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AU524255B2 - Deployable wing - Google Patents

Deployable wing

Info

Publication number
AU524255B2
AU524255B2 AU53879/79A AU5387979A AU524255B2 AU 524255 B2 AU524255 B2 AU 524255B2 AU 53879/79 A AU53879/79 A AU 53879/79A AU 5387979 A AU5387979 A AU 5387979A AU 524255 B2 AU524255 B2 AU 524255B2
Authority
AU
Australia
Prior art keywords
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.)
Ceased
Application number
AU53879/79A
Other versions
AU5387979A (en
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.)
Australian Government
Original Assignee
Commonwealth of Australia Department of Productivity
Australian Government
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 Department of Productivity, Australian Government filed Critical Commonwealth of Australia Department of Productivity
Publication of AU5387979A publication Critical patent/AU5387979A/en
Application granted granted Critical
Publication of AU524255B2 publication Critical patent/AU524255B2/en
Anticipated expiration legal-status Critical
Ceased 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)
AU53879/79A 1978-12-29 1978-12-29 Deployable wing Ceased AU524255B2 (en)

Applications Claiming Priority (2)

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

Publications (2)

Publication Number Publication Date
AU5387979A AU5387979A (en) 1980-07-03
AU524255B2 true AU524255B2 (en) 1982-09-09

Family

ID=3767901

Family Applications (1)

Application Number Title Priority Date Filing Date
AU53879/79A Ceased AU524255B2 (en) 1978-12-29 1978-12-29 Deployable wing

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)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU589730B2 (en) * 1985-11-14 1989-10-19 Grumman Aerospace Corporation Torsion spring powered missile wing deployment system
CN105691593A (en) * 2016-03-11 2016-06-22 胡建令 Folding-wing unmanned aerial vehicle
CN105711812A (en) * 2016-03-11 2016-06-29 胡建令 Folding wing unmanned aerial vehicle for municipal garden
CN105799911A (en) * 2016-05-10 2016-07-27 仲松梅 Folding-wing unmanned plane for energy-saving and environment-friendly constructional engineering
CN105857574A (en) * 2016-05-10 2016-08-17 仲松梅 Unmanned aerial vehicle for municipal building
CN105905276A (en) * 2016-05-10 2016-08-31 仲松梅 Folding wing unmanned aerial vehicle for constructional engineering
CN105947209A (en) * 2016-05-10 2016-09-21 仲松梅 Energy-saving environment-friendly type building municipal unmanned plane
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

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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.
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
ES2349503T3 (en) 2000-02-01 2011-01-04 United Video Properties, Inc. METHODS AND SYSTEMS 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
CN105865271B (en) * 2016-05-27 2017-09-05 中国人民解放军国防科学技术大学 A portable missile with rapidly inflatable wings
CN108548457B (en) * 2018-03-20 2023-12-05 浙江理工大学 A single power source synchronously driven secondary folding and unfolding mechanism for missiles
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
CN112896487B (en) * 2021-01-28 2022-10-21 西安电子科技大学 A UAV 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
CN114485288B (en) * 2021-12-27 2024-05-28 西安现代控制技术研究所 Unfolding and locking method for small-caliber projectile body-large-span space folding tail wing
CN114852314A (en) * 2022-05-20 2022-08-05 大连海事大学 An air-dropped underwater glider that reduces the impact load of folding wings
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
CN118270226B (en) * 2024-06-04 2024-08-06 西安羚控电子科技有限公司 Folding and unfolding device of aircraft
CN119389485B (en) * 2024-12-26 2025-03-11 西北工业大学 Control and unfolding locking system suitable for n-shaped folding wing of tube-jet unmanned aerial vehicle

Family Cites Families (16)

* Cited by examiner, † Cited by third party
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
NL104379C (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

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU589730B2 (en) * 1985-11-14 1989-10-19 Grumman Aerospace Corporation Torsion spring powered missile wing deployment system
CN105691593A (en) * 2016-03-11 2016-06-22 胡建令 Folding-wing unmanned aerial vehicle
CN105711812A (en) * 2016-03-11 2016-06-29 胡建令 Folding wing unmanned aerial vehicle for municipal garden
CN105711812B (en) * 2016-03-11 2017-09-29 深圳市国艺园林建设有限公司 A folding-wing unmanned aerial vehicle for municipal gardens
CN105799911A (en) * 2016-05-10 2016-07-27 仲松梅 Folding-wing unmanned plane for energy-saving and environment-friendly constructional engineering
CN105857574A (en) * 2016-05-10 2016-08-17 仲松梅 Unmanned aerial vehicle for municipal building
CN105905276A (en) * 2016-05-10 2016-08-31 仲松梅 Folding wing unmanned aerial vehicle for constructional engineering
CN105947209A (en) * 2016-05-10 2016-09-21 仲松梅 Energy-saving environment-friendly type building municipal 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
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
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

Also Published As

Publication number Publication date
EP0013096B1 (en) 1983-04-13
EP0013096A1 (en) 1980-07-09
DE2965231D1 (en) 1983-05-19
JPS5592900A (en) 1980-07-14
AU5387979A (en) 1980-07-03
CA1113070A (en) 1981-11-24

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