吴雄.短距起飞/ 垂直降落飞机动力装置特点及关键技术分析[J].航空发动机,2019,45(2):91-96
短距起飞/ 垂直降落飞机动力装置特点及关键技术分析
Analysis on the Characteristics and Key Technologies of the Propulsion System ofthe Short Takeoff / Vertical Landing Aircraft
  
DOI:
中文关键词:  短距起飞  垂直降落  航空发动机  升力风扇  推力矢量
英文关键词:short takeoff  vertical landing  aeroengine  lift fan  thrust vector
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作者单位E-mail
吴雄 海军研究院上海200436 1226197692@qq.com 
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中文摘要:
      动力装置是短距和垂直起落(STOVL)飞机设计的关键,直接影响其研制的成败。对国外3 种典型的STOVL 飞机进行分析, 结合不同STOVL 飞机需求对4 类动力装置特征、结构特点、工作原理及发展状况进行归纳及总结。详细提出STOVL 飞机动力装置的 6 类关键技术并进行了技术评价,对发展装备和开展技术研究提出建议,综合分析认为动力装置技术是中国发展STOVL 飞机的瓶 颈,需要重点研究并予以突破。
英文摘要:
      Abstract: Propulsion system was the key to the design of STOVL aircraft,which directly affected the success or failure of its development. Three kinds of typical STOVL aircraft in foreign countries were analysed. Combined with different STOVL aircraft requirements,the characteristics,structural characteristics,working principles and development of four types of propulsion system were concluded and summarized. Six types of key technologies of STOVL aircraft propulsion system were presented in detail and the technical evaluation was carried out. The suggestion was presented for the development of propulsion system and the research of key technologies. Comprehensive analysis shows that propulsion system technology is the bottleneck of the development of STOVL aircraft in China,which needs to be studied and broken through.
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