METHOD OF GAS TURBINE ENGINE TESTING Russian patent published in 2014 - IPC G01M15/14 

Abstract RU 2525057 C1

FIELD: engines and pumps.

SUBSTANCE: invention relates to definition of tuning gas temperature magnitude for turbine cooling outage at tests and operation of gas turbine engine.

EFFECT: higher accuracy of gas temperature setting owing to allowance for high-pressure compressor distributor set angle.

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RU 2 525 057 C1

Authors

Belov Aleksej Valer'Evich

Kiselev Andrej Leonidovich

Kuprik Viktor Viktorovich

Dates

2014-08-10Published

2013-06-06Filed