Volume 27 Issue 6
Jun.  2012
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ZHU Yong-feng, FANG Yu-feng, FENG Wen-chun. Design and calculation of aircraft nacelle anti-icing system[J]. Journal of Aerospace Power, 2012, 27(6): 1326-1331.
Citation: ZHU Yong-feng, FANG Yu-feng, FENG Wen-chun. Design and calculation of aircraft nacelle anti-icing system[J]. Journal of Aerospace Power, 2012, 27(6): 1326-1331.
shu

Design and calculation of aircraft nacelle anti-icing system

  • 1.

    School of Aeronautics Science and Engineering, Beijing University of Aeronautic and Astronautic,Beijing 100191,China

  • 2.

    The Environment Control and Life Support System Design and Research Department, First Aircraft Institute of Aviation Industry Corporation of China,Xi'an 710089,China

  • 3.

    Aircraft Corporation,Aviation Industry Corporation of China,Beijing 100089,China

  • Received Date: 2011-07-25
  • Publish Date: 2012-06-28
    Abstract
  • The structure and theory of engine nacelle anti-icing (NAI) system were introduced.According to the principle that the heat available should be larger than the heat required,the critical design point and required flows of NAI were determining by calculating the required bleed air at complete evaporation and running wet station respectively.The coefficient of water collection of NAI system was determined using Euler method based on the coefficient of water collection of wing and the data similarity rule.According to the theory of allowed maximum thickness of ice,the performance of NAI system was calculated using the VSAERO/ICE software.The result of simulation shows that the maximum thickness of ice can meet at the critical condition.

     

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