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Sponsored by: Northwestern Polytechnical University  Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University
Research and Analysis on Overheating Protection Design of Aviation Oil-cooled Generator
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Affiliation:

1.Aviation Industry Corporation of China, Ltd (Shenyang Aircraft Design Institute);2.Aviation Industry Corporation of China, Ltd (Shaanxi Aviation Electric Co., Ltd.)

Clc Number:

V242

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    Abstract:

    The thermal field distribution of generator has a great influence on the failure phenomenon of the overheat protection component, which is the key parameter to be considered in the design. Based on the steady-state pressure solver and turbulence model in ANSYS software, the internal thermal field distribution of the motor under fault mode was simulated. The thermal field distribution of the stator, rotor and shell circulating oil circuit were obtained. The results show that the simulated thermal field is consistent with the actual temperature field distribution. The temperature gradient of low-melting alloy in the thermal trip mechanism is accordance with the internal thermal field distribution of the generator. It is helpful to protect the motor from overheating by changing the melting points of some key parts and the special softening temperature points of materials.

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SunLiRong, LaiShuaiLei, LiuZhuo. Research and Analysis on Overheating Protection Design of Aviation Oil-cooled Generator[J]. Advances in Aeronautical Science and Engineering,2023,14(6):153-159

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History
  • Received:October 08,2022
  • Revised:July 02,2023
  • Adopted:July 07,2023
  • Online: August 18,2023
  • Published: