CH413665A - Elastisches Klappleitwerk für bewegte Körper, insbesondere Flugkörper - Google Patents

Elastisches Klappleitwerk für bewegte Körper, insbesondere Flugkörper

Info

Publication number
CH413665A
CH413665A CH813163A CH813163A CH413665A CH 413665 A CH413665 A CH 413665A CH 813163 A CH813163 A CH 813163A CH 813163 A CH813163 A CH 813163A CH 413665 A CH413665 A CH 413665A
Authority
CH
Switzerland
Prior art keywords
moving bodies
flexible folding
folding tail
missiles
especially missiles
Prior art date
Application number
CH813163A
Other languages
English (en)
Inventor
Werner Dr Ing Habil Gohlke
Original Assignee
Gohlke Werner
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=7125167&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=CH413665(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Gohlke Werner filed Critical Gohlke Werner
Publication of CH413665A publication Critical patent/CH413665A/de

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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/34—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members
    • B64C9/36—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members the members being fuselages or nacelles

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
CH813163A 1962-07-11 1963-07-01 Elastisches Klappleitwerk für bewegte Körper, insbesondere Flugkörper CH413665A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEG35435A DE1159314B (de) 1962-07-11 1962-07-11 Elastisches Klappleitwerk, insbesondere fuer Flugkoerper

Publications (1)

Publication Number Publication Date
CH413665A true CH413665A (de) 1966-05-15

Family

ID=7125167

Family Applications (1)

Application Number Title Priority Date Filing Date
CH813163A CH413665A (de) 1962-07-11 1963-07-01 Elastisches Klappleitwerk für bewegte Körper, insbesondere Flugkörper

Country Status (3)

Country Link
US (1) US3165281A (de)
CH (1) CH413665A (de)
DE (1) DE1159314B (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3304030A (en) * 1965-09-24 1967-02-14 James E Weimholt Pyrotechnic-actuated folding fin assembly
SE339646B (de) * 1970-01-08 1971-10-11 Bofors Ab
US3826448A (en) * 1972-09-14 1974-07-30 Nasa Deployable flexible ventral fins for use as an emergency spin-recovery device in aircraft
US3964391A (en) * 1973-09-04 1976-06-22 The United States Of America As Represented By The Secretary Of The Army Dispenser-launched munition with two-stage spin-imparting vanes
US4158447A (en) * 1977-11-29 1979-06-19 The United States Of America As Represented By The Secretary Of The Navy Expanding stabilizing fin cup
US4383831A (en) * 1978-09-05 1983-05-17 Raytheon Company Stabilized suspension system
US4336914A (en) * 1978-12-29 1982-06-29 The Commonwealth Of Australia Deployable wing mechanism
DE3516367A1 (de) * 1985-05-07 1986-11-13 Diehl GmbH & Co, 8500 Nürnberg Flugkoerper mit klappfluegel
US5040746A (en) * 1990-08-14 1991-08-20 The United States Of America As Represented By The Secretary Of The Army Finned projectile with supplementary fins
US5085381A (en) * 1991-03-29 1992-02-04 The United States Of America As Represented By The Secretary Of The Air Force Deployable aerodynamic aerosurface
US5417393A (en) * 1993-04-27 1995-05-23 Hughes Aircraft Company Rotationally mounted flexible band wing
US8816261B1 (en) * 2011-06-29 2014-08-26 Raytheon Company Bang-bang control using tangentially mounted surfaces

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR929040A (fr) * 1946-06-14 1947-12-15 Dispositif pour le repliement et le déploiement d'ailettes de mobiles empennés
FR1061242A (fr) * 1952-08-05 1954-04-09 Perfectionnement aux projectiles-fusées à ailettes d'empennage déployables
NL93582C (de) * 1953-04-23
GB745252A (en) * 1953-07-29 1956-02-22 Ml Aviation Co Ltd Improvements relating to rocket propelled projectiles
NL100549C (de) * 1953-12-21 Brandt Soc Nouv Ets
BE551492A (de) * 1955-10-20 Brandt Soc Nouv Ets
US2918235A (en) * 1955-12-31 1959-12-22 Aberg Lars Douglas Parachute devices

Also Published As

Publication number Publication date
US3165281A (en) 1965-01-12
DE1159314B (de) 1963-12-12

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