Assembling tool of guided missile body

A technology for assembling tooling and projectiles, applied in the direction of workbenches, manufacturing tools, workshop equipment, etc., can solve the problems of underframe and axial rail size increase, cabin collision, unfavorable cabin docking section transportation, etc., to achieve Improve flexibility and scope of application, avoid collisions, hoisting positioning and action execution are convenient and fast

Pending Publication Date: 2018-12-07
上海崎亚电子科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
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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 tran

Method used

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  • Assembling tool of guided missile body
  • Assembling tool of guided missile body
  • Assembling tool of guided missile body

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Embodiment Construction

[0037] The present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, but not to limit the present invention. In addition, it should be noted that, for the convenience of description, only some structures related to the present invention are shown in the drawings but not all structures.

[0038] figure 1 A schematic structural view of the assembly tooling 10 of the projectile provided by the present invention, such as figure 1 As shown, the present embodiment provides an assembly tool 10 for assembling the missile body of the missile 20 so that a plurality of missile body segments 201 are assembled to form a complete missile body. The assembly tool 10 includes a hoisting assembly 2, a plurality of tooling segments 1 and a detection assembly 3, wherein the hoisting assembly 2 is used to lift the bo...

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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...

Claims

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Application Information

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IPC IPC(8): B25H1/10B25H5/00
CPCB25H1/10B25H5/00
Inventor 张建平尚凯丰侯新瑞
Owner 上海崎亚电子科技有限公司
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