FR2457390B1 - - Google Patents

Info

Publication number
FR2457390B1
FR2457390B1 FR7913208A FR7913208A FR2457390B1 FR 2457390 B1 FR2457390 B1 FR 2457390B1 FR 7913208 A FR7913208 A FR 7913208A FR 7913208 A FR7913208 A FR 7913208A FR 2457390 B1 FR2457390 B1 FR 2457390B1
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
FR7913208A
Other versions
FR2457390A1 (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.)
Societe Europeenne de Propulsion SEP SA
Original Assignee
Societe Europeenne de Propulsion SEP SA
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 Europeenne de Propulsion SEP SA filed Critical Societe Europeenne de Propulsion SEP SA
Priority to FR7913208A priority Critical patent/FR2457390A1/fr
Priority to DE19803018948 priority patent/DE3018948A1/de
Priority to US06/150,912 priority patent/US4349155A/en
Priority to IT48744/80A priority patent/IT1127592B/it
Priority to JP6795480A priority patent/JPS5627052A/ja
Publication of FR2457390A1 publication Critical patent/FR2457390A1/fr
Application granted granted Critical
Publication of FR2457390B1 publication Critical patent/FR2457390B1/fr
Granted legal-status Critical Current

Links

Classifications

    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D3/00—Hinges with pins
    • E05D3/06—Hinges with pins with two or more pins
    • E05D3/12—Hinges with pins with two or more pins with two parallel pins and one arm
    • E05D3/122—Gear hinges
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections
    • 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
FR7913208A 1979-05-23 1979-05-23 Divergent deployable de tuyere pour propulseur fusee Granted FR2457390A1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR7913208A FR2457390A1 (fr) 1979-05-23 1979-05-23 Divergent deployable de tuyere pour propulseur fusee
DE19803018948 DE3018948A1 (de) 1979-05-23 1980-05-17 Auffaltbarer duesendiffusor fuer einen raketenmotor
US06/150,912 US4349155A (en) 1979-05-23 1980-05-19 Unfoldable divergent nozzle for a rocket engine
IT48744/80A IT1127592B (it) 1979-05-23 1980-05-21 Diffusore estendibile di ugello per propulsione a razzo
JP6795480A JPS5627052A (en) 1979-05-23 1980-05-23 Foldable divergent nozzle for rocket engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7913208A FR2457390A1 (fr) 1979-05-23 1979-05-23 Divergent deployable de tuyere pour propulseur fusee

Publications (2)

Publication Number Publication Date
FR2457390A1 FR2457390A1 (fr) 1980-12-19
FR2457390B1 true FR2457390B1 (fr) 1983-04-08

Family

ID=9225820

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7913208A Granted FR2457390A1 (fr) 1979-05-23 1979-05-23 Divergent deployable de tuyere pour propulseur fusee

Country Status (5)

Country Link
US (1) US4349155A (fr)
JP (1) JPS5627052A (fr)
DE (1) DE3018948A1 (fr)
FR (1) FR2457390A1 (fr)
IT (1) IT1127592B (fr)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4676436A (en) * 1984-11-02 1987-06-30 Unidynamics Phoenix, Inc. Rocket motor nozzle extension system
US4872612A (en) * 1985-08-05 1989-10-10 Morton Thiokol, Inc. Rocket motor extendible nozzle exit cone
US4787559A (en) * 1985-08-05 1988-11-29 Morton Thiokol, Inc. Rocket motor extendible nozzle exit cone
US4754926A (en) * 1985-08-21 1988-07-05 Morton Thiokol, Inc. Rocket motor extendible nozzle exit cone
US4903918A (en) * 1987-05-28 1990-02-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Raked circular-cone aerobraking orbital transfer vehicle
FR2618488B1 (fr) * 1987-07-20 1989-12-15 Europ Propulsion Divergent a rupture de galbe pour tuyere de moteur-fusee
DE8713225U1 (fr) * 1987-10-01 1987-12-03 Buendoplast Bopla Gehaeuse Systeme Gmbh, 4980 Buende, De
FR2658266B1 (fr) * 1990-02-09 1992-06-12 Aerospatiale Dispositif de protection thermique flexible et permeable a la pression.
US5103639A (en) * 1990-02-26 1992-04-14 General Electric Company Exhaust nozzle having variable contour exhaust flap
FR2705738B1 (fr) * 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à diffuseur éjectable.
FR2705737B1 (fr) * 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à divergent échancré.
FR2705739B1 (fr) * 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à section de sortie sélectivement réduite.
US5730392A (en) * 1995-09-22 1998-03-24 Aeronautical Concept Of Exhaust, Ltd. Adjustable fairing for thrust reversers
FR2754566B1 (fr) 1996-10-11 1999-02-05 Europ Propulsion Tuyere de moteur-fusee a inserts ejectables
US6938408B2 (en) * 2001-04-26 2005-09-06 Propulsion Vectoring, L.P. Thrust vectoring and variable exhaust area for jet engine nozzle
FR2840030B1 (fr) * 2002-05-21 2005-03-04 Eads Launch Vehicles Moteur a tuyere a noyau central pour lanceur spatial
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
US8360509B2 (en) 2007-05-17 2013-01-29 Advanced Transit Dynamics, Inc. Rear-mounted aerodynamic structure for truck cargo bodies
US8100461B2 (en) 2007-05-17 2012-01-24 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
FR2944063B1 (fr) * 2009-04-02 2014-04-25 Snecma Divergent deployable de propulseur
CA2789438A1 (fr) * 2010-02-15 2011-11-17 General Electric Company Glissiere a articulation
RU2455517C1 (ru) * 2011-03-02 2012-07-10 Открытое акционерное общество Научно-производственное объединение "Искра" Сопло переменной степени расширения
FR2975730B1 (fr) * 2011-05-23 2013-06-21 Snecma Systeme de reduction de la dynamique du segment mobile d'une tuyere deployable pour moteur de fusee
US9440689B1 (en) 2011-09-20 2016-09-13 Stemco Lp Aerodynamic structures secured to the underbody of cargo bodies
WO2013043890A1 (fr) 2011-09-20 2013-03-28 Advanced Transit Dynamics, Inc. Structure aérodynamique rétractable à montage arrière pour corps de chargement
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
RU2513064C1 (ru) * 2012-11-27 2014-04-20 Открытое акционерное общество Научно-производственное объединение "Искра" Сопло переменной степени расширения
US10094646B2 (en) * 2015-04-13 2018-10-09 The Boeing Company Spring-assisted deployment of a pivotable rocket motor
CN110310582A (zh) * 2019-08-01 2019-10-08 安德鑫 一种可折叠的led显示屏

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1252094B (fr) * 1967-10-12
US3402422A (en) * 1965-12-10 1968-09-24 Austin R. Baer Hinge
US3526365A (en) * 1968-05-21 1970-09-01 T O Paine Collapsible nozzle extension for rocket engines
US3711027A (en) * 1971-03-17 1973-01-16 Textron Inc Extendible nozzle for rocket engines
US3784109A (en) * 1972-05-22 1974-01-08 Textron Inc Deployable nozzle extension for rocket engines
US3951342A (en) * 1973-02-15 1976-04-20 Aerojet-General Corporation Extendible nozzle for a rocket motor or the like
GB1542244A (en) * 1974-10-17 1979-03-14 Marler Haley Exposystems Ltd Panel systems
US3957206A (en) * 1975-01-27 1976-05-18 The United States Of America As Represented By The Secretary Of The Air Force Extendable rocket motor exhaust nozzle
ZA76614B (en) * 1975-02-21 1977-09-28 Worrallo A C Hinge structures

Also Published As

Publication number Publication date
DE3018948C2 (fr) 1991-02-21
FR2457390A1 (fr) 1980-12-19
IT1127592B (it) 1986-05-21
JPS5627052A (en) 1981-03-16
US4349155A (en) 1982-09-14
IT8048744A0 (it) 1980-05-21
DE3018948A1 (de) 1980-11-27

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Legal Events

Date Code Title Description
DL Decision of the director general to leave to make available licences of right
TP Transmission of property