Projectile-fuse connection structure and initiation device
A connection structure and fuze technology, applied in fuzes, weapon accessories, offensive equipment, etc., can solve the problems of weak stress wave attenuation and filtering, high rigidity of the threaded connection structure, and damage to the fuze, saving assembly and disassembly time, avoiding Fuze damage, the effect of avoiding damage
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Embodiment 1
[0032] This embodiment provides a pop-up connection structure, please refer to figure 1 , figure 2 and image 3 , the elastic connection structure includes a projectile body 1, a fuze 2 and a fuze pressure ring 3; a mounting hole 11 is opened on the projectile body 1, and the fuze pressure ring 3 is configured to crimp the fuze 2 inside the installation hole 11 and make the fuze A gap is formed between the peripheral wall of 2 and the peripheral wall of the mounting hole 11. Specifically, the installation hole 11 can be opened on the tail section of the missile body 1 .
[0033] In this embodiment, the fuze 2 is crimped on the projectile body 1 with the fuze pressure ring 3, and only needs to take off the fuze pressure ring 3 during disassembly. Compared with the fuze 2 and the projectile body 1 in the prior art The multi-turn thread connection between them has the beneficial effect of simple disassembly and can save assembly and disassembly time;
[0034] And, in this em...
Embodiment 2
[0047] This embodiment provides a detonating device, the detonating device includes the spring connection structure provided in the first embodiment.
[0048] see figure 1 , figure 2 and image 3 , the elastic connection structure includes a projectile body 1, a fuze 2 and a fuze pressure ring 3; a mounting hole 11 is opened on the projectile body 1, and the fuze pressure ring 3 is configured to crimp the fuze 2 inside the installation hole 11 and make the fuze A gap is formed between the peripheral wall of 2 and the peripheral wall of the mounting hole 11. Specifically, the installation hole 11 can be opened on the tail section of the missile body 1 .
[0049] In this embodiment, the fuze 2 is crimped on the projectile body 1 with the fuze pressure ring 3, and only needs to take off the fuze pressure ring 3 during disassembly. Compared with the fuze 2 and the projectile body 1 in the prior art The multi-turn thread connection between them has the beneficial effect of sim...
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