INFLUENCE OF TURBINE FIRST STATOR ROW COOLING ON TURBINE INLET GAS TEMPERATURE.

被引：0
|
作者：
Gorelov, G.M.
Fishbein, V.D.
Semenova, T.A.
机构：
来源：
Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika) | 1980年 / 23卷 / 01期
关键词：
D O I：
暂无
中图分类号：
V23 [航空发动机（推进系统）]; V43 [推进系统（发动机、推进器）];
学科分类号：
080703 ; 082502 ;
摘要：
The paper examines the problem of the quantitative influence of the flowrate of the air bled from the compressor to cool the first stator on the increase of the stator inlet gas temperature. The turbine rotor inlet gas temperature and the rotor cooling air flow-rate are assumed to be given. It has been found that in engines with cooled turbine first-stage stator there is always a significant difference between the temperature at the entrance to and exit from the stator, i. e. , at the rotor inlet.
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页码：77 / 80
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