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METHOD OF SELECTION OF AUXILIARY POWER turbojet airplanes and turbojet engines, suitable for carrying out this method
METHOD OF SELECTION OF AUXILIARY POWER turbojet airplanes and turbojet engines, suitable for carrying out this method
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机译：适于执行该方法的辅助动力涡轮喷气飞机和涡轮喷气发动机的选择方法
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摘要
FIELD: engines and pumps.;SUBSTANCE: auxiliary power is taken off by means of shaft brought into action by means of high pressure turbine, and low pressure turbine efficiency is reduced at idle operation so that possibility of high pressure turbine operation at the speed that is sufficient for supply of the required auxiliary power can be provided.;EFFECT: invention allows optimum redistribution of powers of low and high pressure turbines.;4 cl, 2 dwg
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