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Volume 25 Issue 2
Feb.  1999
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Journal of Beijing University of Aeronautics and Astronautics  > 1999  >  25(2): 201-203.
Jiang Libiao, Ni Qiang. Parametric design and analysis of front independent suspension of 6×6 off-road vehicle with ADAMS/View[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(02): 249-252. (in Chinese)
Citation: Chang Shinan, Han Fenghua. Performance Analysis on Hot-Air Anti-Icer of Airplane Engine Inlet[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(2): 201-203. (in Chinese)
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Performance Analysis on Hot-Air Anti-Icer of Airplane Engine Inlet

  • Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics

  • Received Date: 16 Jun 1998
  • Publish Date: 28 Feb 1999
    Abstract
  • Two patterns of air plane engine inlet hot-air anti-icer are introduced in this paper,one is circumferential anti-icer,the other is double skin corrugated chord direction anti-icer.Based on the thermal analysis of the two anti-icers,the heat transfer performance and temperature field of ice protected surface are compared.The results indicate that the structure of frontal anti-icer affects anti-icing effectiveness obviously for a hot-air anti-icing system,the double skin chord direction anti-icer is more efficient,but under the normal conditions,a circumferrential anti-icer can attain the goal of ice protection and its structure is more simple,so it is more practical.

     

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  • 1. 裘燮纲,韩凤华编.飞机防冰系统. 北京:航空专业教材编审组,1985 2. Rosenthal H A,Nelepovitz D O. Performance of a new nose-lip hot-air anti-icing concept.AIAA-85-1117,1985 3. Al-Khalil K M,Keith T G Jr,De Witt K J. Thermal analysis of engine inlet anti-icing systems.AIAA-89-0759,1989 4. Yeoman K E. Efficiency of a bleed air powered inlet icing protective system.AIAA-94-0717,1994
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