GB952960A - Improvements in or relating to a deployable fin arrangement for a projectile - Google Patents
Improvements in or relating to a deployable fin arrangement for a projectileInfo
- Publication number
- GB952960A GB952960A GB4168/63A GB416863A GB952960A GB 952960 A GB952960 A GB 952960A GB 4168/63 A GB4168/63 A GB 4168/63A GB 416863 A GB416863 A GB 416863A GB 952960 A GB952960 A GB 952960A
- Authority
- GB
- United Kingdom
- Prior art keywords
- projectile
- bore
- july
- apertures
- springs
- 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
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
-
- 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
- F42B10/20—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Discharge By Other Means (AREA)
Abstract
952,960. Ammunition projectiles. HOTCHKISS-BRANDT. July 6, 1961 [July 11, 1960], No. 4168/63. Divided out of 945,409. Heading F3A. A fin assembly for a projectile comprises deployable fins 21b pivoted on tubes 22b arranged orthogonally to the longitudinal axis of the assembly which is screwed into the body C of the projectile, the fins being forced to the extended position by hollow pistons 30b arranged in blind bores 31b, the pistons being driven by springs 54. Each spring bears against the bottom of a bore 31b and against the bottom of the cavity 55 in the piston within the bore. The cavity 55 is vented by an aperture 56 to equalize the pressure in the bore 31b and the launching tube for the projectile. The action of the springs may be assisted or replaced by placing powder charges in the apertures 31b. These charges may be ignited through the apertures 56 or openings 58.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR832688A FR1270054A (en) | 1960-07-11 | 1960-07-11 | Deployable tail for self-propelled projectile |
FR865095A FR79945E (en) | 1960-07-11 | 1961-06-15 | Deployable tail for self-propelled projectile |
Publications (1)
Publication Number | Publication Date |
---|---|
GB952960A true GB952960A (en) | 1964-03-18 |
Family
ID=26186750
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24444/61A Expired GB945409A (en) | 1960-07-11 | 1961-07-06 | Deployable fin assemblies for self-propelled projectiles |
GB4168/63A Expired GB952960A (en) | 1960-07-11 | 1961-07-06 | Improvements in or relating to a deployable fin arrangement for a projectile |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24444/61A Expired GB945409A (en) | 1960-07-11 | 1961-07-06 | Deployable fin assemblies for self-propelled projectiles |
Country Status (9)
Country | Link |
---|---|
US (1) | US3098446A (en) |
BE (1) | BE605677A (en) |
CH (1) | CH370677A (en) |
DE (2) | DE1183834B (en) |
ES (1) | ES269713A1 (en) |
FI (1) | FI41122B (en) |
FR (2) | FR1270054A (en) |
GB (2) | GB945409A (en) |
NL (3) | NL266892A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2274904A (en) * | 1993-02-05 | 1994-08-10 | British Aerospace | Deployable wing |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3196793A (en) * | 1963-01-16 | 1965-07-27 | Milenkovic Veljko | Folded fin rocket |
US5439188A (en) * | 1964-09-04 | 1995-08-08 | Hughes Missile Systems Company | Control system |
US3378216A (en) * | 1966-04-29 | 1968-04-16 | Susquehama Corp | Integral fin canister-nozzle exit cone |
US3690595A (en) * | 1970-11-19 | 1972-09-12 | Sarmac Sa | Self-propelled, vaned missile |
DE2264338A1 (en) * | 1972-12-30 | 1974-07-04 | Dynamit Nobel Ag | FOLD-OUT TAIL, ESPECIALLY FOR MISSILE |
FR2221707B1 (en) * | 1973-03-14 | 1976-04-30 | France Etat | |
US3986685A (en) * | 1974-07-30 | 1976-10-19 | The United States Of America As Represented By The Secretary Of The Army | Folding tail fins |
US3946969A (en) * | 1974-07-30 | 1976-03-30 | The United States Of America As Represented By The Secretary Of The Army | Folding tail fins |
US3998407A (en) * | 1974-07-30 | 1976-12-21 | The United States Of America As Represented By The Secretary Of The Army | Folding tail fins |
US3986684A (en) * | 1974-07-30 | 1976-10-19 | The United States Of America As Represented By The Secretary Of The Army | Folding tail fins |
US4523728A (en) * | 1983-03-07 | 1985-06-18 | Ford Aerospace & Communications Corporation | Passive auto-erecting alignment wings for long rod penetrator |
SE444612B (en) * | 1984-12-13 | 1986-04-21 | Ffv Affersverket | GUIDELINES FOR FENOR EXPOSURE OF PROJECTIL |
DE3447852A1 (en) * | 1984-12-31 | 1986-08-28 | Heide, Marion, 4030 Ratingen | FOLDING ASSEMBLY FOR WING-STABILIZED ROCKET BULLETS |
US5235930A (en) * | 1992-05-08 | 1993-08-17 | Rockwell International Corporation | Self propelled underwater device with steerable fin stabilizer |
US6559370B1 (en) * | 2002-08-06 | 2003-05-06 | The United States Of America As Represented By The Secretary Of The Navy | Submarine countermeasure vehicle with folding propeller |
FR2863045B1 (en) * | 2003-11-27 | 2006-01-06 | Giat Ind Sa | DEVICE FOR SECURELY DEPLOYING THE FINS OF A PROJECTILE |
US7083141B2 (en) * | 2003-12-02 | 2006-08-01 | Edward Nitenson | Self-propelled projectile |
KR101074028B1 (en) | 2009-02-12 | 2011-10-17 | 국방과학연구소 | Flying object with fixing device for the deployed wing |
FR2946423A1 (en) * | 2009-06-05 | 2010-12-10 | Tda Armements Sas | DEVICE FOR OPENING AND LOCKING A MUNITION STACK |
CN113237393A (en) * | 2021-04-28 | 2021-08-10 | 北京星途探索科技有限公司 | High-precision stabilizing device |
US11796291B2 (en) * | 2022-01-11 | 2023-10-24 | Raytheon Company | Effector having morphing airframe and method |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR896502A (en) * | 1940-09-23 | 1945-02-23 | Commerciale Caproni Comp | Device for controlling the fins of a projectile fitted with a tail unit |
US2365577A (en) * | 1943-08-26 | 1944-12-19 | Stephen A Moore | Projectile |
BE565999A (en) * | 1953-02-06 | |||
BE552288A (en) * | 1953-10-20 | |||
LU33739A1 (en) * | 1955-07-21 | |||
FR1187193A (en) * | 1957-11-15 | 1959-09-08 | Hotchkiss Brandt | Deployable stabilizer for projectile |
BE567934A (en) * | 1958-05-22 | |||
NL106348C (en) * | 1959-03-09 |
-
0
- NL NL295319D patent/NL295319A/xx unknown
- NL NL113679D patent/NL113679C/xx active
- NL NL266892D patent/NL266892A/xx unknown
-
1960
- 1960-07-11 FR FR832688A patent/FR1270054A/en not_active Expired
-
1961
- 1961-06-15 FR FR865095A patent/FR79945E/en not_active Expired
- 1961-07-03 CH CH778961A patent/CH370677A/en unknown
- 1961-07-03 BE BE605677A patent/BE605677A/en unknown
- 1961-07-06 GB GB24444/61A patent/GB945409A/en not_active Expired
- 1961-07-06 GB GB4168/63A patent/GB952960A/en not_active Expired
- 1961-07-10 ES ES0269713A patent/ES269713A1/en not_active Expired
- 1961-07-10 US US122988A patent/US3098446A/en not_active Expired - Lifetime
- 1961-07-11 FI FI1255/61A patent/FI41122B/fi active
- 1961-07-11 DE DEH43086A patent/DE1183834B/en active Pending
- 1961-07-11 DE DEH47903A patent/DE1195204B/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2274904A (en) * | 1993-02-05 | 1994-08-10 | British Aerospace | Deployable wing |
Also Published As
Publication number | Publication date |
---|---|
FR1270054A (en) | 1961-08-25 |
CH370677A (en) | 1963-07-15 |
US3098446A (en) | 1963-07-23 |
FI41122B (en) | 1969-04-30 |
GB945409A (en) | 1963-12-23 |
ES269713A1 (en) | 1962-01-01 |
FR79945E (en) | 1963-02-15 |
DE1195204B (en) | 1965-06-16 |
NL295319A (en) | |
NL266892A (en) | |
BE605677A (en) | 1961-11-03 |
NL113679C (en) | |
DE1183834B (en) | 1964-12-17 |
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