IL78442A - Penguin missile folding wing configuration - Google Patents
Penguin missile folding wing configurationInfo
- Publication number
- IL78442A IL78442A IL78442A IL7844286A IL78442A IL 78442 A IL78442 A IL 78442A IL 78442 A IL78442 A IL 78442A IL 7844286 A IL7844286 A IL 7844286A IL 78442 A IL78442 A IL 78442A
- Authority
- IL
- Israel
- Prior art keywords
- penguin
- folding wing
- wing configuration
- missile folding
- missile
- Prior art date
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
- F42B10/16—Wrap-around 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)
- Toys (AREA)
- Floor Finish (AREA)
- Aerials With Secondary Devices (AREA)
- Knives (AREA)
- Fluid-Damping Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/764,457 US4717093A (en) | 1985-08-12 | 1985-08-12 | Penguin missile folding wing configuration |
Publications (1)
Publication Number | Publication Date |
---|---|
IL78442A true IL78442A (en) | 1991-01-31 |
Family
ID=25070782
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IL78442A IL78442A (en) | 1985-08-12 | 1986-04-08 | Penguin missile folding wing configuration |
Country Status (8)
Country | Link |
---|---|
US (1) | US4717093A (fr) |
EP (1) | EP0214888B1 (fr) |
JP (1) | JPH073320B2 (fr) |
AU (1) | AU587817B2 (fr) |
CA (1) | CA1267036A (fr) |
DE (1) | DE3685070D1 (fr) |
IL (1) | IL78442A (fr) |
NO (1) | NO167531C (fr) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5085381A (en) * | 1991-03-29 | 1992-02-04 | The United States Of America As Represented By The Secretary Of The Air Force | Deployable aerodynamic aerosurface |
IL101730A (en) * | 1992-04-30 | 1995-12-31 | Israel State | Moving body such as missile having wings erectable upon acceleration |
GB2274904A (en) * | 1993-02-05 | 1994-08-10 | British Aerospace | Deployable wing |
US5372336A (en) * | 1993-04-05 | 1994-12-13 | Grumman Aerospace Corporation | Folding wing assembly |
US5816532A (en) * | 1996-12-17 | 1998-10-06 | Northrop Grumman Corporation | Multiposition folding control surface for improved launch stability in missiles |
US7059566B2 (en) * | 2003-06-20 | 2006-06-13 | The United States Of America As Represented By The Secretary Of The Navy | Unmanned aerial vehicle for logistical delivery |
US7083140B1 (en) * | 2004-09-14 | 2006-08-01 | The United States Of America As Represented By The Secretary Of The Army | Full-bore artillery projectile fin development device and method |
CN102230765B (zh) * | 2011-05-26 | 2013-10-16 | 浙江理工大学 | 直连式折叠翼纵向展开机构 |
CN102226671B (zh) * | 2011-05-26 | 2013-03-13 | 浙江理工大学 | 冗余锁定式折叠翼纵向展开机构 |
GB201209697D0 (en) * | 2012-05-31 | 2012-07-18 | Airbus Uk Ltd | Method of coupling aerofoil surface structures and an aerofoil assembly |
RU2500575C1 (ru) * | 2012-07-26 | 2013-12-10 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") | Устройство фиксации сложенных аэродинамических поверхностей летательного аппарата |
CN103292639A (zh) * | 2013-06-09 | 2013-09-11 | 江西洪都航空工业集团有限责任公司 | 一种导弹用驱动装置机构锁紧 |
CN104976926B (zh) * | 2015-07-15 | 2017-07-21 | 江西洪都航空工业集团有限责任公司 | 一种弹翼单侧翼面折叠机构 |
US10150556B2 (en) | 2016-05-23 | 2018-12-11 | The Boeing Company | Low-profile wing hinge mechanism |
EP3403922A1 (fr) | 2017-05-18 | 2018-11-21 | Airbus Operations GmbH | Agencement d'une aile pour un aéronef |
GB2568738A (en) * | 2017-11-27 | 2019-05-29 | Airbus Operations Ltd | An improved interface between an outer end of a wing and a moveable wing tip device |
FR3074477B1 (fr) * | 2017-12-06 | 2019-12-20 | Airbus Operations | Avion a configuration evolutive en vol |
GB2572150A (en) * | 2018-03-19 | 2019-09-25 | Airbus Operations Ltd | A moveable wing tip device an outer end of a wing, and interface therebetween |
US11440638B2 (en) * | 2018-05-03 | 2022-09-13 | Airbus Operations Gmbh | Wing for an aircraft |
CN110525635A (zh) * | 2018-05-25 | 2019-12-03 | 空中客车德国运营有限责任公司 | 用于飞行器的机翼和飞行器 |
US11319054B2 (en) * | 2018-05-31 | 2022-05-03 | Airbus Operations Gmbh | Wing arrangement for an aircraft |
GB2574391A (en) * | 2018-05-31 | 2019-12-11 | Airbus Operations Ltd | An aircraft wing and wing tip device |
US11370526B2 (en) * | 2018-05-31 | 2022-06-28 | Airbus Operations Gmbh | Latching device for a wing arrangement for an aircraft |
US11214353B2 (en) * | 2018-06-01 | 2022-01-04 | Airbus Operations Gmbh | Wing arrangement for an aircraft and aircraft |
EP3587252A1 (fr) * | 2018-06-28 | 2020-01-01 | Airbus Operations GmbH | Système d'arrêt pour arrêter un premier composant d'aéronef par rapport à un second composant d'aéronef |
RU2708108C1 (ru) * | 2018-10-17 | 2019-12-04 | Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации | Устройство фиксации в сложенном положении консолей крыла летательного аппарата |
CN109631685B (zh) * | 2018-11-28 | 2021-06-29 | 湖北航天技术研究院总体设计所 | 一种栅格舵的折叠展开装置 |
CN109631683B (zh) * | 2018-11-28 | 2021-06-29 | 湖北航天技术研究院总体设计所 | 一种栅格舵的折叠展开装置 |
US11644287B2 (en) | 2019-06-13 | 2023-05-09 | Raytheon Company | Single-actuator rotational deployment mechanism for multiple objects |
US11592272B2 (en) * | 2021-01-26 | 2023-02-28 | Raytheon Company | Aero-assisted missile fin or wing deployment system |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3125956A (en) | 1964-03-24 | Fold able fin | ||
US2468425A (en) * | 1945-07-20 | 1949-04-26 | Carpenter Joseph David | Airplane wing folding mechanism |
US2719682A (en) * | 1953-02-16 | 1955-10-04 | Alfred J Handel | Foldable aircraft wing with mechanism for operating and locking the outboard section thereof |
US4228737A (en) | 1954-10-27 | 1980-10-21 | Aai Corporation | Glide bomb |
US2876677A (en) * | 1956-08-27 | 1959-03-10 | Northrop Aircraft Inc | Airborne missile to carrier aircraft attachment arrangement |
US2925233A (en) * | 1957-02-18 | 1960-02-16 | Chance Vought Aircraft Inc | Aircraft wing fold system |
US2925966A (en) * | 1957-10-08 | 1960-02-23 | Kongelbeck Sverre | Folding fin or wing for missiles |
US2977880A (en) * | 1959-04-07 | 1961-04-04 | Richard B Kershner | Fin erector |
NL101734C (fr) * | 1959-04-13 | |||
US3063375A (en) * | 1960-05-19 | 1962-11-13 | Wilbur W Hawley | Folding fin |
US3065938A (en) * | 1960-05-25 | 1962-11-27 | Eugene M Calkins | Telescoping sectional airplane wing |
US3304030A (en) * | 1965-09-24 | 1967-02-14 | James E Weimholt | Pyrotechnic-actuated folding fin assembly |
CH480613A (de) * | 1967-09-11 | 1969-10-31 | Oerlikon Buehrle Ag | Geschoss mit Bremsflügeln |
US3724373A (en) * | 1970-12-15 | 1973-04-03 | Atomic Energy Commission | Retarded glide bomb |
FR2221707B1 (fr) | 1973-03-14 | 1976-04-30 | France Etat | |
FR2356118A1 (fr) * | 1976-06-25 | 1978-01-20 | Europ Propulsion | Empennage pour projectile |
DE2649643A1 (de) * | 1976-10-29 | 1978-06-15 | Messerschmitt Boelkow Blohm | Raketengetriebener flugkoerper mit entfaltbaren stabilisierungsflaechen |
DE7804927U1 (de) * | 1978-02-18 | 1978-06-01 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Vorrichtung zum ausklappen von schwenkfluegeln |
DE2935044A1 (de) * | 1979-08-30 | 1981-03-19 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | Unbemannter, aus einem transportbehaelter zu startender flugkoerper |
US4523728A (en) * | 1983-03-07 | 1985-06-18 | Ford Aerospace & Communications Corporation | Passive auto-erecting alignment wings for long rod penetrator |
DE3403508A1 (de) * | 1984-02-02 | 1985-08-08 | Dynamit Nobel Ag, 5210 Troisdorf | Flugkoerper |
-
1985
- 1985-08-12 US US06/764,457 patent/US4717093A/en not_active Expired - Fee Related
-
1986
- 1986-04-08 IL IL78442A patent/IL78442A/xx not_active IP Right Cessation
- 1986-04-16 AU AU56160/86A patent/AU587817B2/en not_active Ceased
- 1986-05-12 CA CA000508866A patent/CA1267036A/fr not_active Expired - Fee Related
- 1986-07-08 JP JP61158905A patent/JPH073320B2/ja not_active Expired - Lifetime
- 1986-08-01 DE DE8686401733T patent/DE3685070D1/de not_active Expired - Fee Related
- 1986-08-01 EP EP86401733A patent/EP0214888B1/fr not_active Expired - Lifetime
- 1986-08-11 NO NO863224A patent/NO167531C/no unknown
Also Published As
Publication number | Publication date |
---|---|
EP0214888A3 (en) | 1987-11-11 |
EP0214888B1 (fr) | 1992-04-29 |
EP0214888A2 (fr) | 1987-03-18 |
NO863224D0 (no) | 1986-08-11 |
AU5616086A (en) | 1987-02-19 |
US4717093A (en) | 1988-01-05 |
JPS6239398A (ja) | 1987-02-20 |
NO167531B (no) | 1991-08-05 |
NO863224L (no) | 1987-02-13 |
JPH073320B2 (ja) | 1995-01-18 |
CA1267036A (fr) | 1990-03-27 |
NO167531C (no) | 1991-11-13 |
AU587817B2 (en) | 1989-08-31 |
DE3685070D1 (de) | 1992-06-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
KB | Patent renewed | ||
RH | Patent void |