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 |
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源语言 | 繁体中文 |
页(从-至) | 120-134 |
页数 | 15 |
期刊 | Advances in Aeronautical Science and Engineering |
卷 | 15 |
期 | 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