An adjustable deviation adapter structure

Abstract

The invention discloses an adjustable deviation type adapter structure. The adjustable deviation type adapter structure comprises a metal shell and adapters; the adapters are nonuniformly mounted on the metal shell from dense to sparse; the metal shell is a split columnar structure, and is connected to form a launching cylinder; a missile can be positioned in the launching cylinder; the adapters are matched with the metal shell in appearance, and are arc structures; the adapters include main bodies and embedded parts; the main bodies adopt materials of polyurethane foams; the arc inner surfaces of the adapters are sprayed or bonded with polytetrafluoroethylene; the embedded parts adopt materials of metal, and are embedded in the polyurethane foams of the main bodies in the forming process of the main bodies; the embedded parts are connected with the metal shell through screws; and the heights of the embedded parts are controlled through adjusting screws to adjust clearances between the adapters and the missile. The adapters are fixedly connected with the launching cylinder; and after the missile is launched to deviate from the launching cylinder, the adapters cannot leave from the launching cylinder along with the missile, so that the separation function of the adapters from the missile is realized, and the adapters can be recycled.

Description

Technical field [0001] The invention relates to an adjustable deviation type adaptor structure, which belongs to the field of designing a launching system adjusting support structure. Background technique [0002] The adaptor structure is the connection and support device between the missile and the missile launcher, which plays an extremely important role in the storage, transportation, loading and unloading and launch of the missile in the launcher. The adaptor structure design technology is one of the key technologies of the launching system. [0003] The vertical heat launching concentric tube requires no throwing objects during the missile launch process. Therefore, it is necessary to use a shock-absorbing cushion adapter (hereinafter referred to as "adapter"), that is, the adapter is fixed on the inner wall of the inner tube of the launching tube and does not move with the missile. Achieve separation. In the process of storage and transportation of missiles and launchers, th...

AI Technical Summary

Problems solved by technology

[0004] The existing adapter structures are all high-matching structures with a small adjustment range, which requires high dimensional accuracy of the launch tube, which increases the processing cost of the launch tube and increases the difficulty of adapter installation

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