CH378734A - Tail fin for projectiles, e.g. B. Missiles - Google Patents

Tail fin for projectiles, e.g. B. Missiles

Info

Publication number
CH378734A
CH378734A CH340560A CH340560A CH378734A CH 378734 A CH378734 A CH 378734A CH 340560 A CH340560 A CH 340560A CH 340560 A CH340560 A CH 340560A CH 378734 A CH378734 A CH 378734A
Authority
CH
Switzerland
Prior art keywords
missiles
projectiles
tail fin
fin
tail
Prior art date
Application number
CH340560A
Other languages
German (de)
Inventor
Bertil Olsson Olof
Original Assignee
Bofors Ab
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 Bofors Ab filed Critical Bofors Ab
Publication of CH378734A publication Critical patent/CH378734A/en

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
    • B64C9/02—Mounting or supporting thereof
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Superstructure Of Vehicle (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
CH340560A 1959-04-13 1960-03-26 Tail fin for projectiles, e.g. B. Missiles CH378734A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE350259 1959-04-13

Publications (1)

Publication Number Publication Date
CH378734A true CH378734A (en) 1964-06-15

Family

ID=20262267

Family Applications (1)

Application Number Title Priority Date Filing Date
CH340560A CH378734A (en) 1959-04-13 1960-03-26 Tail fin for projectiles, e.g. B. Missiles

Country Status (6)

Country Link
US (1) US3058422A (en)
BE (1) BE589608A (en)
CH (1) CH378734A (en)
DE (1) DE1147514B (en)
GB (1) GB869410A (en)
NL (2) NL101734C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015004702A1 (en) * 2014-12-11 2016-06-16 Mbda Deutschland Gmbh rudder system

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE331242B (en) * 1969-05-14 1970-12-14 Bofors Ab
US3782668A (en) * 1970-09-25 1974-01-01 Us Army Ramp forward of control fin
US4203569A (en) * 1977-10-17 1980-05-20 Bei Electronics, Inc. Fin and nozzle unit for a free-flight rocket
US4717093A (en) * 1985-08-12 1988-01-05 Grumman Aerospace Corporation Penguin missile folding wing configuration
US4691880A (en) * 1985-11-14 1987-09-08 Grumman Aerospace Corporation Torsion spring powered missile wing deployment system
JP3781311B2 (en) * 1995-12-01 2006-05-31 株式会社小松製作所 Aircraft wing device
US6092264A (en) * 1998-11-13 2000-07-25 Lockheed Martin Corporation Single axis fold actuator and lock for member
CN102774494A (en) * 2012-07-06 2012-11-14 北京林业大学 Aircraft folding rudder capable of stretching automatically
CN104677199B (en) * 2015-01-21 2016-07-13 浙江理工大学 A kind of single driving folds rudder face synchronous expansion mechanism more
EP3971084A1 (en) 2016-02-22 2022-03-23 SZ DJI Technology Co., Ltd. Aéronef multi-rotor pliable
CN106839897B (en) * 2017-01-03 2019-01-15 北京临近空间飞行器系统工程研究所 A kind of straight-line helix unfolded wing mechanism
CN109405669A (en) * 2018-08-31 2019-03-01 江西洪都航空工业集团有限责任公司 A kind of Quick Release aerofoil automatic locking mechanism
CN109253667A (en) * 2018-08-31 2019-01-22 江西洪都航空工业集团有限责任公司 A kind of Missile Folding rudder face longitudinal direction unfolding mechanism

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL173299B (en) * 1951-11-07 Otis Eng Co WINPUT WITH UNDERGROUND SAFETY VALVE.
BE551492A (en) * 1955-10-20 Brandt Soc Nouv Ets
US2923241A (en) * 1957-09-09 1960-02-02 Aerojet General Co Folding stabilizing fins
FR1191519A (en) * 1958-02-13 1959-10-20 Hotchkiss Brandt Deploying tail for artillery projectile

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015004702A1 (en) * 2014-12-11 2016-06-16 Mbda Deutschland Gmbh rudder system
US10006748B2 (en) 2014-12-11 2018-06-26 Mbda Deutschland Gmbh Rudder system

Also Published As

Publication number Publication date
GB869410A (en) 1961-05-31
BE589608A (en) 1960-08-01
NL101734C (en)
DE1147514B (en) 1963-04-18
US3058422A (en) 1962-10-16
NL250199A (en)

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