This invention relates to the field of
thermal simulation technology for aircraft braking systems, specifically to a numerical
simulation method for the temperature field of aircraft wheel brakes based on Ansys
Workbench. The method includes constructing a three-dimensional geometric model of the
braking system; defining the geometry, materials, and contact relationships of each component based on the three-dimensional geometric model and the operating conditions of the aircraft wheel brakes; writing APDL code based on the operating conditions of aircraft taxiing,
takeoff, and landing, and the geometry, materials, and contact relationships of each component; setting boundary conditions according to typical braking conditions; simulating the braking conditions based on the written APDL code using the boundary conditions; and obtaining the temperature field distribution through transient
thermal analysis. This invention, through the synergistic application of APDL command
stream embedding and
parametric analysis techniques, significantly improves the
simulation model's responsiveness and predictive reliability in complex braking environments, providing important
technical support for the thermal management design,
life assessment, and structural optimization of aircraft braking systems.