IL101578A - Jet-jet syringe - Google Patents

Jet-jet syringe

Info

Publication number
IL101578A
IL101578A IL10157892A IL10157892A IL101578A IL 101578 A IL101578 A IL 101578A IL 10157892 A IL10157892 A IL 10157892A IL 10157892 A IL10157892 A IL 10157892A IL 101578 A IL101578 A IL 101578A
Authority
IL
Israel
Prior art keywords
fuel
air flow
injector
flow direction
exit
Prior art date
Application number
IL10157892A
Other languages
English (en)
Hebrew (he)
Other versions
IL101578A0 (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
Publication of IL101578A0 publication Critical patent/IL101578A0/xx
Publication of IL101578A publication Critical patent/IL101578A/en

Links

Classifications

    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
IL10157892A 1991-04-29 1992-04-13 Jet-jet syringe IL101578A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/692,440 US5220787A (en) 1991-04-29 1991-04-29 Scramjet injector

Publications (2)

Publication Number Publication Date
IL101578A0 IL101578A0 (en) 1992-12-30
IL101578A true IL101578A (en) 1994-10-21

Family

ID=24780591

Family Applications (1)

Application Number Title Priority Date Filing Date
IL10157892A IL101578A (en) 1991-04-29 1992-04-13 Jet-jet syringe

Country Status (6)

Country Link
US (1) US5220787A (de)
JP (1) JP2553280B2 (de)
DE (1) DE4214088C2 (de)
FR (1) FR2675850B1 (de)
GB (1) GB2255628B (de)
IL (1) IL101578A (de)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5660040A (en) * 1994-12-20 1997-08-26 United Technologies Corporation Scramjet fuel injection system having independent fuel supplies for supersonic and hypersonic operation
US6207369B1 (en) * 1995-03-10 2001-03-27 Meso Scale Technologies, Llc Multi-array, multi-specific electrochemiluminescence testing
FR2750169B1 (fr) * 1996-06-24 1998-08-21 Aerospatiale Dispositif d'injection de combustible pour statoreacteur fonctionnant a un nombre de mach eleve
FR2750170B1 (fr) * 1996-06-24 1998-08-21 Aerospatiale Mat d'injection de combustible pour statoreacteur fonctionnant a un nombre de mach eleve
GB2324147B (en) 1997-04-10 2001-09-05 Europ Gas Turbines Ltd Fuel-injection arrangement for a gas turbine combuster
US6470672B1 (en) 2000-07-17 2002-10-29 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Minimally intrusive and nonintrusive supersonic injectors for LANTR and RBCC/Scramjet propulsion systems
JP4522558B2 (ja) * 2000-08-11 2010-08-11 実 屋我 スクラムジェットエンジン用燃料混合促進方法並びに装置
US6568171B2 (en) 2001-07-05 2003-05-27 Aerojet-General Corporation Rocket vehicle thrust augmentation within divergent section of nozzle
JP3932329B2 (ja) * 2002-03-29 2007-06-20 独立行政法人科学技術振興機構 スクラムジェット燃焼器およびその制御法
US7823376B2 (en) * 2005-09-13 2010-11-02 Aerojet-General Corporation Thrust augmentation in plug nozzles and expansion-deflection nozzles
US7484494B2 (en) * 2006-01-27 2009-02-03 Gm Global Technology Operations, Inc. Method and apparatus for a spark-ignited direct injection engine
US8448881B2 (en) * 2006-10-13 2013-05-28 Rolls-Royce Power Engineering Plc Fuel injector
US7797943B2 (en) * 2006-10-18 2010-09-21 Aerojet-General Corporation Core burning for scramjet engines
US8359825B2 (en) * 2008-05-21 2013-01-29 Florida State University Research Foundation Microjet creation and control of shock waves
US8863525B2 (en) 2011-01-03 2014-10-21 General Electric Company Combustor with fuel staggering for flame holding mitigation
US9353704B2 (en) 2011-08-19 2016-05-31 Gulfstream Aerospace Corporation Air inlet arrangement and method of making the same
US9121369B2 (en) * 2011-08-19 2015-09-01 Gulfstream Aerospace Corporation Nozzle arrangement and method of making the same
JP6258101B2 (ja) * 2014-03-28 2018-01-10 三菱重工業株式会社 ジェットエンジン、飛しょう体及びジェットエンジンの動作方法
US10203114B2 (en) 2016-03-04 2019-02-12 General Electric Company Sleeve assemblies and methods of fabricating same
US10228141B2 (en) 2016-03-04 2019-03-12 General Electric Company Fuel supply conduit assemblies
US10865992B2 (en) 2016-12-30 2020-12-15 General Electric Company Fuel injectors and methods of use in gas turbine combustor
US10851999B2 (en) 2016-12-30 2020-12-01 General Electric Company Fuel injectors and methods of use in gas turbine combustor
US10816208B2 (en) 2017-01-20 2020-10-27 General Electric Company Fuel injectors and methods of fabricating same
US10502426B2 (en) 2017-05-12 2019-12-10 General Electric Company Dual fuel injectors and methods of use in gas turbine combustor
US10718523B2 (en) 2017-05-12 2020-07-21 General Electric Company Fuel injectors with multiple outlet slots for use in gas turbine combustor
US10690349B2 (en) 2017-09-01 2020-06-23 General Electric Company Premixing fuel injectors and methods of use in gas turbine combustor
KR102429643B1 (ko) * 2018-05-15 2022-08-04 에어 프로덕츠 앤드 케미칼스, 인코오포레이티드 가스 터빈의 연소 안정성 개선 시스템 및 방법
KR101954034B1 (ko) * 2018-10-11 2019-03-04 국방과학연구소 초음속 연료 분사 장치
CN114985127B (zh) * 2022-07-15 2022-11-01 中国空气动力研究与发展中心低速空气动力研究所 一种改变射流形状的方法
CN116335852B (zh) * 2023-02-07 2023-09-01 中国空气动力研究与发展中心空天技术研究所 集成增强火箭的冲压发动机尾喷管及设计、工作方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3273334A (en) * 1959-09-10 1966-09-20 Frank I Tanczos Ramjet missile
US3334485A (en) * 1962-07-26 1967-08-08 Barry V Rhodes Ramjet powered craft
US4291533A (en) * 1965-12-30 1981-09-29 The United States Of America As Represented By The Secretary Of The Navy Supersonic ramjet missile
DE1800611A1 (de) * 1968-10-02 1970-05-27 Hertel Dr Ing Heinrich Anordnung zum Einspritzen von Kraftstoff in einen an einer Einspritzduese mit UEberschallgeschwindigkeit vorbeistroemenden Luftstrom
US3699773A (en) * 1968-12-23 1972-10-24 Gen Electric Fuel cooled fuel injectors
US3664588A (en) * 1969-10-22 1972-05-23 Us Air Force Platelet injector
US4601638A (en) * 1984-12-21 1986-07-22 United Technologies Corporation Airfoil trailing edge cooling arrangement
US4653983A (en) * 1985-12-23 1987-03-31 United Technologies Corporation Cross-flow film cooling passages
US4951463A (en) * 1988-09-16 1990-08-28 General Electric Company Hypersonic scramjet engine fuel injector
US4903480A (en) * 1988-09-16 1990-02-27 General Electric Company Hypersonic scramjet engine fuel injector
GB2227965B (en) * 1988-10-12 1993-02-10 Rolls Royce Plc Apparatus for drilling a shaped hole in a workpiece
US5072582A (en) * 1989-03-23 1991-12-17 General Electric Company Scramjet combustor

Also Published As

Publication number Publication date
FR2675850B1 (fr) 1994-11-10
US5220787A (en) 1993-06-22
IL101578A0 (en) 1992-12-30
DE4214088C2 (de) 1996-11-21
GB9208312D0 (en) 1992-06-03
GB2255628A (en) 1992-11-11
JPH0681713A (ja) 1994-03-22
GB2255628B (en) 1995-01-11
JP2553280B2 (ja) 1996-11-13
FR2675850A1 (fr) 1992-10-30
DE4214088A1 (de) 1992-11-05

Similar Documents

Publication Publication Date Title
US5220787A (en) Scramjet injector
US6679048B1 (en) Apparatus and method for controlling primary fluid flow using secondary fluid flow injection
DE69829385T2 (de) Staustrahltriebwerk mit ejektor
EP1718857B1 (de) Integriertes lufteinlasssystem für mehrfachantrieb-flugzeugtreibwerke
US5085048A (en) Scramjet including integrated inlet and combustor
RU2213240C2 (ru) Шевронное выхлопное сопло
US4311291A (en) Nozzle structure with notches
US3667233A (en) Dual mode supersonic combustion ramjet engine
US5694766A (en) Method and apparatus for controlling the throat area, expansion ratio and thrust vector angle of an aircraft turbine engine exhaust nozzle using regions of locally separated flow
EP1898080A2 (de) Gestuftes Einspritzsystem für eine Brennkammer
US4595144A (en) Injection device, more particularly for direct-injection diesel engines
US20040088967A1 (en) Suppression of part of the noise from a gas turbine engine
JPH09324700A (ja) ラムジェット用燃料噴射装置
US20070251211A1 (en) Exhaust assembly forming a horizontal propulsion gas elbow in an aircraft
US4934632A (en) Aerothermal ultra hypersonic aircraft
JPH10510221A (ja) 極低温粒子ブラストシステム用ノズル
JP6937389B2 (ja) 障害物を有するアイソレータを備えたフライトビークルエアブリージング推進システム
WO2007022315A2 (en) Integrated pulse detonation engine in a lifting surface with supercirculation
US20040244357A1 (en) Divergent chevron nozzle and method
US8701414B2 (en) Injection device for combustion chambers of liquid-fueled rocket engines
WO2004061286A1 (en) Apparatus and method for controlling primary fluid flow using secondary fluid flow injection
JPH05272411A (ja) スクラムジェットエンジン
CN113123898B (zh) 一种基于分隔板后缘射流扰动的超声速流混合装置
US2934896A (en) Variable-area propelling nozzle combined with a thrust spoiler
JP3042206B2 (ja) スクラムジェットエンジン

Legal Events

Date Code Title Description
KB Patent renewed
KB Patent renewed
KB Patent renewed