DE3569151D1 - Tail unit with collapsible wings - Google Patents

Tail unit with collapsible wings

Info

Publication number
DE3569151D1
DE3569151D1 DE8585904619T DE3569151T DE3569151D1 DE 3569151 D1 DE3569151 D1 DE 3569151D1 DE 8585904619 T DE8585904619 T DE 8585904619T DE 3569151 T DE3569151 T DE 3569151T DE 3569151 D1 DE3569151 D1 DE 3569151D1
Authority
DE
Germany
Prior art keywords
tail unit
collapsible wings
collapsible
wings
tail
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.)
Expired
Application number
DE8585904619T
Other languages
English (en)
Inventor
Dieter Boder
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
Priority to DE8585904619T priority Critical patent/DE3569151D1/de
Application granted granted Critical
Publication of DE3569151D1 publication Critical patent/DE3569151D1/de
Expired 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)
  • Pivots And Pivotal Connections (AREA)
  • Tents Or Canopies (AREA)
DE8585904619T 1984-09-25 1985-09-06 Tail unit with collapsible wings Expired DE3569151D1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE8585904619T DE3569151D1 (en) 1984-09-25 1985-09-06 Tail unit with collapsible wings

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE3435063 1984-09-25
DE8585904619T DE3569151D1 (en) 1984-09-25 1985-09-06 Tail unit with collapsible wings
PCT/EP1985/000452 WO1986002154A1 (en) 1984-09-25 1985-09-06 Tail unit with collapsible wings

Publications (1)

Publication Number Publication Date
DE3569151D1 true DE3569151D1 (en) 1989-05-03

Family

ID=6246238

Family Applications (3)

Application Number Title Priority Date Filing Date
DE8428118U Expired DE8428118U1 (de) 1984-09-25 1984-09-25 Leitwerk mit entfaltbaren Flügeln
DE8585904619T Expired DE3569151D1 (en) 1984-09-25 1985-09-06 Tail unit with collapsible wings
DE3533994A Expired - Fee Related DE3533994C2 (de) 1984-09-25 1985-09-24 Leitwerk mit entfaltbaren Flügeln

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE8428118U Expired DE8428118U1 (de) 1984-09-25 1984-09-25 Leitwerk mit entfaltbaren Flügeln

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE3533994A Expired - Fee Related DE3533994C2 (de) 1984-09-25 1985-09-24 Leitwerk mit entfaltbaren Flügeln

Country Status (5)

Country Link
US (1) US4699334A (de)
EP (1) EP0232267B1 (de)
DE (3) DE8428118U1 (de)
ES (1) ES296987Y (de)
WO (1) WO1986002154A1 (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3618958C1 (de) * 1986-06-05 1987-06-25 Rheinmetall Gmbh Leitwerk mit entfaltbaren Fluegeln
DE3618956C1 (de) * 1986-06-05 1987-11-19 Rheinmetall Gmbh Leitwerk mit entfaltbaren Fluegeln fuer Geschosse und Flugkoerper
US4796835A (en) * 1986-12-17 1989-01-10 The Marquardt Company Projectile
US4752052A (en) * 1986-12-17 1988-06-21 The Marquardt Company Projectile
DE3916690C1 (de) * 1989-05-23 1998-10-01 Bodenseewerk Geraetetech Ausklappbare Flügelanordnung für Flugkörper
US5615846A (en) * 1994-11-04 1997-04-01 Gec Marconi Dynamics Inc. Extendable wing for guided missles and munitions
SE508858C2 (sv) * 1997-03-25 1998-11-09 Bofors Ab Fenstabiliserad granat
SE508857C2 (sv) * 1997-03-25 1998-11-09 Bofors Ab Fenstabiliserad base-bleedgranat
US6186443B1 (en) 1998-06-25 2001-02-13 International Dynamics Corporation Airborne vehicle having deployable wing and control surface
DE102006006160B4 (de) * 2006-02-10 2017-05-24 Mbda Deutschland Gmbh Wickelflügel für einen Flugkörper
US7841559B1 (en) 2006-02-16 2010-11-30 Mbda Incorporated Aerial vehicle with variable aspect ratio deployable wings
DE102006022248B3 (de) * 2006-05-12 2007-11-08 Lfk-Lenkflugkörpersysteme Gmbh Vorrichtung an Wickelflügeln eines Flugkörpers
DE102006044945A1 (de) * 2006-09-22 2008-04-03 Lfk-Lenkflugkörpersysteme Gmbh Lagerung und Verriegelung für einen Wickelflügel
RU2453476C2 (ru) * 2010-02-08 2012-06-20 Юрий Михайлович Киселев Авиационный контейнер для эвакуации пассажиров
US8946607B2 (en) 2011-12-13 2015-02-03 The Boeing Company Mechanisms for deploying and actuating airfoil-shaped bodies on unmanned aerial vehicles
US8698059B2 (en) * 2012-05-03 2014-04-15 Raytheon Company Deployable lifting surface for air vehicle
US10124880B1 (en) * 2016-02-03 2018-11-13 Lockheed Martin Corporation Rotatable control surface assembly for an unmanned aerial vehicle
DE102017003797A1 (de) 2017-04-19 2018-10-25 Mbda Deutschland Gmbh Zweigeteilter klappflügel für flugkörperleitwerke

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE30264C (de) * CH. TH. M. V. de bange in Paris Abfeuerungsvorrichtung für Geschütze
GB189523823A (en) * 1895-12-12 1896-11-14 Martns Stevenson Calvert Improvements in Projectiles.
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
US4203569A (en) * 1977-10-17 1980-05-20 Bei Electronics, Inc. Fin and nozzle unit for a free-flight rocket
US4351499A (en) * 1979-09-24 1982-09-28 General Dynamics Double fabric, retractable, self-erecting wing for missle

Also Published As

Publication number Publication date
EP0232267B1 (de) 1989-03-29
ES296987U (es) 1988-09-01
DE3533994C2 (de) 1996-10-24
US4699334A (en) 1987-10-13
ES296987Y (es) 1989-03-16
WO1986002154A1 (en) 1986-04-10
DE3533994A1 (de) 1986-04-30
EP0232267A1 (de) 1987-08-19
DE8428118U1 (de) 1986-07-03

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: RHEINMETALL GMBH, 40882 RATINGEN, DE

8327 Change in the person/name/address of the patent owner

Owner name: RHEINMETALL INDUSTRIE GMBH, 40882 RATINGEN, DE

8327 Change in the person/name/address of the patent owner

Owner name: RHEINMETALL INDUSTRIE AG, 40882 RATINGEN, DE

8339 Ceased/non-payment of the annual fee