NO20053824D0 - Winger device. - Google Patents
Winger device.Info
- Publication number
- NO20053824D0 NO20053824D0 NO20053824A NO20053824A NO20053824D0 NO 20053824 D0 NO20053824 D0 NO 20053824D0 NO 20053824 A NO20053824 A NO 20053824A NO 20053824 A NO20053824 A NO 20053824A NO 20053824 D0 NO20053824 D0 NO 20053824D0
- Authority
- NO
- Norway
- Prior art keywords
- winger
- winger device
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200410039770 DE102004039770A1 (en) | 2004-08-16 | 2004-08-16 | wing assembly |
Publications (2)
Publication Number | Publication Date |
---|---|
NO20053824D0 true NO20053824D0 (en) | 2005-08-15 |
NO20053824L NO20053824L (en) | 2006-02-17 |
Family
ID=35295672
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO20053824A NO20053824L (en) | 2004-08-16 | 2005-08-15 | Winger device. |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP1628112A1 (en) |
DE (1) | DE102004039770A1 (en) |
NO (1) | NO20053824L (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007002948B4 (en) * | 2007-01-19 | 2009-04-02 | Diehl Bgt Defence Gmbh & Co. Kg | Device for wing deployment |
IL189785A (en) | 2008-02-26 | 2013-07-31 | Elbit Systems Ltd | Foldable and deployable panel |
US8847134B2 (en) | 2012-02-16 | 2014-09-30 | Lockheed Martin Corporation | Deployable wing and fin control surface actuation |
RU2549047C1 (en) * | 2014-03-04 | 2015-04-20 | Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" | Device to lock aircraft folded airfoils |
EP3032213B1 (en) | 2014-12-11 | 2018-06-20 | MBDA Deutschland GmbH | Folding fin system |
DE102015004703B4 (en) | 2014-12-11 | 2019-12-12 | Mbda Deutschland Gmbh | Folding wing system |
CN104677200B (en) * | 2015-01-21 | 2016-05-18 | 浙江理工大学 | One twice-folded aerofoil horizontal spreading mechanism |
FR3035493B1 (en) * | 2015-04-21 | 2018-09-14 | Nexter Munitions | BALLISTIC PROJECTILE COMPRISING A WING OPENING MECHANISM AND METHOD OF USING SUCH A BALLISTIC PROJECTILE |
DE102015014794A1 (en) * | 2015-08-25 | 2017-03-02 | Diehl Bgt Defence Gmbh & Co. Kg | Wing arrangement and missile with wing arrangement |
SE544987C2 (en) * | 2020-08-19 | 2023-02-21 | Saab Ab | A wing arrangement, a projectile, a use and a method for deploying a wing blade |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1199664B (en) * | 1962-09-11 | 1965-08-26 | Dynamit Nobel Ag | Folding tail, especially for rocket projectiles |
US3633846A (en) * | 1970-05-28 | 1972-01-11 | Us Navy | Expandable aerodynamic fin |
DE2635676A1 (en) * | 1976-08-07 | 1978-02-09 | Dynamit Nobel Ag | Guide fin with extension for rocket - has sliding fin in cavity pushed out by spring force after launching |
DE2649643A1 (en) * | 1976-10-29 | 1978-06-15 | Messerschmitt Boelkow Blohm | Rocket missile extending stabilising fins - have sections extended progressively by springs and releasing charges |
DE3010027C2 (en) * | 1978-09-26 | 1985-07-11 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Pivoting arrangement of a tail unit, especially for missiles or projectiles |
AU524255B2 (en) * | 1978-12-29 | 1982-09-09 | Commonwealth Of Australia, The | Deployable wing |
DE2926933A1 (en) * | 1979-07-04 | 1981-01-22 | Grs Ges Fuer Raketen Systeme M | Missile stabilising mechanism with extensible rigid fins - which act both as braking and guide surfaces according to adjusted position |
DE3417082A1 (en) * | 1984-05-09 | 1985-11-14 | Diehl GmbH & Co, 8500 Nürnberg | FOLDING WING, IN PARTICULAR FOR ONE STOREY |
US4667899A (en) * | 1984-11-28 | 1987-05-26 | General Dynamics, Pomona Division | Double swing wing self-erecting missile wing structure |
US4778127A (en) * | 1986-09-02 | 1988-10-18 | United Technologies Corporation | Missile fin deployment device |
-
2004
- 2004-08-16 DE DE200410039770 patent/DE102004039770A1/en not_active Ceased
-
2005
- 2005-08-03 EP EP05016830A patent/EP1628112A1/en not_active Withdrawn
- 2005-08-15 NO NO20053824A patent/NO20053824L/en not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
DE102004039770A1 (en) | 2006-03-02 |
NO20053824L (en) | 2006-02-17 |
EP1628112A1 (en) | 2006-02-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FC2A | Withdrawal, rejection or dismissal of laid open patent application |