IL102162A - מנוע מגח-סילון בעל מפלט במיוחד עבור טילים - Google Patents

מנוע מגח-סילון בעל מפלט במיוחד עבור טילים

Info

Publication number
IL102162A
IL102162A IL10216292A IL10216292A IL102162A IL 102162 A IL102162 A IL 102162A IL 10216292 A IL10216292 A IL 10216292A IL 10216292 A IL10216292 A IL 10216292A IL 102162 A IL102162 A IL 102162A
Authority
IL
Israel
Prior art keywords
fluid
primary
nozzle
flow
jet
Prior art date
Application number
IL10216292A
Other languages
English (en)
Original Assignee
Aerojet General Co
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 Co filed Critical Aerojet General Co
Priority to IL11226092A priority Critical patent/IL112260A/he
Publication of IL102162A publication Critical patent/IL102162A/he

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)
IL10216292A 1991-06-14 1992-06-10 מנוע מגח-סילון בעל מפלט במיוחד עבור טילים IL102162A (he)

Priority Applications (1)

Application Number Priority Date Filing Date Title
IL11226092A IL112260A (he) 1991-06-14 1992-06-10 מנוע מגח-סילון בעל מפלט במיוחד עבורטילים

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 (1)

Publication Number Publication Date
IL102162A true IL102162A (he) 1996-11-14

Family

ID=24873442

Family Applications (2)

Application Number Title Priority Date Filing Date
IL10216292A IL102162A (he) 1991-06-14 1992-06-10 מנוע מגח-סילון בעל מפלט במיוחד עבור טילים
IL11226095A IL112260A0 (en) 1991-06-14 1995-01-05 Ejector ramjet engine particularly for missiles

Family Applications After (1)

Application Number Title Priority Date Filing Date
IL11226095A IL112260A0 (en) 1991-06-14 1995-01-05 Ejector ramjet engine particularly for missiles

Country Status (6)

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

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2120595C (en) * 1994-04-05 1997-03-25 Charles D. Maclennan Saw tooth for circular saw
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 (en) * 2005-02-24 2018-04-11 Rolls-Royce plc Thrust vectoring using fluid jets
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
US8381528B2 (en) 2007-12-21 2013-02-26 Grossi Aerospace, Inc. Ramjet superheater
FR2933744B1 (fr) * 2008-07-11 2011-06-03 Snecma Moteur-fusee et reacteur comportant une pluralite de tels moteurs-fusees.
CA2671914A1 (en) * 2009-07-13 2011-01-13 Zine Aidoun A jet pump system for heat and cold management, apparatus, arrangement and methods of use
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
CA2911964C (en) * 2013-07-11 2017-04-18 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
USD868627S1 (en) 2018-04-27 2019-12-03 Jetoptera, Inc. Flying car
CN108137149B (zh) 2015-09-02 2021-07-06 杰托普特拉股份有限公司 喷射器和翼型构型
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US11965456B2 (en) * 2015-09-02 2024-04-23 Jetoptera, Inc. Fluidic turbo heater system
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
CN115387930B (zh) * 2022-08-12 2025-02-11 中国科学院力学研究所 自适应可控喷流冲压组合发动机及其工作方法和应用

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
JPH0663485B2 (ja) 1994-08-22
GB2256677B (en) 1995-05-10
GB2256677A (en) 1992-12-16
GB9211016D0 (en) 1992-07-08
DE4219037A1 (de) 1992-12-17
FR2677706A1 (fr) 1992-12-18
US5327721A (en) 1994-07-12
FR2677706B1 (fr) 1995-01-13
IL112260A0 (en) 1995-03-30
US5205119A (en) 1993-04-27
JPH05187320A (ja) 1993-07-27

Similar Documents

Publication Publication Date Title
US5205119A (en) Ejector ramjet
US6308740B1 (en) Method and system of pulsed or unsteady ejector
US5946904A (en) Ejector ramjet engine
US6494034B2 (en) Pulsed detonation engine with backpressure
US6786040B2 (en) Ejector based engines
EP1918561B1 (en) Combustion nozzle fluidic injection assembly
US20110215204A1 (en) System and method for generating thrust
JPH0656132B2 (ja) ジエツトエンジン用ガスコンプレツサ
US20090162213A1 (en) Pumping Ejector
US6516605B1 (en) Pulse detonation aerospike engine
US4930309A (en) Gas compressor for jet engine
US4707981A (en) Variable expansion ratio reaction engine
US3407603A (en) Reaction propulsion engines
IL112260A (he) מנוע מגח-סילון בעל מפלט במיוחד עבורטילים
US4319201A (en) Self compressing supersonic flow device
RU2059852C1 (ru) Пульсирующий гиперзвуковой прямоточный воздушно-реактивный двигатель
GB756288A (en) Improvements relating to thrust augmenters for rocket motors
EP0871582B1 (en) Apparatus and method for controlling the motion of a fluid medium
RU2795488C2 (ru) Реактивный двигатель с устройством для продления времени работы исходящих из камеры сгорания газов
Struchtrup Compressible Flow: Nozzles and Diffusers
RU2187011C2 (ru) Реактивный двигатель
Harvey et al. Steady Flow in a pure fluid valve TVC System
Ebrahimi Numerical Investigation of Multi-Tube Pulse Detonation Engine1
Mark et al. Unobstructed Supersonic Combustion in Scramjets using Rotating Combustor and Flow Stabilizer for High Speed Operation

Legal Events

Date Code Title Description
FF Patent granted
KB Patent renewed
KB Patent renewed
MM9K Patent not in force due to non-payment of renewal fees