DE2264338A1 - Ausklappbares leitwerk, insbesondere fuer raketen - Google Patents

Ausklappbares leitwerk, insbesondere fuer raketen

Info

Publication number
DE2264338A1
DE2264338A1 DE2264338A DE2264338A DE2264338A1 DE 2264338 A1 DE2264338 A1 DE 2264338A1 DE 2264338 A DE2264338 A DE 2264338A DE 2264338 A DE2264338 A DE 2264338A DE 2264338 A1 DE2264338 A1 DE 2264338A1
Authority
DE
Germany
Prior art keywords
tail
ring
counterpart
unit according
tail unit
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.)
Pending
Application number
DE2264338A
Other languages
German (de)
English (en)
Inventor
Rainer Schoeffl
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
Priority to DE2264338A priority Critical patent/DE2264338A1/de
Priority to FR7345852A priority patent/FR2212528B1/fr
Priority to IT54663/73A priority patent/IT1002569B/it
Priority to US429271A priority patent/US3861627A/en
Publication of DE2264338A1 publication Critical patent/DE2264338A1/de
Pending 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)
DE2264338A 1972-12-30 1972-12-30 Ausklappbares leitwerk, insbesondere fuer raketen Pending DE2264338A1 (de)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE2264338A DE2264338A1 (de) 1972-12-30 1972-12-30 Ausklappbares leitwerk, insbesondere fuer raketen
FR7345852A FR2212528B1 (enrdf_load_stackoverflow) 1972-12-30 1973-12-20
IT54663/73A IT1002569B (it) 1972-12-30 1973-12-28 Perfezionamento negli impennaggi per razzi e simili
US429271A US3861627A (en) 1972-12-30 1973-12-28 Foldable control flap unit, especially for rockets

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 (1)

Publication Number Publication Date
DE2264338A1 true DE2264338A1 (de) 1974-07-04

Family

ID=5865891

Family Applications (1)

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

Country Status (4)

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

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
ES2299902T3 (es) * 2003-09-05 2008-06-01 Selex Sensors And Airborne Systems Limited Dispositivos que producen resistencia al avance.
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
US8312813B2 (en) * 2009-07-31 2012-11-20 Raytheon Company Deployable fairing and method for reducing aerodynamic drag on a gun-launched artillery shell
WO2011126970A2 (en) * 2010-04-07 2011-10-13 Bae Systems Information And Electronic Systems Integration Inc. Compression spring wing deployment initiator
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
NL266892A (enrdf_load_stackoverflow) * 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
FR2212528A1 (enrdf_load_stackoverflow) 1974-07-26
FR2212528B1 (enrdf_load_stackoverflow) 1977-08-19
US3861627A (en) 1975-01-21
IT1002569B (it) 1976-05-20

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