PL2354755T3 - Urządzenie do synchronicznego rozkładania powierzchni sterowych pocisków - Google Patents
Urządzenie do synchronicznego rozkładania powierzchni sterowych pociskówInfo
- Publication number
- PL2354755T3 PL2354755T3 PL11290029T PL11290029T PL2354755T3 PL 2354755 T3 PL2354755 T3 PL 2354755T3 PL 11290029 T PL11290029 T PL 11290029T PL 11290029 T PL11290029 T PL 11290029T PL 2354755 T3 PL2354755 T3 PL 2354755T3
- Authority
- PL
- Poland
- Prior art keywords
- projectile
- control surfaces
- simultaneously deploying
- deploying control
- deploying
- Prior art date
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
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
- Aerials With Secondary Devices (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1000344A FR2955653A1 (fr) | 2010-01-28 | 2010-01-28 | Dispositif de deploiement simultane de gouvernes d'un projectile |
EP11290029A EP2354755B1 (fr) | 2010-01-28 | 2011-01-19 | Dispositif de déploiement simultané de gouvernes d'un projectile |
Publications (1)
Publication Number | Publication Date |
---|---|
PL2354755T3 true PL2354755T3 (pl) | 2013-03-29 |
Family
ID=42563191
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL11290029T PL2354755T3 (pl) | 2010-01-28 | 2011-01-19 | Urządzenie do synchronicznego rozkładania powierzchni sterowych pocisków |
Country Status (5)
Country | Link |
---|---|
US (1) | US8592737B2 (pl) |
EP (1) | EP2354755B1 (pl) |
ES (1) | ES2398733T3 (pl) |
FR (1) | FR2955653A1 (pl) |
PL (1) | PL2354755T3 (pl) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2709655T3 (es) * | 2011-05-13 | 2019-04-17 | Leigh Aerosystems Corp | Sistema de guiado de proyectil terrestre |
FR2986319B1 (fr) * | 2012-01-27 | 2014-03-14 | Tda Armements Sas | Troncon de pilotage pour munition guidee |
FR2995074A1 (fr) | 2012-08-31 | 2014-03-07 | Nexter Munitions | Projectile a gouvernes orientables et procede de commande des gouvernes d'un tel projectile |
US9429402B2 (en) | 2013-04-24 | 2016-08-30 | Simmonds Precision Products, Inc. | Multi-stage drive mechanisms |
US20160187111A1 (en) * | 2014-08-10 | 2016-06-30 | Jahangir S Rastegar | Methods and Devices For Guidance and Control of High-Spin Stabilized Rounds |
US9702673B1 (en) * | 2014-09-24 | 2017-07-11 | The United States Of America As Represented By The Secretary Of The Army | Projectile tail boom with self-locking fin |
WO2017035126A1 (en) | 2015-08-24 | 2017-03-02 | Leigh Aerosystems Corporation | Ground-projectile guidance system |
FR3041744B1 (fr) * | 2015-09-29 | 2018-08-17 | Nexter Munitions | Projectile d'artillerie ayant une phase pilotee. |
US10280786B2 (en) | 2015-10-08 | 2019-05-07 | Leigh Aerosystems Corporation | Ground-projectile system |
US11150062B1 (en) * | 2016-06-23 | 2021-10-19 | Orbital Research Inc. | Control actuation system, devices and methods for missiles, munitions and projectiles |
FR3054030B1 (fr) * | 2016-07-18 | 2018-08-24 | Nexter Munitions | Projectile comprenant un dispositif de deploiement d'une voilure ou ailette |
US10308347B2 (en) * | 2016-10-26 | 2019-06-04 | Simmonds Precision Products, Inc. | Wing tip aileron actuation system |
US10641590B2 (en) | 2016-10-26 | 2020-05-05 | Simmonds Precision Products, Inc. | Wing deployment and lock mechanism |
US11040772B2 (en) * | 2017-09-11 | 2021-06-22 | Defendtex Pty Ltd | Unmanned aerial vehicle |
EP3543640A3 (de) * | 2018-03-21 | 2020-01-08 | Diehl Defence GmbH & Co. KG | Geschoss mit ausschwenkbaren flügeln und einem gemeinsamen, um die längsachse verdrehbaren arretierbauteil zum lösbaren arretieren der flügel in der eingeschwenkten position |
CN113091524B (zh) * | 2021-03-18 | 2022-08-30 | 中北大学 | 可重复展开的一维弹道阻力片连续修正机构及方法 |
CN114370790B (zh) * | 2021-12-22 | 2024-02-06 | 山西中辐核仪器有限责任公司 | 一种弹道二维修正机构 |
US20230400285A1 (en) * | 2022-06-14 | 2023-12-14 | Raytheon Company | Passively jettisoned control surface restraint and cover for tactical flight vehicles |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB759679A (en) * | 1949-04-29 | 1956-10-24 | Vickers Armstrongs Aircraft | Improvements in guided missiles |
FR1328459A (fr) * | 1962-04-18 | 1963-05-31 | Soc Tech De Rech Ind | Roquette à propulseur largable |
DE1533909B2 (de) | 1967-06-28 | 1975-04-10 | Demag Ag, 4100 Duisburg | Metallurgisches Gefäß, insbesondere kippbarer und/oder umlaufender Stahlwerkskonverter |
DE3328520C1 (de) * | 1983-08-06 | 1985-03-07 | Diehl GmbH & Co, 8500 Nürnberg | Schwenkleitwerk fuer Flugkoerper |
DE3838735C2 (de) * | 1988-11-15 | 1997-12-18 | Diehl Gmbh & Co | Klapp-Flügel, insbes. für ein Geschoss |
US6224013B1 (en) * | 1998-08-27 | 2001-05-01 | Lockheed Martin Corporation | Tail fin deployment device |
SE519764C2 (sv) * | 2000-08-31 | 2003-04-08 | Bofors Defence Ab | Canardfenaggregat |
GB2367598A (en) | 2000-10-04 | 2002-04-10 | Combined Engineering Concepts | A drive transmission for a stern or outboard drive of a watercraft |
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 |
FR2864612B1 (fr) * | 2003-12-24 | 2007-11-23 | Giat Ind Sa | Dispositif de deploiement des ailettes d'un projectile |
FR2864613B1 (fr) | 2003-12-31 | 2006-03-17 | Giat Ind Sa | Dispositif de deploiement et d'entrainement de gouvernes d'un projectile |
FR2891618B1 (fr) * | 2005-10-05 | 2010-06-11 | Giat Ind Sa | Dispositif d'entrainement de gouvernes de projectile. |
US7851734B1 (en) * | 2007-08-21 | 2010-12-14 | Lockheed Martin Corporation | Acceleration activated fin release mechanism |
-
2010
- 2010-01-28 FR FR1000344A patent/FR2955653A1/fr not_active Withdrawn
-
2011
- 2011-01-18 US US13/008,454 patent/US8592737B2/en active Active
- 2011-01-19 PL PL11290029T patent/PL2354755T3/pl unknown
- 2011-01-19 EP EP11290029A patent/EP2354755B1/fr active Active
- 2011-01-19 ES ES11290029T patent/ES2398733T3/es active Active
Also Published As
Publication number | Publication date |
---|---|
ES2398733T3 (es) | 2013-03-21 |
US8592737B2 (en) | 2013-11-26 |
EP2354755B1 (fr) | 2012-11-07 |
FR2955653A1 (fr) | 2011-07-29 |
EP2354755A1 (fr) | 2011-08-10 |
US20110180655A1 (en) | 2011-07-28 |
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