| 发明名称 |
METHOD OF GAS TURBINE ENGINE TESTING |
| 摘要 |
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. |
| 申请公布号 |
RU2525057(C1) |
申请公布日期 |
2014.08.10 |
| 申请号 |
RU20130126081 |
申请日期 |
2013.06.06 |
| 申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "UFIMSKOE MOTOROSTROITEL'NOE PROIZVODSTVENNOE OB"EDINENIE" OAO "UMPO" ROSSIJSKAJA FEDERATSIJA RESPUBLIKA BASHKORTOSTAN |
发明人 |
BELOV ALEKSEJ VALER'EVICH;KISELEV ANDREJ LEONIDOVICH;KUPRIK VIKTOR VIKTOROVICH |
| 分类号 |
G01M15/14 |
主分类号 |
G01M15/14 |
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