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Assembly method of interference fit steel ring structural member

An assembly method and interference fit technology, applied in the field of aerospace, can solve the problems of high cost, difficult assembly, difficulty in coping with the speed of aerospace technology, etc., achieve strong field applicability and avoid low processing efficiency

Active Publication Date: 2022-03-04
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Without the assistance of special tooling, there is the problem of difficult assembly, and the parts are stuck at the assembly interference point, and the installation cannot be completed
For example, the dispatch of special tooling involves the design and manufacture of the tooling. The whole process has a long cycle and high cost, and it is difficult to cope with the corresponding speed in the field of aerospace technology.

Method used

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  • Assembly method of interference fit steel ring structural member
  • Assembly method of interference fit steel ring structural member
  • Assembly method of interference fit steel ring structural member

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0019] This embodiment specifically provides an assembly method for the interference fit steel ring structure. According to the size of the snap ring, select the appropriate needle-nose pliers and wrench, and generally choose the same size.

[0020] Place the elastic open steel ring on the snap ring, use needle-nose pliers to split the steel ring, fit the steel ring on the snap ring, and use a wrench to assist in pressing the steel ring. After the steel ring is assembled to the boss of the snap ring, use Tap the steel ring into the groove in the snap ring with needle nose pliers and / or a wrench.

[0021] Use the chuck of the hand electric drill to clamp the steel ring of the snap ring to complete the installation step, so that the steel ring is on the same plane as the outer surface of the open ring; insert the mounting end of the snap ring in the clamped state into the matching hole, and at the same time the chuck and the outer surface of the open ring are on the same plane; ...

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Abstract

According to the assembly method of the interference fit steel ring structural member, proper sharp-nose pliers and wrenches are selected according to the size of the clamping ring, and generally, the sharp-nose pliers and the wrenches with the same size are selected. The elastic opening steel ring is placed on the clamping ring, the sharp-nose pliers are used for breaking off the steel ring, the clamping ring is tightly sleeved with the steel ring, the wrench is used for assisting in pressing the steel ring, and after the steel ring is assembled to the boss of the clamping ring, the sharp-nose pliers and / or the wrench are / is used for knocking the steel ring into the groove of the clamping ring. According to the assembling method, complex feature assembling is completed only through the sharp-nose pliers, the wrench and the electric hand drill chuck. By means of the assembling method, for assembling of the interference fit steel ring structural parts, special clamps do not need to be manufactured, the technical effect of a complete set of tools can be achieved only through simple tools, the field applicability is high, the tools can be used at any time, and the problem that the machining efficiency is low due to the fact that the tools cannot move or are difficult to move is solved.

Description

technical field [0001] The invention relates to the field of aerospace technology, and in particular provides an assembly method for an interference fit of an open steel ring. Background technique [0002] In the field of aerospace, it is necessary to set the interference snap ring in the positioning ring groove, and assemble the combined structural parts into the interference fit hole. Without the assistance of special tooling, there is the problem of difficult assembly, and the parts are stuck at the assembly interference point, and the installation cannot be completed. For example, the dispatch of special tooling involves the design and manufacture of the tooling. The whole process has a long cycle and high cost, and it is difficult to cope with the corresponding speed in the field of aerospace technology. Therefore, a fast, convenient, feasible and effective assembly method is imminent. Contents of the invention [0003] The purpose of the present invention is to pro...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B25B27/02
CPCB25B27/02Y02E10/72
Inventor 姜珊于浩康靖宇王婷赵世藩
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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