SE320609B - - Google Patents
Info
- Publication number
- SE320609B SE320609B SE17665/66A SE1766566A SE320609B SE 320609 B SE320609 B SE 320609B SE 17665/66 A SE17665/66 A SE 17665/66A SE 1766566 A SE1766566 A SE 1766566A SE 320609 B SE320609 B SE 320609B
- Authority
- SE
- Sweden
- Prior art keywords
- sleeve
- locking component
- rocket
- tube
- held
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B4/00—Fireworks, i.e. pyrotechnic devices for amusement, display, illumination or signal purposes
- F42B4/22—Fireworks, i.e. pyrotechnic devices for amusement, display, illumination or signal purposes characterised by having means to separate article or charge from casing without destroying the casing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A19/00—Firing or trigger mechanisms; Cocking mechanisms
- F41A19/06—Mechanical firing mechanisms, e.g. counterrecoil firing, recoil actuated firing mechanisms
- F41A19/25—Mechanical firing mechanisms, e.g. counterrecoil firing, recoil actuated firing mechanisms having only slidably-mounted striker elements, i.e. percussion or firing pins
- F41A19/27—Mechanical firing mechanisms, e.g. counterrecoil firing, recoil actuated firing mechanisms having only slidably-mounted striker elements, i.e. percussion or firing pins the percussion or firing pin being movable relative to the breech-block
- F41A19/29—Mechanical firing mechanisms, e.g. counterrecoil firing, recoil actuated firing mechanisms having only slidably-mounted striker elements, i.e. percussion or firing pins the percussion or firing pin being movable relative to the breech-block propelled by a spring under tension
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/042—Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/045—Rocket or torpedo launchers for rockets adapted to be carried and used by a person, e.g. bazookas
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/077—Doors or covers for launching tubes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C7/00—Fuzes actuated by application of a predetermined mechanical force, e.g. tension, torsion, pressure
- F42C7/12—Percussion fuzes of the double-action type, i.e. fuzes cocked and fired in a single movement, e.g. by pulling an incorporated percussion pin or hammer
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Portable Nailing Machines And Staplers (AREA)
Abstract
1,174,049. Rocket launchers. OERLIKONBUHRLE HOLDING A.G. 21 Dec., 1966 [23 Dec., 1965], No. 57258/66. Heading F3C. A rocket launcher device comprises a launcher tube 2 having a rocket 8 held therein by a launching release mechanism fitted to the forward end of the tube 2 and a rocket motor ignition device fitted to the rearward end of the tube 2. The ignition device comprises a spring loaded, striker pin 16 guided within, and lockable to a sleeve 5 which in turn is guided within a locking component 9. The locking component is slidably guided axially in an end portion of the launcher tube 2. A spring 11 urges the locking component 9 towards the rocket 8 but the locking component is held against this spring pressure by means of the launching release mechanism which may include a cap 31 resiliently held in the mouth of the launcher tube 2 by a plurality of leaf springs 33, and a plurality of safety balls 30 urged into a groove 32 by the cap 31. The striker pin 16 is held in its cocked position by the sleeve 15 wherein the locking is effected by a plurality of balls 19 seated in holes 18 in the sleeve 15 and urged into a recess 17 in the striker pin by the walls of a bore in the locking component 9. The sleeve 15 is held against movement with respect to the launcher tube 2 by an arming spacer fork 21. On release of the launching release mechanism by pulling a ring 56 having a lanyard 34 connected thereto, the locking component 9 urges the rocket 8 forwardly, movement of the locking component releasing the balls 19 and allowing the preloaded striker pin 16 to be thrown against a primer charge 10. If the arming spacer fork 21 is not placed about the sleeve 15, the enlarged head 20 of the sleeve 15, on release of the launching release mechanism, enters the bore, in which the locking component 9 slides so that the sleeve 15 and striker pin 16 combination follow the motion of the locking component 9 such that the striker pin 16 does not engage the primer charge 10. In a modification (Figs. 3, 4, not shown) the rocket is held in the launching tube by a ball passing through an aperture in the wall of the tube and held therein by a rotatable sleeve, rotation of the sleeve freeing the ball. Also a further spring loading is applied the rocket.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH1774265A CH449472A (en) | 1965-12-23 | 1965-12-23 | Missile launcher |
Publications (1)
Publication Number | Publication Date |
---|---|
SE320609B true SE320609B (en) | 1970-02-09 |
Family
ID=4427752
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE17665/66A SE320609B (en) | 1965-12-23 | 1966-12-23 |
Country Status (9)
Country | Link |
---|---|
US (1) | US3398640A (en) |
AT (1) | AT267969B (en) |
BE (1) | BE691283A (en) |
CH (1) | CH449472A (en) |
DE (1) | DE1578033A1 (en) |
FR (1) | FR1506020A (en) |
GB (1) | GB1174049A (en) |
NL (2) | NL6616326A (en) |
SE (1) | SE320609B (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2625800B1 (en) * | 1988-01-12 | 1990-07-06 | Lacroix E Tous Artifices | SHOULDER WEAPON FOR ROCKET LAUNCHER |
FR2718838B1 (en) * | 1994-04-15 | 1996-06-28 | Giat Ind Sa | Electrical initiation device with contactor. |
US20090308274A1 (en) * | 2008-06-11 | 2009-12-17 | Lockheed Martin Corporation | Integrated Pusher Plate for a Canister- or Gun-Launched Projectile and System Incorporating Same |
RU2584358C1 (en) * | 2015-02-17 | 2016-05-20 | Акционерное общество "Конструкторское бюро приборостроения им. академика А.Г. Шипунова" | Guided missile |
US9841256B2 (en) * | 2016-01-17 | 2017-12-12 | Wilcox Industries Corp. | Combined launch and storage tube for missile |
CN113606059B (en) * | 2021-06-22 | 2022-08-26 | 南阳北方向东工业有限公司 | Solid rocket safety insurance structure |
CN113800012B (en) * | 2021-09-30 | 2023-09-19 | 北京中科宇航技术有限公司 | Drag release device and system thereof |
CN113879569A (en) * | 2021-10-09 | 2022-01-04 | 航天科工火箭技术有限公司 | Low-impact unlocking satellite-arrow separation device and satellite-arrow separation system |
CN115096132B (en) * | 2022-06-22 | 2023-09-29 | 北京中科宇航技术有限公司 | Rocket support ring leveling device and launching pad |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1803366A (en) * | 1929-08-30 | 1931-05-05 | Charles C Stetson | Signal rocket |
US2436837A (en) * | 1943-10-14 | 1948-03-02 | John B Traylor | Fuse for antitank mines |
US2717042A (en) * | 1950-03-31 | 1955-09-06 | Specialties Dev Corp | Impact operated valve |
US2845002A (en) * | 1957-07-29 | 1958-07-29 | Jr Joseph I Ackerman | Ejection device |
US3242810A (en) * | 1962-09-27 | 1966-03-29 | Pointe Andre E La | Water launched missile |
-
0
- NL NL136198D patent/NL136198C/xx active
-
1965
- 1965-12-23 CH CH1774265A patent/CH449472A/en unknown
-
1966
- 1966-11-21 NL NL6616326A patent/NL6616326A/xx unknown
- 1966-11-30 AT AT1105466A patent/AT267969B/en active
- 1966-12-09 DE DE19661578033 patent/DE1578033A1/en active Pending
- 1966-12-14 US US601689A patent/US3398640A/en not_active Expired - Lifetime
- 1966-12-15 BE BE691283D patent/BE691283A/xx unknown
- 1966-12-21 GB GB57258/66A patent/GB1174049A/en not_active Expired
- 1966-12-23 SE SE17665/66A patent/SE320609B/xx unknown
- 1966-12-23 FR FR88599A patent/FR1506020A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
AT267969B (en) | 1969-01-27 |
GB1174049A (en) | 1969-12-10 |
US3398640A (en) | 1968-08-27 |
BE691283A (en) | 1967-05-16 |
NL136198C (en) | |
CH449472A (en) | 1967-12-31 |
NL6616326A (en) | 1967-06-26 |
DE1578033A1 (en) | 1970-12-03 |
FR1506020A (en) | 1967-12-15 |
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