CA1113070A - Deployable wing mechanism - Google Patents

Deployable wing mechanism

Info

Publication number
CA1113070A
CA1113070A CA341,765A CA341765A CA1113070A CA 1113070 A CA1113070 A CA 1113070A CA 341765 A CA341765 A CA 341765A CA 1113070 A CA1113070 A CA 1113070A
Authority
CA
Canada
Prior art keywords
wing
segment
segments
hinge
wing segment
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
Application number
CA341,765A
Other languages
English (en)
French (fr)
Inventor
Keith D. Thomson
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.)
Commonwealth of Australia
Original Assignee
Commonwealth of Australia
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 Commonwealth of Australia filed Critical Commonwealth of Australia
Application granted granted Critical
Publication of CA1113070A publication Critical patent/CA1113070A/en
Expired 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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aerials With Secondary Devices (AREA)
  • Details Of Aerials (AREA)
CA341,765A 1978-12-29 1979-12-12 Deployable wing mechanism Expired CA1113070A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AUPD723878 1978-12-29
AUPD7238/78 1979-12-29

Publications (1)

Publication Number Publication Date
CA1113070A true CA1113070A (en) 1981-11-24

Family

ID=3767901

Family Applications (1)

Application Number Title Priority Date Filing Date
CA341,765A Expired CA1113070A (en) 1978-12-29 1979-12-12 Deployable wing mechanism

Country Status (5)

Country Link
EP (1) EP0013096B1 (de)
JP (1) JPS5592900A (de)
AU (1) AU524255B2 (de)
CA (1) CA1113070A (de)
DE (1) DE2965231D1 (de)

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SE433261B (sv) * 1980-03-31 1984-05-14 Andersson Kurt Goeran En inledningsvis rotationsstabiliserad ballistisk artilleriprojektil forsedd med utfellbara fenor
US4842218A (en) * 1980-08-29 1989-06-27 The United States Of America As Represented By The Secretary Of The Navy Pivotal mono wing cruise missile with wing deployment and fastener mechanism
GB2205798B (en) * 1983-08-11 1989-06-01 Secr Defence Improvements in or relating to unmanned aircraft.
US4691880A (en) * 1985-11-14 1987-09-08 Grumman Aerospace Corporation Torsion spring powered missile wing deployment system
FR2600618A1 (fr) * 1986-06-27 1987-12-31 Thomson Brandt Armements Aile a deploiement multiple, et son application a un engin volant
FR2812936A1 (fr) * 1986-08-12 2002-02-15 Aerospatiale Missile a voilure variable
FR2623898B1 (fr) * 1987-11-26 1990-03-23 France Etat Armement Dispositif de deploiement d'une ailette de projectile
US4869442A (en) * 1988-09-02 1989-09-26 Aerojet-General Corporation Self-deploying airfoil
GB2369177A (en) * 1989-06-02 2002-05-22 British Aerospace Aerofoil deployment system
FR2655722B1 (fr) * 1989-12-12 1992-03-13 Aerospatiale Missile supersonique a pilotage en couple par spouilers.
US5829715A (en) * 1996-04-19 1998-11-03 Lockheed Martin Vought Systems Corp. Multi-axis unfolding mechanism with rate controlled synchronized movement
US6742183B1 (en) 1998-05-15 2004-05-25 United Video Properties, Inc. Systems and methods for advertising television networks, channels, and programs
US6092264A (en) * 1998-11-13 2000-07-25 Lockheed Martin Corporation Single axis fold actuator and lock for member
DE60142774D1 (de) 2000-02-01 2010-09-23 United Video Properties Inc Methoden und systeme zum erzwingen von reklame
US6581871B2 (en) * 2001-06-04 2003-06-24 Smiths Aerospace, Inc. Extendable and controllable flight vehicle wing/control surface assembly
DE102004039770A1 (de) * 2004-08-16 2006-03-02 Diehl Bgt Defence Gmbh & Co. Kg Flügelanordnung
US8949901B2 (en) 2011-06-29 2015-02-03 Rovi Guides, Inc. Methods and systems for customizing viewing environment preferences in a viewing environment control application
RU2501712C1 (ru) * 2012-10-10 2013-12-20 Алексей Александрович Пирогов Винт пирогова махового действия с асимметрично поворотной лопастью
US9288521B2 (en) 2014-05-28 2016-03-15 Rovi Guides, Inc. Systems and methods for updating media asset data based on pause point in the media asset
CN107310729A (zh) * 2016-03-11 2017-11-03 甘丽霞 一种机翼
CN105691593B (zh) * 2016-03-11 2018-01-02 国网浙江省电力公司信息通信分公司 一种折叠翼无人机
CN105799911B (zh) * 2016-05-10 2017-11-21 哈尔滨讯建科技有限公司 一种节能环保建筑工程用折叠翼无人机
CN105947209B (zh) * 2016-05-10 2018-04-17 菁果国际教育科技（广州）有限公司 一种节能环保型建筑市政用无人机
CN105905276B (zh) * 2016-05-10 2018-02-09 吉林省山河艮盛科技有限公司 一种建筑工程用折叠翼无人机
CN105857574B (zh) * 2016-05-10 2017-12-08 江苏福莱尔航空科技有限公司 一种建筑市政用无人机
CN105865271B (zh) * 2016-05-27 2017-09-05 中国人民解放军国防科学技术大学 一种采用快速充气弹翼的便携式导弹
CN108548457B (zh) * 2018-03-20 2023-12-05 浙江理工大学 一种导弹用单一动力源同步驱动式二次折叠展开机构
CN109533241B (zh) * 2018-12-14 2023-08-15 南京信息工程大学 一种智能折翼水下机器人
CN109405643A (zh) * 2018-12-17 2019-03-01 江南机电设计研究所 一种高刚度横向折叠式翼面
US11644287B2 (en) 2019-06-13 2023-05-09 Raytheon Company Single-actuator rotational deployment mechanism for multiple objects
CN111268075A (zh) * 2020-03-09 2020-06-12 中国船舶科学研究中心（中国船舶重工集团公司第七0二研究所） 一种用于水下滑翔器可缩放翼装置
CN112896487B (zh) * 2021-01-28 2022-10-21 西安电子科技大学 一种无人机同步展开折叠系统、方法及应用
CN112960107B (zh) * 2021-02-26 2022-12-09 珠海天晴航空航天科技有限公司 一种折叠无人机
CN113665792B (zh) * 2021-08-11 2023-12-05 广东空天科技研究院 一种折叠机翼及适用于折叠机翼高承载状态的锁定机构
CN114056524A (zh) * 2021-12-07 2022-02-18 中国海洋大学 一种水下防旋转尾翼和具有该尾翼的直读式ctd
CN114485288B (zh) * 2021-12-27 2024-05-28 西安现代控制技术研究所 小口径弹体-大翼展空间折叠尾翼的展开、锁紧方法
CN114852314A (zh) * 2022-05-20 2022-08-05 大连海事大学 一种降低折叠翼冲击载荷的空投型水下滑翔机
CN115060124B (zh) * 2022-07-08 2023-11-03 江西洪都航空工业集团有限责任公司 一种通用性便携式导弹弹翼锁紧装置
CN116513448B (zh) * 2023-07-04 2023-10-13 西安羚控电子科技有限公司 一种折叠机翼的限位装置及折叠机翼
CN117585215B (zh) * 2024-01-18 2024-03-26 成都金支点科技有限公司 一种小型无人机折叠机翼展开及锁止机构及无人机
CN118270226B (zh) * 2024-06-04 2024-08-06 西安羚控电子科技有限公司 一种飞行器的折叠和展开装置

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US1485163A (en) * 1923-01-30 1924-02-26 Braun Frank Flying machine
US2572421A (en) * 1947-09-20 1951-10-23 Jr Edmund Abel Aircraft folding wing construction
US2790104A (en) * 1952-01-18 1957-04-23 Smitsvonk N V Res Lab Comp Surface discharge spark plug and method for making such a spark plug
NL211396A (de) * 1955-10-20 Brandt Soc Nouv Ets
US3218005A (en) * 1961-12-06 1965-11-16 Calderon Alberto Alvarez High lift system for high speed aircraft
DE1199664B (de) * 1962-09-11 1965-08-26 Dynamit Nobel Ag Klappleitwerk, insbesondere fuer Raketengeschosse
US3133716A (en) * 1962-10-19 1964-05-19 Boeing Co Motion transfer means in aircraft controls
US3197158A (en) * 1963-04-29 1965-07-27 Francis M Rogallo Flexible wing vehicle configurations
DE1241268B (de) * 1963-10-03 1967-05-24 Ver Flugtechnische Werke Ges M Flugkoerper, insbesondere Rakete oder Hoehensonde, mit Faltufluegeln zur Rueckfuehrung des Flugkoerpers aus dem Luftraum zur Erde
FR1505851A (fr) * 1965-12-20 1967-12-15 United Kingdom Government Ailettes de stabilisation et de guidage repliables pour fusées
US3743218A (en) * 1968-06-28 1973-07-03 T Sweeney Semi-rigid airfoil for airborne vehicles
US3643599A (en) * 1968-07-22 1972-02-22 Us Navy Retractable stabilizer fins and drag brakes for missiles
SE325802B (de) * 1968-11-01 1970-07-06 Bofors Ab
US3788578A (en) * 1971-05-19 1974-01-29 T Sweeney Semi-rigid airfoil for airborne vehicles
US3790104A (en) * 1973-03-12 1974-02-05 Us Navy High/low aspect ratio dual-mode fin design
US4022403A (en) * 1976-01-28 1977-05-10 Louis Francois Chiquet Convertible aircraft

Also Published As

Publication number Publication date
AU524255B2 (en) 1982-09-09
DE2965231D1 (en) 1983-05-19
EP0013096A1 (de) 1980-07-09
AU5387979A (en) 1980-07-03
EP0013096B1 (de) 1983-04-13
JPS5592900A (en) 1980-07-14

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Legal Events

Date Code Title Description
MKEX Expiry