IL118455A - Aerodynamic level and control surface and control system using it - Google Patents

Aerodynamic level and control surface and control system using it

Info

Publication number
IL118455A
IL118455A IL11845596A IL11845596A IL118455A IL 118455 A IL118455 A IL 118455A IL 11845596 A IL11845596 A IL 11845596A IL 11845596 A IL11845596 A IL 11845596A IL 118455 A IL118455 A IL 118455A
Authority
IL
Israel
Prior art keywords
grid
control surface
outer panels
flexible material
aerodynamic
Prior art date
Application number
IL11845596A
Other languages
English (en)
Hebrew (he)
Other versions
IL118455A0 (en
Original Assignee
Hughes Missile Systems
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 Hughes Missile Systems filed Critical Hughes Missile Systems
Publication of IL118455A0 publication Critical patent/IL118455A0/xx
Publication of IL118455A publication Critical patent/IL118455A/en

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)
IL11845596A 1995-06-06 1996-05-28 Aerodynamic level and control surface and control system using it IL118455A (en)

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
IL118455A0 IL118455A0 (en) 1996-09-12
IL118455A true IL118455A (en) 1998-12-27

Family

ID=23871753

Family Applications (1)

Application Number Title Priority Date Filing Date
IL11845596A IL118455A (en) 1995-06-06 1996-05-28 Aerodynamic level and control surface and control system using it

Country Status (8)

Country Link
US (1) US5642867A (ko)
EP (1) EP0747659B1 (ko)
JP (1) JP2807437B2 (ko)
KR (1) KR0179432B1 (ko)
AU (1) AU690444B2 (ko)
CA (1) CA2176608C (ko)
DE (1) DE69603232T2 (ko)
IL (1) IL118455A (ko)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1073040C (zh) * 1995-05-11 2001-10-17 危姆派尔国家机械建筑设计局 带格栅式控制面的火箭
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
EP3842345B1 (en) * 2020-10-29 2022-10-19 Airbus Defence and Space, S.A.U. Air to air active refuelling system and method for generating aerodynamic radial loads at a hose-end
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 (ko) * 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
CA2176608A1 (en) 1996-12-07
JP2807437B2 (ja) 1998-10-08
EP0747659A1 (en) 1996-12-11
DE69603232D1 (de) 1999-08-19
KR970002250A (ko) 1997-01-24
JPH09105599A (ja) 1997-04-22
KR0179432B1 (ko) 1999-04-01
AU690444B2 (en) 1998-04-23
EP0747659B1 (en) 1999-07-14
AU5227596A (en) 1996-12-19
CA2176608C (en) 1999-11-02
IL118455A0 (en) 1996-09-12
DE69603232T2 (de) 1999-12-02
US5642867A (en) 1997-07-01

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