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Acta Armamentarii ›› 2025, Vol. 46 ›› Issue (3): 240017-.doi: 10.12382/bgxb.2024.0017

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Simulation Research on Deformation Laws of a Titanium Alloy Skin-skeleton Structure during Laser Beam Welding

WANG Lei1,2, DU Shaofeng2, LI Hongxing3, LIU Gang1, ZHANG Lei2, PENG Yong1,*()   

  1. 1 School of Materials Science and Engineering, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China
    2 National Key Laboratory of Special Vehicle Design and Manufacturing Integration Technology, Baotou 014030, Inner Mongolia, China
    3 Jiangsu Automation Research Institute, Lianyungang 222006, Jiangsu, China
  • Received:2024-01-04 Online:2024-04-13
  • Contact: PENG Yong

Abstract:

Titanium alloy is commonly used in the skin-skeleton structure of various aircraft rudder and wing components,which has received widespread attention in the weapons,aviation and aerospace industries.In this work,the laser welding deformation of a titanium alloy skin-skeleton structure is taken as the research object.The influence of welding sequences on welding deformation and stress is simulated and investigated using the thermal cycling method,and the welding sequences are optimized.The welding deformation and stress are significantly reduced by adding the turnover process in the welding.The results show that the peak welding stress is reduced by 27.4% from the original 1027.18MPa to 745.30MPa by prioritizing welding in the center area of the skin and adding multiple overturns during welding.The deformations at the feature points P1,P2 and P3 are decreased from the original 0.168mm,0.178mm and 0.198mm to 0.066mm,0.028mm and 0.021mm,respectively,by 60.7%,84.3% and 89.4%.The laser welding deformation of skin-skeleton structure is measured by a 3D laser scanner.Compared with the experimental results,the average error of the calculated results is 9.98%,which verifies the accuracy of the finite element model and the optimized welding sequence.

Key words: aircraft skin-skeleton structure, laser welding deformation, welding sequence optimization, thermal cycling curve algorithm

CLC Number: