Method and device for assembling multiple shaft parts with angle requirements in deep hole

A technology of shaft parts and deep holes, which is applied in the field of mechanical assembly, can solve problems such as a large amount of time spent on assembly, secondary pollution of the shell, and narrow space, and achieve stable and reliable operation, improve production efficiency, and meet production needs.

Active Publication Date: 2020-04-17
XIAN AERO ENGINE CONTROLS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

If the pin 5 is used to assemble the first shaft 1, the second shaft 2 and the third shaft 3 sequentially outside the housing and then put them into the housing assembly 4, there will be problems due to the narrow space and the lack of visual inspection. Failure to fit or damage seals installed on the shaft
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  • Method and device for assembling multiple shaft parts with angle requirements in deep hole
  • Method and device for assembling multiple shaft parts with angle requirements in deep hole
  • Method and device for assembling multiple shaft parts with angle requirements in deep hole

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Embodiment Construction

[0028] The invention provides a method for assembling a plurality of shaft parts with angular requirements in a deep hole. The method includes the following steps:

[0029] 1) Determine the position of the pin hole on the shell assembly when the last shaft part among the multiple shaft parts is assembled in the deep hole of the shell assembly;

[0030] 2) Based on the position of the pin hole on the shell assembly, assemble the first shaft part among the multiple shaft parts in the deep hole of the shell assembly along the axial direction of the shell assembly;

[0031] 3) Based on the position of the pin hole on the shell assembly, install the connecting pin at the end of the second shaft part, and extend the second shaft part into the deep hole of the shell assembly along the axial direction of the shell assembly , so that the end face of the second shaft part is in contact with the end face of the first shaft part and connected with the first shaft part through a connecting...

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Abstract

The invention belongs to the field of machine assembling and relates to a method and a device for assembling multiple shaft parts with angle requirements in a deep hole. The method comprises the following steps of 1) determining the position a pin hole in a shell assembly when the last shaft part in the multiple shaft parts is assembled in the deep hole of the shell assembly; 2) assembling the first shaft part in the multiple shaft parts in the deep hole of the shell assembly based on the position of the pin hole in the shell assembly; 3) assembling the second shaft part in the multiple shaftparts in the deep hole of the shell assembly based on the position of the pin hole in the shell assembly, wherein the end surface of the second shaft part is in contact with the end surface of the first shaft part; and 4) repeating the step 3) till the multiple shaft parts are assembled in the deep hole of the shell assembly. The invention provides the method and the device for assembling multipleshaft parts with angle requirements in the deep hole, wherein the method and the device are accurate to position, convenient to assemble and stable and reliable in operating process and can improve the production efficiency.

Description

technical field [0001] The invention belongs to the field of mechanical assembly, and relates to an assembly method of shaft parts, in particular to a method and a device for assembling a plurality of shaft parts with angular requirements in a deep hole. Background technique [0002] Shaft parts are one of the common parts in all kinds of mechanical products. Due to functional requirements, such parts usually have clearance fit with the housing components, and the different cavities in the housing are separated by sealing rings. The structure of a part of an aeroengine is as follows: figure 1 As shown, the component includes a housing assembly 4 , and a first shaft 1 , a second shaft 2 and a third shaft 3 assembled inside the housing assembly 4 from inside to outside and along the axial direction of the housing assembly 4 . Among them, sealing rings 6, 7 and 8 need to be assembled between the first shaft 1, the second shaft 2 and the third shaft 3 and the housing assembly 4...

Claims

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Application Information

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IPC IPC(8): B23P19/00
CPCB23P19/00
Inventor 杨晨胡永文贾双良赵晨红李力徐敏
Owner XIAN AERO ENGINE CONTROLS
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