DE69603232D1 - Aerodynamische Steuerfläche und Steuersystem, das eine solche Fläche verwendet - Google Patents

Aerodynamische Steuerfläche und Steuersystem, das eine solche Fläche verwendet

Info

Publication number
DE69603232D1
DE69603232D1 DE69603232T DE69603232T DE69603232D1 DE 69603232 D1 DE69603232 D1 DE 69603232D1 DE 69603232 T DE69603232 T DE 69603232T DE 69603232 T DE69603232 T DE 69603232T DE 69603232 D1 DE69603232 D1 DE 69603232D1
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
Application number
DE69603232T
Other languages
English (en)
Other versions
DE69603232T2 (de
Inventor
Ralph H Klestadt
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.)
Raytheon Co
Original Assignee
Raytheon Co
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 Raytheon Co filed Critical Raytheon Co
Publication of DE69603232D1 publication Critical patent/DE69603232D1/de
Application granted granted Critical
Publication of DE69603232T2 publication Critical patent/DE69603232T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Body Structure For Vehicles (AREA)
  • Photovoltaic Devices (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Springs (AREA)
DE69603232T 1995-06-06 1996-05-17 Aerodynamische Steuerfläche und Steuersystem, das eine solche Fläche verwendet Expired - Lifetime DE69603232T2 (de)

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 true DE69603232D1 (de) 1999-08-19
DE69603232T2 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)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
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
DE102004061977B4 (de) * 2004-12-23 2008-04-10 Lfk-Lenkflugkörpersysteme Gmbh Klein-Flugkörper
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
ES2929595T3 (es) * 2020-10-29 2022-11-30 Airbus Defence & Space Sau Sistema de repostaje aire-aire activo y método para generar cargas radiales aerodinámicas en un extremo de manguera
CN115808103A (zh) * 2022-11-16 2023-03-17 北京星际荣耀科技有限责任公司 一种栅格舵折叠展开装置及运载火箭

Family Cites Families (11)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
JP2807437B2 (ja) 1998-10-08
AU5227596A (en) 1996-12-19
JPH09105599A (ja) 1997-04-22
IL118455A (en) 1998-12-27
US5642867A (en) 1997-07-01
EP0747659B1 (de) 1999-07-14
CA2176608A1 (en) 1996-12-07
KR970002250A (ko) 1997-01-24
AU690444B2 (en) 1998-04-23
EP0747659A1 (de) 1996-12-11
DE69603232T2 (de) 1999-12-02
IL118455A0 (en) 1996-09-12
CA2176608C (en) 1999-11-02
KR0179432B1 (ko) 1999-04-01

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