DE502007000219D1 - Winding wings of a missile - Google Patents

Winding wings of a missile

Info

Publication number
DE502007000219D1
DE502007000219D1 DE502007000219T DE502007000219T DE502007000219D1 DE 502007000219 D1 DE502007000219 D1 DE 502007000219D1 DE 502007000219 T DE502007000219 T DE 502007000219T DE 502007000219 T DE502007000219 T DE 502007000219T DE 502007000219 D1 DE502007000219 D1 DE 502007000219D1
Authority
DE
Germany
Prior art keywords
wings
missile
wing
fixtures
rest position
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.)
Active
Application number
DE502007000219T
Other languages
German (de)
Inventor
Juergen Ruehe
Friedrich Plank
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.)
LFK Lenkflugkoerpersysteme GmbH
Original Assignee
LFK Lenkflugkoerpersysteme GmbH
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 LFK Lenkflugkoerpersysteme GmbH filed Critical LFK Lenkflugkoerpersysteme GmbH
Publication of DE502007000219D1 publication Critical patent/DE502007000219D1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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

Abstract

A device on wrapped wings (1, 2, 3) of a flying object (5) having n (at least 2) wings rotatably mounted on the object outer surface on axes in the flying direction, lying on the surface in rest position and opened by a drive into working position, comprises first fixtures on the tip side regions of (n - 1) wings, corresponding in the rest position to further fixtures on the outer side of the wing underneath and gripping a controlled-release holder on the tip side region of the n'th wing.
DE502007000219T 2006-05-12 2007-05-04 Winding wings of a missile Active DE502007000219D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102006022248A DE102006022248B3 (en) 2006-05-12 2006-05-12 Retaining device on wrapped wings of flying object, allowing reliable release of wings into working position, comprises controlled release holder on one wing and cooperating fixtures on others

Publications (1)

Publication Number Publication Date
DE502007000219D1 true DE502007000219D1 (en) 2008-12-18

Family

ID=38038728

Family Applications (2)

Application Number Title Priority Date Filing Date
DE102006022248A Expired - Fee Related DE102006022248B3 (en) 2006-05-12 2006-05-12 Retaining device on wrapped wings of flying object, allowing reliable release of wings into working position, comprises controlled release holder on one wing and cooperating fixtures on others
DE502007000219T Active DE502007000219D1 (en) 2006-05-12 2007-05-04 Winding wings of a missile

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE102006022248A Expired - Fee Related DE102006022248B3 (en) 2006-05-12 2006-05-12 Retaining device on wrapped wings of flying object, allowing reliable release of wings into working position, comprises controlled release holder on one wing and cooperating fixtures on others

Country Status (4)

Country Link
EP (1) EP1855076B1 (en)
AT (1) ATE413580T1 (en)
DE (2) DE102006022248B3 (en)
NO (1) NO339122B1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2911954B1 (en) * 2007-01-31 2009-04-24 Nexter Munitions Sa DEVICE FOR CONTROLLING AMMUNITION WITH DEPLOYABLE GOVERNMENTS
US8899515B2 (en) * 2012-05-18 2014-12-02 Textron Systems Corporation Folding configuration for air vehicle
DE102015014368A1 (en) 2015-11-06 2017-05-11 Mbda Deutschland Gmbh Folding wing for a missile and a missile with at least one folding wing arranged thereon
DE102015014367B4 (en) 2015-11-06 2020-07-16 Mbda Deutschland Gmbh Folding wing for a missile and missile with at least one folding wing arranged thereon
DE102017113058B4 (en) 2017-06-14 2023-04-27 Deutsches Zentrum für Luft- und Raumfahrt e.V. space transport aircraft

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE533456A (en) * 1953-12-21 Brandt Soc Nouv Ets
US4004514A (en) * 1976-01-20 1977-01-25 The United States Of America As Represented By The Secretary Of The Navy Roll rate stabilized wrap around missile fins
FR2356118A1 (en) * 1976-06-25 1978-01-20 Europ Propulsion EMPENNAGE FOR PROJECTILE
DE8428118U1 (en) * 1984-09-25 1986-07-03 Rheinmetall GmbH, 4000 Düsseldorf Tail unit with deployable wings
FR2659433B1 (en) * 1990-03-09 1992-05-15 Thomson Brandt Armements IMPROVEMENTS ON FENDERING WING TANKS.
JP3781311B2 (en) * 1995-12-01 2006-05-31 株式会社小松製作所 Aircraft wing device

Also Published As

Publication number Publication date
ATE413580T1 (en) 2008-11-15
DE102006022248B3 (en) 2007-11-08
EP1855076A1 (en) 2007-11-14
NO20072442L (en) 2007-11-13
NO339122B1 (en) 2016-11-14
EP1855076B1 (en) 2008-11-05

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition