DE2264338A1 - Ausklappbares leitwerk, insbesondere fuer raketen - Google Patents
Ausklappbares leitwerk, insbesondere fuer raketenInfo
- 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
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)
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 (fr) | 1972-12-30 | 1973-12-20 | |
US429271A US3861627A (en) | 1972-12-30 | 1973-12-28 | Foldable control flap unit, especially for rockets |
IT54663/73A IT1002569B (it) | 1972-12-30 | 1973-12-28 | Perfezionamento negli impennaggi per razzi e simili |
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 (fr) |
DE (1) | DE2264338A1 (fr) |
FR (1) | FR2212528B1 (fr) |
IT (1) | IT1002569B (fr) |
Families Citing this family (23)
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 |
ATE386921T1 (de) * | 2003-09-05 | 2008-03-15 | Selex Sensors & Airborne Sys | Luftwiderstand erzeugende vorrichtungen |
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 |
WO2011014806A1 (fr) * | 2009-07-31 | 2011-02-03 | Raytheon Company | Carénage pouvant être déployé et procédé pour réduire la traînée aérodynamique sur un obus d'artillerie lancé par un canon |
US8754352B2 (en) * | 2010-04-07 | 2014-06-17 | 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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1187193A (fr) * | 1957-11-15 | 1959-09-08 | Hotchkiss Brandt | Empennage déployant perfectionné pour projectile |
NL266892A (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 |
-
1972
- 1972-12-30 DE DE2264338A patent/DE2264338A1/de active Pending
-
1973
- 1973-12-20 FR FR7345852A patent/FR2212528B1/fr not_active Expired
- 1973-12-28 IT IT54663/73A patent/IT1002569B/it active
- 1973-12-28 US US429271A patent/US3861627A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US3861627A (en) | 1975-01-21 |
IT1002569B (it) | 1976-05-20 |
FR2212528A1 (fr) | 1974-07-26 |
FR2212528B1 (fr) | 1977-08-19 |
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