FR2677706B1 - Statoreacteur a ejecteur. - Google Patents

Statoreacteur a ejecteur.

Info

Publication number
FR2677706B1
FR2677706B1 FR9207115A FR9207115A FR2677706B1 FR 2677706 B1 FR2677706 B1 FR 2677706B1 FR 9207115 A FR9207115 A FR 9207115A FR 9207115 A FR9207115 A FR 9207115A FR 2677706 B1 FR2677706 B1 FR 2677706B1
Authority
FR
France
Prior art keywords
statoreactor
ejector
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 - Fee Related
Application number
FR9207115A
Other languages
English (en)
Other versions
FR2677706A1 (fr
Inventor
John Bulman Melvin
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.)
Aerojet Rocketdyne Inc
Original Assignee
Aerojet General 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 Aerojet General Corp filed Critical Aerojet General Corp
Publication of FR2677706A1 publication Critical patent/FR2677706A1/fr
Application granted granted Critical
Publication of FR2677706B1 publication Critical patent/FR2677706B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases
    • 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
    • F02K7/12—Injection-induction 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
FR9207115A 1991-06-14 1992-06-12 Statoreacteur a ejecteur. Expired - Fee Related FR2677706B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/715,291 US5205119A (en) 1991-06-14 1991-06-14 Ejector ramjet

Publications (2)

Publication Number Publication Date
FR2677706A1 FR2677706A1 (fr) 1992-12-18
FR2677706B1 true FR2677706B1 (fr) 1995-01-13

Family

ID=24873442

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9207115A Expired - Fee Related FR2677706B1 (fr) 1991-06-14 1992-06-12 Statoreacteur a ejecteur.

Country Status (6)

Country Link
US (2) US5205119A (fr)
JP (1) JPH0663485B2 (fr)
DE (1) DE4219037A1 (fr)
FR (1) FR2677706B1 (fr)
GB (1) GB2256677B (fr)
IL (2) IL102162A (fr)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2120595C (fr) * 1994-04-05 1997-03-25 Charles D. Maclennan Dent de scie pour scie circulaire
FR2720122B1 (fr) * 1994-05-20 1996-06-28 Inst Francais Du Petrole Pompe polyphasique bi-turbojets.
US5806303A (en) * 1996-03-29 1998-09-15 General Electric Company Turbofan engine with a core driven supercharged bypass duct and fixed geometry nozzle
US5740985A (en) * 1996-09-16 1998-04-21 Scott; Harry Low earth orbit payload launch system
US5946904A (en) * 1997-08-12 1999-09-07 Boehnlein; John J. Ejector ramjet engine
US6058846A (en) * 1998-06-03 2000-05-09 Lockhead Martin Corporation Rocket and ramjet powered hypersonic stealth missile having alterable radar cross section
US6857261B2 (en) * 2003-01-07 2005-02-22 Board Of Regents, The University Of Texas System Multi-mode pulsed detonation propulsion system
US6981364B2 (en) * 2003-07-22 2006-01-03 National Aerospace Laboratory Of Japan Combine engine for single-stage spacecraft
GB2404952B (en) * 2003-08-12 2006-08-30 Rolls Royce Plc Air breathing reaction propulsion engines
SE527789C2 (sv) * 2004-11-05 2006-06-07 Volvo Aero Corp Utloppsanordning för styrning av ett gasflöde från en jetmotor
EP1696116B1 (fr) * 2005-02-24 2018-04-11 Rolls-Royce plc Orientation de la poussée avec jets de fluide
GB0503874D0 (en) * 2005-02-24 2005-04-06 Rolls Royce Plc Fluid vectoring nozzle
US8256203B1 (en) * 2007-01-26 2012-09-04 The University Of Alabama In Huntsville Rocket based combined cycle propulsion unit having external rocket thrusters
US20090158705A1 (en) * 2007-12-21 2009-06-25 Grossi Fabio G Hypermixing Fluid Ejector
FR2933744B1 (fr) * 2008-07-11 2011-06-03 Snecma Moteur-fusee et reacteur comportant une pluralite de tels moteurs-fusees.
CA2671914A1 (fr) * 2009-07-13 2011-01-13 Zine Aidoun Systeme de pompe a jet pour gestion de la chaleur et du froid, appareillage, montage et methodes d'utilisation
CN103143461B (zh) * 2013-02-05 2015-09-16 中国人民解放军国防科学技术大学 滑块式变马赫数喷管及其壁面确定方法
US10273932B2 (en) * 2013-07-11 2019-04-30 Edouard KASSIANOFF Oscillating propulsor
CN105089851B (zh) * 2014-05-06 2016-11-16 中国航天科技集团公司第六研究院第十一研究所 可重复拆装推力室及该推力室推力向量精度的调节方法
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
AU2016338382B2 (en) 2015-09-02 2021-04-01 Jetoptera, Inc. Ejector and airfoil configurations
USD868627S1 (en) 2018-04-27 2019-12-03 Jetoptera, Inc. Flying car
DE102016112619A1 (de) * 2016-06-24 2017-12-28 Christian Bauer Triebwerkzündgerat für ein Triebwerk sowie Zündverfahren
RU2641178C1 (ru) * 2016-12-05 2018-01-16 Владимир Ильич Юркин Способ образования реактивных сил движения из воздушно-динамической части реактивной струи и устройство его осуществления
DE102019118580B4 (de) * 2019-07-09 2023-02-09 Deutsches Zentrum für Luft- und Raumfahrt e.V. Triebwerksvorrichtung, Luftfahrzeug, Raumfahrzeug, kombiniertes Luft-/Raumfahrzeug und Verfahren zum Betreiben einer Triebwerksvorrichtung

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1030483A (fr) * 1951-01-04 1953-06-15 Snecma Procédé et dispositifs de réglage d'un écoulement et leurs diverses applications
US3046732A (en) * 1956-06-20 1962-07-31 Research Corp Method of energy exchange and apparatus for carrying out the same
DE1209809B (de) * 1959-04-08 1966-01-27 Paul Sommer Kontinuierlich arbeitendes Strahltriebwerk
US3046372A (en) * 1959-05-25 1962-07-24 Michael J Civitano Fused outlet device and the like
US3279185A (en) * 1963-07-18 1966-10-18 George D Lewis Rocket steering system
US3143856A (en) * 1963-07-30 1964-08-11 United Aircraft Corp Directional control means for rockets or the like
US3357191A (en) * 1964-10-20 1967-12-12 Berner Felix Propulsion means
US3568443A (en) * 1969-08-14 1971-03-09 Robert S Estes Starting apparatus for a fluid-dynamic engine
US3925982A (en) * 1973-09-11 1975-12-16 Martin Marietta Corp Fluid-dynamic shock ring for controlled flow separation in a rocket engine exhaust nozzle
US4030289A (en) * 1973-10-29 1977-06-21 Chandler Evans Inc. Thrust augmentation technique and apparatus
US3952982A (en) * 1975-01-07 1976-04-27 Lewis David P All angle camera mount with vernier adjustment
IL52613A (en) * 1977-07-28 1980-11-30 Univ Ramot Method and apparatus for controlling the mixing of two fluids
USH1007H (en) * 1985-05-24 1992-01-07 The United States Of America As Represented By The Secretary Of The Navy Solid fuel ramjet combustor
US4644746A (en) * 1985-12-30 1987-02-24 L. W. Fleckenstein, Inc. Gas compressor for jet engine

Also Published As

Publication number Publication date
FR2677706A1 (fr) 1992-12-18
GB9211016D0 (en) 1992-07-08
US5327721A (en) 1994-07-12
GB2256677A (en) 1992-12-16
US5205119A (en) 1993-04-27
IL112260A0 (en) 1995-03-30
IL102162A (en) 1996-11-14
GB2256677B (en) 1995-05-10
JPH05187320A (ja) 1993-07-27
JPH0663485B2 (ja) 1994-08-22
DE4219037A1 (de) 1992-12-17

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Legal Events

Date Code Title Description
ST Notification of lapse