WU Ying-xiang 1 , WEI Xun-kai 2 , FENG Guo-quan 1 , ZHAO Zi-hao 3 , LI Lun-xu 3 , CHEN Guo 4.A Spalling Fault Simulation Method of Aeroengine Main Bearing Based on Hybrid Finite Element Model[J].航空发动机,2024,50(3):79-86
A Spalling Fault Simulation Method of Aeroengine Main Bearing Based on Hybrid Finite Element Model
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Key Words:main bearing  spalling fault  dynamic simulation  finite element  aeroengine
Author NameAffiliation
WU Ying-xiang 1 , WEI Xun-kai 2 , FENG Guo-quan 1 , ZHAO Zi-hao 3 , LI Lun-xu 3 , CHEN Guo 4 1. AECC Shenyang Engine Research Institute Shenyang 110015 China 2. Beijing Aviation Engineering and Technology Research Center Beijing 100076 China 3. College of Civil Aviation Nanjing University of Aeronautics and Astronautics Nanjing 210016 China 4. College of General Aviation and Flight Nanjing University of Aeronautics and Astronautics Liyang Jiangsu 213300 China 
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Abstract:A high-fidelity whole engine solid finite element model can realistically reflect the vibration characteristics of the aeroengine, however, it is difficult to take into account the complex dynamic model rolling element bearing fault, and its computational workload is too large to handle the whole engine nonlinear dynamic simulation under the excitation of main bearing spalling faults. In order to effectively diagnose main bearing faults, it is crucial to study the vibration response mechanism of the whole engine under the excitation of main bearing spalling faults. A hybrid simulation analysis method of main bearing fault dynamics based on solid finite element model and beam element finite element model was proposed. The support reaction forces of the main bearing connected to the casing were obtained by the simulation analysis of the whole engine beam element model, then, the rotor solid finite element model was removed from the whole engine solid finite element model, and the support reaction forces were directly applied to the bearing housing at each support, and the transient response analysis method was used to obtain the whole engine vibration response under the excitation of main bearing faults. Finally, the method was verified using the whole engine beam element model. The results show that the simulation signal under the excitation of main bearing faults can be obtained by using the hybrid finite element simulation method, with errors less than 1%, indicating the correctness and effectiveness of the proposed method.
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