Journal of Civil Aviation University of China ›› 2025, Vol. 43 ›› Issue (4): 29-35.

• Future airports and smart equipment • Previous Articles     Next Articles

Numerical simulation of laser cladding of T-shaped components

  

  1. 1. College of Aeronautical Engineering, CAUC, Tianjin 300300, China ;
    2. Civil Aircraft Test Flight Centre, COMAC, Shanghai 200232, China; 3. AMECO, Beijing 100621, China 
  • Received:2024-07-18 Revised:2024-11-24 Online:2025-09-22 Published:2025-09-22

Abstract:

In order to explore the laser cladding process to minimize the residual stress and deformation of T-shaped components, different process parameters were designed and the results of temperature field, residual stress field and deformation field were calculated under different process parameters in this paper. It was found that the constraint
mode affects the peak value and distribution of residual stress and deformation displacement of components, while
different cladding paths and speeds mainly affect the peak value of residual stress and deformation displacement.
The peak values of residual stress and deformation displacement under free placement constraint mode are 89.4%
and 71.1%, 66.3% and 61.6% lower than those under restraint mode of four-corner fixation and two-side fixation,
respectively. The peak values of residual stress and deformation displacement in reciprocating cladding path process are 26.9% and 6.8% lower than those in unidirectional sequential path process, and the peak values of residual
stress and deformation displacement in cladding speed of 10 mm/s are 11.0% and 4.9%, 35.5% and 34.8% lower
than those in cladding speed of 2.5 mm/s and 5.0 mm/s, respectively. According to the index analysis of reducing
residual stress and deformation, the optimal cladding process is to adopt the process of free placement constraint,
reciprocating cladding path and a higher cladding speed.

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