DE2965231D1 - Deployable wing mechanism - Google Patents

Deployable wing mechanism

Info

Publication number
DE2965231D1
DE2965231D1 DE7979302854T DE2965231T DE2965231D1 DE 2965231 D1 DE2965231 D1 DE 2965231D1 DE 7979302854 T DE7979302854 T DE 7979302854T DE 2965231 T DE2965231 T DE 2965231T DE 2965231 D1 DE2965231 D1 DE 2965231D1
Authority
DE
Germany
Prior art keywords
wing mechanism
deployable wing
deployable
wing
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
DE7979302854T
Other languages
German (de)
Inventor
Keith Donald 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
Commonwealth of Australia Department of Defence
Original Assignee
Commonwealth of Australia
Commonwealth of Australia Department of Defence
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, Commonwealth of Australia Department of Defence filed Critical Commonwealth of Australia
Application granted granted Critical
Publication of DE2965231D1 publication Critical patent/DE2965231D1/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
DE7979302854T 1978-12-29 1979-12-11 Deployable wing mechanism Expired DE2965231D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AUPD723878 1978-12-29

Publications (1)

Publication Number Publication Date
DE2965231D1 true DE2965231D1 (en) 1983-05-19

Family

ID=3767901

Family Applications (1)

Application Number Title Priority Date Filing Date
DE7979302854T Expired DE2965231D1 (en) 1978-12-29 1979-12-11 Deployable wing mechanism

Country Status (5)

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

Families Citing this family (39)

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SE433261B (en) * 1980-03-31 1984-05-14 Andersson Kurt Goeran AN INTRODUCTORY ROTATION-STABILIZED BALLISTIC ARTILLERY PROJECT PROVIDED WITH FALLABLE 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 (en) * 1986-06-27 1987-12-31 Thomson Brandt Armements WING WITH MULTIPLE DEPLOYMENT AND ITS APPLICATION TO A FLYING DEVICE
FR2812936A1 (en) * 1986-08-12 2002-02-15 Aerospatiale Missile with variable wing configuration has moving wings extending from slots in hollow fixed wings on missile body
FR2623898B1 (en) * 1987-11-26 1990-03-23 France Etat Armement DEVICE FOR DEPLOYING A PROJECTILE FIN
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 (en) * 1989-12-12 1992-03-13 Aerospatiale SUPERSONIC MISSILE WITH TORQUE DRIVING BY 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
JP4750996B2 (en) 2000-02-01 2011-08-17 ユナイテッド ビデオ プロパティーズ インク Method and system for forced advertising
US6581871B2 (en) * 2001-06-04 2003-06-24 Smiths Aerospace, Inc. Extendable and controllable flight vehicle wing/control surface assembly
DE102004039770A1 (en) * 2004-08-16 2006-03-02 Diehl Bgt Defence Gmbh & Co. Kg wing assembly
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 (en) * 2012-10-10 2013-12-20 Алексей Александрович Пирогов Pirogov's flapping propeller with asymmetric rotary blade
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 (en) * 2016-03-11 2017-11-03 甘丽霞 A kind of wing
CN105691593B (en) * 2016-03-11 2018-01-02 国网浙江省电力公司信息通信分公司 A kind of folding wings unmanned plane
CN105905276B (en) * 2016-05-10 2018-02-09 吉林省山河艮盛科技有限公司 A kind of architectural engineering folding wings unmanned plane
CN105799911B (en) * 2016-05-10 2017-11-21 哈尔滨讯建科技有限公司 A kind of energy-conserving and environment-protective architectural engineering folding wings unmanned plane
CN105947209B (en) * 2016-05-10 2018-04-17 菁果国际教育科技（广州）有限公司 A kind of energy saving and environment friendly building municipal administration unmanned plane
CN105857574B (en) * 2016-05-10 2017-12-08 江苏福莱尔航空科技有限公司 One kind building municipal administration unmanned plane
CN105865271B (en) * 2016-05-27 2017-09-05 中国人民解放军国防科学技术大学 A kind of portable missile of use fast aeration missile wing
CN108548457B (en) * 2018-03-20 2023-12-05 浙江理工大学 Single power source synchronous driving type secondary folding unfolding mechanism for guided missile
CN109533241B (en) * 2018-12-14 2023-08-15 南京信息工程大学 Intelligent flap underwater robot
CN109405643A (en) * 2018-12-17 2019-03-01 江南机电设计研究所 A kind of laterally folded formula aerofoil of high rigidity
US11644287B2 (en) 2019-06-13 2023-05-09 Raytheon Company Single-actuator rotational deployment mechanism for multiple objects
CN111268075A (en) * 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） Scalable wing device for underwater glider
CN112896487B (en) * 2021-01-28 2022-10-21 西安电子科技大学 Unmanned aerial vehicle synchronous unfolding and folding system, method and application
CN112960107B (en) * 2021-02-26 2022-12-09 珠海天晴航空航天科技有限公司 Folding unmanned aerial vehicle
CN113665792B (en) * 2021-08-11 2023-12-05 广东空天科技研究院 Folding wing and locking mechanism suitable for high bearing state of folding wing
CN114056524A (en) * 2021-12-07 2022-02-18 中国海洋大学 Underwater rotation-preventing tail wing and direct-reading CTD with same
CN114485288A (en) * 2021-12-27 2022-05-13 西安现代控制技术研究所 Unfolding and locking method of small-caliber projectile body-large wingspan space folding tail wing
CN115060124B (en) * 2022-07-08 2023-11-03 江西洪都航空工业集团有限责任公司 Portable missile wing locking device of commonality
CN116513448B (en) * 2023-07-04 2023-10-13 西安羚控电子科技有限公司 Limiting device of folding wing and folding wing
CN117585215B (en) * 2024-01-18 2024-03-26 成都金支点科技有限公司 Folding wing of small unmanned aerial vehicle expands and locking mechanism and unmanned aerial vehicle

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Publication number Priority date Publication date Assignee Title
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
BE551492A (en) * 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 (en) * 1962-09-11 1965-08-26 Dynamit Nobel Ag Folding tail, especially for rocket projectiles
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 (en) * 1963-10-03 1967-05-24 Ver Flugtechnische Werke Ges M Missiles, especially rockets or altitude probes, with folding wings for returning the missile from the air space to the earth
FR1505851A (en) * 1965-12-20 1967-12-15 United Kingdom Government Folding stabilization and guide fins for rockets
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 (en) * 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
EP0013096B1 (en) 1983-04-13
JPS5592900A (en) 1980-07-14
CA1113070A (en) 1981-11-24
EP0013096A1 (en) 1980-07-09
AU5387979A (en) 1980-07-03
AU524255B2 (en) 1982-09-09

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Legal Events

Date Code Title Description
8339 Ceased/non-payment of the annual fee