NO20072442L - Device for folding wings on an aircraft body - Google Patents

Device for folding wings on an aircraft body

Info

Publication number
NO20072442L
NO20072442L NO20072442A NO20072442A NO20072442L NO 20072442 L NO20072442 L NO 20072442L NO 20072442 A NO20072442 A NO 20072442A NO 20072442 A NO20072442 A NO 20072442A NO 20072442 L NO20072442 L NO 20072442L
Authority
NO
Norway
Prior art keywords
wings
aircraft body
folding wings
wing
fixtures
Prior art date
Application number
NO20072442A
Other languages
Norwegian (no)
Other versions
NO339122B1 (en
Inventor
Juergen Ruehe
Friedrich Plank
Original Assignee
Lfk 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 Gmbh filed Critical Lfk Gmbh
Publication of NO20072442L publication Critical patent/NO20072442L/en
Publication of NO339122B1 publication Critical patent/NO339122B1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/16Wrap-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.
NO20072442A 2006-05-12 2007-05-11 Device by folding wings on a fuselage NO339122B1 (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 (2)

Publication Number Publication Date
NO20072442L true NO20072442L (en) 2007-11-13
NO339122B1 NO339122B1 (en) 2016-11-14

Family

ID=38038728

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20072442A NO339122B1 (en) 2006-05-12 2007-05-11 Device by folding wings on a fuselage

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
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
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
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
NL236992A (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
NO339122B1 (en) 2016-11-14
DE502007000219D1 (en) 2008-12-18
EP1855076B1 (en) 2008-11-05
DE102006022248B3 (en) 2007-11-08
EP1855076A1 (en) 2007-11-14

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Legal Events

Date Code Title Description
CHAD Change of the owner's name or address (par. 44 patent law, par. patentforskriften)

Owner name: LFK LENKFLUGKOERPERSYSTEME GMBH, DE

CHAD Change of the owner's name or address (par. 44 patent law, par. patentforskriften)

Owner name: MBDA DEUTSCHLAND GMBH, DE

MM1K Lapsed by not paying the annual fees