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
Links
- 238000000926 separation method Methods 0.000 title abstract 2
- 230000004308 accommodation Effects 0.000 abstract 3
- 230000005484 gravity Effects 0.000 abstract 1
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
-
- 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
- B64G1/6457—Springs; Shape memory actuators
-
- 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)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
- Connection Of Plates (AREA)
- Portable Nailing Machines And Staplers (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.
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)
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)
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 |
-
1990
- 1990-04-27 FR FR9005450A patent/FR2661465B1/fr not_active Expired - Fee Related
-
1991
- 1991-04-17 ES ES91401017T patent/ES2067171T3/es not_active Expired - Lifetime
- 1991-04-17 DE DE69106426T patent/DE69106426T2/de not_active Expired - Fee Related
- 1991-04-17 EP EP91401017A patent/EP0454545B1/fr not_active Expired - Lifetime
- 1991-04-23 CA CA002041046A patent/CA2041046A1/en not_active Abandoned
- 1991-04-23 US US07/690,546 patent/US5115708A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE69106426D1 (de) | 1995-02-16 |
FR2661465A1 (fr) | 1991-10-31 |
FR2661465B1 (fr) | 1992-08-14 |
CA2041046A1 (en) | 1991-10-28 |
EP0454545A1 (fr) | 1991-10-30 |
DE69106426T2 (de) | 1995-06-14 |
US5115708A (en) | 1992-05-26 |
EP0454545B1 (fr) | 1995-01-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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