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1. 发明专利

NO147433C 未知
公开(公告)号：NO147433C
公开(公告)日：1983-04-06
申请号：NO794350
申请日：1979-12-28
申请人： HUGHES AIRCRAFT CO
发明人： LEIGH MICHAEL L , STUBBS RICHARD D
IPC分类号： F41F3/052 , F41F3/04
摘要： A missile or rocket detent and positive release mechanism is actuated by the thrustor of a rocket (10). The mechanism is mounted on a housing (42) to which a rocket launcher tube (15) is secured. A spring-loaded lever (50), having a notch (52) and a cam follower (55) at opposite ends, lies parallel to the rocket and is pivoted to the housing. Its notched end extends into the launch tube for positively locking the rocket into place. A spring-loaded sear (62) also lies parallel to the housing, is reciprocable on the launcher, and has a cam (64) which rests against the first lever's follower. At its other end, the sear is pivoted to a toggle (44) lying perpendicular to the housing so that one end (48b) nests against a housing end surface (46) and its other end (48a) extends into the path of the exhaust from the rocket's thrustor. The rocket blast pivots the toggle around on its pivot point against the housing end surface to linearly move the sear and its cam, which pushes against the follower-end of the first lever and pivots the spring-loaded lever sufficiently to withdraw its notched-end from engagement with, and to release the rocket.

2. 发明专利

IT7951221D0 未知
公开(公告)号：IT7951221D0
公开(公告)日：1979-12-28
申请号：IT5122179
申请日：1979-12-28
申请人： HUGHES AIRCRAFT CO
发明人： LEIGH MICHAEL L , STUBBS RICHARD D
IPC分类号： F41F3/052 , B64G
摘要： A missile or rocket detent and positive release mechanism is actuated by the thrustor of a rocket (10). The mechanism is mounted on a housing (42) to which a rocket launcher tube (15) is secured. A spring-loaded lever (50), having a notch (52) and a cam follower (55) at opposite ends, lies parallel to the rocket and is pivoted to the housing. Its notched end extends into the launch tube for positively locking the rocket into place. A spring-loaded sear (62) also lies parallel to the housing, is reciprocable on the launcher, and has a cam (64) which rests against the first lever's follower. At its other end, the sear is pivoted to a toggle (44) lying perpendicular to the housing so that one end (48b) nests against a housing end surface (46) and its other end (48a) extends into the path of the exhaust from the rocket's thrustor. The rocket blast pivots the toggle around on its pivot point against the housing end surface to linearly move the sear and its cam, which pushes against the follower-end of the first lever and pivots the spring-loaded lever sufficiently to withdraw its notched-end from engagement with, and to release the rocket.

3. 发明专利

IT1164799B 未知
公开(公告)号：IT1164799B
公开(公告)日：1987-04-15
申请号：IT5122179
申请日：1979-12-28
申请人： HUGHES AIRCRAFT CO
发明人： LEIGH MICHAEL L , STUBBS RICHARD D
IPC分类号： F41F3/052 , B64G
摘要： A missile or rocket detent and positive release mechanism is actuated by the thrustor of a rocket (10). The mechanism is mounted on a housing (42) to which a rocket launcher tube (15) is secured. A spring-loaded lever (50), having a notch (52) and a cam follower (55) at opposite ends, lies parallel to the rocket and is pivoted to the housing. Its notched end extends into the launch tube for positively locking the rocket into place. A spring-loaded sear (62) also lies parallel to the housing, is reciprocable on the launcher, and has a cam (64) which rests against the first lever's follower. At its other end, the sear is pivoted to a toggle (44) lying perpendicular to the housing so that one end (48b) nests against a housing end surface (46) and its other end (48a) extends into the path of the exhaust from the rocket's thrustor. The rocket blast pivots the toggle around on its pivot point against the housing end surface to linearly move the sear and its cam, which pushes against the follower-end of the first lever and pivots the spring-loaded lever sufficiently to withdraw its notched-end from engagement with, and to release the rocket.

4. 发明专利

NO794350L 未知
公开(公告)号：NO794350L
公开(公告)日：1980-07-01
申请号：NO794350
申请日：1979-12-28
申请人： HUGHES AIRCRAFT CO
发明人： LEIGH MICHAEL L , STUBBS RICHARD D
IPC分类号： F41F3/052 , F41F
摘要： A missile or rocket detent and positive release mechanism is actuated by the thrustor of a rocket (10). The mechanism is mounted on a housing (42) to which a rocket launcher tube (15) is secured. A spring-loaded lever (50), having a notch (52) and a cam follower (55) at opposite ends, lies parallel to the rocket and is pivoted to the housing. Its notched end extends into the launch tube for positively locking the rocket into place. A spring-loaded sear (62) also lies parallel to the housing, is reciprocable on the launcher, and has a cam (64) which rests against the first lever's follower. At its other end, the sear is pivoted to a toggle (44) lying perpendicular to the housing so that one end (48b) nests against a housing end surface (46) and its other end (48a) extends into the path of the exhaust from the rocket's thrustor. The rocket blast pivots the toggle around on its pivot point against the housing end surface to linearly move the sear and its cam, which pushes against the follower-end of the first lever and pivots the spring-loaded lever sufficiently to withdraw its notched-end from engagement with, and to release the rocket.

5. 发明专利

NO794350A 未知
公开(公告)号：NO794350A
公开(公告)日：1980-07-01
申请号：NO794350
申请日：1979-12-28
申请人： HUGHES AIRCRAFT CO
发明人： LEIGH MICHAEL L , STUBBS RICHARD D
IPC分类号： F41F3/052 , F41F
CPC分类号： F41F3/052

6. 发明专利

CA1153597A AUTOMATIC BLAST ACTUATED POSITIVE RELEASE MISSILE DETENT 未知
公开(公告)号：CA1153597A
公开(公告)日：1983-09-13
申请号：CA338177
申请日：1979-10-23
申请人： HUGHES AIRCRAFT CO
发明人： LEIGH MICHAEL L , STUBBS RICHARD D
IPC分类号： F41F3/052 , F41F9/00 , F41F11/00 , F41F13/00
摘要： PD-77264 AUTOMATIC BLAST ACTUATED POSITIVE Michael L. Leigh RELEASE MYSSILE DETENT Richard D. Stubbs A missile or rocket detent and positive release mechanism actuated by the rocket's thrustor. The mechanism is mounted on the outside of a rocket launcher tube and the notched-end of a spring-loaded lever extends into the launch tube for positively locking a rocket into place. The lever has a centrally located pivot point and a cam at the other end. One end of a sear is connected to a second lever which extends into the rocket's blast region. The other end of the sear has a cam actuating surface which is disposed against the first lever's cam. The blast from the rocket's thrustor pushes the second lever around on its pivot point such that the sear actuates the cam-end of the first lever, rotating it a small distance on its pivot point thereby withdrawing its notched-end and releasing the rocket.

7. 发明专利

NO147433B 未知
公开(公告)号：NO147433B
公开(公告)日：1982-12-27
申请号：NO794350
申请日：1979-12-28
申请人： HUGHES AIRCRAFT CO
发明人： LEIGH MICHAEL L , STUBBS RICHARD D
IPC分类号： F41F3/052 , F41F3/04
摘要： A missile or rocket detent and positive release mechanism is actuated by the thrustor of a rocket (10). The mechanism is mounted on a housing (42) to which a rocket launcher tube (15) is secured. A spring-loaded lever (50), having a notch (52) and a cam follower (55) at opposite ends, lies parallel to the rocket and is pivoted to the housing. Its notched end extends into the launch tube for positively locking the rocket into place. A spring-loaded sear (62) also lies parallel to the housing, is reciprocable on the launcher, and has a cam (64) which rests against the first lever's follower. At its other end, the sear is pivoted to a toggle (44) lying perpendicular to the housing so that one end (48b) nests against a housing end surface (46) and its other end (48a) extends into the path of the exhaust from the rocket's thrustor. The rocket blast pivots the toggle around on its pivot point against the housing end surface to linearly move the sear and its cam, which pushes against the follower-end of the first lever and pivots the spring-loaded lever sufficiently to withdraw its notched-end from engagement with, and to release the rocket.

8. 发明专利

CA1131477A BLAST-ENABLED MISSILE DETENT RELEASE MECHANISM 未知
公开(公告)号：CA1131477A
公开(公告)日：1982-09-14
申请号：CA338178
申请日：1979-10-23
申请人： HUGHES AIRCRAFT CO
发明人： FALLON RAY D , STUBBS RICHARD D
IPC分类号： F41F3/052 , F41F3/06
摘要： PD-77265 BLAST ENABLED MISSILE Ray D. Fallon DETENT/RELEASE MECHANISM Richard D. Stubbs A missile or rocket detent and positive release mechanism actuated by the rocket's thrustor. The mechanism is mounted on the outside of a rocket launcher tube and the notched-end of a spring-loaded lever extends into the launch tube for positively locking a rocket into-place. One end of a sear extends over the spring lever for maintaining the lever in a locked position. A lever is connected to the other end of the sear and pivots thereon. The second lever extends into a rockets blast region and the high speed exhaust gasses cause it to be pivoted out of the way. The pivoting lever withdraws the sear from the spring loaded lever, releasing the rocket.

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