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开式转子发动机对转桨扇设计 被引量:10

Open Rotor Contra-Rotating Prop-Fan Design
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摘要 高推进效率的对转桨扇是开式转子发动机最关键的部件之一。国外航空强国对其开展了大量的CFD计算分析及试验验证工作,优化气动性能,降低噪声等级,以满足适航标准;国内目前尚缺乏对开式转子对转桨扇设计技术和CFD分析的相关研究。本文在现有压气机设计技术的基础上,改进CFD设计分析方法,探索设计出开式转子发动机的对转桨扇,并进行了三维定常流场分析。通过与国外文献研究结果的分析对比,初步验证了本文设计和计算结果的合理性。 Contra-rotating prop-fan (CRP) with high propulsive efficiency is one of the most critical compo-nents on open rotor engine. Western countries have completed numerous CFD investigations and test dem-onstration on CRP to improve its aerodynamic performance and noise level to satisfy airworthiness require-ments. However, few investigations can be found in China concerning CRP design and CFD analysis. Based on current compressor design technique, CFD design and analysis method was improved. Using this meth-od, a kind of contra-rotating prop-fan adaptive to open rotor engine was designed and 3D steady flow analy-sis was carried out. The design and calculation results were initially demonstrated the sound through the comparison with outcomes of some foreign research.
出处 《燃气涡轮试验与研究》 北大核心 2014年第1期1-5,共5页 Gas Turbine Experiment and Research
关键词 航空发动机 开式转子 对转桨扇 叶片造型 CFD分析 aero-engine open rotors contra-rotating prop-fan blade shaping CFD analysis
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参考文献5

  • 1Envia E. NASA Open Rotor Noise Research[C]//.14th CEAS-ASC Workshop & 5'h Scientific Workshop of X3-Noise Aeroacoustics of High-Speed Aircraft Propel- lers and Open Rotors. Warsaw, Poland: Institute of Avia- tion, 2010.
  • 2胡晓煜.A320/B737客机2020年后换代,开式转子发动机显露希望[J].燃气涡轮试验与研究,2009,22(3):60-62. 被引量:4
  • 3刘红霞,梁春华.开式转子发动机研制与进展[J].国际航空,2010(4):75-77. 被引量:7
  • 4GE Aircraft Engines, GE36 Project Department. Full Scale Technology Demonstration of a Modern Counterrotat- ing Unducted Fan Engine Concept: Design Report[R]. NASA CR-180867, 1987.
  • 5Busch E R, Ke$1er M, Krimer E. Numerical Investigation of Counter-rotating Open Rotor Noise Emission in Differ- ent Flight Conditions[R]. ASME GT2012-68625,2012.

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