EP2083238A3 - Aile pliable dotée d'un dispositif de dépliage - Google Patents
Aile pliable dotée d'un dispositif de dépliage Download PDFInfo
- Publication number
- EP2083238A3 EP2083238A3 EP09000744.4A EP09000744A EP2083238A3 EP 2083238 A3 EP2083238 A3 EP 2083238A3 EP 09000744 A EP09000744 A EP 09000744A EP 2083238 A3 EP2083238 A3 EP 2083238A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- wing
- unfolding device
- folding
- folding fin
- folding 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.)
- Granted
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
-
- 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)
- Storing, Repeated Paying-Out, And Re-Storing Of Elongated Articles (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200810005705 DE102008005705A1 (de) | 2008-01-24 | 2008-01-24 | Klappflügel mit Entfaltvorrichtung |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2083238A2 EP2083238A2 (fr) | 2009-07-29 |
EP2083238A3 true EP2083238A3 (fr) | 2013-05-22 |
EP2083238B1 EP2083238B1 (fr) | 2014-01-08 |
Family
ID=40578683
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20090000744 Ceased EP2083238B1 (fr) | 2008-01-24 | 2009-01-21 | Aile pliable dotée d'un dispositif de dépliage |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP2083238B1 (fr) |
DE (2) | DE202008018033U1 (fr) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104677199B (zh) * | 2015-01-21 | 2016-07-13 | 浙江理工大学 | 一种单驱动多折叠舵面同步展开机构 |
DE102015014368A1 (de) | 2015-11-06 | 2017-05-11 | Mbda Deutschland Gmbh | Klappflügel für einen Flugkörper sowie einen Flugkörper mit mindestens einem daran angeordneten Klappflügel |
DE102015014367B4 (de) | 2015-11-06 | 2020-07-16 | Mbda Deutschland Gmbh | Klappflügel für einen Flugkörper und Flugkörper mit mindestens einem daran angeordneten Klappflügel |
DE102017113058B4 (de) | 2017-06-14 | 2023-04-27 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Raumtransport-Fluggerät |
CN108688793B (zh) * | 2018-07-27 | 2023-11-24 | 中国工程物理研究院总体工程研究所 | 筒式发射无人机机翼折叠展开机构 |
US11685510B2 (en) | 2018-11-01 | 2023-06-27 | Viettel Group | Wing deployment mechanism and design method using pneumatic technique |
RU2730903C1 (ru) * | 2019-09-10 | 2020-08-26 | Акционерное общество "Машиностроительное конструкторское бюро "Факел" имени Академика П.Д. Грушина" | Механизм раскрытия и стопорения аэродинамического руля с двумя осями складывания |
CN112985190A (zh) * | 2021-04-13 | 2021-06-18 | 西安航天动力技术研究所 | 一种涡卷弹簧式折叠弹翼展开机构 |
RU2770956C1 (ru) * | 2021-12-21 | 2022-04-25 | Акционерное общество "Машиностроительное конструкторское бюро "Факел" имени академика П.Д. Грушина | Механизм раскрытия и стопорения рулей с двумя складывающимися секциями |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2045687A1 (de) * | 1970-09-16 | 1972-03-23 | Dynamit Nobel Ag | Thermische Auslösung von Flugkörperfunktionen |
GB2140136A (en) * | 1983-05-14 | 1984-11-21 | British Aerospace | Folding fin assembly for missiles |
DE3838735A1 (de) * | 1988-11-15 | 1990-05-31 | Diehl Gmbh & Co | Klapp-fluegel, insbesondere fuer ein geschoss |
US5762294A (en) * | 1997-03-31 | 1998-06-09 | The United States Of America As Represented By The Secretary Of The Army | Wing deployment device |
GB2369177A (en) * | 1989-06-02 | 2002-05-22 | British Aerospace | Aerofoil deployment system |
US20040159227A1 (en) * | 2003-02-18 | 2004-08-19 | Lockheed Martin Corporation | Apparatus and method for restraining and releasing a control surface |
-
2008
- 2008-01-24 DE DE202008018033U patent/DE202008018033U1/de not_active Expired - Lifetime
- 2008-01-24 DE DE200810005705 patent/DE102008005705A1/de not_active Ceased
-
2009
- 2009-01-21 EP EP20090000744 patent/EP2083238B1/fr not_active Ceased
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2045687A1 (de) * | 1970-09-16 | 1972-03-23 | Dynamit Nobel Ag | Thermische Auslösung von Flugkörperfunktionen |
GB2140136A (en) * | 1983-05-14 | 1984-11-21 | British Aerospace | Folding fin assembly for missiles |
DE3838735A1 (de) * | 1988-11-15 | 1990-05-31 | Diehl Gmbh & Co | Klapp-fluegel, insbesondere fuer ein geschoss |
GB2369177A (en) * | 1989-06-02 | 2002-05-22 | British Aerospace | Aerofoil deployment system |
US5762294A (en) * | 1997-03-31 | 1998-06-09 | The United States Of America As Represented By The Secretary Of The Army | Wing deployment device |
US20040159227A1 (en) * | 2003-02-18 | 2004-08-19 | Lockheed Martin Corporation | Apparatus and method for restraining and releasing a control surface |
Also Published As
Publication number | Publication date |
---|---|
DE102008005705A1 (de) | 2009-07-30 |
EP2083238A2 (fr) | 2009-07-29 |
DE202008018033U1 (de) | 2011-04-14 |
EP2083238B1 (fr) | 2014-01-08 |
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