ES2100040T3 - Mecanismo de retencion por inercia para misiles montados sobre railes. - Google Patents
Mecanismo de retencion por inercia para misiles montados sobre railes.Info
- Publication number
- ES2100040T3 ES2100040T3 ES94903279T ES94903279T ES2100040T3 ES 2100040 T3 ES2100040 T3 ES 2100040T3 ES 94903279 T ES94903279 T ES 94903279T ES 94903279 T ES94903279 T ES 94903279T ES 2100040 T3 ES2100040 T3 ES 2100040T3
- Authority
- ES
- Spain
- Prior art keywords
- missile
- retaining
- rail
- inertia
- response
- 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
Classifications
-
- 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
- F41F3/052—Means for securing the rocket in the launching apparatus
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Warehouses Or Storage Devices (AREA)
- Intermediate Stations On Conveyors (AREA)
- Chain Conveyers (AREA)
- Chutes (AREA)
- Vibration Dampers (AREA)
Abstract
UN MECANISMO DE RETENCION INERCIAL QUE RETIENE UN MISIL MONTADO SOBRE UN RAIL (10), EVITANDO EL MOVIMIENTO DE AVANCE A LO LARGO DE UN RAIL DE LANZAMIENTO DE MISIL (12), EN RESPUESTA A UNA FUERZA DE DECELERACION. EL MECANISMO DE RETENCION COMPRENDE UNA MASA (36), CUYO MOVIMIENTO ES FRENADO POR UNA FUERZA DE MUELLE (44). CUANDO LA MASA SUPERA LA FUERZA DEL MUELLE DEBIDO A UNA FUERZA DE DECELERACION POR ENCIMA DE UNA MAGNITUD LIMITE, UN MECANISMO DE CIERRE (53) ES ACTIVADO A UNA POSICION DE RETENCION DEL MISIL, RETENIENDO ASI EL MISIL Y EVITANDO UN MOVIMIENTO DE AVANCE. EL MECANISMO DE RETENCION SE CIERRA (62,65) EN LA POSICION DE RETENCION DEL MISIL PARA EVITAR LA LIBERACION DE UN MISIL EN RESPUESTA A FUERZAS DE DECELERACION MULTIPLES A LAS QUE SE SOMETE EL MISIL Y EL RAIL DE LANZAMIENTO. ADICIONALMENTE, PUEDE SER PROPORCIONADO UN RETEN (75) QUE EVITA LA ACTUACION DEL MECANISMO DE RETENCION A LA POSICION DE RETENCION DEL MISIL, A MENOS QUE EL MISIL ESTE ALMACENADO EN UN COMPARTIMENTO DE ALMACENAMIENTO.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/988,612 US5291820A (en) | 1992-12-10 | 1992-12-10 | Inertial restraint mechanism for rail-mounted missiles |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2100040T3 true ES2100040T3 (es) | 1997-06-01 |
Family
ID=25534311
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES94903279T Expired - Lifetime ES2100040T3 (es) | 1992-12-10 | 1993-11-19 | Mecanismo de retencion por inercia para misiles montados sobre railes. |
Country Status (10)
Country | Link |
---|---|
US (1) | US5291820A (es) |
EP (1) | EP0673497B1 (es) |
JP (1) | JPH08504502A (es) |
KR (1) | KR950704667A (es) |
AU (1) | AU670169B2 (es) |
CA (1) | CA2147506A1 (es) |
DE (1) | DE69308889T2 (es) |
ES (1) | ES2100040T3 (es) |
IL (1) | IL107925A (es) |
WO (1) | WO1994014022A1 (es) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE9210369U1 (de) * | 1992-08-03 | 1992-10-29 | Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen | Verriegelungsbaugruppe bei einem Startgerät für Flugkörper |
US5463927A (en) * | 1994-08-03 | 1995-11-07 | Loral Aerospace Corp. | Load assist apparatus for missiles |
DE19530563A1 (de) * | 1995-08-19 | 1997-02-20 | Bodenseewerk Geraetetech | Einrichtung zur Aufnahme und Halterung von Flugkörpern in einem Startgerät |
DE19648609A1 (de) * | 1996-11-14 | 1998-05-20 | Bodenseewerk Geraetetech | Verriegelungs-Baugruppe bei einem Startgerät für Flugkörper |
KR100753488B1 (ko) * | 2006-06-09 | 2007-08-31 | 국방과학연구소 | 미사일 발사가이드 장치 |
US8256339B1 (en) * | 2006-12-29 | 2012-09-04 | Lockheed Martin Corporation | Missile launch system and apparatus therefor |
US7506570B1 (en) | 2007-12-10 | 2009-03-24 | The United States Of America As Represented By The Secretary Of The Navy | Mechanism to hold and release |
US8091460B2 (en) * | 2010-04-29 | 2012-01-10 | The United States Of America As Represented By The Secretary Of The Army | Missile secure-release mechanism having wheel lock detent |
DE102011008395A1 (de) * | 2011-01-12 | 2012-07-12 | Howaldtswerke - Deutsche Werft Aktiengesellschaft | Waffenkupplung zum Festlegen einer Waffe in einer Waffen-Transport- und Staueinrichtung |
US8813629B1 (en) * | 2012-06-12 | 2014-08-26 | The United States Of America As Represented By The Secretary Of The Army | Positional lock for carrier assembly of breech-loaded weapon |
US9618293B1 (en) * | 2013-09-26 | 2017-04-11 | The United States Of America As Represented By The Secretary Of The Army | Munitions storage container with disabling device for single-use weapon stored therein |
CN107966073A (zh) * | 2017-12-11 | 2018-04-27 | 中国航天空气动力技术研究院 | 一种快速释放装置 |
CN112432555B (zh) * | 2020-11-11 | 2023-10-13 | 河南北方红阳机电有限公司 | 一种模拟机载弹发射用地面投放装置 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3228297A (en) * | 1963-03-26 | 1966-01-11 | Robert L Kossan | Adapter rail restraining mechanism |
US3166981A (en) * | 1963-09-04 | 1965-01-26 | Robert M Harris | Forward motion latch and lock |
US3983785A (en) * | 1974-06-17 | 1976-10-05 | General Dynamics Corporation | Missile launcher arming device |
US4012988A (en) * | 1976-06-07 | 1977-03-22 | The United States Of America As Represented By The Secretary Of The Army | Mechanical fly-away latching mechanism |
DE3301567A1 (de) * | 1983-01-19 | 1984-08-02 | Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen | Verriegelungsvorrichtung fuer luft-luft-lenkflugkoerper |
US4660456A (en) * | 1983-10-03 | 1987-04-28 | Frazer-Nash Limited | Airborne missile launcher of modular construction |
US5094140A (en) * | 1991-03-11 | 1992-03-10 | Techteam, Inc. | Missile launcher assembly |
-
1992
- 1992-12-10 US US07/988,612 patent/US5291820A/en not_active Expired - Lifetime
-
1993
- 1993-11-19 ES ES94903279T patent/ES2100040T3/es not_active Expired - Lifetime
- 1993-11-19 EP EP94903279A patent/EP0673497B1/en not_active Expired - Lifetime
- 1993-11-19 DE DE69308889T patent/DE69308889T2/de not_active Expired - Fee Related
- 1993-11-19 WO PCT/US1993/011252 patent/WO1994014022A1/en active IP Right Grant
- 1993-11-19 AU AU57279/94A patent/AU670169B2/en not_active Ceased
- 1993-11-19 KR KR1019950702343A patent/KR950704667A/ko not_active Application Discontinuation
- 1993-11-19 JP JP6514185A patent/JPH08504502A/ja active Pending
- 1993-11-19 CA CA002147506A patent/CA2147506A1/en not_active Abandoned
- 1993-12-07 IL IL10792593A patent/IL107925A/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
IL107925A0 (en) | 1994-07-31 |
EP0673497A1 (en) | 1995-09-27 |
JPH08504502A (ja) | 1996-05-14 |
WO1994014022A1 (en) | 1994-06-23 |
CA2147506A1 (en) | 1994-06-23 |
DE69308889D1 (de) | 1997-04-17 |
US5291820A (en) | 1994-03-08 |
AU670169B2 (en) | 1996-07-04 |
AU5727994A (en) | 1994-07-04 |
DE69308889T2 (de) | 1997-10-16 |
KR950704667A (ko) | 1995-11-20 |
EP0673497B1 (en) | 1997-03-12 |
IL107925A (en) | 1999-03-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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