涡喷发动机压气机失速、喘振及喘振点参数的测量和分析

本文介绍涡喷发动机在“净”和畸变进气下,涡轮一导面积减小12％或标准一导时,进行旋转失速和喘振试验的试验方法、测量方法及其试验的结果和分析。还介绍两种逼喘方法的试验,一种是静态逼喘,另一种是动态逼喘。试验结果表明,逼喘方式与喘振点参数有关联,动态逼喘的喘振点上的压比值与流量值分别比静态逼喘的低2.8％和1.7％。

MEASUREMENTS AND ANALYSIS OF SURGE,STALL AND SURGE POINT PARAMETERS IN TURBOJET COMPRESSORS

This paper presents the testing and measuring method of three kinds of flow instability test(rotating stall and surge),the test results and analysis of them for a turbojet engine with "clean" or distorted inlet flow. The tests have been carriedout as follows. ( 1 )testing of the"upper"and"lower"stall-point on the stall line of the engine with and without distorted inlet flow; ( 2 )tests of surge in the engine with "clean" or distorted inlet flow at n= 1.0, 0.933, 0.9, 0.87 and with rated Anb (area of first-stage turbine nozzle) or Anb decreased by 12%; (3)tests of static-forced surge(decreasing the area of engine nozzle very very slowly)and dynamic-forced surge for an engine with"clean" or distorted inlet flow. The results from the tests comprise.