Welding deformation control method and device for gas turbine flame tube rectifying ring assembly

A gas turbine, welding deformation technology, applied in the direction of auxiliary equipment, welding equipment, welding equipment, etc., can solve the problems of large deviation of cross-sectional area, poor coaxiality, position degree of horseshoe-shaped plate column exceeding the design requirements, etc., and achieve high dimensional consistency , Strong operability and remarkable effect

Active Publication Date: 2021-04-02
CHINA HANGFA GUIZHOU LIYANG AVIATION POWER CO LTD
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Problems solved by technology

[0003] The present invention aims to provide a method and device for controlling the welding deformation of the gas turbine flame tube rectifying ring assembly, which solves the problem that the cross-sectional area of ​​the diffuser box of the above flame tube rectifier ring assembly has a large deviation after welding, and the welding height of the diffuser box exceeds 4±0.3mm. And the coaxiality difference between the inner and outer rings after welding, the position of multiple horseshoe-shaped plate columns exceeds the design requirements

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  • Welding deformation control method and device for gas turbine flame tube rectifying ring assembly
  • Welding deformation control method and device for gas turbine flame tube rectifying ring assembly
  • Welding deformation control method and device for gas turbine flame tube rectifying ring assembly

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Embodiment Construction

[0038] The technical solutions of the present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0039] The basic train of thought of the welding deformation control method of the gas turbine flame cylinder rectifying ring assembly in the present invention is:

[0040] (1) Weld the 10 horseshoe-shaped connecting plate columns of the rectification outer ring and the rectification inner ring to form a cavity with a specific cross-sectional area of ​​the flow channel (such as figure 1 shown).

[0041] (2) Group the diffuser boxes according to the assembly rules, and the grouped diffuser boxes are respectively welded with the inner support ring of the diffuser box and the outer support ring of the diffuser box, so as to complete the welding of 40 diffuser boxes (such as figure 2 shown)

[0042] (3) Put the 40 diffuser box assemblies in step (2) into the cavity body in step (1), and complete the assembly and weldin...

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Abstract

The invention discloses a welding deformation control method and device for a gas turbine flame tube rectifying ring assembly. The device comprises a first pressing plate, a positional tolerance positioning pin, diffusion box simulation blocks, an outer ring positioning groove, an inner ring positioning groove and a second pressing plate. According to the method, a rectifying outer ring, a rectifying inner ring and connecting plate columns are welded to form a first annular assembly which comprises an annular flow channel cavity located between the rectifying outer ring and the rectifying inner ring; then, multiple diffusion boxes are grouped and welded to a diffusion box inner supporting ring and a diffusion box outer supporting ring to form a second annular assembly; and finally, the second annular assembly is integrally arranged in the annular flow channel cavity of the first annular assembly, spot welding positioning is conducted, and the first annular assembly and the second annular assembly are welded.

Description

technical field [0001] The invention relates to the technical field of gas turbine welding deformation control, and mainly relates to a method and a control device for controlling the deformation of the cross-sectional area of ​​a flow channel during welding of a gas turbine flame tube rectifying ring assembly. Background technique [0002] The rectification ring assembly of the gas turbine flame tube is mainly combined with argon arc welding and vacuum brazing, and 40 diffuser boxes and 10 horseshoe-shaped plate columns are connected with the outer rectification ring and the inner rectification ring to form a rectification ring assembly. According to the design requirements, the installation height of the diffuser box is not greater than 4±0.3mm, and the roundness of the outer rectifying ring and the inner rectifying ring after welding is not greater than 2.0mm. Therefore, in order to ensure the design requirements, it is necessary to have a reasonable processing method and...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23K31/02B23K9/16B23K31/00B23K37/04
CPCB23K31/02B23K9/16B23K9/0026B23K31/003B23K37/0435
Inventor 陈昊丁清国李富宽吴欣星何强邓元贵陈成何刚
Owner CHINA HANGFA GUIZHOU LIYANG AVIATION POWER CO LTD
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