DE602004005957D1 - Vorrichtung zur Entfaltung und Steuerung der Steuerflächen eines Projektils - Google Patents

Vorrichtung zur Entfaltung und Steuerung der Steuerflächen eines Projektils

Info

Publication number
DE602004005957D1
DE602004005957D1 DE602004005957T DE602004005957T DE602004005957D1 DE 602004005957 D1 DE602004005957 D1 DE 602004005957D1 DE 602004005957 T DE602004005957 T DE 602004005957T DE 602004005957 T DE602004005957 T DE 602004005957T DE 602004005957 D1 DE602004005957 D1 DE 602004005957D1
Authority
DE
Germany
Prior art keywords
projectile
deploying
controlling
rudders
control surfaces
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
DE602004005957T
Other languages
English (en)
Other versions
DE602004005957T2 (de
Inventor
Dominique Dion
Rene Dodu
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 DE602004005957D1 publication Critical patent/DE602004005957D1/de
Application granted granted Critical
Publication of DE602004005957T2 publication Critical patent/DE602004005957T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements
    • F42B10/62Steering by movement of flight surfaces
    • F42B10/64Steering by movement of flight surfaces of fins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Devices For Conveying Motion By Means Of Endless Flexible Members (AREA)
  • Laser Surgery Devices (AREA)
  • Aerials With Secondary Devices (AREA)
  • Preliminary Treatment Of Fibers (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
DE602004005957T 2003-12-31 2004-12-02 Vorrichtung zur Entfaltung und Steuerung der Steuerflächen eines Projektils Active DE602004005957T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0315601 2003-12-31
FR0315601A FR2864613B1 (fr) 2003-12-31 2003-12-31 Dispositif de deploiement et d'entrainement de gouvernes d'un projectile

Publications (2)

Publication Number Publication Date
DE602004005957D1 true DE602004005957D1 (de) 2007-05-31
DE602004005957T2 DE602004005957T2 (de) 2008-01-10

Family

ID=34566366

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004005957T Active DE602004005957T2 (de) 2003-12-31 2004-12-02 Vorrichtung zur Entfaltung und Steuerung der Steuerflächen eines Projektils

Country Status (6)

Country Link
US (1) US7175131B2 (de)
EP (1) EP1550837B1 (de)
AT (1) ATE360186T1 (de)
DE (1) DE602004005957T2 (de)
ES (1) ES2285382T3 (de)
FR (1) FR2864613B1 (de)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2885213B1 (fr) 2005-05-02 2010-11-05 Giat Ind Sa Procede de commande d'une munition ou sous-munition, systeme d'attaque, munition et designateur mettant en oeuvre un tel procede
FR2891618B1 (fr) * 2005-10-05 2010-06-11 Giat Ind Sa Dispositif d'entrainement de gouvernes de projectile.
FR2895496B1 (fr) 2005-12-26 2008-03-28 Giat Ind Sa Dispositif de mesure de la position angulaire d'une ailette ou gouverne d'un projectile et procede de montage d'un tel dispositif
US7800032B1 (en) * 2006-11-30 2010-09-21 Raytheon Company Detachable aerodynamic missile stabilizing system
FR2911954B1 (fr) 2007-01-31 2009-04-24 Nexter Munitions Sa Dispositif de pilotage d'une munition a gouvernes deployables
US7700902B2 (en) * 2007-10-18 2010-04-20 Hr Textron, Inc. Locking assembly for rotary shafts
US8080772B2 (en) * 2007-11-02 2011-12-20 Honeywell International Inc. Modular, harnessless electromechanical actuation system assembly
US7952055B2 (en) * 2007-11-21 2011-05-31 Raytheon Company Methods and apparatus for deploying control surfaces sequentially
US8076623B2 (en) * 2009-03-17 2011-12-13 Raytheon Company Projectile control device
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
EP2556327B1 (de) * 2010-04-07 2016-06-08 BAE Systems Information and Electronic Systems Integration Inc. Flügelspaltdichtung
TR201901397T4 (tr) * 2011-05-13 2019-02-21 Leigh Aerosystems Corp Karadan fırlatılan roket güdüm sistemi.
US8816261B1 (en) * 2011-06-29 2014-08-26 Raytheon Company Bang-bang control using tangentially mounted surfaces
IL214191A (en) * 2011-07-19 2017-06-29 Elkayam Ami Ammunition guidance system and method for assembly
CN102507200A (zh) * 2011-10-27 2012-06-20 中国航天科技集团公司第四研究院四O一所 一种舵片旋转退出装置
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
WO2015138687A1 (en) * 2014-03-13 2015-09-17 Moog Inc. Fin retention and release mechanism
FR3038042B1 (fr) * 2015-06-26 2017-06-23 Nexter Munitions Dispositif de controle de trajectoire pour un projectile et projectile equipe d'un tel dispositif
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
US10458764B2 (en) * 2016-10-24 2019-10-29 Rosemount Aerospace Inc. Canard stowage lock
FR3080912B1 (fr) 2018-05-02 2020-04-03 Nexter Munitions Projectile propulse par statoreacteur
CN109470090B (zh) * 2018-12-26 2023-08-29 湖南省军合科技有限公司 一种3d打印巡飞弹弹翼折叠展开机构
IL266249B (en) * 2019-04-18 2020-08-31 Pearlsof Wisdom Advanced Tech Ltd A system and method for detecting the release of a UAV
FR3098491B1 (fr) * 2019-07-09 2021-06-18 Safran Electrical & Power Doigt de verrouillage d’un arbre de moteur électrique
US11340052B2 (en) 2019-08-27 2022-05-24 Bae Systems Information And Electronic Systems Integration Inc. Wing deployment initiator and locking mechanism
US11852211B2 (en) 2020-09-10 2023-12-26 Bae Systems Information And Electronic Systems Integration Inc. Additively manufactured elliptical bifurcating torsion spring
CN112659011B (zh) * 2020-11-12 2023-03-24 北京星航机电装备有限公司 一种舵面折叠、释放工装及舵面折叠和释放方法
CN112829924B (zh) * 2020-12-31 2022-12-13 上海机电工程研究所 一种可伸缩式鸭舵机构
CN113280689A (zh) * 2021-06-16 2021-08-20 重庆航天工业有限公司 一种舵系统
EP4396078A1 (de) * 2021-09-01 2024-07-10 Raytheon Company Steuerflächenverriegelungssystem für taktisches fluggerät
CN113804066B (zh) * 2021-09-18 2023-01-10 天津爱思达航天科技有限公司 一种带有同步旋转折叠翼的尾舱结构
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
CN114963884A (zh) * 2022-03-01 2022-08-30 宁波天擎航天科技有限公司 一种靶弹舵片气动可控展开机构及安装有该机构的靶弹
CN115406311B (zh) * 2022-09-14 2023-09-29 北京中科宇航技术有限公司 一种栅格舵装置

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4175720A (en) * 1978-04-05 1979-11-27 The United States Of America As Represented By The Secretary Of The Navy Retainer/release mechanism for use on fin stabilized gun fired projectiles
GB2150092B (en) * 1983-11-25 1987-07-22 British Aerospace Deployment and actuation mechanisms
DE4020897C2 (de) * 1990-06-30 1993-11-11 Diehl Gmbh & Co Einrichtung zum Entriegeln und Ausschwenken der Ruderblätter eines Projektiles
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
US6446906B1 (en) 2000-04-06 2002-09-10 Versatron, Inc. Fin and cover release system
SE519764C2 (sv) 2000-08-31 2003-04-08 Bofors Defence Ab Canardfenaggregat
US6726147B1 (en) * 2003-05-15 2004-04-27 Moog Inc. Multi-function actuator, and method of operating same

Also Published As

Publication number Publication date
US20050151000A1 (en) 2005-07-14
US7175131B2 (en) 2007-02-13
FR2864613B1 (fr) 2006-03-17
ATE360186T1 (de) 2007-05-15
EP1550837B1 (de) 2007-04-18
DE602004005957T2 (de) 2008-01-10
ES2285382T3 (es) 2007-11-16
FR2864613A1 (fr) 2005-07-01
EP1550837A1 (de) 2005-07-06

Similar Documents

Publication Publication Date Title
ATE360186T1 (de) Vorrichtung zur entfaltung und steuerung der steuerflächen eines projektils
WO2007070797A3 (en) Detachment actuator for use with medical device deployment systems
ATE450769T1 (de) Gasabnahmeanordnung und lauf bzw. waffe mit einer gasabnahmeanordnung
ATE355445T1 (de) Brennkraftmaschine mit einer einzigen obenliegenden nockenwelle zur mechanischen steuerung der auslassventile und zur elektrohydraulischen steuerung der einlassventile
BRPI0514621A (pt) faixa de pulso ou outro tipo de faixa tendo uma antena ajustável para uso com uma leitora de sensor
ATE385490T1 (de) Aerodynamische verkleidung für ein flugzeugfahrwerk
DE502006006679D1 (de) Vorrichtung zum Laden einer Maschinenkanone
ATE429572T1 (de) Sehr kompakte vorrichtung zum verstellen des verdichtungsverhältnisses eines brennkraftmotors
WO2007070792A3 (en) Actuator handle for use with medical device deployment systems
DE502008002507D1 (de) Vorrichtung zur variablen einstellung der steuerzeiten von gaswechselventilen einer brennkraftmaschine
BRPI0513279A (pt) pigmento de marcação de tecido modificado e método para modificar o pigmento de marcação de tecido
BR0301028A (pt) Caixa da culatra para armas de fogo
EP1988315A3 (de) Schnellwirkendes Entlüftungsprüfventil für Flugzeugmotoren
ES2155431T1 (es) Encendedor resistente a los niños.
ATE333345T1 (de) Verbinder für den pneumatikanschluss eines pneumatischen werkzeugs und dessen kombination
BRPI0603144A (pt) membro para controlar fluxo de ar para um motor de combustão interna de um veìculo a motor
RU2019124105A (ru) Узел подачи газа для привода двери самолета и эвакуационная система
ATE391848T1 (de) Einspritzdüse
DE602004019794D1 (de) Vorrichtung zur kontinuierlichen steuerung von in einer mühle gemahlenen würzmitteln
ATE322622T1 (de) Pyrotechnischer stellantrieb mit variabler schubkraft
ES2113716T3 (es) Valvula de dos etapas para la alimentacion de aire a inyectores de motores de combustion interna.
SV1996000041A (es) Encendedor selectivamente accionable
WO2007017130A3 (de) Verriegelungseinrichtung für einen nockenwellenversteller einer brennkraftmaschine
ATE410627T1 (de) Sicherheitsventil zum automatischen absperren von gasleitungen
DE502005002563D1 (de) Vorrichtung zum Aufhängen eines Stammes

Legal Events

Date Code Title Description
8364 No opposition during term of opposition