DE602006015582D1 - Antreibvorrichtung für die Ruder eines Geschosses - Google Patents

Antreibvorrichtung für die Ruder eines Geschosses

Info

Publication number
DE602006015582D1
DE602006015582D1 DE602006015582T DE602006015582T DE602006015582D1 DE 602006015582 D1 DE602006015582 D1 DE 602006015582D1 DE 602006015582 T DE602006015582 T DE 602006015582T DE 602006015582 T DE602006015582 T DE 602006015582T DE 602006015582 D1 DE602006015582 D1 DE 602006015582D1
Authority
DE
Germany
Prior art keywords
projectile
oars
rotation
driving device
motors
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.)
Active
Application number
DE602006015582T
Other languages
English (en)
Inventor
Simon Huguenin
Richard Roy
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.)
Nexter Munitions SA
Original Assignee
Nexter Munitions SA
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 Nexter Munitions SA filed Critical Nexter Munitions SA
Publication of DE602006015582D1 publication Critical patent/DE602006015582D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F42B10/60—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)
  • Stroboscope Apparatuses (AREA)
  • Bakery Products And Manufacturing Methods Therefor (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Catching Or Destruction (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Control Of Electric Motors In General (AREA)
  • Control Of Multiple Motors (AREA)
  • Elimination Of Static Electricity (AREA)
DE602006015582T 2005-10-05 2006-09-27 Antreibvorrichtung für die Ruder eines Geschosses Active DE602006015582D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0510164A FR2891618B1 (fr) 2005-10-05 2005-10-05 Dispositif d'entrainement de gouvernes de projectile.

Publications (1)

Publication Number Publication Date
DE602006015582D1 true DE602006015582D1 (de) 2010-09-02

Family

ID=36551894

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006015582T Active DE602006015582D1 (de) 2005-10-05 2006-09-27 Antreibvorrichtung für die Ruder eines Geschosses

Country Status (7)

Country Link
US (1) US7923671B1 (de)
EP (1) EP1772698B1 (de)
AT (1) ATE475060T1 (de)
DE (1) DE602006015582D1 (de)
ES (1) ES2349303T3 (de)
FR (1) FR2891618B1 (de)
IL (1) IL178325A (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8026465B1 (en) * 2009-05-20 2011-09-27 The United States Of America As Represented By The Secretary Of The Navy Guided fuse with variable incidence panels
FR2949848B1 (fr) 2009-09-10 2012-09-28 Nexter Munitions Dispositif d'ouverture et verrouillage d'une ailette canard.
FR2955653A1 (fr) * 2010-01-28 2011-07-29 Nexter Munitions Dispositif de deploiement simultane de gouvernes d'un projectile
IL207800B (en) * 2010-08-25 2018-12-31 Bae Systems Rokar Int Ltd Control apparatus for guiding a cannon shell in flight and method of using same
US8624172B2 (en) * 2010-10-13 2014-01-07 Woodward Hrt, Inc. Shift lock assembly
TR201901397T4 (tr) * 2011-05-13 2019-02-21 Leigh Aerosystems Corp Karadan fırlatılan roket güdüm sistemi.
FR2995074A1 (fr) * 2012-08-31 2014-03-07 Nexter Munitions Projectile a gouvernes orientables et procede de commande des gouvernes d'un tel projectile
US8921749B1 (en) * 2013-07-10 2014-12-30 The United States Of America As Represented By The Secretary Of The Navy Perpendicular drive mechanism for a missile control actuation system
US20160187111A1 (en) * 2014-08-10 2016-06-30 Jahangir S Rastegar Methods and Devices For Guidance and Control of High-Spin Stabilized Rounds
DE102015005135A1 (de) * 2015-04-22 2016-10-27 Diehl Bgt Defence Gmbh & Co. Kg Flugkörperrudersystem
EP3341677A4 (de) 2015-08-24 2019-04-24 Leigh Aerosystems Corporation Bodenprojektil-führungssystem
WO2017062563A1 (en) 2015-10-08 2017-04-13 Leigh Aerosystems Corporation Ground-projectile system
KR101903254B1 (ko) * 2016-12-28 2018-10-01 주식회사 한화 정밀유도키트용 롤 및 피치카나드 구동장치
FR3078152B1 (fr) * 2018-02-22 2021-11-05 Nexter Munitions Projectile a gouvernes orientables
FR3080912B1 (fr) 2018-05-02 2020-04-03 Nexter Munitions Projectile propulse par statoreacteur
US11650033B2 (en) * 2020-12-04 2023-05-16 Bae Systems Information And Electronic Systems Integration Inc. Control plate-based control actuation system
US11892275B2 (en) * 2022-05-25 2024-02-06 Raytheon Company Drive mechanism for control surface actuation

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2150092B (en) * 1983-11-25 1987-07-22 British Aerospace Deployment and actuation mechanisms
FR2657703B1 (fr) * 1990-01-26 1992-04-10 Thomson Brandt Armements Dispositif pour la commande d'attitude en roulis d'un projectile stabilise par empennage.
US5505408A (en) * 1993-10-19 1996-04-09 Versatron Corporation Differential yoke-aerofin thrust vector control system
IL115749A (en) * 1994-10-27 2000-02-29 Thomson Csf Missile launching and orientating system
US5806791A (en) * 1995-05-26 1998-09-15 Raytheon Company Missile jet vane control system and method
US6073880A (en) * 1998-05-18 2000-06-13 Versatron, Inc. Integrated missile fin deployment system
US6186443B1 (en) * 1998-06-25 2001-02-13 International Dynamics Corporation Airborne vehicle having deployable wing and control surface
US6247666B1 (en) * 1998-07-06 2001-06-19 Lockheed Martin Corporation Method and apparatus for non-propulsive fin control in an air or sea vehicle using planar actuation
FR2792400B1 (fr) * 1999-04-16 2002-05-03 Giat Ind Sa Dispositif de freinage en translation d'un projectile sur trajectoire
SE519764C2 (sv) * 2000-08-31 2003-04-08 Bofors Defence Ab Canardfenaggregat
GB2374055B (en) * 2000-10-07 2004-08-04 Bayern Chemie Gmbh Flugchemie A rudder blade guidance arrangement for missiles
US6637699B2 (en) * 2002-03-25 2003-10-28 Lockheed Martin Corporation Method and apparatus for controlling a trajectory of a projectile
FR2846079B1 (fr) 2002-10-17 2006-08-18 Giat Ind Sa Dispositif de verrouillage/deverrouillage et d'entrainement de gouvernes de projectile
FR2846080B1 (fr) 2002-10-17 2007-05-25 Giat Ind Sa Dispositif de deploiement et d'entrainement de gouvernes de projectile
US6827310B1 (en) * 2003-09-22 2004-12-07 The United States Of America As Represented By The Secretary Of The Navy Apparatus and method for fin actuation in a portable missile
FR2864613B1 (fr) 2003-12-31 2006-03-17 Giat Ind Sa Dispositif de deploiement et d'entrainement de gouvernes d'un projectile
US7219579B2 (en) * 2004-03-10 2007-05-22 Lockheed Martin Corporation Apparatus and method for actuating control surfaces
US7246539B2 (en) * 2005-01-12 2007-07-24 Lockheed Martin Corporation Apparatus for actuating a control surface
US20080029641A1 (en) * 2005-02-07 2008-02-07 Bae Systems Information And Electronic Systems Three Axis Aerodynamic Control of Guided Munitions

Also Published As

Publication number Publication date
FR2891618B1 (fr) 2010-06-11
ATE475060T1 (de) 2010-08-15
ES2349303T3 (es) 2010-12-29
IL178325A0 (en) 2007-02-11
EP1772698B1 (de) 2010-07-21
US7923671B1 (en) 2011-04-12
IL178325A (en) 2012-12-31
EP1772698A1 (de) 2007-04-11
US20110073705A1 (en) 2011-03-31
FR2891618A1 (fr) 2007-04-06

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