DE69625081T2 - Ausfahrbare raketentriebwerkdüse - Google Patents

Ausfahrbare raketentriebwerkdüse

Info

Publication number
DE69625081T2
DE69625081T2 DE69625081T DE69625081T DE69625081T2 DE 69625081 T2 DE69625081 T2 DE 69625081T2 DE 69625081 T DE69625081 T DE 69625081T DE 69625081 T DE69625081 T DE 69625081T DE 69625081 T2 DE69625081 T2 DE 69625081T2
Authority
DE
Germany
Prior art keywords
extendable
rocket engine
engine nozzle
nozzle
rocket
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
DE69625081T
Other languages
English (en)
Other versions
DE69625081D1 (de
Inventor
Bruno Perrier
Jean-Luc Sans
Alain Henault
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of DE69625081D1 publication Critical patent/DE69625081D1/de
Application granted granted Critical
Publication of DE69625081T2 publication Critical patent/DE69625081T2/de
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
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97—Rocket nozzles
    • F02K9/976—Deployable nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/324—Arrangement of components according to their shape divergent
DE69625081T 1995-12-28 1996-12-27 Ausfahrbare raketentriebwerkdüse Expired - Lifetime DE69625081T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9515634A FR2743110B1 (fr) 1995-12-28 1995-12-28 Divergent deployable de propulseur
PCT/FR1996/002093 WO1997024521A1 (fr) 1995-12-28 1996-12-27 Tuyere divergent deployable de propulseur

Publications (2)

Publication Number Publication Date
DE69625081D1 DE69625081D1 (de) 2003-01-09
DE69625081T2 true DE69625081T2 (de) 2003-10-30

Family

ID=9486067

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69625081T Expired - Lifetime DE69625081T2 (de) 1995-12-28 1996-12-27 Ausfahrbare raketentriebwerkdüse

Country Status (7)

Country Link
US (1) US6205772B1 (de)
EP (1) EP0870105B1 (de)
JP (1) JP4070238B2 (de)
DE (1) DE69625081T2 (de)
FR (1) FR2743110B1 (de)
UA (1) UA37286C2 (de)
WO (1) WO1997024521A1 (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2840030B1 (fr) * 2002-05-21 2005-03-04 Eads Launch Vehicles Moteur a tuyere a noyau central pour lanceur spatial
KR100463056B1 (ko) * 2002-10-08 2004-12-23 현대자동차주식회사 머플러의 가변 테일 파이프 구조
DE10312776B4 (de) * 2003-03-21 2008-10-02 Eads Space Transportation Gmbh Ausfahrbare Schubdüsenglocke für ein Raketentriebwerk
US8627738B2 (en) * 2005-06-29 2014-01-14 Thomas Scott Breidenbach Linear-curvilinear actuating apparatus with rotating joints
US7374230B2 (en) * 2005-12-01 2008-05-20 Thomas Scott Breidenbach Aerodynamic drag reducing apparatus
US7380868B2 (en) * 2005-06-29 2008-06-03 Thomas Scott Breidenbach Aerodynamic drag reducing apparatus
US7845708B2 (en) 2007-06-06 2010-12-07 Adaptive Aerodynamic, Llc Aerodynamic drag reducing apparatus
US7618086B2 (en) 2005-12-01 2009-11-17 Thomas Scott Breidenbach Aerodynamic drag reducing apparatus
US8100461B2 (en) 2007-05-17 2012-01-24 Advanced Transit Dynamics, Inc. Rear-mounted aerodynamic structure for truck cargo bodies
US8360509B2 (en) 2007-05-17 2013-01-29 Advanced Transit Dynamics, Inc. Rear-mounted aerodynamic structure for truck cargo bodies
US7857376B2 (en) 2008-02-21 2010-12-28 Adaptive Aerodynamic, Llc Aerodynamic drag reducing apparatus
US9810085B2 (en) * 2011-08-22 2017-11-07 United Technologies Corporation Flap seal for gas turbine engine movable nozzle flap
US9440689B1 (en) 2011-09-20 2016-09-13 Stemco Lp Aerodynamic structures secured to the underbody of cargo bodies
WO2013043890A1 (en) 2011-09-20 2013-03-28 Advanced Transit Dynamics, Inc. Rear-mounted retractable aerodynamic structure for cargo bodies
MX2014005097A (es) 2011-10-27 2015-03-13 Advanced Transit Dynamics Inc Estructuras aerodinamicas de montaje trasero para carrocerias de carga.
US9145177B2 (en) 2012-07-11 2015-09-29 Advanced Transit Dynamics, Inc. Retractable aerodynamic structures for cargo bodies and methods of controlling positioning of the same
RU2647022C1 (ru) * 2015-12-22 2018-03-13 Акционерное общество "Корпорация "Московский институт теплотехники" (АО "Корпорация "МИТ") Поворотное управляющее сопло с гибким раскладным насадком
US10815936B2 (en) 2016-11-09 2020-10-27 Northrop Grumman Innovation Systems, Inc. Flexible bearing assemblies, rocket motors including such assemblies, and methods of forming flexible bearings

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3526365A (en) * 1968-05-21 1970-09-01 T O Paine Collapsible nozzle extension for rocket engines
US3561679A (en) * 1968-06-25 1971-02-09 Sam E Lager Collapsible nozzle for aircraft rocket motors
US4169555A (en) * 1977-07-25 1979-10-02 United Technologies Corporation Extendible exit cone
US4213566A (en) * 1978-08-25 1980-07-22 Hercules Incorporated Nested cone extendible nozzle system for a rocket motor
US4676436A (en) * 1984-11-02 1987-06-30 Unidynamics Phoenix, Inc. Rocket motor nozzle extension system
FR2622931B1 (fr) * 1987-11-10 1991-01-11 Messerschmitt Boelkow Blohm Mecanisme d'actionnement de tuyere de poussee prolongeable de moteur-fusee
FR2677080B1 (fr) * 1991-05-30 1995-01-06 Europ Propulsion Mecanisme autoverrouillable et reversible de deploiement de divergent de tuyere de moteur-fusee.

Also Published As

Publication number Publication date
FR2743110A1 (fr) 1997-07-04
UA37286C2 (uk) 2001-05-15
EP0870105A1 (de) 1998-10-14
DE69625081D1 (de) 2003-01-09
WO1997024521A1 (fr) 1997-07-10
JP2000502773A (ja) 2000-03-07
US6205772B1 (en) 2001-03-27
JP4070238B2 (ja) 2008-04-02
FR2743110B1 (fr) 1998-03-27
EP0870105B1 (de) 2002-11-27

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