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ES2180908T3 - Sistema de obturacion para un orificio de entrada de aire en la camara de combustion de un estatorreactor. - Google Patents

Sistema de obturacion para un orificio de entrada de aire en la camara de combustion de un estatorreactor.

Info

Publication number
ES2180908T3
ES2180908T3 ES97402549T ES97402549T ES2180908T3 ES 2180908 T3 ES2180908 T3 ES 2180908T3 ES 97402549 T ES97402549 T ES 97402549T ES 97402549 T ES97402549 T ES 97402549T ES 2180908 T3 ES2180908 T3 ES 2180908T3
Authority
ES
Spain
Prior art keywords
statorreactor
combustion chamber
air inlet
inlet hole
shutter system
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
ES97402549T
Other languages
English (en)
Inventor
Michel Hallais
Vincent Protat
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.)
Aerospatiale Matra
Original Assignee
Aerospatiale Matra
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 Aerospatiale Matra filed Critical Aerospatiale Matra
Application granted granted Critical
Publication of ES2180908T3 publication Critical patent/ES2180908T3/es
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
    • 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
    • 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)
  • Toys (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)
  • Nozzles (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

LA PRESENTE INVENCION CONSISTE EN UN SISTEMA DE OBTURACION DE ORIFICIOS DE ENTRADA DE AIRE EN LA CAMARA DE COMBUSTION DE UN ESTATORREACTOR CON PROPULSOR AUXILIAR CONSUMIBLE (14). SEGUN LA INVENCION, EL SISTEMA DE OBTURACION COMPRENDE: - UN SISTEMA ELASTICO (28, 29, 31, 32) CONECTADO CON LA TRAMPILLA DE OBTURACION (20A, 20B); Y - UN ELEMENTO DE RETENCION (33), DESTINADO A MANTENER DICHO SISTEMA ELASTICO EN ESTADO DE TENSION DURANTE LA FASE INICIAL DE FUNCIONAMIENTO EN COHETE, SIENDO SENSIBLE ESTE ELEMENTO DE RETENCION A LOS GASES CALIENTES QUE EMITE EL PROPULSOR AUXILIAR CONSUMIBLE (14) DE TAL MANERA QUE, AL FINAL DE LA COMBUSTION DE ESTE, EL ELEMENTO DE RETENCION (33) LIBERA EL SISTEMA ELASTICO, QUE PASA ESPONTANEAMENTE DEL ESTADO EN TENSION AL ESTADO EN DISTENSION, ARRASTRANDO LA TRAMPILLA DE LA POSICION DE OBTURACION A LA POSICION DE APERTURA.
ES97402549T 1996-10-30 1997-10-28 Sistema de obturacion para un orificio de entrada de aire en la camara de combustion de un estatorreactor. Expired - Lifetime ES2180908T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9613237A FR2755182B1 (fr) 1996-10-30 1996-10-30 Systeme d'obturation pour un orifice d'entree d'air dans la chambre de combustion d'un statoreacteur

Publications (1)

Publication Number Publication Date
ES2180908T3 true ES2180908T3 (es) 2003-02-16

Family

ID=9497171

Family Applications (1)

Application Number Title Priority Date Filing Date
ES97402549T Expired - Lifetime ES2180908T3 (es) 1996-10-30 1997-10-28 Sistema de obturacion para un orificio de entrada de aire en la camara de combustion de un estatorreactor.

Country Status (8)

Country Link
US (1) US6116019A (es)
EP (1) EP0839999B1 (es)
JP (1) JP3996200B2 (es)
CA (1) CA2220892C (es)
DE (1) DE69715770T2 (es)
ES (1) ES2180908T3 (es)
FR (1) FR2755182B1 (es)
WO (1) WO1998019063A1 (es)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2755182B1 (fr) * 1996-10-30 1998-12-31 Aerospatiale Systeme d'obturation pour un orifice d'entree d'air dans la chambre de combustion d'un statoreacteur
FR2813344B1 (fr) * 2000-08-28 2002-11-29 Aerospatiale Matra Missiles Systeme d'obturation pour un orifice d'un conduit, en particulier pour un orifice d'une voie d'introduction d'air dans la chambre de combustion d'un statoreacteur
FR2819556B1 (fr) * 2001-01-12 2003-04-04 Aerospatiale Matra Missiles Systeme d'obturation pour un orifice d'un conduit, en particulier pour un orifice d'une voie d'introduction d'air dans la chambre de combustion d'un statoreacteur
FR2824106B1 (fr) 2001-04-30 2003-08-29 Aerospatiale Matra Missiles Manche a air et engin volant, en particulier un missile, muni d'une telle manche a air
RU2527800C1 (ru) * 2013-05-23 2014-09-10 Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Воздухозаборное устройство с заглушкой воздушно-реактивного двигателя
RU2555069C1 (ru) * 2014-03-20 2015-07-10 Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Пиротолкатель заглушки воздухозаборного устройства воздушно-реактивного устройства
RU171406U1 (ru) * 2016-10-27 2017-05-30 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Заглушка воздухозаборного устройства ракетно-прямоточного двигателя
RU181164U1 (ru) * 2017-07-31 2018-07-05 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Заглушка воздухозаборного устройства ракетно-прямоточного двигателя
RU182771U1 (ru) * 2017-08-14 2018-08-31 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Заглушка входа воздухозаборного устройства ракетно-прямоточного двигателя
RU180227U1 (ru) * 2017-11-02 2018-06-06 Закрытое акционерное общество "Институт телекоммуникаций" Комбинированный трехрежимный реактивный двигатель

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3115008A (en) * 1959-02-03 1963-12-24 Cohen William Integral rocket ramjet missile propulsion system
BE790265A (fr) * 1971-10-20 1973-02-15 Trox Gmbh Geb Clapet de protection contre l'incendie
US4028886A (en) * 1975-10-23 1977-06-14 Mcdonnell Douglas Corporation Passive chamber wall fragmenter
FR2402773A1 (fr) * 1977-09-07 1979-04-06 Europ Propulsion Chambre de combustion de stato-fusee a booster integre
FR2627808A1 (fr) * 1978-05-17 1989-09-01 Onera (Off Nat Aerospatiale) Perfectionnements apportes aux ensembles propulseurs a statoreacteurs et a leurs procedes de mise en oeuvre
DE3002977C2 (de) * 1980-01-29 1982-11-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Deckel aus leicht zerstörbarem Material zum Verschließen der in die Brennkammer von Staustrahl-Raketentriebwerken einmündenden Lufteinlauföffnungen, mit pyrotechnisch funktionierender Schlagvorrichtung zum Zerstören des Deckels
DE3003004C2 (de) * 1980-01-29 1982-06-03 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Deckel aus leicht zerstörbarem Material zum Verschließen der in die Brennkammer von kombinierten Staustrahl-Raketentriebwerken einmündenden Lufteinlauföffnungen, und Schlagvorrichtung zum Zerstören des Deckels
DE3242585C2 (de) * 1982-11-18 1985-01-10 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verschlußeinrichtung für einen in die Brennkammer von Staustrahl-Raketentriebwerken einmündenden Lufteinlaufkanal
FR2661454B1 (fr) * 1985-07-12 1994-02-11 Onera Perfectionnements apportes aux propulseurs de type statoreacteur.
JPH079216B2 (ja) * 1989-07-24 1995-02-01 防衛庁技術研究本部長 ラムロケット
JP2800395B2 (ja) * 1990-10-05 1998-09-21 日産自動車株式会社 ラムロケット
JP2707821B2 (ja) * 1990-10-05 1998-02-04 日産自動車株式会社 ラムロケット
JPH04148051A (ja) * 1990-10-08 1992-05-21 Nissan Motor Co Ltd ラムロケット
JP3044576B2 (ja) * 1991-02-12 2000-05-22 防衛庁技術研究本部長 ラムロケット
FR2755182B1 (fr) * 1996-10-30 1998-12-31 Aerospatiale Systeme d'obturation pour un orifice d'entree d'air dans la chambre de combustion d'un statoreacteur

Also Published As

Publication number Publication date
CA2220892C (fr) 2007-01-16
CA2220892A1 (fr) 1998-04-30
DE69715770T2 (de) 2003-05-08
EP0839999A1 (fr) 1998-05-06
DE69715770D1 (de) 2002-10-31
EP0839999B1 (fr) 2002-09-25
JP3996200B2 (ja) 2007-10-24
JP2000503365A (ja) 2000-03-21
WO1998019063A1 (fr) 1998-05-07
FR2755182A1 (fr) 1998-04-30
FR2755182B1 (fr) 1998-12-31
US6116019A (en) 2000-09-12

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