GB1143967A - Projectile assembly - Google Patents
Projectile assemblyInfo
- Publication number
- GB1143967A GB1143967A GB13326/66A GB1332666A GB1143967A GB 1143967 A GB1143967 A GB 1143967A GB 13326/66 A GB13326/66 A GB 13326/66A GB 1332666 A GB1332666 A GB 1332666A GB 1143967 A GB1143967 A GB 1143967A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sabot
- projectile
- abutment
- locking member
- threaded
- 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
- F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
- F42B14/06—Sub-calibre projectiles having sabots; Sabots therefor
- F42B14/064—Sabots enclosing the rear end of a kinetic energy projectile, i.e. having a closed disk shaped obturator base and petals extending forward from said base
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
1,143,967. Sabot projectiles. OERLIKONBœHRLE HOLDING A.G. 25 March, 1966 [1 April, 1965], No. 13326/66. Heading F3A. A rotary discarding sabot projectile assembly comprises a sabot 10 and a projectile 11 which is supported at its rear face by a first abutment 107 and is secured by a locking member, e.g. a split ring 15, which engages a surface 114 in a recess in the projectile and the surface 171 of a screw-threaded second abutment 17 which is axially movable in the sabot to adjust its clamping action but which is normally locked against rotation by a screw 20, the first abutment 107 being deformable axially by the rear face of the projectile 11 when the assembly is fired to permit the projectile to move rearwardly, under inertia, with respect to the sabot, to disengage the locking member from the surface 171 and to bring the rear face of the projectile into operative engagement with the sabot, whereby the rotary motion of the sabot is transmitted to the projectile 11 and locking member 15, which, under the action of centrifugal force, expands radially outwardly to free the projectile. Faces 112 provided at the rear of the projectile increase its grip in the sabot on axial displacement. A threaded, projectileguiding member 14 at the front end of the sabot permits air to enter the body of the sabot, whereby the rate of separation of the projectile and sabot after firing is increased. Rotation is transmitted to the assembly by driving bands 12 and 13. In a modification (Fig. 7, not shown), the locking member comprises a sleeve (15d) divided into a plurality of fingers (28) which bend outwardly under centrifugal force. In another embodiment the first abutment (23, Fig. 4, not shown) is screw-threaded into the rear of the sabot and the second abutment (173a) is a fixture in the sabot. In further embodiments the first abutment comprises a resilient spring (107c, Fig. 6, not shown) which also assists in the separation of the sabot and projectile, or an upsettable element (107b, Fig. 5, not shown).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DK162766A DK130569B (en) | 1965-03-30 | 1966-03-29 | Cigarette with a rod-shaped tobacco part wrapped in paper. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH452365A CH435039A (en) | 1965-04-01 | 1965-04-01 | Sabot bullet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1143967A true GB1143967A (en) | 1969-02-26 |
Family
ID=4277674
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB13326/66A Expired GB1143967A (en) | 1965-03-30 | 1966-03-25 | Projectile assembly |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US3359905A (en) |
| AT (1) | AT260733B (en) |
| BE (1) | BE678906A (en) |
| CH (1) | CH435039A (en) |
| DE (1) | DE1578185A1 (en) |
| GB (1) | GB1143967A (en) |
| NL (2) | NL6603145A (en) |
| SE (1) | SE302733B (en) |
Families Citing this family (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| LU51611A1 (en) * | 1966-07-21 | 1968-03-14 | ||
| US3447466A (en) * | 1967-09-05 | 1969-06-03 | Oerlikon Buhrie Holding Ltd | Sabot projectile with core guiding means |
| LU54786A1 (en) * | 1967-11-03 | 1969-06-27 | ||
| US3927618A (en) * | 1971-03-29 | 1975-12-23 | Oerlikon Buehrle Ag | Sabot projectile |
| DE2232866C3 (en) * | 1972-03-07 | 1980-10-02 | Dynamit Nobel Ag, 5210 Troisdorf | Detachable connection between projectile and propellant charge case |
| US3961580A (en) * | 1975-02-27 | 1976-06-08 | The United States Of America As Represented By The Secretary Of The Navy | Energy-absorbing sabot |
| US5182419A (en) * | 1978-05-26 | 1993-01-26 | Asi Systems International | Saboted projectile |
| US4709638A (en) * | 1981-09-24 | 1987-12-01 | Honeywell Inc. | Discarding sabot projectile |
| US4469027A (en) * | 1983-04-15 | 1984-09-04 | The United States Of America As Represented By The Secretary Of The Army | Armor piercing ammunition having interlocking means |
| US4735148A (en) * | 1986-03-18 | 1988-04-05 | United Technologies Corporation | Plastic composite sabot |
| US4881466A (en) * | 1988-12-23 | 1989-11-21 | General Electric Company | High velocity sabot for spin stabilized penetrator |
| DE4026902C2 (en) * | 1990-08-25 | 1995-01-05 | Rheinmetall Gmbh | Bullet |
| AT399583B (en) * | 1991-07-17 | 1995-06-26 | Steyr Daimler Puch Ag | SUB-CALIBRARY BULLET WITH REJECTABLE CAGE |
| US10502515B2 (en) * | 2017-01-17 | 2019-12-10 | Raytheon Company | Launch piston brake |
| CN107115610B (en) * | 2017-06-09 | 2019-08-30 | 娄文忠 | A kind of fire extinguisher bomb jettison system of individual equipment and its method of jettisoninging |
| CN107137845B (en) * | 2017-06-09 | 2019-09-17 | 娄文忠 | A kind of integral type fire extinguisher bomb jettison system of individual equipment and method of jettisoninging |
| AU2020261387A1 (en) * | 2019-04-26 | 2021-12-23 | University Of Kansas | Maneuvering aeromechanically stable sabot system |
| CN112607552B (en) * | 2020-12-18 | 2022-04-05 | 亿涛建设集团有限公司 | Multiple anti-falling hoisting mechanism |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE301298C (en) * | ||||
| US1209611A (en) * | 1916-02-29 | 1916-12-19 | Henry C Mustin | Projectile. |
| BE397466A (en) * | 1932-07-19 | |||
| US2389846A (en) * | 1941-08-26 | 1945-11-27 | George R Ericson | High velocity projectile |
| US2669930A (en) * | 1946-01-05 | 1954-02-23 | Remington Arms Co Inc | Sabot projectile |
-
0
- NL NL133127D patent/NL133127C/xx active
-
1965
- 1965-04-01 CH CH452365A patent/CH435039A/en unknown
-
1966
- 1966-03-09 NL NL6603145A patent/NL6603145A/xx unknown
- 1966-03-11 SE SE3236/66A patent/SE302733B/xx unknown
- 1966-03-18 DE DE19661578185 patent/DE1578185A1/en active Pending
- 1966-03-24 AT AT279166A patent/AT260733B/en active
- 1966-03-25 GB GB13326/66A patent/GB1143967A/en not_active Expired
- 1966-03-28 US US537816A patent/US3359905A/en not_active Expired - Lifetime
- 1966-04-01 BE BE678906D patent/BE678906A/xx unknown
Also Published As
| Publication number | Publication date |
|---|---|
| AT260733B (en) | 1968-03-25 |
| US3359905A (en) | 1967-12-26 |
| CH435039A (en) | 1967-04-30 |
| BE678906A (en) | 1966-09-16 |
| NL6603145A (en) | 1966-10-03 |
| DE1578185A1 (en) | 1970-02-12 |
| SE302733B (en) | 1968-07-29 |
| NL133127C (en) |
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