Volume 36 Issue 2
Feb.  2021
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QI Lei, ZHANG Lei, PENG Yan, WANG Xi. Simulation and optimization design of aviation nickel resistance temperature sensor[J]. Journal of Aerospace Power, 2021, 36(2): 440-448. doi: 10.13224/j.cnki.jasp.2021.02.023
Citation: QI Lei, ZHANG Lei, PENG Yan, WANG Xi. Simulation and optimization design of aviation nickel resistance temperature sensor[J]. Journal of Aerospace Power, 2021, 36(2): 440-448. doi: 10.13224/j.cnki.jasp.2021.02.023
shu

Simulation and optimization design of aviation nickel resistance temperature sensor

doi: 10.13224/j.cnki.jasp.2021.02.023
  • 1.

    Airworthiness Certification Center,Civil Aviation Administration of China,Beijing 100102,China

  • 2.

    Suzhou Changfeng Avionics Company Limited,Aviation Industry Corporation of China Limited,Suzhou Jiangsu 215151,China

  • 3.

    School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China

  • Received Date: 2020-06-03
  • Publish Date: 2021-02-28
    Abstract
  • In order to meet the dynamic thermal response requirements of a aviation nickel resistance temperature sensor, the mathematical model was constructed, and the simulation analysis of six groups of design schemes was completed. The optimal design was determined through trial productions and verification tests. The sensor of a helical skeleton, which was composed of copper and filled with thermal conductive silicon grease, had the fastest dynamic thermal response. The simulation result of time constant was 17.3 s, and the test result was 16.58 s. This design of the sensor can meet the technical requirements.

     

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