EP0254796A3 - Plan stabilisateur avec ailes déployables pour projectiles et missiles - Google Patents

Plan stabilisateur avec ailes déployables pour projectiles et missiles Download PDF

Info

Publication number
EP0254796A3
EP0254796A3 EP87102419A EP87102419A EP0254796A3 EP 0254796 A3 EP0254796 A3 EP 0254796A3 EP 87102419 A EP87102419 A EP 87102419A EP 87102419 A EP87102419 A EP 87102419A EP 0254796 A3 EP0254796 A3 EP 0254796A3
Authority
EP
European Patent Office
Prior art keywords
assenbly
missiles
projectiles
fin
wings
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.)
Withdrawn
Application number
EP87102419A
Other languages
German (de)
English (en)
Other versions
EP0254796A2 (fr
Inventor
Dieter Böder
Michael Primus
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.)
Rheinmetall Industrie AG
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 EP0254796A2 publication Critical patent/EP0254796A2/fr
Publication of EP0254796A3 publication Critical patent/EP0254796A3/fr
Withdrawn legal-status Critical Current

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)
EP87102419A 1986-06-05 1987-02-20 Plan stabilisateur avec ailes déployables pour projectiles et missiles Withdrawn EP0254796A3 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3618956A DE3618956C1 (de) 1986-06-05 1986-06-05 Leitwerk mit entfaltbaren Fluegeln fuer Geschosse und Flugkoerper
DE3618956 1986-06-05

Publications (2)

Publication Number Publication Date
EP0254796A2 EP0254796A2 (fr) 1988-02-03
EP0254796A3 true EP0254796A3 (fr) 1990-05-23

Family

ID=6302354

Family Applications (1)

Application Number Title Priority Date Filing Date
EP87102419A Withdrawn EP0254796A3 (fr) 1986-06-05 1987-02-20 Plan stabilisateur avec ailes déployables pour projectiles et missiles

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 (9)

* 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

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1986002154A1 (fr) * 1984-09-25 1986-04-10 Rheinmetall Gmbh Empennage avec ailes escamotables

Family Cites Families (4)

* 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

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1986002154A1 (fr) * 1984-09-25 1986-04-10 Rheinmetall Gmbh Empennage avec ailes escamotables

Also Published As

Publication number Publication date
NO871149L (no) 1987-12-07
US4736909A (en) 1988-04-12
EP0254796A2 (fr) 1988-02-03
DE3618956C1 (de) 1987-11-19
NO871149D0 (no) 1987-03-20

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Inventor name: PRIMUS, MICHAEL

Inventor name: BOEDER, DIETER