GB1355366A - Finned tail-assembly for fin-stabilised projectiles - Google Patents
Finned tail-assembly for fin-stabilised projectilesInfo
- Publication number
- GB1355366A GB1355366A GB2865171A GB2865171A GB1355366A GB 1355366 A GB1355366 A GB 1355366A GB 2865171 A GB2865171 A GB 2865171A GB 2865171 A GB2865171 A GB 2865171A GB 1355366 A GB1355366 A GB 1355366A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fin
- fins
- tube
- assembly
- june
- 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
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
- F42B10/04—Stabilising arrangements using fixed fins
- F42B10/06—Tail fins
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Earth Drilling (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
- Toys (AREA)
Abstract
1355366 Making projectiles TAMPELLA AB OY 10 June 1971 [11 June 1970] 28651/71 Heading B3A [Also in Division F3] A fin assembly for a projectile is made by radially pressing a number of separate steel fins 2 into the softer material of a light metal alloy tube 10. Undulations 7 and 8 along the foot of each fin provide increased anchorage. The fins are pressed into the full material of the tube or into previously prepared grooves of smaller dimensions than the feet of the fins. The pressing is carried out either in the cold state, where a groove is provided, or, if not, after the tube has been heated to 250-350 C.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2034568A DE2034568C3 (en) | 1970-07-11 | 1970-07-11 | Wing control for wing-stabilized projectiles and process for its manufacture |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1355366A true GB1355366A (en) | 1974-06-05 |
Family
ID=5776548
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2865171A Expired GB1355366A (en) | 1970-07-11 | 1971-06-18 | Finned tail-assembly for fin-stabilised projectiles |
Country Status (10)
Country | Link |
---|---|
US (1) | US3765620A (en) |
CA (1) | CA948479A (en) |
DE (1) | DE2034568C3 (en) |
DK (1) | DK138616C (en) |
FI (1) | FI55584C (en) |
FR (1) | FR2099880A5 (en) |
GB (1) | GB1355366A (en) |
IL (1) | IL36996A (en) |
NO (1) | NO129819B (en) |
SE (1) | SE385733B (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4231536A (en) * | 1977-10-11 | 1980-11-04 | The Boeing Company | Airfoil for controlling refueling boom |
US4477084A (en) * | 1983-03-07 | 1984-10-16 | Austin Charles W | Vane structure for arrows |
EP0174082A1 (en) * | 1984-07-23 | 1986-03-12 | Judd Engineering Limited | Projectile stabilising fin unit |
ES8706942A1 (en) * | 1986-04-16 | 1987-07-01 | Esperanza & Cie Sa | Mortar grenade |
US5158509A (en) * | 1990-12-14 | 1992-10-27 | The United States Of America As Represented By The United States Department Of Energy | Composite stabilizer unit |
US5668347A (en) * | 1996-09-13 | 1997-09-16 | The United States Of America As Represented By The Secretary Of The Army | Kinetic energy projectile with fin leading edge protection mechanisms |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1032036A (en) * | 1951-02-03 | 1953-06-29 | Projectile tail and manufacturing process | |
US3032857A (en) * | 1958-07-21 | 1962-05-08 | Lyon Inc | Apparatus for forming integral ribs upon the circumference of a rigid tubular shape |
NL285423A (en) * | 1962-04-27 |
-
1970
- 1970-07-11 DE DE2034568A patent/DE2034568C3/en not_active Expired
-
1971
- 1971-06-07 IL IL36996A patent/IL36996A/en unknown
- 1971-06-18 GB GB2865171A patent/GB1355366A/en not_active Expired
- 1971-06-24 FR FR7123001A patent/FR2099880A5/fr not_active Expired
- 1971-07-06 CA CA117,466A patent/CA948479A/en not_active Expired
- 1971-07-08 NO NO02613/71A patent/NO129819B/no unknown
- 1971-07-08 FI FI1942/71A patent/FI55584C/en active
- 1971-07-09 SE SE7108914A patent/SE385733B/en unknown
- 1971-07-09 US US00161367A patent/US3765620A/en not_active Expired - Lifetime
- 1971-07-09 DK DK339171A patent/DK138616C/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
FR2099880A5 (en) | 1972-03-17 |
FI55584C (en) | 1979-08-10 |
CA948479A (en) | 1974-06-04 |
NO129819B (en) | 1974-05-27 |
IL36996A0 (en) | 1972-02-29 |
DK138616C (en) | 1979-03-12 |
DK138616B (en) | 1978-10-02 |
FI55584B (en) | 1979-04-30 |
IL36996A (en) | 1974-10-22 |
DE2034568A1 (en) | 1972-01-13 |
DE2034568B2 (en) | 1973-07-05 |
US3765620A (en) | 1973-10-16 |
SE385733B (en) | 1976-07-19 |
DE2034568C3 (en) | 1974-01-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PLE | Entries relating assignments, transmissions, licences in the register of patents | ||
PCNP | Patent ceased through non-payment of renewal fee |