GB976483A - A monotabular device for projectiles having stabilising fins and projectiles fitted with this device - Google Patents
A monotabular device for projectiles having stabilising fins and projectiles fitted with this deviceInfo
- Publication number
- GB976483A GB976483A GB584361A GB584361A GB976483A GB 976483 A GB976483 A GB 976483A GB 584361 A GB584361 A GB 584361A GB 584361 A GB584361 A GB 584361A GB 976483 A GB976483 A GB 976483A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tuyere
- fins
- projectile
- projectiles
- fitted
- 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
- 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)
- Guides For Winding Or Rewinding, Or Guides For Filamentary Materials (AREA)
Abstract
976,483. Projectiles. LES FORGES DE ZEEBRUGGE S.A. Feb. 16, 1961 [Feb. 26, 1960], No. 5843/61. Heading F3A. [Also in Division F1] The stabilizing fins 10 of a self-propelled projectile are unfolded away from the longitudinal axis of the projectile by the propelling gases when the projectile leaves the bore of the launching device and are locked in position by a sliding tuyere 11 fitted with a smooth friction fit in a tuyere plate 2 rigidly connected to the rear end of the body 1 of the projectile. The propelling gases pass through the tuyere 11 and act directly on the fins 10 causing them to pivot on their respective pins 9 until they reach their maximum unfolded position. The propelling gases also act on the tuyere 11 and move it from the position shown in Fig. 1 to that shown in Fig. 5. In order not to damage the fins 10 by violent action of the tuyere 11 the velocity of the latter is checked by an annular chamber 12 which acts as a shock absorber and contains a fluid such as air or oil, or other compressible material. In order to maintain the tuyere 11 in its outer position after unfolding of the fins 10, a keying means may be provided between the contacting surfaces of the tuyere 11 and the plate 2, for example, a rough or uneven part 14 may be provided on at least one of these two surfaces by grinding.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| BE2039600 | 1960-02-26 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB976483A true GB976483A (en) | 1964-11-25 |
Family
ID=3864720
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB584361A Expired GB976483A (en) | 1960-02-26 | 1961-02-16 | A monotabular device for projectiles having stabilising fins and projectiles fitted with this device |
Country Status (4)
| Country | Link |
|---|---|
| DE (1) | DE1249729B (en) |
| DK (1) | DK128463B (en) |
| GB (1) | GB976483A (en) |
| NL (1) | NL261692A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3349708A (en) * | 1964-12-16 | 1967-10-31 | Paget Win Withers | Rocket projectile |
| GB2256622A (en) * | 1991-06-14 | 1992-12-16 | Diehl Gmbh & Co | Flying body with mechanism for deploying control fins. |
| WO2012118536A1 (en) * | 2011-03-03 | 2012-09-07 | Alliant Techsystems Inc. | Rocket nozzle assembly |
| WO2012141641A1 (en) * | 2011-04-14 | 2012-10-18 | Bae System Bofors Ab | Fin deployment mechanism and projectile with such a mechanism |
| RU2607126C1 (en) * | 2015-08-25 | 2017-01-10 | Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" | Method of missile movement stabilization at underwater launch and device for its implementation |
-
0
- DE DENDAT1249729D patent/DE1249729B/de active Pending
- NL NL261692D patent/NL261692A/xx unknown
-
1961
- 1961-02-16 GB GB584361A patent/GB976483A/en not_active Expired
- 1961-02-17 DK DK66161AA patent/DK128463B/en unknown
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3349708A (en) * | 1964-12-16 | 1967-10-31 | Paget Win Withers | Rocket projectile |
| GB2256622A (en) * | 1991-06-14 | 1992-12-16 | Diehl Gmbh & Co | Flying body with mechanism for deploying control fins. |
| GB2256622B (en) * | 1991-06-14 | 1995-01-04 | Diehl Gmbh & Co | A flying body having rudder or control blades |
| WO2012118536A1 (en) * | 2011-03-03 | 2012-09-07 | Alliant Techsystems Inc. | Rocket nozzle assembly |
| GB2505574A (en) * | 2011-03-03 | 2014-03-05 | Alliant Techsystems Inc | Rocket nozzle assembly |
| US8952304B2 (en) | 2011-03-03 | 2015-02-10 | Alliant Techsystems, Inc. | Rocket nozzle assembly |
| GB2505574B (en) * | 2011-03-03 | 2017-03-22 | Orbital Atk Inc | Rocket nozzle assembly |
| WO2012141641A1 (en) * | 2011-04-14 | 2012-10-18 | Bae System Bofors Ab | Fin deployment mechanism and projectile with such a mechanism |
| US9719760B2 (en) | 2011-04-14 | 2017-08-01 | Bae Systems Bofors Ab | Fin deployment mechanism and projectile with such a mechanism |
| RU2607126C1 (en) * | 2015-08-25 | 2017-01-10 | Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" | Method of missile movement stabilization at underwater launch and device for its implementation |
Also Published As
| Publication number | Publication date |
|---|---|
| DK128463B (en) | 1974-05-06 |
| DE1249729B (en) | |
| NL261692A (en) |
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