Flexible assembly operation table for rocket projectile guidance cabin

Abstract

The invention relates to a flexible assembly operation table for a rocket projectile guidance cabin, and belongs to the technical field of flexible assembly. The flexible assembly operation table can be rapidly switched and used in general assembly of projectile bodies of three different models I, II and III, a rear positioning component 2 is used for positioning and supporting rear cabins of the three projectile bodies, and a sliding component 3 is used for positioning and supporting front cabins of the three projectile bodies and slides backwards to conduct butt joint of the front cabins and the rear cabins of the projectile bodies. A quick-change rear positioning block 10 and a quick-change supporting angle block 11 in the rear positioning component 2 of the flexible assembly operation table are of a quick-change positioning structure and are used for quick change among three different projectile models, and the coaxiality of the front cabins and the rear cabins is guaranteed. The sliding component (3) of the flexible assembly operation table uses rubber covered rollers to support the projectile bodies, and the projectile bodies can axially rotate on a front sliding component, so that a workpiece can be rapidly aligned in the axial rotation direction. The flexible assembly operation table is simple in structure and ingenious in design, the labor intensity of workers is relieved, the manufacturing cost of enterprises is reduced, and the production efficiency of the enterprises is improved.

Description

technical field [0001] The invention belongs to the technical field of flexible assembly, and in particular relates to a flexible assembly operating platform for a rocket guidance cabin. Background technique [0002] In the past, the assembly of the rocket guidance cabin was mainly carried out manually on the workbench, with the assistance of necessary tooling and fixtures. Because each type of guidance cabin has different dimensions, internal structure, and different assembly methods, resulting in different tooling for each type of guidance cabin, and does not have the ability to switch production flexibly, which wastes space and increases the labor of workers. Intensity, and more labor and equipment are required, which increases the manufacturing cost and reduces the production efficiency. Contents of the invention [0003] (1) Technical problems to be solved [0004] The technical problem to be solved by the present invention is how to provide a flexible assembly cons...

AI Technical Summary

Problems solved by technology

[0004] The technical problem to be solved by the present invention is how to provide a flexible assembly console for the rocket guidance cabin, so as to solve the problem that the assembly of the rocket guidance cabin does not have the ability to switch production flexibly, which wastes space and increases the labor intensity of workers, and Need more labor and equipment, increase manufacturing costs, low production efficiency and other issues

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