Volume 39 Issue 5
Jan.  2024
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ZHAO Zhao, XIONG Jianjun, RAN Lin, et al. Hot air supply anti/de-icing test technology in large-scale icing wind tunnel[J]. Journal of Aerospace Power, 2024, 39(5):20210582 doi: 10.13224/j.cnki.jasp.20210582
Citation: ZHAO Zhao, XIONG Jianjun, RAN Lin, et al. Hot air supply anti/de-icing test technology in large-scale icing wind tunnel[J]. Journal of Aerospace Power, 2024, 39(5):20210582 doi: 10.13224/j.cnki.jasp.20210582

Hot air supply anti/de-icing test technology in large-scale icing wind tunnel

doi: 10.13224/j.cnki.jasp.20210582
  • Received Date: 2021-10-13
    Available Online: 2023-12-28
  • The establishment of hot air supply anti/de-icing test system in icing wind tunnel is the main means to carry out hot air anti/de-icing test. In order to meet the requirements of anti/de-icing system design and icing airworthiness certification for a series of domestic aircrafts, China Aerodynamics Research and Development Center (CARDC) carried out research on the hot air supply anti/de-icing test technology based on the 3 m×2 m large-scale icing wind tunnel, and independently developed the hot air supply anti/de-icing system. The digital valve flow control unit, electric heater unit, flow control unit and other test systems were designed and developed, and the test process and method were established. The perfect multi-channel hot sir supply anti/de-icing test technology was constructed, moreover, the dual-channel hot sir supply anti/de-icing test of a small aero-engine inlet was carried out. The test results indicated that the hot air supply anti/de-icing test system can simulate the hot air from the real compressor, allowing for multi-channel hot air supply test. The temperature control accuracy can reach ±1 ℃ and the flow control accuracy can reach ±1%. Meanwhile, it can provide a strong support for the anti/de-icing test system design and airworthiness certification of aircraft in China.

     

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