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进气道温度畸变问题的研究
引用本文:胡主根.进气道温度畸变问题的研究[J].洪都科技,1999(4):1-5,12.
作者姓名:胡主根
作者单位:洪都航空集团650所
摘    要:重点研究稳态温度畸变对发动机稳定工作的影响。温度畸变分为周向温度畸变和径向温度畸变两种情况。温度畸变将使发动机喘振裕度降低。情况严重时可使发动机工作不稳定,或发动机熄火,从而危及飞行安全。本文半给出进气道温度畸变和稳定性因子的确定方法,作为进气道/发动机匹配研究的基础。

关 键 词:航空发动机  进气道  匹配  周向温度畸变  径向温度畸变  稳定性因子

Study on Intake Temperature Distortion
Hu Zhugen.Study on Intake Temperature Distortion[J].Hongdu Science and Technology,1999(4):1-5,12.
Authors:Hu Zhugen
Abstract:This paper is to emphatically study the influence of steady - state tem-perature distortion on the engine stable operation. The temperature distortion is classified astwo modes-the circumferential temperature distortion and radial temperature distortion. Theternperature distortion will cause the engine surge margin reduce and even the severe con-(Iilion will cause the engine operation unstable or flame - out to endanger the safetyflight. The paper is to provide the methods for determination of intake temperature distortionand stability factor as the basis for study of intake and engine compatibility.
Keywords:Circumferential temperature distortion Radial temperature distortion Stability factor
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