DE2922576C2 - Strahltriebwerk mit Schubvektorsteuerung - Google Patents

Strahltriebwerk mit Schubvektorsteuerung

Info

Publication number
DE2922576C2
DE2922576C2 DE2922576A DE2922576A DE2922576C2 DE 2922576 C2 DE2922576 C2 DE 2922576C2 DE 2922576 A DE2922576 A DE 2922576A DE 2922576 A DE2922576 A DE 2922576A DE 2922576 C2 DE2922576 C2 DE 2922576C2
Authority
DE
Germany
Prior art keywords
thrust
control
jet
nozzle
pressure
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
Application number
DE2922576A
Other languages
German (de)
English (en)
Other versions
DE2922576A1 (de
Inventor
Walter 8021 Taufkirchen Kranz
Heinz 8012 Ottobrunn Tillmann
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
Priority to DE2922576A priority Critical patent/DE2922576C2/de
Priority to GB8017300A priority patent/GB2053820B/en
Priority to FR8011857A priority patent/FR2457983A1/fr
Priority to US06/154,428 priority patent/US4351479A/en
Publication of DE2922576A1 publication Critical patent/DE2922576A1/de
Application granted granted Critical
Publication of DE2922576C2 publication Critical patent/DE2922576C2/de
Expired 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)
DE2922576A 1979-06-02 1979-06-02 Strahltriebwerk mit Schubvektorsteuerung Expired DE2922576C2 (de)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE2922576A DE2922576C2 (de) 1979-06-02 1979-06-02 Strahltriebwerk mit Schubvektorsteuerung
GB8017300A GB2053820B (en) 1979-06-02 1980-05-27 Deflecting propulsion jets
FR8011857A FR2457983A1 (fr) 1979-06-02 1980-05-28 Statoreacteur a commande du vecteur de poussee
US06/154,428 US4351479A (en) 1979-06-02 1980-05-29 Jet engine with a thrust vector control

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
DE2922576A1 DE2922576A1 (de) 1981-04-23
DE2922576C2 true DE2922576C2 (de) 1982-02-18

Family

ID=6072378

Family Applications (1)

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

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
GB2053820B (en) 1983-02-23
FR2457983B1 (enExample) 1983-02-04
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
OP8 Request for examination as to paragraph 44 patent law
D2 Grant after examination
8320 Willingness to grant licences declared (paragraph 23)
8339 Ceased/non-payment of the annual fee