出口静子安装角对压气机/吊架干涉的影响

推进技术 ›› 2004, Vol. 25 ›› Issue (2): 122-125.

出口静子安装角对压气机/吊架干涉的影响

张永新,陈懋章,蒋浩康,张辉

北京航空航天大学能源与动力工程学院北京100083;北京航空航天大学能源与动力工程学院北京100083;北京航空航天大学能源与动力工程学院北京100083;北京航空航天大学能源与动力工程学院北京100083

发布日期:2021-08-15
基金资助:
重点实验室基金(51459020101ZS4801和00JS48 3 1 HK5402)。

Effects of restaggering OGV on a compressor/pylon interaction

School of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;School of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;School of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;School of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China

Published:2021-08-15

摘要/Abstract

摘要： 针对调整出口导流叶片来减小吊架对压气机流场影响的方法,采用非定常数值模拟和实验方法,对分离式和一体化式吊架进行了研究。分离式吊架情况下,对减小扰动的作用不明显;一体化式吊架情况下,通过适当调整出口导流叶片安装角可以有效地降低转子后的压力扰动,改善流场。该优化方法适合于一体化式吊架。

关键词: 航空发动机;挂架;导流叶片;角度调制;轴流式压缩机;数值仿真;非定常空气动力学

Abstract: Unsteady numerical simulations and experiments were carried out to investigate the method of restaggering OGV to shield influence of pylons on a low-speed compressor, including separated pylon and separated pylon cases. Results show that restaggering OGV is more effective to reduce disturbance in integrated pylon case but with less effective in separated pylon case. The method of restaggering OGV is more suitable for integrated pylon case.

Key words: Aircraft engine;Pylon;Guide vane;Augular modulation;Axial flow compressor;Numerical simulations;Unsteady aerodynamics

张永新,陈懋章,蒋浩康,张辉. 出口静子安装角对压气机/吊架干涉的影响[J]. 推进技术, 2004, 25(2): 122-125.