DE69603232T2 - Aerodynamische Steuerfläche und Steuersystem, das eine solche Fläche verwendet - Google Patents
Aerodynamische Steuerfläche und Steuersystem, das eine solche Fläche verwendetInfo
- Publication number
- DE69603232T2 DE69603232T2 DE69603232T DE69603232T DE69603232T2 DE 69603232 T2 DE69603232 T2 DE 69603232T2 DE 69603232 T DE69603232 T DE 69603232T DE 69603232 T DE69603232 T DE 69603232T DE 69603232 T2 DE69603232 T2 DE 69603232T2
- Authority
- DE
- Germany
- Prior art keywords
- control
- aerodynamic
- control system
- aerodynamic control
- control surface
- 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.)
- Expired - Lifetime
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
-
- 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
- F42B10/143—Lattice or grid fins
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/471,469 US5642867A (en) | 1995-06-06 | 1995-06-06 | Aerodynamic lifting and control surface and control system using same |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69603232D1 DE69603232D1 (de) | 1999-08-19 |
DE69603232T2 true DE69603232T2 (de) | 1999-12-02 |
Family
ID=23871753
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69603232T Expired - Lifetime DE69603232T2 (de) | 1995-06-06 | 1996-05-17 | Aerodynamische Steuerfläche und Steuersystem, das eine solche Fläche verwendet |
Country Status (8)
Country | Link |
---|---|
US (1) | US5642867A (de) |
EP (1) | EP0747659B1 (de) |
JP (1) | JP2807437B2 (de) |
KR (1) | KR0179432B1 (de) |
AU (1) | AU690444B2 (de) |
CA (1) | CA2176608C (de) |
DE (1) | DE69603232T2 (de) |
IL (1) | IL118455A (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004061977A1 (de) * | 2004-12-23 | 2006-07-06 | Lfk-Lenkflugkörpersysteme Gmbh | Klein-Flugkörper |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1996035613A1 (fr) * | 1995-05-11 | 1996-11-14 | Vympel State Machine Building Design Bureau (Gosmkb 'vympel') | Fusee a gouvernes en treillis et gouverne en treillis pour fusee |
US5762291A (en) * | 1996-10-28 | 1998-06-09 | The United States Of America As Represented By The Secretary Of The Army | Drag control module for stabilized projectiles |
US5927643A (en) * | 1997-11-05 | 1999-07-27 | Atlantic Research Corporation | Self-deploying airfoil for missile or the like |
US6727485B2 (en) * | 2001-05-25 | 2004-04-27 | Omnitek Partners Llc | Methods and apparatus for increasing aerodynamic performance of projectiles |
KR100566204B1 (ko) * | 2003-04-22 | 2006-03-29 | 삼성전자주식회사 | 성조가 표기된 한어 병음 입력 방법 및 장치 |
US20070018033A1 (en) * | 2005-03-22 | 2007-01-25 | Fanucci Jerome P | Precision aerial delivery of payloads |
US7429017B2 (en) * | 2005-07-21 | 2008-09-30 | Raytheon Company | Ejectable aerodynamic stability and control |
US7854410B2 (en) * | 2006-05-15 | 2010-12-21 | Kazak Composites, Incorporated | Powered unmanned aerial vehicle |
US7800032B1 (en) * | 2006-11-30 | 2010-09-21 | Raytheon Company | Detachable aerodynamic missile stabilizing system |
US8698059B2 (en) * | 2012-05-03 | 2014-04-15 | Raytheon Company | Deployable lifting surface for air vehicle |
CN104567548B (zh) * | 2013-10-29 | 2019-02-26 | 北京精密机电控制设备研究所 | 一种栅格舵锁定装置 |
CN108216574A (zh) * | 2017-12-21 | 2018-06-29 | 北京有色金属研究总院 | 一种梯度结构栅格翼 |
EP3842345B1 (de) * | 2020-10-29 | 2022-10-19 | Airbus Defence and Space, S.A.U. | System zur luft-zu-luft-betankung und verfahren zur erzeugung von aerodynamischen radialen lasten an einem schlauchende |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH220097A (de) * | 1941-05-16 | 1942-03-15 | Theod Hausheer Gottlieb | Flugzeug. |
US3506220A (en) * | 1968-04-11 | 1970-04-14 | Anthony Sbrilli | Horizontal axis,flat lifting rotor and control system for aircraft |
US4158447A (en) * | 1977-11-29 | 1979-06-19 | The United States Of America As Represented By The Secretary Of The Navy | Expanding stabilizing fin cup |
US4664339A (en) | 1984-10-11 | 1987-05-12 | The Boeing Company | Missile appendage deployment mechanism |
DE3618956C1 (de) | 1986-06-05 | 1987-11-19 | Rheinmetall Gmbh | Leitwerk mit entfaltbaren Fluegeln fuer Geschosse und Flugkoerper |
US5240203A (en) * | 1987-10-01 | 1993-08-31 | Hughes Missile Systems Company | Folding wing structure with a flexible cover |
DE3838735C2 (de) * | 1988-11-15 | 1997-12-18 | Diehl Gmbh & Co | Klapp-Flügel, insbes. für ein Geschoss |
IL90903A0 (de) * | 1989-07-07 | 1990-02-09 | ||
US5048773A (en) * | 1990-06-08 | 1991-09-17 | The United States Of America As Represented By The Secretary Of The Army | Curved grid fin |
US5211358A (en) * | 1991-05-13 | 1993-05-18 | General Dynamics Corporation | Airfoil deployment system for missile or aircraft |
US5417393A (en) * | 1993-04-27 | 1995-05-23 | Hughes Aircraft Company | Rotationally mounted flexible band wing |
-
1995
- 1995-06-06 US US08/471,469 patent/US5642867A/en not_active Expired - Lifetime
-
1996
- 1996-05-14 CA CA002176608A patent/CA2176608C/en not_active Expired - Fee Related
- 1996-05-15 AU AU52275/96A patent/AU690444B2/en not_active Ceased
- 1996-05-17 EP EP96303503A patent/EP0747659B1/de not_active Expired - Lifetime
- 1996-05-17 DE DE69603232T patent/DE69603232T2/de not_active Expired - Lifetime
- 1996-05-28 IL IL11845596A patent/IL118455A/en not_active IP Right Cessation
- 1996-06-05 JP JP8143334A patent/JP2807437B2/ja not_active Expired - Fee Related
- 1996-06-05 KR KR1019960019970A patent/KR0179432B1/ko not_active IP Right Cessation
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004061977A1 (de) * | 2004-12-23 | 2006-07-06 | Lfk-Lenkflugkörpersysteme Gmbh | Klein-Flugkörper |
DE102004061977B4 (de) * | 2004-12-23 | 2008-04-10 | Lfk-Lenkflugkörpersysteme Gmbh | Klein-Flugkörper |
Also Published As
Publication number | Publication date |
---|---|
DE69603232D1 (de) | 1999-08-19 |
CA2176608C (en) | 1999-11-02 |
EP0747659A1 (de) | 1996-12-11 |
JPH09105599A (ja) | 1997-04-22 |
CA2176608A1 (en) | 1996-12-07 |
KR970002250A (ko) | 1997-01-24 |
US5642867A (en) | 1997-07-01 |
EP0747659B1 (de) | 1999-07-14 |
IL118455A (en) | 1998-12-27 |
AU5227596A (en) | 1996-12-19 |
AU690444B2 (en) | 1998-04-23 |
JP2807437B2 (ja) | 1998-10-08 |
IL118455A0 (en) | 1996-09-12 |
KR0179432B1 (ko) | 1999-04-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |