A connection and separation device for spacecraft
A technology for connecting and separating devices and spacecraft, which is applied to the docking devices of aerospace vehicles, weapon types, projectiles, etc., can solve the problems of failure of unlocking and separation, low reliability of theoretical unlocking and separation, and insufficient reliability of connection strength or separation. Advanced problems, to achieve the effect of improved reliability, strong versatility, and reliable connection
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[0018] The specific implementation process of the present invention will be further described below in conjunction with the accompanying drawings:
[0019] Such as figure 1 As shown, the present invention consists of detonating element 8, main charge 9, tail cap 10, piston 11, piston rod 12, sleeve 13, lock nut 14, first shear pin 15, steel ball 16, lock block 17, shell Body 18, lock bar 19, second shear pin 20 and so on. The lock nut 14 is connected with the first connection object, and the lock bar 19 is connected with the second connection object. The piston 11, the piston rod 12, the steel ball 16 and the second shear pin 20 constitute the inner actuator, and the sleeve 13, the first shear pin 15, the steel ball 16 and the lock block 17 constitute the outer actuator.
[0020] The tail cover 10 separates the inner actuator from the outer actuator. The inner actuator is located in the cavity inside the tail cover 10 , and the outer actuator is located in the cavity formed ...
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