13—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having variable working fluid interconnections between turbines or compressors or stages of different rotors
    • 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
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/18—Composite ram-jet/rocket engines
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/402—Propellant tanks; Feeding propellants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
JP2064473A 1989-03-18 1990-03-16 組合せ式駆動装置 Expired - Lifetime JPH076455B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3909050.7 1989-03-18
DE3909050A DE3909050C1 (US06168776-20010102-C00041.png) 1989-03-18 1989-03-18

Publications (2)

Publication Number Publication Date
JPH02283846A JPH02283846A (ja) 1990-11-21
JPH076455B2 true JPH076455B2 (ja) 1995-01-30

Family

ID=6376739

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2064473A Expired - Lifetime JPH076455B2 (ja) 1989-03-18 1990-03-16 組合せ式駆動装置

Country Status (4)

Country Link
US (1) US5014508A (US06168776-20010102-C00041.png)
EP (1) EP0388613B1 (US06168776-20010102-C00041.png)
JP (1) JPH076455B2 (US06168776-20010102-C00041.png)
DE (2) DE3909050C1 (US06168776-20010102-C00041.png)

Families Citing this family (112)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5077968A (en) * 1990-04-06 1992-01-07 United Technologies Corporation Vaneless contrarotating turbine
FR2687433B1 (fr) * 1992-02-14 1994-05-06 Onera Propulseur a composants inverses, a alimentation modulee.
FR2701293B1 (fr) * 1993-02-05 1995-04-28 Europ Propulsion Moteur combiné intégrant les modes éjecteur à air turbocomprimé refroidi ou liquéfié statoréacteur et super-statoréacteur.
DE29710244U1 (de) * 1997-06-12 1997-08-21 Kähler, Kai, 20355 Hamburg Raumschiff
WO2000034122A1 (de) 1998-12-05 2000-06-15 Fuersich Manfred Verfahren zum transport einer nutzlast in den weltraum
US6148609A (en) * 1999-05-27 2000-11-21 Provitola; Anthony Italo Turbo-rocket thruster
EP1172544A1 (fr) * 2000-07-14 2002-01-16 Techspace Aero S.A. Moteur d'un lanceur spatial avec dispositif de collecte et séparation d'air
US6647707B2 (en) * 2000-09-05 2003-11-18 Sudarshan Paul Dev Nested core gas turbine engine
US6942451B1 (en) 2003-06-03 2005-09-13 Hamilton Sundstrand Corporation Damping system for an expendable gas turbine engine
US7194866B1 (en) 2003-06-20 2007-03-27 Hamilton Sundstrand Corporation Static structure for an expendable gas turbine engine
FR2858999B1 (fr) * 2003-08-18 2005-11-11 Snecma Moteurs Turbomachine pour aeronef a emissions de bruit reduites
US8438858B1 (en) 2003-08-20 2013-05-14 Hamilton Sundstrand Corporation Rotational system for an expendable gas turbine engine
US7854112B2 (en) * 2004-12-01 2010-12-21 United Technologies Corporation Vectoring transition duct for turbine engine
WO2006059973A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine with a heat exchanger
US7959406B2 (en) 2004-12-01 2011-06-14 United Technologies Corporation Close coupled gearbox assembly for a tip turbine engine
WO2006060000A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
US8468795B2 (en) * 2004-12-01 2013-06-25 United Technologies Corporation Diffuser aspiration for a tip turbine engine
EP1828568B1 (en) 2004-12-01 2011-03-23 United Technologies Corporation Fan-turbine rotor assembly for a tip turbine engine
EP1828545A2 (en) 2004-12-01 2007-09-05 United Technologies Corporation Annular turbine ring rotor
US8033092B2 (en) 2004-12-01 2011-10-11 United Technologies Corporation Tip turbine engine integral fan, combustor, and turbine case
WO2006060004A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Combustor for turbine engine
EP1819907A2 (en) 2004-12-01 2007-08-22 United Technologies Corporation Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
WO2006059989A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine support structure
US8757959B2 (en) 2004-12-01 2014-06-24 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
EP1825117B1 (en) 2004-12-01 2012-06-13 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
US9845727B2 (en) 2004-12-01 2017-12-19 United Technologies Corporation Tip turbine engine composite tailcone
US7631480B2 (en) 2004-12-01 2009-12-15 United Technologies Corporation Modular tip turbine engine
WO2006059994A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Seal assembly for a fan-turbine rotor of a tip turbine engine
WO2006059985A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Axial compressor for tip turbine engine
EP1841959B1 (en) 2004-12-01 2012-05-09 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
EP1834067B1 (en) 2004-12-01 2008-11-26 United Technologies Corporation Fan blade assembly for a tip turbine engine and method of assembly
US8083030B2 (en) 2004-12-01 2011-12-27 United Technologies Corporation Gearbox lubrication supply system for a tip engine
WO2006060014A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Starter generator system for a tip turbine engine
WO2006060010A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Compressor inlet guide vane for tip turbine engine and corresponding control method
EP1825116A2 (en) * 2004-12-01 2007-08-29 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
US7921636B2 (en) * 2004-12-01 2011-04-12 United Technologies Corporation Tip turbine engine and corresponding operating method
EP1825128B1 (en) 2004-12-01 2011-03-02 United Technologies Corporation Regenerative turbine blade and vane cooling for a tip turbine engine
WO2006059993A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine with multiple fan and turbine stages
EP1825112B1 (en) 2004-12-01 2013-10-23 United Technologies Corporation Cantilevered tip turbine engine
US8641367B2 (en) 2004-12-01 2014-02-04 United Technologies Corporation Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method
US8061968B2 (en) 2004-12-01 2011-11-22 United Technologies Corporation Counter-rotating compressor case and assembly method for tip turbine engine
WO2006059986A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
US8365511B2 (en) 2004-12-01 2013-02-05 United Technologies Corporation Tip turbine engine integral case, vane, mount and mixer
DE602004019710D1 (de) 2004-12-01 2009-04-09 United Technologies Corp Fernbetätigung für eine verstellbare stufe eines verdichters für einen turbinenmotor
DE602004027766D1 (de) 2004-12-01 2010-07-29 United Technologies Corp Hydraulische dichtung für ein getriebe eines spitzenturbinenmotors
WO2006059968A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
WO2006059987A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Particle separator for tip turbine engine
US7976272B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Inflatable bleed valve for a turbine engine
WO2006112807A2 (en) 2004-12-01 2006-10-26 United Technologies Corporation Turbine engine and method for starting a turbine engine
US8087885B2 (en) * 2004-12-01 2012-01-03 United Technologies Corporation Stacked annular components for turbine engines
WO2006060009A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Turbine blade engine comprising turbine clusters and radial attachment lock arrangement therefor
US7883315B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
DE602004028297D1 (de) * 2004-12-01 2010-09-02 United Technologies Corp Umfangsbrennkammer für spitzenturbinenmotor
US9109537B2 (en) 2004-12-04 2015-08-18 United Technologies Corporation Tip turbine single plane mount
JPWO2006103774A1 (ja) * 2005-03-30 2008-09-04 力也 石川 垂直移動可能な飛行体
WO2007013058A2 (en) * 2005-07-27 2007-02-01 Aryeh Yaakov Kohn Combined rocket- jet engine propulsion system
US20070175222A1 (en) * 2006-01-31 2007-08-02 United Technologies Corporation Multipurpose gas generator ramjet/scramjet cold start system
US7721524B2 (en) * 2006-02-15 2010-05-25 United Technologies Corporation Integrated airbreathing and non-airbreathing engine system
GB2449095B (en) * 2007-05-10 2009-05-27 Rolls Royce Plc Re-Pressurisation device
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
CN103893843B (zh) 2008-05-02 2017-03-01 凯希特许有限公司 具有调节压力能力的手动致动减压治疗泵
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
CN102146858A (zh) * 2010-08-12 2011-08-10 靳北彪 风动透平冲压发动机
US20120110976A1 (en) * 2010-11-08 2012-05-10 Marius Angelo Paul Universal aero space , naval eternal technology systems
FR2967725B1 (fr) 2010-11-23 2012-12-14 Snecma Propulseur combine turboreacteur et statoreacteur
CN102826227B (zh) * 2012-08-22 2015-09-09 冯加伟 无人空天战机
US20140165568A1 (en) * 2012-12-14 2014-06-19 Electro-Motive Diesel, Inc. Energy Recovery System for a Mobile Machine
FR3001260B1 (fr) * 2013-01-18 2017-04-21 Astrium Sas Dispositif de demarrage d'une turbopompe de moteur fusee
US9709069B2 (en) 2013-10-22 2017-07-18 Dayspring Church Of God Apostolic Hybrid drive engine
RU2554392C1 (ru) * 2014-01-10 2015-06-27 Николай Борисович Болотин Водородный газотурбинный двигатель
RU2561764C1 (ru) * 2014-01-10 2015-09-10 Николай Борисович Болотин Водородный газотурбинный двигатель
RU2561757C1 (ru) * 2014-01-14 2015-09-10 Николай Борисович Болотин Трехкомпонентный воздушно-реактивный двигатель
DE102014000991A1 (de) * 2014-01-29 2015-07-30 Bayern Chemie Gmbh Flugkörper mit Turbine-Verdichter-Einheit
RU2561773C1 (ru) * 2014-01-29 2015-09-10 Николай Борисович Болотин Двухтопливный воздушно-реактивный двигатель
RU2594091C1 (ru) * 2015-01-12 2016-08-10 Николай Борисович Болотин Двигательная установка гиперзвукового самолета
RU2591361C1 (ru) * 2015-01-13 2016-07-20 Николай Борисович Болотин Двигательная установка гиперзвукового самолета
US10337401B2 (en) 2015-02-13 2019-07-02 United Technologies Corporation Turbine engine with a turbo-compressor
US10041408B2 (en) * 2015-02-13 2018-08-07 United Technologies Corporation Turbine engine with a turbo-compressor
US10125722B2 (en) 2015-02-13 2018-11-13 United Technologies Corporation Turbine engine with a turbo-compressor
US10060316B2 (en) 2015-06-29 2018-08-28 General Electric Company Power generation system exhaust cooling
US9840953B2 (en) 2015-06-29 2017-12-12 General Electric Company Power generation system exhaust cooling
US9938874B2 (en) 2015-06-29 2018-04-10 General Electric Company Power generation system exhaust cooling
US9850818B2 (en) 2015-06-29 2017-12-26 General Electric Company Power generation system exhaust cooling
US10077694B2 (en) 2015-06-29 2018-09-18 General Electric Company Power generation system exhaust cooling
US9850794B2 (en) 2015-06-29 2017-12-26 General Electric Company Power generation system exhaust cooling
US10087801B2 (en) * 2015-06-29 2018-10-02 General Electric Company Power generation system exhaust cooling
US9856768B2 (en) 2015-06-29 2018-01-02 General Electric Company Power generation system exhaust cooling
US10030558B2 (en) 2015-06-29 2018-07-24 General Electric Company Power generation system exhaust cooling
US10215070B2 (en) 2015-06-29 2019-02-26 General Electric Company Power generation system exhaust cooling
RU2609547C1 (ru) * 2015-11-06 2017-02-02 Николай Борисович Болотин Возвращаемая ступень ракеты-носителя и способ ее работы
RU2609549C1 (ru) * 2015-11-09 2017-02-02 Николай Борисович Болотин Возвращаемая ступень ракеты-носителя и способ ее работы
RU2609664C1 (ru) * 2015-11-10 2017-02-02 Николай Борисович Болотин Возвращаемая ступень ракеты-носителя, способ ее работы и газотурбинный двигатель
DE102015120046B4 (de) 2015-11-19 2020-10-01 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Fahrzeug mit Kombinationsantrieb
US10316759B2 (en) 2016-05-31 2019-06-11 General Electric Company Power generation system exhaust cooling
RU174498U1 (ru) * 2017-04-28 2017-10-17 Федеральное государственное унитарное предприятие Тушинское машиностроительное конструкторское бюро "Союз" ФГУП ТМКБ "Союз" Силовая установка гиперзвукового летательного аппарата
US10718264B2 (en) * 2018-03-16 2020-07-21 The Boeing Company Inlet diffusers for jet engines, jet engines, jet aircraft, and methods for diffusing incoming air of jet engines
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US11391247B1 (en) 2019-01-24 2022-07-19 Firefly Aerospace Inc. Liquid rocket engine cooling channels
US11333104B1 (en) 2019-01-24 2022-05-17 Firefly Aerospace Inc. Liquid rocket engine cross impinged propellant injection
US11008977B1 (en) 2019-09-26 2021-05-18 Firefly Aerospace Inc. Liquid rocket engine tap-off power source
US11846251B1 (en) * 2020-04-24 2023-12-19 Firefly Aerospace Inc. Liquid rocket engine booster engine with combustion gas fuel source
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US11635022B1 (en) 2022-02-11 2023-04-25 Raytheon Technologies Corporation Reducing contrails from an aircraft powerplant
GB202204068D0 (en) 2022-03-23 2022-05-04 Rolls Royce Plc Fuel system
CN115680940A (zh) * 2022-10-15 2023-02-03 中国科学院力学研究所 冠生涡轮变循环涡轮火箭发动机和发动机推力实现方法
WO2024132162A1 (en) * 2022-12-22 2024-06-27 Destinus Sa Air turborocket apparatus with precooler heat exchanger at the air intake
US12071890B1 (en) 2023-03-08 2024-08-27 Rtx Corporation Recovering water and/or heat energy from powerplant combustion products
CN117329025B (zh) * 2023-12-01 2024-02-23 陕西天回航天技术有限公司 一种涡轮排气冲压增推组合循环发动机及航天飞行器

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2995893A (en) * 1957-07-03 1961-08-15 Napier & Son Ltd Compound ramjet-turborocket engine
FR1280103A (fr) * 1960-11-18 1961-12-29 Snecma Moteur à réaction composite pour aérodynes à grand écart de vitesse
US3635577A (en) * 1968-04-11 1972-01-18 Aerostatic Ltd Coaxial unit
US3818695A (en) * 1971-08-02 1974-06-25 Rylewski Eugeniusz Gas turbine
DE3005864A1 (de) * 1980-02-16 1981-09-03 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zum steuern der stroemungsquerschnitte von kanaelen, insbesondere von gasleitrohren eines raketen-staustrahltriebwerks
DE3617915C1 (de) * 1986-05-28 1987-09-17 Messerschmitt Boelkow Blohm Kombinationsantrieb
DE3738703A1 (de) * 1987-05-27 1988-12-08 Mtu Muenchen Gmbh Kombiniertes, umschaltbares strahltriebwerk zum antrieb von flugzeugen und raumfahrzeugen
FR2628790A1 (fr) * 1988-03-16 1989-09-22 Snecma Propulseur combine turbofusee aerobie

Also Published As

Publication number Publication date
DE59000220D1 (de) 1992-09-03
EP0388613A1 (de) 1990-09-26
JPH02283846A (ja) 1990-11-21
US5014508A (en) 1991-05-14
DE3909050C1 (US06168776-20010102-C00041.png) 1990-08-16
EP0388613B1 (de) 1992-07-29

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