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Method for repairing high-temperature alloy thin-walled cartridge receiver part through precision pulse welding

A technology of pulse welding and high temperature alloys, applied in welding equipment, welding equipment, auxiliary welding equipment, etc., can solve the problems of non-concentration of welding arc and deformation of parts, and achieve control of welding deformation, interlayer temperature, and reduction of welding stress level. Effect

Inactive Publication Date: 2016-02-03
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0005] In the prior art, the assembly accuracy of the thin-walled casing parts is relatively high. Due to the non-concentration of the welding arc, the parts after welding are deformed and cannot meet the repair requirements of the parts. The technical problem to be solved by the present invention is to provide a A method for repairing superalloy thin-wall casing parts by precision pulse welding that can meet the performance and dimensional accuracy requirements after welding and repairing parts

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  • Method for repairing high-temperature alloy thin-walled cartridge receiver part through precision pulse welding
  • Method for repairing high-temperature alloy thin-walled cartridge receiver part through precision pulse welding
  • Method for repairing high-temperature alloy thin-walled cartridge receiver part through precision pulse welding

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Embodiment Construction

[0035] The present invention will be further elaborated below in conjunction with the accompanying drawings of the description.

[0036] The method for repairing superalloy thin-wall casing parts by precision pulse welding in the present invention mainly includes: 1) predicting the welding deformation trend and analyzing the internal stress state of the parts after use; 2) reducing heat input and optimizing the welding process route; 3) Design special welding tooling to control parts deformation and welding pollution oxidation. Specifically include the following steps:

[0037] According to the defect length and position of thin-walled casing parts, combined with numerical simulation technology, the failure mode and stress state of parts are analyzed;

[0038] Accurately measure the front and rear mounting edges of the casing and other relevant dimensions before welding;

[0039] Use X-ray inspection and color inspection to determine defect location and size;

[0040] Proce...

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Abstract

The invention relates to a method for repairing a high-temperature alloy thin-walled cartridge receiver part through precision pulse welding. The method comprises the following steps: according to the length and position of the flaw of the thin-walled cartridge receiver part, analyzing the failure mode and the stress state of the part in combination with a numerical simulation technique; before welding, carrying out precision measurement on the front and rear mounting edges and other related sizes of a cartridge receiver; determining the position and size of the flaw by using X-ray examination and dyeing examination; carrying out pre-welding technical preparation; adopting a special welding protecting tool according to the position to be repaired; in combination with the failure mode and the stress state of the part, on account of the position and the size of the flaw, determining a single pulse or continuous pulse mode, welding technical parameters and welding order technical factors so as to reduce the stress level of the part after welding; and carrying out welding by a welding repairing technology determined in the above step. The method has the advantages that the weld joint performance reaches more than 90% of base metal performance, and standard requirements are met; and after welding, the radial run-out of the inner and outer mounting edges of the cartridge receiver is smaller than 0.08mm, the end surface run-out is smaller than 0.10mm, and assembling requirements are met.

Description

technical field [0001] The invention relates to the technical field of aero-engine manufacturing, in particular to a method for repairing superalloy thin-wall casing parts by precision pulse welding. Background technique [0002] After a life cycle of high-temperature alloy sheet metal welding casing, due to high-temperature gas, it is exposed to thermal stress, vibration and high-temperature environment for a long time. At the same time, it is also affected by factors such as stress release during the manufacturing process, which eventually leads to its Defects such as cracks often appear at the support plate. At present, the failure rate of casing parts is about 70%. [0003] Before the repair, the casing parts are already in the final dimensional accuracy state. Due to the large heat input of the conventional TIG welding repair process, the energy is not easy to control stably, etc., the thin-walled casing parts will have large deformation after welding, which cannot meet...

Claims

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Application Information

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IPC IPC(8): B23K31/02B23K37/00B23P6/00
CPCB23K31/02B23K37/00B23P6/00
Inventor 曲伸邵天巍杨涧石李晓光单忠宝
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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