DE602004015221D1 - Vorrichtung zum Ausklappen des Leitwerks eines Projektils - Google Patents

Vorrichtung zum Ausklappen des Leitwerks eines Projektils

Info

Publication number
DE602004015221D1
DE602004015221D1 DE602004015221T DE602004015221T DE602004015221D1 DE 602004015221 D1 DE602004015221 D1 DE 602004015221D1 DE 602004015221 T DE602004015221 T DE 602004015221T DE 602004015221 T DE602004015221 T DE 602004015221T DE 602004015221 D1 DE602004015221 D1 DE 602004015221D1
Authority
DE
Germany
Prior art keywords
projectile
fin
support
axis
unfolding
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
DE602004015221T
Other languages
English (en)
Inventor
Christian Trouillot
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 DE602004015221D1 publication Critical patent/DE602004015221D1/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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Tents Or Canopies (AREA)
  • Jib Cranes (AREA)
  • Massaging Devices (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Amplifiers (AREA)
  • Bidet-Like Cleaning Device And Other Flush Toilet Accessories (AREA)
DE602004015221T 2003-10-06 2004-09-16 Vorrichtung zum Ausklappen des Leitwerks eines Projektils Active DE602004015221D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0311642A FR2860577B1 (fr) 2003-10-06 2003-10-06 Dispositif de deploiement d'une ailette d'un projectile

Publications (1)

Publication Number Publication Date
DE602004015221D1 true DE602004015221D1 (de) 2008-09-04

Family

ID=34307425

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004015221T Active DE602004015221D1 (de) 2003-10-06 2004-09-16 Vorrichtung zum Ausklappen des Leitwerks eines Projektils

Country Status (6)

Country Link
US (1) US7059561B2 (de)
EP (1) EP1524488B1 (de)
AT (1) ATE402389T1 (de)
DE (1) DE602004015221D1 (de)
FR (1) FR2860577B1 (de)
IL (1) IL164293A (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7642492B2 (en) * 2005-01-26 2010-01-05 Raytheon Company Single-axis fin deployment system
FR2895071B1 (fr) 2005-12-19 2008-01-18 Giat Ind Sa Dispositif de verrouillage anti-rebond d'une ailette deployable d'un projectile.
US7856929B2 (en) 2007-06-29 2010-12-28 Taser International, Inc. Systems and methods for deploying an electrode using torsion
FR2949848B1 (fr) * 2009-09-10 2012-09-28 Nexter Munitions Dispositif d'ouverture et verrouillage d'une ailette canard.
WO2011126970A2 (en) * 2010-04-07 2011-10-13 Bae Systems Information And Electronic Systems Integration Inc. Compression spring wing deployment initiator
FR3041744B1 (fr) * 2015-09-29 2018-08-17 Nexter Munitions Projectile d'artillerie ayant une phase pilotee.
EP3488176B1 (de) * 2016-07-21 2023-04-26 Chairman, Defence Research & Development Organisation (DRDO) Bidirektionaler flügelentfaltungsmechanismus
CN106927017B (zh) * 2017-03-29 2023-12-12 河北全疆科技有限公司 一种多旋翼无人机机臂折叠机构
EP3403922A1 (de) * 2017-05-18 2018-11-21 Airbus Operations GmbH Flügelanordnung für ein flugzeug
US11300390B1 (en) * 2018-03-05 2022-04-12 Dynamic Structures And Materials, Llc Control surface deployment apparatus and method of use
US11067371B2 (en) * 2019-03-22 2021-07-20 Bae Systems Information And Electronic Systems Integration Inc. Trimmable tail kit rudder
DE102020105188B4 (de) * 2020-02-27 2023-08-31 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugkörper-Finnenausklappeinrichtung, Flugkörper und Verfahren zum Betrieb eines Flugkörpers

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3063375A (en) * 1960-05-19 1962-11-13 Wilbur W Hawley Folding fin
DE3010027C2 (de) * 1978-09-26 1985-07-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schwenkbare Anordnung eines Leitwerks, insbesondere bei Flugkörpern oder Geschossen
US4323208A (en) * 1980-02-01 1982-04-06 British Aerospace Folding fins
US4664339A (en) * 1984-10-11 1987-05-12 The Boeing Company Missile appendage deployment mechanism
DE3507677A1 (de) * 1985-03-05 1986-09-11 Diehl GmbH & Co, 8500 Nürnberg Flugkoerper mit ueberkalibrigem leitwerk
US4869442A (en) * 1988-09-02 1989-09-26 Aerojet-General Corporation Self-deploying airfoil
IL107844A (en) * 1993-12-02 1996-06-18 Ministry Of Defence Armaments Flying object control system
US5480111A (en) * 1994-05-13 1996-01-02 Hughes Missile Systems Company Missile with deployable control fins
US5762294A (en) * 1997-03-31 1998-06-09 The United States Of America As Represented By The Secretary Of The Army Wing deployment device
FR2797946B1 (fr) * 1999-08-31 2002-10-04 Aerospatiale Matra Missiles Dispositif de montage d'un appendice rigide sur un engin apte a etre lance depuis le tube, et engin correspondant
US6761331B2 (en) * 2002-03-19 2004-07-13 Raytheon Company Missile having deployment mechanism for stowable fins

Also Published As

Publication number Publication date
FR2860577A1 (fr) 2005-04-08
EP1524488B1 (de) 2008-07-23
ATE402389T1 (de) 2008-08-15
EP1524488A1 (de) 2005-04-20
US20050082420A1 (en) 2005-04-21
IL164293A (en) 2012-02-29
IL164293A0 (en) 2005-12-18
US7059561B2 (en) 2006-06-13
FR2860577B1 (fr) 2006-01-27

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition