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 likeInfo
- 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
Links
- 230000000712 assembly Effects 0.000 title 1
- 238000000429 assembly Methods 0.000 title 1
- 230000000284 resting effect Effects 0.000 abstract 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract 1
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)
- 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.
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)
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)
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 |
-
1948
- 1948-05-10 GB GB12843/48A patent/GB647366A/en not_active Expired
-
1949
- 1949-02-16 US US76812A patent/US2661689A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US2661689A (en) | 1953-12-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US7143976B2 (en) | UAV arresting hook for use with UAV recovery system | |
US2958260A (en) | Missile launching apparatus | |
US2953377A (en) | High speed externally carried tow target | |
US2898058A (en) | Tow target | |
ES295123A1 (en) | Toy missile with delayed opening device | |
US2282315A (en) | Catapult | |
GB647366A (en) | Improvements in or relating to fin assemblies for projectiles and the like | |
US2183540A (en) | Target towing device | |
GB624852A (en) | Improvements in or relating to releasing devices | |
US3002708A (en) | Aircraft tow reel system | |
US2486418A (en) | Automatically self-releasing | |
GB1603227A (en) | Activating devices for releasable load | |
US3100093A (en) | Apparatus for towed aircraft | |
US2310249A (en) | Aerodynamic release drag for tow targets | |
US2483402A (en) | Antiaircraft target | |
US2723812A (en) | Glider pick-up | |
GB473958A (en) | Aeroplane bomb | |
US3662645A (en) | Coupler for interconnection of tandem launched aerial flares | |
GB667202A (en) | Improvements relating to apparatus for towing targets and the like | |
US2385813A (en) | Le roy s | |
US2959416A (en) | Tow member launching and recovery apparatus | |
US2971792A (en) | Store retaining device | |
US2874921A (en) | Mooring device for seaplanes | |
US2991960A (en) | Pickup, tow and release unit | |
US3318042A (en) | Tethered bomber plane and mechanism for releasing bombs |