FR2212528B1 - - Google Patents

Info

Publication number
FR2212528B1
FR2212528B1 FR7345852A FR7345852A FR2212528B1 FR 2212528 B1 FR2212528 B1 FR 2212528B1 FR 7345852 A FR7345852 A FR 7345852A FR 7345852 A FR7345852 A FR 7345852A FR 2212528 B1 FR2212528 B1 FR 2212528B1
Authority
FR
France
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
Application number
FR7345852A
Other versions
FR2212528A1 (fr
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.)
Dynamit Nobel AG
Original Assignee
Dynamit Nobel AG
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 Dynamit Nobel AG filed Critical Dynamit Nobel AG
Publication of FR2212528A1 publication Critical patent/FR2212528A1/fr
Application granted granted Critical
Publication of FR2212528B1 publication Critical patent/FR2212528B1/fr
Expired legal-status Critical Current

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
    • 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
    • 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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Testing Of Engines (AREA)
FR7345852A 1972-12-30 1973-12-20 Expired FR2212528B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2264338A DE2264338A1 (de) 1972-12-30 1972-12-30 Ausklappbares leitwerk, insbesondere fuer raketen

Publications (2)

Publication Number Publication Date
FR2212528A1 FR2212528A1 (fr) 1974-07-26
FR2212528B1 true FR2212528B1 (fr) 1977-08-19

Family

ID=5865891

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7345852A Expired FR2212528B1 (fr) 1972-12-30 1973-12-20

Country Status (4)

Country Link
US (1) US3861627A (fr)
DE (1) DE2264338A1 (fr)
FR (1) FR2212528B1 (fr)
IT (1) IT1002569B (fr)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE444612B (sv) * 1984-12-13 1986-04-21 Ffv Affersverket Styrverk for utfellning av fenor hos projektil
DE3712704A1 (de) * 1987-04-14 1988-11-03 Diehl Gmbh & Co Flugkoerper mit ausklappbaren fluegeln
US5417139A (en) * 1993-10-01 1995-05-23 Unisys Corporation Delivery system and method for flexible array
FR2721702B1 (fr) * 1994-06-28 1996-08-14 Luchaire Defense Sa Dispositif de déploiement d'une ailette de projectile.
US5671899A (en) * 1996-02-26 1997-09-30 Lockheed Martin Corporation Airborne vehicle with wing extension and roll control
US5927643A (en) * 1997-11-05 1999-07-27 Atlantic Research Corporation Self-deploying airfoil for missile or the like
US6224013B1 (en) * 1998-08-27 2001-05-01 Lockheed Martin Corporation Tail fin deployment device
DE19960738C1 (de) * 1999-12-16 2001-08-23 Lfk Gmbh Ruderanbindung für Lenkflugkörper
SE518656C2 (sv) * 2000-07-03 2002-11-05 Bofors Defence Ab Fenstabiliserad artillerigranat
WO2005026651A1 (fr) * 2003-09-05 2005-03-24 Selex Sensors And Airborne Systems Limited Dispositifs generateurs de trainee
US7262394B2 (en) * 2004-03-05 2007-08-28 The Boeing Company Mortar shell ring tail and associated method
US7475846B2 (en) * 2005-10-05 2009-01-13 General Dynamics Ordnance And Tactical Systems, Inc. Fin retention and deployment mechanism
EP2459956B1 (fr) * 2009-07-31 2014-12-24 Raytheon Company Carénage pouvant être déployé et procédé pour réduire la traînée aérodynamique sur un obus d'artillerie lancé par un canon
WO2011126970A2 (fr) * 2010-04-07 2011-10-13 Bae Systems Information And Electronic Systems Integration Inc. Initiateur de déploiement d'aile à ressort de compression
CN104833276B (zh) * 2015-05-18 2016-09-14 中国船舶重工集团公司第七○二研究所 栅格翼同步展开机构
CN105424314B (zh) * 2015-12-18 2018-02-09 中国航天空气动力技术研究院 自由飞模型舵面展开风洞试验装置
CN107421403A (zh) * 2017-09-20 2017-12-01 成都云鼎智控科技有限公司 一种用于纵向折叠弹翼的多杆联动式折叠机构
CN109141143A (zh) * 2018-07-26 2019-01-04 重庆长安工业(集团)有限责任公司 一种折叠翼面卡锁机构
CN109696088B (zh) * 2018-12-07 2021-06-08 上海机电工程研究所 紧凑式弹翼缩展机构及导弹
US11340052B2 (en) 2019-08-27 2022-05-24 Bae Systems Information And Electronic Systems Integration Inc. Wing deployment initiator and locking mechanism
CN110906807B (zh) * 2019-12-13 2021-11-16 北京中科宇航探索技术有限公司 一种火箭用嵌入式气动控制舵面
US11852211B2 (en) 2020-09-10 2023-12-26 Bae Systems Information And Electronic Systems Integration Inc. Additively manufactured elliptical bifurcating torsion spring
CN114216647B (zh) * 2021-12-16 2024-06-14 中国航天空气动力技术研究院 一种风洞试验用舵翼瞬态展收装置

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1187193A (fr) * 1957-11-15 1959-09-08 Hotchkiss Brandt Empennage déployant perfectionné pour projectile
NL113679C (fr) * 1960-07-11
FR1418696A (fr) * 1963-12-28 1965-11-19 Breda Mecc Bresciana Gouvernail à ailettes pliantes pour fusées
CH493819A (de) * 1968-07-11 1970-07-15 Oerlikon Buehrle Ag Drallfreies Geschoss mit Abschussrohr
DE1906028C3 (de) * 1969-02-07 1973-12-06 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Leitwerk fur Geschosse und Flug korper mit einer Einrichtung zur Über fuhrung der Flossen des Leitwerkes in ihre wirksame Stellung

Also Published As

Publication number Publication date
IT1002569B (it) 1976-05-20
DE2264338A1 (de) 1974-07-04
FR2212528A1 (fr) 1974-07-26
US3861627A (en) 1975-01-21

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Legal Events

Date Code Title Description
ST Notification of lapse