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Experimental Analysis of Tubed Vortex Reducers in a Rotating Cavity with Radial Inflow

  • Jian He
  • , Xiang Luo*
  • , Xi Du
  • *此作品的通讯作者
  • Beihang University
  • PLA Air Force

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

The cooling air provided by the secondary air system is used for cooling and sealing the hot end components of the aero-engine. Vortex reducer is set to reduce the pressure loss of the bleed air section. Experimental research was performed to determine the pressure drop of tubed vortex reducer in a rotating cavity with radial inflow. The experiment revealed that the performance of a vortex reducer is determined by geometry length, the rotational Reynolds number and the mass-flow coefficient. Within the condition scope of the present study, the pressure loss increases as the increase of tube length. According to the experimental data, fitting curves of the pressure loss coefficient, which related with Rossby number, is given. It can provide the reference for the design of the tubed vortex reducer.

源语言英语
主期刊名Computational and Experimental Simulations in Engineering - Proceedings of ICCES 2023—Volume 1
编辑Shaofan Li
出版商Springer Science and Business Media B.V.
1021-1031
页数11
ISBN(印刷版)9783031425141
DOI
出版状态已出版 - 2024
活动29th International Conference on Computational and Experimental Engineering and Sciences, ICCES 2023 - Shenzhen, 中国
期限: 26 5月 202329 5月 2023

出版系列

姓名Mechanisms and Machine Science
143
ISSN(印刷版)2211-0984
ISSN(电子版)2211-0992

会议

会议29th International Conference on Computational and Experimental Engineering and Sciences, ICCES 2023
国家/地区中国
Shenzhen
时期26/05/2329/05/23

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