RU2018143495A3 - - Google Patents
Download PDFInfo
- Publication number
- RU2018143495A3 RU2018143495A3 RU2018143495A RU2018143495A RU2018143495A3 RU 2018143495 A3 RU2018143495 A3 RU 2018143495A3 RU 2018143495 A RU2018143495 A RU 2018143495A RU 2018143495 A RU2018143495 A RU 2018143495A RU 2018143495 A3 RU2018143495 A3 RU 2018143495A3
- Authority
- RU
- Russia
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)
- Air Bags (AREA)
- Seats For Vehicles (AREA)
- Connection Of Plates (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IN201611024976 | 2016-07-21 | ||
| IN201611024976 | 2016-07-21 | ||
| PCT/IB2017/054165 WO2018015838A1 (en) | 2016-07-21 | 2017-07-11 | Bi-directional wing unfolding mechanism |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| RU2018143495A RU2018143495A (ru) | 2020-08-21 |
| RU2018143495A3 true RU2018143495A3 (ru) | 2020-08-21 |
| RU2736430C2 RU2736430C2 (ru) | 2020-11-17 |
Family
ID=60991989
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2018143495A RU2736430C2 (ru) | 2016-07-21 | 2017-07-11 | Механизм двухступенчатого раскрытия крыла |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US11175117B2 (ru) |
| EP (1) | EP3488176B1 (ru) |
| AU (1) | AU2017300113B2 (ru) |
| RU (1) | RU2736430C2 (ru) |
| WO (1) | WO2018015838A1 (ru) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102020105188B4 (de) | 2020-02-27 | 2023-08-31 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Flugkörper-Finnenausklappeinrichtung, Flugkörper und Verfahren zum Betrieb eines Flugkörpers |
| SE544263C2 (en) | 2020-07-03 | 2022-03-22 | Saab Ab | A wing arrangement, a projectile, a method for deploying a wing blade, a use and a method for assembly |
| CN112078766B (zh) * | 2020-08-17 | 2023-06-02 | 河北汉光重工有限责任公司 | 一种水下航行器 |
| CN113148111A (zh) * | 2021-04-29 | 2021-07-23 | 四川傲势科技有限公司 | 一种无人机的折叠展开机构 |
| CN114537640B (zh) * | 2022-02-15 | 2023-08-25 | 中天长光(青岛)装备科技有限公司 | 一种双自由度折叠翼机构 |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3063375A (en) * | 1960-05-19 | 1962-11-13 | Wilbur W Hawley | Folding fin |
| CH479849A (it) * | 1967-07-22 | 1969-10-15 | Bombrini Parodi Delfino Spa | Porietto autopropulso o semiautopropulso con governale ad alette retrattili |
| US4323208A (en) * | 1980-02-01 | 1982-04-06 | British Aerospace | Folding fins |
| US4664339A (en) * | 1984-10-11 | 1987-05-12 | The Boeing Company | Missile appendage deployment mechanism |
| US4667899A (en) * | 1984-11-28 | 1987-05-26 | General Dynamics, Pomona Division | Double swing wing self-erecting missile wing structure |
| US4869442A (en) * | 1988-09-02 | 1989-09-26 | Aerojet-General Corporation | Self-deploying airfoil |
| IL101730A (en) * | 1992-04-30 | 1995-12-31 | Israel State | Moving body such as missile having wings erectable upon acceleration |
| RU199U1 (ru) * | 1993-08-10 | 1995-01-16 | Машиностроительное Конструкторское Бюро "Факел" | Механизм раскрытия крыльев |
| US5762294A (en) * | 1997-03-31 | 1998-06-09 | The United States Of America As Represented By The Secretary Of The Army | Wing deployment device |
| US6092264A (en) * | 1998-11-13 | 2000-07-25 | Lockheed Martin Corporation | Single axis fold actuator and lock for member |
| US6761331B2 (en) * | 2002-03-19 | 2004-07-13 | Raytheon Company | Missile having deployment mechanism for stowable fins |
| FR2860577B1 (fr) * | 2003-10-06 | 2006-01-27 | Giat Ind Sa | Dispositif de deploiement d'une ailette d'un projectile |
| RU2478907C1 (ru) * | 2011-12-14 | 2013-04-10 | Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" | Раскрываемое крыло двухступенчатой ракеты |
| RU2520846C1 (ru) * | 2013-03-29 | 2014-06-27 | Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" | Аэродинамический руль ракеты |
-
2017
- 2017-07-11 WO PCT/IB2017/054165 patent/WO2018015838A1/en unknown
- 2017-07-11 EP EP17830564.5A patent/EP3488176B1/en active Active
- 2017-07-11 AU AU2017300113A patent/AU2017300113B2/en active Active
- 2017-07-11 US US16/319,176 patent/US11175117B2/en active Active
- 2017-07-11 RU RU2018143495A patent/RU2736430C2/ru active
Also Published As
| Publication number | Publication date |
|---|---|
| AU2017300113B2 (en) | 2020-04-02 |
| EP3488176A4 (en) | 2020-07-29 |
| AU2017300113A1 (en) | 2018-12-20 |
| RU2018143495A (ru) | 2020-08-21 |
| EP3488176B1 (en) | 2023-04-26 |
| EP3488176A1 (en) | 2019-05-29 |
| RU2736430C2 (ru) | 2020-11-17 |
| US11175117B2 (en) | 2021-11-16 |
| WO2018015838A1 (en) | 2018-01-25 |
| US20190154420A1 (en) | 2019-05-23 |