直 升 机 整 体 式 惯 性 粒 子 分 离 器 研 究 现 状

Yongli Zhang, Xiaotian Shan, Zhou Du, Cunliang Liu, Changxian Zhang

科研成果: 期刊稿件文章同行评审

摘要

The integral inertial particle separator is a helicopter air inlet protection device. It has excellent performance and wide application,which is of great significance to ensure the regular operation and improve the service life of helicopter engines. This paper summarizes the research progress of integral inertial particle separators,including the following aspects:the classification and aerodynamic parameters of the integral inertial particle separators are introduced. The research methods and their results of the integral inertial particle separators are sorted out. The factors affecting the performance of the integral inertial particle separators are summarized and analyzed. The future development of integral inertial particle separators is predicted. This paper can be the reference for future study and the guide to integral inertial particle separators' optimization design.

投稿的翻译标题Review status of helicopter integral inertial particle separators
源语言繁体中文
页(从-至)120-134
页数15
期刊Advances in Aeronautical Science and Engineering
15
3
DOI
出版状态已出版 - 6月 2024

关键词

  • factors affected
  • integral inertial particle separator
  • research method
  • separation efficiency
  • total inlet pressure loss

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