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Method for processing thin wall welder cases of revolving body structures

A technology of welding casing and processing method, which is applied to the manufacture of thin-walled welded casing of the rear mounting side, and the processing field of the thin-walled welded casing of the belt front and rotary structure, can solve the residual stress distribution of welded components Unbalanced, main body coaxiality is out of tolerance, size is out of tolerance, etc., to achieve the effect of improving machining quality and processing efficiency, good structure and size, and small welding deformation

Inactive Publication Date: 2012-11-28
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Aiming at the problem that the size of the welding receiver mounting edge of the existing rotary structure is out of tolerance, the coaxiality of the front and rear mounting edges with the main body is out of tolerance after welding, and the residual stress distribution of the welded components is unbalanced, the present invention provides a rotary body The processing method of structural thin-wall welded casing
This method adopts the integral pre-deformation welding / forming method, which solves the deformation problem that may be caused by the engine assembly stress

Method used

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  • Method for processing thin wall welder cases of revolving body structures
  • Method for processing thin wall welder cases of revolving body structures
  • Method for processing thin wall welder cases of revolving body structures

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Embodiment Construction

[0021] A method for processing a thin-wall welded casing with a rotary structure, comprising the following steps:

[0022] Step 1: The material selected in this embodiment is gh3128. According to the plastic deformation characteristics of the selected material, it is judged that the welding shrinkage (that is, the welding deformation) is 1.5 mm, and the welding deformation in the diameter direction is 3 mm; The size and structure compensation design of the main body of the box, design and manufacture the front and rear mounting sides and the main body of the inner runner with a small margin structure, compared with the traditional processing method: the diameter of the main body is reduced by 3, and the diameter of the non-processing part of the mounting side The size is reduced by 3, the margin is reduced by 2, and the diameter of the overall front and rear mounting edges is reduced by 5; that is, the size of the front mounting edge is Ф456mm, the size of the rear mounting edg...

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Abstract

The invention discloses a method for processing thin wall welder cases of revolving body structures, belonging to the technical field of aero-engine metal plate forming and welding. According to the invention, a whole pre-deformation welding / forming method is used for solving the problems that sizes of mounting edges are out of tolerance, coaxiality of front and rear mounting edges with main bodies after welding is out of tolerance and residual stress distribution of welding components is unbalanced. The method provided by the invention comprises the following steps of: carrying out technological structure welding deformation allowance compensation design on a mounting edge and a main body of a thin wall welder case before the welding according to the plastic deformation characteristics of materials; plastically forming an expansion block according to an expander work part, size and final structural size requirement of parts; carrying out automatic argon arc welding on the mounting edge and the main body; assembling the welded welder case and expansion block on the expander work part to carry out expansion plastic forming and controlling the expansion forming size through adjusting pressure of the expander; and unloading the pressure of the expander, recovering the expander work part and unloading the parts to complete the welding / forming process.

Description

technical field [0001] The invention belongs to the technical field of sheet metal forming and welding manufacturing of aero-engines, and in particular relates to a processing method for a thin-walled welded casing of a rotary structure, which is applied to the manufacture of thin-walled welded casings with front and rear mounting edges. . Background technique [0002] Welded casing with rotary structure (such as figure 1 (shown) The most prominent technical problem in manufacturing is the coaxiality of the front and rear mounting edges and the main body. This quality problem will cause a series of problems that affect engine performance, such as changes in the section of the engine’s working flow channel and deformation caused by assembly stress. . The reason for analyzing the misalignment is mainly from the welding deformation and the additional stress deformation during the heat treatment process. Since the welding and heat treatment process is a material thermal proces...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23P15/00B23K9/167
Inventor 黄青松石竖鲲高献娟齐晓丽周勇
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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