NO871149L - Styreanordning med innfoldbare vinger for prosjektil og skudd. - Google Patents

Styreanordning med innfoldbare vinger for prosjektil og skudd.

Info

Publication number
NO871149L
NO871149L NO871149A NO871149A NO871149L NO 871149 L NO871149 L NO 871149L NO 871149 A NO871149 A NO 871149A NO 871149 A NO871149 A NO 871149A NO 871149 L NO871149 L NO 871149L
Authority
NO
Norway
Prior art keywords
wing
projectile
wings
buckling
blades
Prior art date
Application number
NO871149A
Other languages
English (en)
Norwegian (no)
Other versions
NO871149D0 (no
Inventor
Dieter Boder
Michael Primus
Original Assignee
Rheinmetall 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 Rheinmetall Gmbh filed Critical Rheinmetall Gmbh
Publication of NO871149D0 publication Critical patent/NO871149D0/no
Publication of NO871149L publication Critical patent/NO871149L/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)
  • Control Of Electric Motors In General (AREA)
  • Feedback Control In General (AREA)
NO871149A 1986-06-05 1987-03-20 Styreanordning med innfoldbare vinger for prosjektil og skudd. NO871149L (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3618956A DE3618956C1 (de) 1986-06-05 1986-06-05 Leitwerk mit entfaltbaren Fluegeln fuer Geschosse und Flugkoerper

Publications (2)

Publication Number Publication Date
NO871149D0 NO871149D0 (no) 1987-03-20
NO871149L true NO871149L (no) 1987-12-07

Family

ID=6302354

Family Applications (1)

Application Number Title Priority Date Filing Date
NO871149A NO871149L (no) 1986-06-05 1987-03-20 Styreanordning med innfoldbare vinger for prosjektil og skudd.

Country Status (4)

Country Link
US (1) US4736909A (fr)
EP (1) EP0254796A3 (fr)
DE (1) DE3618956C1 (fr)
NO (1) NO871149L (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE460738B (sv) * 1988-03-16 1989-11-13 Bofors Ab Foer missiler och andra projektiler avsedd utfaellbar vinge
DE3933100A1 (de) * 1988-12-19 1990-06-28 Diehl Gmbh & Co Leitwerk fuer ein unterkalibriges uebungspfeilgeschoss
DE3916690C1 (de) * 1989-05-23 1998-10-01 Bodenseewerk Geraetetech Ausklappbare Flügelanordnung für Flugkörper
US5642867A (en) 1995-06-06 1997-07-01 Hughes Missile Systems Company Aerodynamic lifting and control surface and control system using same
US5927643A (en) * 1997-11-05 1999-07-27 Atlantic Research Corporation Self-deploying airfoil for missile or the like
US6834828B1 (en) 2003-09-23 2004-12-28 The United States Of America As Represented By The Secretary Of The Navy Fin deployment system
DE102006006160B4 (de) * 2006-02-10 2017-05-24 Mbda Deutschland Gmbh Wickelflügel für einen Flugkörper
DE102006044945A1 (de) * 2006-09-22 2008-04-03 Lfk-Lenkflugkörpersysteme Gmbh Lagerung und Verriegelung für einen Wickelflügel
US8698059B2 (en) * 2012-05-03 2014-04-15 Raytheon Company Deployable lifting surface for air vehicle
US12241727B2 (en) * 2022-12-14 2025-03-04 Raytheon Company Mechanism for securing then deploying a rotationally coupled rigid member to and from a frame via retention then release of tension in a curved member

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB745252A (en) * 1953-07-29 1956-02-22 Ml Aviation Co Ltd Improvements relating to rocket propelled projectiles
US2923241A (en) * 1957-09-09 1960-02-02 Aerojet General Co Folding stabilizing fins
US3103886A (en) * 1960-10-13 1963-09-17 Charles H Popenoe Coiling fin for tube launched missiles
DE1297514B (de) * 1965-08-03 1969-06-12 Dynamit Nobel Ag Leitwerk fuer Raketen
DE8428118U1 (de) * 1984-09-25 1986-07-03 Rheinmetall GmbH, 4000 Düsseldorf Leitwerk mit entfaltbaren Flügeln

Also Published As

Publication number Publication date
NO871149D0 (no) 1987-03-20
DE3618956C1 (de) 1987-11-19
EP0254796A3 (fr) 1990-05-23
US4736909A (en) 1988-04-12
EP0254796A2 (fr) 1988-02-03

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