The invention discloses a
thermal analysis method of a heterogeneous material combined component considering multi-scale contact
thermal resistance, and belongs to the technical field of aero-engine thermal management. The method comprises the following steps: firstly, establishing a period calculation model of a CMC outer ring and
metal casing combined member, secondly, setting
anisotropy of CMC heat conduction according to geometric profile change of a gas outer ring, and finally, introducing an empirical relation expression of contact
thermal resistance by setting equivalent heat conduction of a contact area between the CMC outer ring and the
metal casing in CFD calculation. The difference between the two is explored by comparing the temperature field results of the combined component with or without the contact
thermal resistance, and the influence of the contact thermal resistance on flowing heat exchange is explored. According to the method, by considering the multi-scale contact thermal resistance between different materials, the influence of the contact thermal resistance on the
turbine flow heat exchange result is researched, meanwhile, the temperature field of the
turbine component in CFD calculation is corrected, and a guidance basis is provided for improving the prediction precision of the temperature result of the gas
turbine component under the complex gas
thermal load.