等离子体激励式压气机

推进技术 ›› 2017, Vol. 38 ›› Issue (10): 2164-2171.

等离子体激励式压气机

李应红,吴云,张海灯,李军

空军工程大学航空航天工程学院，等离子体动力学重点实验室，陕西西安 710038,空军工程大学航空航天工程学院，等离子体动力学重点实验室，陕西西安 710038,空军工程大学航空航天工程学院，等离子体动力学重点实验室，陕西西安 710038,空军工程大学航空航天工程学院，等离子体动力学重点实验室，陕西西安 710038

发布日期:2021-08-15
作者简介:李应红，男，中国科学院院士，教授，博士生导师，研究领域为航空推进技术。
基金资助:
国家自然科学基金重点项目(51336011)。

Plasma Actuated Compressor

Science and Technology on Plasma Dynamics Laboratory，College of Aeronautics and Astronautics Engineering， Air Force Engineering University，Xi’an 710038，China,Science and Technology on Plasma Dynamics Laboratory，College of Aeronautics and Astronautics Engineering， Air Force Engineering University，Xi’an 710038，China,Science and Technology on Plasma Dynamics Laboratory，College of Aeronautics and Astronautics Engineering， Air Force Engineering University，Xi’an 710038，China and Science and Technology on Plasma Dynamics Laboratory，College of Aeronautics and Astronautics Engineering， Air Force Engineering University，Xi’an 710038，China

Published:2021-08-15

摘要/Abstract

摘要： 受吴仲华先生“叶轮机械三元流动理论”的启发，在前期压气机等离子体流动控制研究的基础上，进一步提出等离子体激励式压气机的概念，即将等离子体激励融入到S1，S2流面压气机气动设计之中，以释放常规压气机设计中失速裕度、负荷极限等因素的约束。本文旨在探讨等离子体流动控制在新一代高负荷压气机中应用的前景和研究趋势，通过原理论证与实例分析，首先阐述了等离子体激励式压气机的概念，然后梳理了压气机等离子体流动控制研究的若干进展，以论述等离子体激励式压气机设计的研究基础，最后给出了等离子体激励式压气机的典型技术路径和理论基础。

关键词: 等离子体激励；压气机造型；耦合优化；气动设计；流动控制

Abstract: Inspired by the “Theory of Three-Dimensional Flow in Turbomachines” of Dr Wu Chung-Hua， and based on the previous researches on plasma flow control of compressors， the notion of plasma actuated compressor， which intends to combine the plasma actuation with the compressor aerodynamic design in S1/S2 stream surfaces， is proposed to release the restriction of stall margin and loading limit in traditional compressor aerodynamic design. This paper aims at discussing the prospects and research trends of the applications of plasma flow control in modern highly-loaded compressors. Through theoretical argumentations and case studies， the notion of plasma actuated compressor is introduced firstly， and then to discourse the research basis for the design of plasma actuated compressor， some research progress on the plasma flow control of compressor by the authors are listed. The results provide the typical technological routes and theoretical basis of the plasma actuated compressor.

Key words: Plasma actuation；Compressor shaping；Coupling optimization；Aerodynamic design；Flow control

李应红,吴云,张海灯,李军. 等离子体激励式压气机[J]. 推进技术, 2017, 38(10): 2164-2171.

LI Ying-hong,WU Yun,ZHANG Hai-deng,LI Jun. Plasma Actuated Compressor[J]. Journal of Propulsion Technology, 2017, 38(10): 2164-2171.

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