COOLING OF GAS TURBINES BLADES.

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作者：
Mukherjee, D.K.
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| 1600年 / 64期
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中图分类号：
TK [能源与动力工程];
学科分类号：
0807 ;
摘要：
Due to the high inlet temperature of gas turbines, the blades in the first rows have to be cooled. Using appropriate methods of cooling. Brown Boveri have succeeded in achieving a high cooling efficiency. Sophisticated computer programs are used in the design of blades and to predict the useful life of blading. Exhaustive experimental studies have confirmed the suitability of the method of calculation.
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