Assembling tool of guided missile body

Abstract

The invention belongs to the technical field of missile assembling, and particularly discloses an assembling tool of a guided missile body. The assembling tool comprises a plurality of tool sections,each tool section comprises a substrate, a supporting frame, a fixing assembly and a connecting assembly, wherein at least four base trundles are arranged at the lower ends of the substrates; the supporting frames are arranged above the substrates in the width direction of the substrates, the supporting frames are in sliding connection with the substrates and can slide along the length direction of the substrates, and the upper end faces of the supporting frames are used for connecting with guided missile body sections; and the fixing assemblies are used for fixing the guided missile body sections and the corresponding supporting frames; the connecting assemblies are used for connecting two adjacent tool sections. The assembling tool can conveniently and rapidly carried out assembly and disassembly, the section assemblies of a guided missile is convenient and fast, and universality, flexibility and reliability of the guided missile body assembling sections are improved.

Description

technical field [0001] The invention relates to the technical field of missile assembly, in particular to an assembly tool for a missile body. Background technique [0002] At present, missiles generally adopt a multi-section cabin design. When the multi-section missile parts are assembled and combined, assembly tooling is required to assemble, transport and assist assembly of the missile parts. [0003] The prior art discloses a docking tool for a small-sized missile cabin, which includes an underframe, an axial rail, a lifting fine-tuning mechanism, a lateral fine-tuning mechanism and an axial force adding mechanism. The axial track is fixed on the bottom frame, the axial force mechanism is located at both ends of the axial track and fixed on the bottom frame, the lifting fine-tuning mechanism and the horizontal fine-tuning mechanism are installed on the axial track, and can move along the The axial track moves to realize the rectilinear reciprocating motion of each cabin...

AI Technical Summary

Problems solved by technology

[0004] The cabin docking tool disclosed in the prior art is an integral structure, which is suitable for docking assembly of small missiles. When the size of the missile is large, the size of the chassis and the axial rail will increase, which is not conducive to the docking of the cabin. Section transportation

Moreover, the cabin docking tool disclosed in the prior art needs to hoist each cabin to different positions above the chassis, and since each cabin needs to be hoisted to the docking tool, it is easy to cause the Collisions between cabins increase the complexity and danger of cabin hoisting

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