GB647366A - Improvements in or relating to fin assemblies for projectiles and the like - Google Patents

Improvements in or relating to fin assemblies for projectiles and the like

Info

Publication number
GB647366A
GB647366A GB12843/48A GB1284348A GB647366A GB 647366 A GB647366 A GB 647366A GB 12843/48 A GB12843/48 A GB 12843/48A GB 1284348 A GB1284348 A GB 1284348A GB 647366 A GB647366 A GB 647366A
Authority
GB
United Kingdom
Prior art keywords
mine
frame
fins
bracket
arm
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
GB12843/48A
Inventor
Evelyn Cecil Muschamp Fonseca
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.)
Bristol Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane Co Ltd
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 Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Priority to GB12843/48A priority Critical patent/GB647366A/en
Priority to US76812A priority patent/US2661689A/en
Publication of GB647366A publication Critical patent/GB647366A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/16Wrap-around fins

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Catching Or Destruction (AREA)

Abstract

647,366. Ammunition projectiles. BRISTOL AEROPLANE CO., Ltd. May 10, 1948, No. 12843. [Classes 9 (i) and 9 (ii)] A fin assembly for a projectile is provided wherein the fins are pivotally mounted on a frame and each is independently held in the folded position by a catch, all the catches being simultaneously unfastened from the frame and connected with a common release gear, when the assembly is fitted on the projectile. A sea-mine 10 adapted to be dropped from aircraft comprises a mine body 11 and a detachable fin system 12. The fin system' comprises four fins 13 hinged at 14 to a frame 15, Fig. 2, the fins swinging outwards when the mine is dropped and the fin' system being automatically thrown off when the mine hits the sea. The frame 15 comprises a cylindrical member 16 with axially spaced flanges 17, Figs. 2 and 3. The pivoted fins, mounted on tubes 18 extending between the corners of the flanges, Fig. 3, are held in the folded position, Fig. 4, by two-headed pins 19. Each fin has an upstanding flange 22 with a slot 23 receiving one end of a pin 19, the opposite end resting in a slot 24 in the member 16. Each pin is connected by a rod 25 to a bracket 27 and held there by a hook 28. Normally the bracket lies within the member 16, but when the frame is placed on the mine, the bracket is pushed out so that the rods 25 are disengaged from the member 16. On launching, a cable removes the hook 28 whereupon the fins fly outwardly under the action of springs 36.' Each fin carries an arm 29 pivotally connected to a link 30, the free end 39 of which moves on a slide 33 secured to the member 16, and comes to rest in slot 34 when the fins are extended (dotted lines in Fig. 4). The spring 36 is anchored to the link 30 and to a bracket on the member 16. A device 50 is provided for releasing the frame 15 when the mine strikes the water. This device consists of a bracket 40 on the member 16 connected to a flange 17 by a rod 41, Fig. 3. The bracket also carries a lever 42, one arm 43 of which, acted on by a spring 45, passes through an opening in the member 16 to engage the mine 11. The other arm 46 of the lever lies behind a weight 47 slidable on the rod 41. A locking wire 48 holds the weight clear of the arm 46. On impact the weight 47 shears the wire 48 and strikes the arm 46 so that the arm 43 is released and the mine is freed from the frame. Two devices 50 are placed at diagonally opposite corners, Fig. 2.
GB12843/48A 1948-05-10 1948-05-10 Improvements in or relating to fin assemblies for projectiles and the like Expired GB647366A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB12843/48A GB647366A (en) 1948-05-10 1948-05-10 Improvements in or relating to fin assemblies for projectiles and the like
US76812A US2661689A (en) 1948-05-10 1949-02-16 Holding means for projectile fins

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB12843/48A GB647366A (en) 1948-05-10 1948-05-10 Improvements in or relating to fin assemblies for projectiles and the like

Publications (1)

Publication Number Publication Date
GB647366A true GB647366A (en) 1950-12-13

Family

ID=10012145

Family Applications (1)

Application Number Title Priority Date Filing Date
GB12843/48A Expired GB647366A (en) 1948-05-10 1948-05-10 Improvements in or relating to fin assemblies for projectiles and the like

Country Status (2)

Country Link
US (1) US2661689A (en)
GB (1) GB647366A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6224013B1 (en) 1998-08-27 2001-05-01 Lockheed Martin Corporation Tail fin deployment device
US6857249B1 (en) * 2003-08-11 2005-02-22 Che Ting Hsu Safety catch device of sealing machine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1442345A (en) * 1917-07-23 1923-01-16 Charles L Kee Aircraft-launched temporary drifting mine
BE379532A (en) * 1930-05-22
GB589346A (en) * 1944-07-01 1947-06-18 Walter Lennard Lax Improvements in or relating to bombs and other missiles for dropping from aircraft

Also Published As

Publication number Publication date
US2661689A (en) 1953-12-08

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