FR2457983B1 - - Google Patents

Info

Publication number
FR2457983B1
FR2457983B1 FR8011857A FR8011857A FR2457983B1 FR 2457983 B1 FR2457983 B1 FR 2457983B1 FR 8011857 A FR8011857 A FR 8011857A FR 8011857 A FR8011857 A FR 8011857A FR 2457983 B1 FR2457983 B1 FR 2457983B1
Authority
FR
France
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
Application number
FR8011857A
Other languages
French (fr)
Other versions
FR2457983A1 (fr
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2457983A1 publication Critical patent/FR2457983A1/fr
Application granted granted Critical
Publication of FR2457983B1 publication Critical patent/FR2457983B1/fr
Granted 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
  • General Details Of Gearings (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Fuel-Injection Apparatus (AREA)
FR8011857A 1979-06-02 1980-05-28 Statoreacteur a commande du vecteur de poussee Granted FR2457983A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2922576A DE2922576C2 (de) 1979-06-02 1979-06-02 Strahltriebwerk mit Schubvektorsteuerung

Publications (2)

Publication Number Publication Date
FR2457983A1 FR2457983A1 (fr) 1980-12-26
FR2457983B1 true FR2457983B1 (enExample) 1983-02-04

Family

ID=6072378

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8011857A Granted FR2457983A1 (fr) 1979-06-02 1980-05-28 Statoreacteur a commande du vecteur de poussee

Country Status (4)

Country Link
US (1) US4351479A (enExample)
DE (1) DE2922576C2 (enExample)
FR (1) FR2457983A1 (enExample)
GB (1) GB2053820B (enExample)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4754927A (en) * 1986-12-08 1988-07-05 Colt Industries Inc. Control vanes for thrust vector control nozzle
FR2705737B1 (fr) * 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à divergent échancré.
JP3042301B2 (ja) 1994-04-28 2000-05-15 日産自動車株式会社 サイドスラスタ
US6112512A (en) 1997-08-05 2000-09-05 Lockheed Martin Corporation Method and apparatus of pulsed injection for improved nozzle flow control
US6112513A (en) * 1997-08-05 2000-09-05 Lockheed Martin Corporation Method and apparatus of asymmetric injection at the subsonic portion of a nozzle flow
FR2791398B1 (fr) * 1999-03-25 2001-05-18 Agence Spatiale Europeenne Tuyere de moteur fusee comportant un systeme de controle de separation de jet
US6298658B1 (en) 1999-12-01 2001-10-09 Williams International Co., L.L.C. Multi-stable thrust vectoring nozzle
RU2190115C2 (ru) * 2000-05-18 2002-09-27 Общество с ограниченной ответственностью Научно-производственное предприятие "Краев" Двигательная установка
US6758032B2 (en) * 2002-02-07 2004-07-06 Lockheed Martin Corporation System of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans
RU2213878C1 (ru) * 2002-05-23 2003-10-10 Военный инженерно-космический университет им. А.Ф. Можайского Способ регулирования тяги ракетного двигателя
GB0226228D0 (en) * 2002-11-09 2002-12-18 Rolls Royce Plc Suppression of part of the noise from a gas turbine engine
SE527829C2 (sv) * 2004-11-05 2006-06-13 Volvo Aero Corp Utloppsmunstycke till en jetmotor och förfarande för styrning av ett gasflöde från jetmotorn
RU2296875C2 (ru) * 2005-03-05 2007-04-10 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") Способ отклонения вектора тяги воздушно-реактивного двигателя
DE102007057275A1 (de) * 2007-11-28 2009-06-10 Möcker, Jochen Pulsationstriebwerk mit innenliegender Treibstoff-Einspritzung
US20130043352A1 (en) * 2011-08-18 2013-02-21 Patrick R.E. Bahn Throttleable propulsion launch escape systems and devices
CN113482799B (zh) * 2021-08-20 2022-06-14 北京理工大学 一种用于火箭发动机的可控式开槽喷管

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1240747C2 (de) * 1962-02-08 1975-07-10 Societe Bertin & Cie., Paris Strahlschubduese fuer heisse gase mit strahlablenkung durch einfuehren eines hilfsstroemungsmittels
FR82940E (fr) * 1963-01-15 1964-05-08 Bertin & Cie Procédé et dispositif de déviation du jet d'une fusée
US3221498A (en) * 1962-08-06 1965-12-07 Lester T Bankston Secondary fluid injection thrust vectoring methods and apparatus
US3646762A (en) * 1962-09-04 1972-03-07 Moog Inc Secondary injection thrust vector control
FR1407213A (fr) * 1964-06-02 1965-07-30 Bertin & Cie Dispositif d'injection, notamment pour déviateur de jet de tuyère
US3325103A (en) * 1964-08-05 1967-06-13 Aerospace Corp Thrust vector control for reaction engines
US3420060A (en) * 1966-04-22 1969-01-07 Mc Donnell Douglas Corp Pressure induced jet vectoring augmentation apparatus
US3698642A (en) * 1966-11-04 1972-10-17 Thiokol Chemical Corp Thrust vector control system
US3737103A (en) * 1969-08-28 1973-06-05 Trw Inc Digital liquid vector control system
DE2102240C3 (de) * 1971-01-19 1975-04-30 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Fluidische Steuereinrichtung
US3780763A (en) * 1971-06-02 1973-12-25 Us Army Pulse ratio modulation valve
US4063685A (en) * 1976-07-30 1977-12-20 The United States Of America As Represented By The Secretary Of The Army Thrust vector control by circulation control over aerodynamic surfaces in a supersonic nozzle

Also Published As

Publication number Publication date
DE2922576C2 (de) 1982-02-18
GB2053820B (en) 1983-02-23
US4351479A (en) 1982-09-28
FR2457983A1 (fr) 1980-12-26
DE2922576A1 (de) 1981-04-23
GB2053820A (en) 1981-02-11

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Legal Events

Date Code Title Description
ST Notification of lapse