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。温度略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。本文将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。
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.
出处
《洪都科技》
1999年第4期1-5,12,共6页
Hongdu Science and Technology