NO20053824L - Vingeanordning. - Google Patents

Vingeanordning.

Info

Publication number
NO20053824L
NO20053824L NO20053824A NO20053824A NO20053824L NO 20053824 L NO20053824 L NO 20053824L NO 20053824 A NO20053824 A NO 20053824A NO 20053824 A NO20053824 A NO 20053824A NO 20053824 L NO20053824 L NO 20053824L
Authority
NO
Norway
Prior art keywords
wing
winger
projectile
longitudinal axis
wing element
Prior art date
Application number
NO20053824A
Other languages
English (en)
Other versions
NO20053824D0 (no
Inventor
Erich Locher
Michael Feuerstein
Original Assignee
Diehl Bgt Defence Gmbh & Co Kg
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 Diehl Bgt Defence Gmbh & Co Kg filed Critical Diehl Bgt Defence Gmbh & Co Kg
Publication of NO20053824D0 publication Critical patent/NO20053824D0/no
Publication of NO20053824L publication Critical patent/NO20053824L/no

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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)

Abstract

Oppfinnelsen vedrører en vingeanordning (10) for et prosjektil omfattende to vingeelementer (12, 14), med hvilken et første vingeelement (12) er utfoldbart festet langs dets lengdeakse via en forbindelsesinnretning (24) ved prosjektilet, og med hvilken det andre svingeelementet (14) er således forbundet med det første vingeelementet (12), at det er svingbart om en akse som står loddrett i forhold til lengdeaksen for det første vingeelementet (12).
NO20053824A 2004-08-16 2005-08-15 Vingeanordning. NO20053824L (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200410039770 DE102004039770A1 (de) 2004-08-16 2004-08-16 Flügelanordnung

Publications (2)

Publication Number Publication Date
NO20053824D0 NO20053824D0 (no) 2005-08-15
NO20053824L true NO20053824L (no) 2006-02-17

Family

ID=35295672

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20053824A NO20053824L (no) 2004-08-16 2005-08-15 Vingeanordning.

Country Status (3)

Country Link
EP (1) EP1628112A1 (no)
DE (1) DE102004039770A1 (no)
NO (1) NO20053824L (no)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007002948B4 (de) 2007-01-19 2009-04-02 Diehl Bgt Defence Gmbh & Co. Kg Vorrichtung zur Tragflächenentfaltung
IL189785A (en) 2008-02-26 2013-07-31 Elbit Systems Ltd Foldable and layout board
US8847134B2 (en) 2012-02-16 2014-09-30 Lockheed Martin Corporation Deployable wing and fin control surface actuation
RU2549047C1 (ru) * 2014-03-04 2015-04-20 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Устройство фиксации сложенных аэродинамических поверхностей летательного аппарата
DE102015004703B4 (de) * 2014-12-11 2019-12-12 Mbda Deutschland Gmbh Klappflügelsystem
EP3032213B1 (de) 2014-12-11 2018-06-20 MBDA Deutschland GmbH Klappflügelsystem
CN104677200B (zh) * 2015-01-21 2016-05-18 浙江理工大学 一种二次折叠翼面横向展开机构
FR3035493B1 (fr) * 2015-04-21 2018-09-14 Nexter Munitions Projectile balistique comprenant un mecanisme d'ouverture d'ailes et procede d'utilisation d'un tel projectile balistique
DE102015014794A1 (de) * 2015-08-25 2017-03-02 Diehl Bgt Defence Gmbh & Co. Kg Flügelanordnung und Flugkörper mit Flügelanordnung
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)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1199664B (de) * 1962-09-11 1965-08-26 Dynamit Nobel Ag Klappleitwerk, insbesondere fuer Raketengeschosse
US3633846A (en) * 1970-05-28 1972-01-11 Us Navy Expandable aerodynamic fin
DE2635676A1 (de) * 1976-08-07 1978-02-09 Dynamit Nobel Ag Leitwerk fuer raketen
DE2649643A1 (de) * 1976-10-29 1978-06-15 Messerschmitt Boelkow Blohm Raketengetriebener flugkoerper mit entfaltbaren stabilisierungsflaechen
DE3010027C2 (de) * 1978-09-26 1985-07-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schwenkbare Anordnung eines Leitwerks, insbesondere bei Flugkörpern oder Geschossen
AU524255B2 (en) * 1978-12-29 1982-09-09 Commonwealth Of Australia, The Deployable wing
DE2926933A1 (de) * 1979-07-04 1981-01-22 Grs Ges Fuer Raketen Systeme M Stabilisierungseinrichtung mit ausklappbaren starren stabilisierungsflaechen
DE3417082A1 (de) * 1984-05-09 1985-11-14 Diehl GmbH & Co, 8500 Nürnberg Klapp-fluegel, insbesondere fuer ein geschoss
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

Also Published As

Publication number Publication date
NO20053824D0 (no) 2005-08-15
EP1628112A1 (de) 2006-02-22
DE102004039770A1 (de) 2006-03-02

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Legal Events

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FC2A Withdrawal, rejection or dismissal of laid open patent application