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Method for assembling wheel disc and shaft in large interference fit in non-detachable rotor

A technology of interference and matching disks, which is applied in transportation and packaging, aircraft parts, metal processing, etc., can solve the problems of increasing the risk of assembly controllability and unsuitable assembly requirements, so as to improve assembly efficiency and assembly quality, and facilitate Promote and reduce the effect of human factors

Inactive Publication Date: 2017-05-31
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The original press-fitting method is only suitable for small interference fit between two parts. For the new structure rotor with large interference fit of the multi-stage disk shaft assembly, the original manual press-fitting assembly method is still used, which increases the Assembly controllability risk, it is not suitable to ensure that the design puts forward new assembly requirements. In order to realize the assembly of the new rotor disk shaft, a new assembly process method must be studied to meet the assembly requirements of the disk shaft

Method used

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  • Method for assembling wheel disc and shaft in large interference fit in non-detachable rotor
  • Method for assembling wheel disc and shaft in large interference fit in non-detachable rotor

Examples

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Embodiment 1

[0018] The non-detachable rotor has a large interference fit with the disc shaft assembly method. The rotor disc assembly 1 is set on the outside of the shaft 2. The large interference between the disc assembly 1 and the shaft 2 is 0.35-0.52mm, which needs to be calculated Given the temperature and holding time for the heating of the wheel assembly 1 and the cooling of the shaft 2, the assembly clearance range is obtained to meet the final assembly requirements. The assembly steps of the large interference fit disk shaft in the non-detachable rotor are as follows:

[0019] ① Put the wheel assembly 1 and the shaft 2 on the precision turntable, the wheel assembly 1 is set on the outside of the shaft 2, and the center line of the shaft 2 is perpendicular to the positioning surface 111 of the wheel assembly 1;

[0020] ②Mark the initial assembly line 1-1 and the initial assembly line 2-2 at the interference fit position of axis 2, and mark the initial assembly line 1-1 and 2-2 on t...

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Abstract

The invention discloses a method for assembling a wheel disc and a shaft in large interference fit in a non-detachable rotor. The method comprises the following steps: (1) a wheel disc component (1) and the shaft (2) are placed on a precision rotary table, the wheel disc component (1) sleeves the shaft (2), and the midline of the shaft (2) is perpendicular to a positioning surface (111) of the wheel disc component (1). The method for assembling the wheel disc and the shaft in large interference fit in the non-detachable rotor breaks through technical difficulty of large interference assembly in blind assembly, realizes assembly of a low-pressure compressor rotor, lowers influence of artificial factors, improves the assembly efficiency and the assembly quality, realizes gradual conversion of engine component assembly from traditional manual operation to intelligence and is wider in application range and convenient to popularize.

Description

technical field [0001] The invention relates to the technical field of disk shaft assembly methods, and in particular provides a large interference fit disk shaft assembly method in a non-detachable rotor. Background technique [0002] With the increasing development of domestic aero-engine technology, aero-engines with different functions in various fields are constantly being introduced. The design structure of the new low-pressure rotor of the engine will be widely used in modern aero-engines. The design of the rotor with this new structure Angle considerations also add more stringent new assembly technology requirements. Traditional aero-engine low-pressure rotors mostly adopt a disc-and-drum two-stage structure, and the material is made of stainless steel. The matching precision of parts and components requires a small interference connection. The emergence of this new structure of low-pressure rotors poses new challenges for rotor assembly. [0003] Over the years, th...

Claims

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Application Information

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IPC IPC(8): B25B27/02B23P19/02
CPCB25B27/02B23P19/02B23P2700/01
Inventor 杜宝玉荀于凌侯东旭刘丛辉王涛
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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