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Journal of Graphics ›› 2025, Vol. 46 ›› Issue (5): 1061-1071.DOI: 10.11996/JG.j.2095-302X.2025051061

• Digital Design and Manufacture • Previous Articles     Next Articles

Simulation technology for braiding process of composite materials based on kinematic principles

WU Haoyu1(), YANG Xiaochao2, WANG Wei2,3(), ZHAO Gang1,2,3   

  1. 1 Research Institute of Aero-Engine, Beihang University, Beijing 102206, China
    2 School of Mechanical Engineering and Automation, Beihang University, Beijing 102206, China
    3 State Key Laboratory of Virtual Reality Technology and Systems, Beijing 100191, China
  • Received:2024-11-11 Accepted:2025-03-19 Online:2025-10-30 Published:2025-09-10
  • Contact: WANG Wei
  • About author:First author contact:

    WU Haoyu (1999-), PhD candidate. His main research interests cover computer aided design, computer aided engineering, etc. E-mail:buaawhy@buaa.edu.cn

  • Supported by:
    National Natural Science Foundation of China(61972011)

Abstract:

A simulation algorithm for the braiding process of composite materials is presented, specifically addressing the calculation and prediction of braiding machine control parameters, yarn trajectories, and braid angles. The algorithm operates through two complementary subprocesses: inverse solution generates machine control data based on target braid structures, while forward solution computes yarn trajectories and braid angle distributions using predefined control parameters. Initially, the surface of the mandrel is discretized into a set of triangular patches as program inputs. The mandrel centerline is extracted, and local solutions are performed according to kinematic principles. The inverse solution algorithm generates the braid structure of the preset braid angle and determines the corresponding take-up speed, while the forward solution algorithm calculates the yarn trajectories and braid angle distribution of specific take-up speed and control parameters. The BraidSim module, developed on the FreeCAD platform, integrates functionalities including mandrel surface meshing, trajectory generation, and dynamic yarn deposition simulation. The proposed algorithm has been validated through typical braiding cases including circular variable cross-section mandrel, square variable cross-section mandrel, aero-engine intake mandrel and spatial curve mandrel. Results demonstrate that the obtained take-up speed and braid angle distributions align closely with design expectations. Additional simulations are conducted for variable cross-section mandrel and curved centerline mandrel, generating corresponding inverse solution machine control data and forward solution braid angle distribution, demonstrating the applicability of the algorithm to complex mandrels.

Key words: composite material manufacturing, two-dimensional triaxial fabric, virtual simulation, FreeCAD, software design

CLC Number: