轴流压缩系统不稳定形态的实验研究  

EXPERIMENTAL STUDY ON UNSTABLE BEHAVIOR OF AXIAL COMPRESSION SYSTEM

作　　者：李军[1] 刘志伟[2] 

机构地区：[1]西安市空军工程学院一系发动机教研室,710038 [2]西北工业大学

出　　处：《航空动力学报》1993年第1期34-36,共3页Journal of Aerospace Power

摘　　要：本文测取了一轴流压缩系统的不稳定形态。依据实验结果 ,确定了该系统不稳定型式的转换特征 ,分析了排气部件的影响规律 ,详细对比了单级压气机与孤立转子不稳定形态的差异。实验发现 ,在高转速下该压缩系统将形成“不可恢复性”Unstable behavior of an axial flow single stage compressor has been researched successfully by use of a simple dynamic measuring system.The character and the influence factors of the unstable behavior have been analyzed from systematic view.The experimental results demonstrate that the unstable types of the compressor could convert each other in certain conditions.The compressor rotor speed,the construction and size of the exhaust parts are the main factors influencing the convertion.The surge occurs in the compressor on condition of high rotor speed or large exhaust volume,otherwise the rotating stall appears.The decrease of the exhaust volume leads to increment of the surge frequency.There is an obvious difference of the unstable behavior between the single stage compressor and the isolated rotor compared.In the condition of high rotor speed ( >0 85),a stall phenomona of nonrecoverable stall appears.It′s character is also considered.

关 键 词：轴流压缩系统 不稳定形态 喘振 

分 类 号：V235.113[航空宇航科学与技术—航空宇航推进理论与工程]