ES2067171T3 - Dispositivo de ensamblaje mecanico temporal y de separacion rapida de un objeto a expulsar unido a un soporte. - Google Patents

Dispositivo de ensamblaje mecanico temporal y de separacion rapida de un objeto a expulsar unido a un soporte.

Info

Publication number
ES2067171T3
ES2067171T3 ES91401017T ES91401017T ES2067171T3 ES 2067171 T3 ES2067171 T3 ES 2067171T3 ES 91401017 T ES91401017 T ES 91401017T ES 91401017 T ES91401017 T ES 91401017T ES 2067171 T3 ES2067171 T3 ES 2067171T3
Authority
ES
Spain
Prior art keywords
support
expulsion
accommodation
ejected
joined
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
ES91401017T
Other languages
English (en)
Inventor
Jacques Spariat
Jean-Pierre Aubret
Michel Barriere
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 Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2067171T3 publication Critical patent/ES2067171T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/645—Separators
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641—Interstage or payload connectors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/048—Means for imparting spin to the rocket before launching
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F7/00—Launching-apparatus for projecting missiles or projectiles otherwise than from barrels, e.g. using spigots

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Connection Of Plates (AREA)
  • Clamps And Clips (AREA)

Abstract

UN MECANISMO DE SUJECCION TEMPORAL DE UN OBJETO (A) A UN SOPORTE (B), DE SEPARACION Y DE EXPULSION DE ESTE OBJETO, COMPRENDE UN RECEPTACULO DESTINADO A FIJARSE AL SOPORTE EN EL QUE UNA VARILLA DE EXPULSION (2) ESTA MONTADA DESLIZANTE. ESTA VARILLA DE EXPULSION COMPRENDE UNA PARTE POSTERIOR SOMETIDA A UNA PRESION DE EXPULSION Y UN EXTREMO DELANTERO QUE SE APOYA CONTRA UN ASIENTO DE SOPORTE (5A) ESTA DISPUESTO CERCA DEL CENTRO DE GRAVEDAD (G) DEL OBJETO, EN EL FONDO DE UN ALOJAMIENTO ALARGADO (4) EN EL QUE PENETRA LA VARILLA DE EXPULSION (2) HASTA ESTE ASIENTO DE APOYO. EL CUERPO COMPRENDE UNA PARTE TERMINAL ANULAR ACOPLADA A DICHO CUERPO POR UNA ZONA FRANGIBLE DE ENLACE. EN EL OBJETO, ESTAN DISPUESTAS, POR UNA PARTE, UNA ZONA CENTRAL DE CENTRADO DELANTERO (5) SITUADA EN EL FONDO DEL ALOJAMIENTO Y EN LA QUE PENETRA CON COMO MAXIMO UNA ESCASA HOLGURA EL EXTREMO LIBRE DE LA VARILLA DE EXPULSION, Y POR OTRA PARTE UNA ZONA TERMINAL DE CENTRADO TRASERO (6) SITUADA CERCA DE LA EMBOCADURA DEL ALOJAMIENTO Y EN LA QUE PENETRA CON UNA ESCASA HOLGURA UNA PARTE MACHO DE CENTRADO TRASERO (40) SOLIDARIO DEL CUERPO DEL RECEPTACULO.
ES91401017T 1990-04-27 1991-04-17 Dispositivo de ensamblaje mecanico temporal y de separacion rapida de un objeto a expulsar unido a un soporte. Expired - Lifetime ES2067171T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9005450A FR2661465B1 (fr) 1990-04-27 1990-04-27 Dispositif d'assemblage mecanique temporaire et de separation rapide d'un objet a ejecter lie a un support.

Publications (1)

Publication Number Publication Date
ES2067171T3 true ES2067171T3 (es) 1995-03-16

Family

ID=9396209

Family Applications (1)

Application Number Title Priority Date Filing Date
ES91401017T Expired - Lifetime ES2067171T3 (es) 1990-04-27 1991-04-17 Dispositivo de ensamblaje mecanico temporal y de separacion rapida de un objeto a expulsar unido a un soporte.

Country Status (6)

Country Link
US (1) US5115708A (es)
EP (1) EP0454545B1 (es)
CA (1) CA2041046A1 (es)
DE (1) DE69106426T2 (es)
ES (1) ES2067171T3 (es)
FR (1) FR2661465B1 (es)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2678989B1 (fr) * 1991-07-09 1993-11-19 Aerospatiale Ste Nationale Indle Dispositif de fixation mecanique temporaire souple en flexion et a rupture calibree en traction, et un procede pour sa fabrication.
US5402728A (en) * 1992-08-13 1995-04-04 Trw Inc. Low shock separation bolt
FR2705945B1 (fr) * 1993-06-04 1995-08-04 Aerospatiale Dispositif pour éjecter un objet lié, de façon amovible, à une structure.
GB2278909A (en) * 1993-06-09 1994-12-14 Richmond Electronics & Enginee Projection device
FR2707750B1 (fr) * 1993-06-28 1995-09-22 Aerospatiale Dispositif d'éjection, par voie pyrotechnique, d'un objet par rapport à une structure.
FR2712970B1 (fr) * 1993-11-23 1996-01-26 Aerospatiale Dispositif d'éjection, par un gaz sous pression, d'un objet par rapport à une structure.
FR2723912B1 (fr) * 1994-08-30 1997-04-11 Aerospatiale Dispositif de commande d'ecartement multicontact, applicable notamment a l'ejection d'un objet a partir d'un engin spatial.
US6269748B1 (en) * 1998-06-18 2001-08-07 Nea Electronics, Inc. Release mechanism
US6508157B1 (en) * 2002-03-04 2003-01-21 James S. Brown Tool for unblocking heavy machinery
US6758142B1 (en) * 2003-01-28 2004-07-06 Northrop Grumman Corporation Pneumatic stage separation system for two stage launch vehicle
US8117847B2 (en) * 2008-03-07 2012-02-21 Raytheon Company Hybrid missile propulsion system with reconfigurable multinozzle grid
FR3063006A1 (fr) * 2017-02-20 2018-08-24 Pytheas Navigation Systeme d'orientation chirurgical utilisant la geometrie des os pour un positionnement repetable
CN112373732B (zh) * 2020-10-29 2022-07-05 北京航天长征飞行器研究所 一种低冲击小型空间飞行器分离释放机构
CN115675938B (zh) * 2022-11-21 2024-04-26 北京中科宇航技术有限公司 低轨移动堆栈星座卫星解锁分配器

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3104521A (en) * 1961-04-10 1963-09-24 Ling Temco Vought Inc Ballistic-type impulse actuator
US3119302A (en) * 1961-06-05 1964-01-28 Aircraft Armaments Inc Gas sealed explosive propelling arrangement
US3196745A (en) * 1963-06-07 1965-07-27 Martin Marietta Corp Separation and pin puller mechanism
US3262351A (en) * 1964-03-20 1966-07-26 James E Webb Separation nut
US3530759A (en) * 1969-02-20 1970-09-29 Gus Francis Explosively severable element
US3643545A (en) * 1969-11-13 1972-02-22 Us Navy Zero breech grenade-launching system
US3887150A (en) * 1973-02-05 1975-06-03 Mc Donnell Douglas Corp Internal ejector mechanism
US3910154A (en) * 1973-05-02 1975-10-07 Hi Shear Corp Separation nut
US4002120A (en) * 1975-07-31 1977-01-11 The United States Of America As Represented By The Secretary Of The Navy Missile stage coupler
US4064783A (en) * 1977-01-27 1977-12-27 The United States Of America As Represented By The Secretary Of The Navy Pressure-balanced underwater structural release system
US4187759A (en) * 1977-09-16 1980-02-12 The United States Of America As Represented By The Secretary Of The Navy Separation nut system
US4171663A (en) * 1977-11-22 1979-10-23 The United States Of America As Represented By The Secretary Of The Army Tension fracture fitting in missile separation thruster
US4403435A (en) * 1981-04-02 1983-09-13 Brunswick Corporation Release and alignment mechanism for jet-propelled projectiles
US4554905A (en) * 1984-04-05 1985-11-26 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Space probe/satellite ejection apparatus for spacecraft
US4682804A (en) * 1984-04-23 1987-07-28 Trw Inc. Releasable coupling assembly
US4625619A (en) * 1984-07-02 1986-12-02 The United States Of America As Represented By The Secretary Of The Navy Device for separation and launch of a body with linear and rotational velocity
JPS6213861A (ja) * 1985-07-09 1987-01-22 Toyoda Mach Works Ltd ねじ送り装置
FR2616856B1 (fr) * 1987-06-16 1991-12-13 Aerospatiale Mecanisme de commande d'ecartement rapide et controle de deux pieces en contact
FR2637037B1 (fr) * 1988-09-23 1993-07-09 Chorin Christian Dispositif pour transformer un mouvement lineaire en mouvement rotatif avec possibilite de reversibilite, d'efforts et vitesses variables
FR2637252B1 (fr) * 1988-10-05 1990-12-28 Aerospatiale Dispositif de solidarisation/desolidarisation provisoire de deux elements l'un a l'autre, et de separation ulterieure
US4964595A (en) * 1989-03-28 1990-10-23 Scot, Inc. Entrapped gas ejector arrangement for aircraft store racks

Also Published As

Publication number Publication date
EP0454545A1 (fr) 1991-10-30
DE69106426T2 (de) 1995-06-14
EP0454545B1 (fr) 1995-01-04
US5115708A (en) 1992-05-26
CA2041046A1 (en) 1991-10-28
FR2661465B1 (fr) 1992-08-14
FR2661465A1 (fr) 1991-10-31
DE69106426D1 (de) 1995-02-16

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