Large-size thin-walled rocket tank cylinder segment laser welding system and method

CN121339686BActive Publication Date: 2026-08-28BEIJING JIUTIANXINGGE AEROSPACE TECH CO LTD +1
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Patent Information

Application Number
CN202511908935.4
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2025-12-17
Publication Date
2026-08-28
Estimated Expiration
2045-12-17

AI Technical Summary

Technical Problem

[0006]本发明的目的在于解决针对大尺寸薄壁贮箱筒段焊接过程中出现的工件结构变形显著、焊缝精度不易把控导致出现的错边、间隙不均等问题,提供一种大尺寸薄壁火箭贮箱筒段激光焊接系统及方法

Benefits of technology

1、设置支撑单元,能够为待焊工件或贮箱筒段提供有效的支撑平台以及灵活的调整平台,为提高火箭贮箱的制造成品率提供了有利保障;

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Abstract

The application discloses a large-size thin-wall rocket tank cylinder segment laser welding system and method, and belongs to the technical field of aerospace equipment manufacturing equipment. The welding system comprises a support unit configured to provide support and adjustment platform for the workpiece to be welded; a longitudinal seam cutting and welding unit configured to position, edge cut, longitudinally gap adjust and longitudinally seam weld a plurality of workpieces to be welded; a girth seam cutting and welding unit configured to edge cut, position, girth gap adjust and girth seam weld two tank cylinder segments; and a control unit electrically connected with the support unit, the longitudinal seam cutting and welding unit and the girth seam cutting and welding unit, configured to control the running state of the support unit, the longitudinal seam cutting and welding unit and the girth seam cutting and welding unit. The application aims to solve the problems of workpiece structure deformation, misalignment, uneven gap and the like caused by the difficulty in controlling the welding seam precision in the welding process of the large-size thin-wall tank cylinder segment.
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Citation Information

Patent Citations

  • Robotic variable polarity plasma arc welding system for the bottom of launch vehicle propellant tanks

    CN106342007B