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吹气式旋转帽罩防冰特性 被引量:4

Anti-icing Properties of Blowing Rotating Spinner
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摘要 为研究吹气式旋转帽罩防冰特性,采用三维模拟技术对其进行数值分析,从流场、水撞击和积冰特性3个方面分析了吹气式旋转帽罩的防冰机理和效果,并利用防冰试验器开展了试验研究,从帽罩表面积冰厚度和范围两方面分析防冰情况,验证了在结冰环境下吹气式旋转帽罩的防冰效果。结果表明,吹气式旋转帽罩防冰结构具有良好的防冰效果。 In order to obtain the properties of anti-icing on the blowing rotating spinner,this paper analyzes the anti-icing principles and effects of the blowing rotating spinner in three aspects of air flow,impaction of water droplets and icing properties,using three-dimensional numerical simulation technology.Meanwhile,the experimental research is carried out using icing wind tunnel.The anti-icing conditions are analyzed from both of the icing thickness and range on the spinner surface,and the anti-icing effects of the blowing rotating spinner are validated in the icing environment.Above analysis shows that the anti-icing structure of the blowing rotating spinner has an excellent effect on anti-icing.
出处 《南京航空航天大学学报》 EI CAS CSCD 北大核心 2016年第3期359-365,共7页 Journal of Nanjing University of Aeronautics & Astronautics
关键词 旋转帽罩 吹气式防冰 数值模拟 试验验证 防冰效果 rotating spinner blowing-air anti-icing numerical simulation experimental validation effects of anti-icing
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  • 1Chaput M. Use of water vapor for engine deicing applica- tions[R]. Seville, Spain: 2007.SAE Aircraft & Engine Ic- ing Conference and Exhibition,2007.
  • 2Graversen P. Grand based measuring and warning of weather conditions in which engine icing may occur[R]. Seville,Spain:2007 SAE Aircraft & Engine Icing Confer- ence and Exhibition, 2007.
  • 3Frankenberger C. United States Army helicopter icing qualifications 1980[R]. AIAA-81-0406,1981.
  • 4Korkan K, Cross E. Experimental study of performance degradation of a model helicopter main rotor with simula- ted ice shapes[R]. AIAA-84-0184,1984.
  • 5Shaw R,Richter G. The UH-1H helicopter icing flight test program: an over[R]. AIAA-85 0338,1985.
  • 6Belz R,Brasier C, Murphy P, et al. A turbine engine inlet viewing system[R]. AIAA-86-1647,1986.
  • 7Kwon D,Sankar L. Numerical study of the effects of icing on fixed and rotary wing performance[R]. AIAA-91-0662, 1991.
  • 8Reddy E, Abumeri G. Structural tailoring of aircraft engine blade subject to ice impact constraints[R]. AIAA-92- 4710,1992.
  • 9Baruzzi G, Tran P, Habashi W. Actuator disk implementa- tion in FENSAP-ICE, a 3D Navier-Stokes in-flight icing simulation system[R]. AIAA 2003-619,2003.
  • 10Tsao J C,Kreeger R E. Evaluation of scaling methods for rotorcraft icing[R]. NASA/TM-2010-215801,2010.

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