FR2986319B1 - Troncon de pilotage pour munition guidee - Google Patents
Troncon de pilotage pour munition guideeInfo
- Publication number
- FR2986319B1 FR2986319B1 FR1200246A FR1200246A FR2986319B1 FR 2986319 B1 FR2986319 B1 FR 2986319B1 FR 1200246 A FR1200246 A FR 1200246A FR 1200246 A FR1200246 A FR 1200246A FR 2986319 B1 FR2986319 B1 FR 2986319B1
- Authority
- FR
- France
- Prior art keywords
- pilotage
- trunk
- guided munition
- munition
- guided
- 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 - Fee Related
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/60—Steering arrangements
- F42B10/62—Steering by movement of flight surfaces
- F42B10/64—Steering by movement of flight surfaces of fins
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
- F42B10/18—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel using a longitudinally slidable support member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
- F42B10/20—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Lock And Its Accessories (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1200246A FR2986319B1 (fr) | 2012-01-27 | 2012-01-27 | Troncon de pilotage pour munition guidee |
EP13152424.1A EP2620738B1 (fr) | 2012-01-27 | 2013-01-23 | Tronçon de pilotage pour munition guidée |
IL224406A IL224406A (en) | 2012-01-27 | 2013-01-24 | Steering part for guided ammunition |
US13/750,573 US8890043B2 (en) | 2012-01-27 | 2013-01-25 | Steering section for guided munition |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1200246A FR2986319B1 (fr) | 2012-01-27 | 2012-01-27 | Troncon de pilotage pour munition guidee |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2986319A1 FR2986319A1 (fr) | 2013-08-02 |
FR2986319B1 true FR2986319B1 (fr) | 2014-03-14 |
Family
ID=46785463
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1200246A Expired - Fee Related FR2986319B1 (fr) | 2012-01-27 | 2012-01-27 | Troncon de pilotage pour munition guidee |
Country Status (4)
Country | Link |
---|---|
US (1) | US8890043B2 (fr) |
EP (1) | EP2620738B1 (fr) |
FR (1) | FR2986319B1 (fr) |
IL (1) | IL224406A (fr) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3041744B1 (fr) * | 2015-09-29 | 2018-08-17 | Nexter Munitions | Projectile d'artillerie ayant une phase pilotee. |
FR3054030B1 (fr) * | 2016-07-18 | 2018-08-24 | Nexter Munitions | Projectile comprenant un dispositif de deploiement d'une voilure ou ailette |
US10458764B2 (en) * | 2016-10-24 | 2019-10-29 | Rosemount Aerospace Inc. | Canard stowage lock |
RU2655059C1 (ru) * | 2017-06-19 | 2018-05-23 | Акционерное общество "Опытное конструкторское бюро "Новатор" | Механизм раскрытия аэродинамических поверхностей |
EP3543640A3 (fr) * | 2018-03-21 | 2020-01-08 | Diehl Defence GmbH & Co. KG | Projectile à ailettes déployables qui sont maintenues en position repliée par un élément de blocage commun rotatif autour l'axe longitudinal |
US11754378B1 (en) * | 2018-04-30 | 2023-09-12 | The Charles Stark Draper Laboratory, Inc. | Deployable flap for high-G maneuvers |
CN111220032B (zh) * | 2019-11-18 | 2022-05-27 | 中国空空导弹研究院 | 一种小型折叠舵面的四通道联动解锁机构 |
CN111006554B (zh) * | 2019-11-22 | 2022-04-19 | 北京宇航***工程研究所 | 一种兼具连接承载和分离推冲功能的重复使用运载火箭冷气分离*** |
DE102019008539A1 (de) * | 2019-12-10 | 2021-06-10 | Diehl Defence Gmbh & Co. Kg | Flugkörper mit pyrotechnischer Entriegelung |
CN112504031A (zh) * | 2020-11-27 | 2021-03-16 | 北京宇航***工程研究所 | 一种适用于整流罩旋抛的变力线长行程作动装置 |
CN114427808A (zh) * | 2022-01-19 | 2022-05-03 | 湖北三江航天红峰控制有限公司 | 一种折叠式舵机 |
CN117125492B (zh) * | 2023-10-27 | 2024-01-02 | 山西雅美德印刷科技有限公司 | 一种平面印刷用成品输送装置 |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1187193A (fr) * | 1957-11-15 | 1959-09-08 | Hotchkiss Brandt | Empennage déployant perfectionné pour projectile |
US3819132A (en) * | 1973-02-21 | 1974-06-25 | Sarmac Sa | Self propelled projectile with fins |
FR2530332B1 (fr) * | 1982-07-16 | 1987-01-02 | Europ Propulsion | Dispositif d'ouverture de l'empennage d'un projectile |
DE3328520C1 (de) * | 1983-08-06 | 1985-03-07 | Diehl GmbH & Co, 8500 Nürnberg | Schwenkleitwerk fuer Flugkoerper |
SE444612B (sv) * | 1984-12-13 | 1986-04-21 | Ffv Affersverket | Styrverk for utfellning av fenor hos projektil |
FR2635178B1 (fr) * | 1988-08-04 | 1990-10-12 | France Etat Armement | Dispositif d'ouverture d'empennage pour obus |
DE4020897C2 (de) * | 1990-06-30 | 1993-11-11 | Diehl Gmbh & Co | Einrichtung zum Entriegeln und Ausschwenken der Ruderblätter eines Projektiles |
US5668347A (en) * | 1996-09-13 | 1997-09-16 | The United States Of America As Represented By The Secretary Of The Army | Kinetic energy projectile with fin leading edge protection mechanisms |
US5762291A (en) * | 1996-10-28 | 1998-06-09 | The United States Of America As Represented By The Secretary Of The Army | Drag control module for stabilized projectiles |
US6126109A (en) * | 1997-04-11 | 2000-10-03 | Raytheon Company | Unlocking tail fin assembly for guided projectiles |
DE10015514B4 (de) * | 2000-03-30 | 2007-10-04 | Rheinmetall Waffe Munition Gmbh | Flügelstabilisiertes Geschoß |
GB0111171D0 (en) * | 2001-05-08 | 2001-06-27 | Special Cartridge Company Ltd | Projictile |
US6880780B1 (en) * | 2003-03-17 | 2005-04-19 | General Dynamics Ordnance And Tactical Systems, Inc. | Cover ejection and fin deployment system for a gun-launched projectile |
US7851734B1 (en) * | 2007-08-21 | 2010-12-14 | Lockheed Martin Corporation | Acceleration activated fin release mechanism |
US8338769B1 (en) * | 2008-02-07 | 2012-12-25 | Simmonds Precision Products, Inc. | Pyrotechnic fin deployment and retention mechanism |
US8148670B2 (en) * | 2008-08-26 | 2012-04-03 | Woodward Hrt, Inc. | Rotary actuator ball-detent locking mechanism |
FR2955653A1 (fr) * | 2010-01-28 | 2011-07-29 | Nexter Munitions | Dispositif de deploiement simultane de gouvernes d'un projectile |
US8324544B2 (en) * | 2010-06-02 | 2012-12-04 | Woodward Hrt, Inc. | Multi-stage fin deployment assembly |
US8624172B2 (en) * | 2010-10-13 | 2014-01-07 | Woodward Hrt, Inc. | Shift lock assembly |
-
2012
- 2012-01-27 FR FR1200246A patent/FR2986319B1/fr not_active Expired - Fee Related
-
2013
- 2013-01-23 EP EP13152424.1A patent/EP2620738B1/fr not_active Not-in-force
- 2013-01-24 IL IL224406A patent/IL224406A/en not_active IP Right Cessation
- 2013-01-25 US US13/750,573 patent/US8890043B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US20130193265A1 (en) | 2013-08-01 |
EP2620738A1 (fr) | 2013-07-31 |
US8890043B2 (en) | 2014-11-18 |
FR2986319A1 (fr) | 2013-08-02 |
IL224406A (en) | 2016-11-30 |
EP2620738B1 (fr) | 2014-05-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 4 |
|
ST | Notification of lapse |
Effective date: 20160930 |