| 发明名称 |
COOLED ROTOR PERFORATED TURBINE BLADE |
| 摘要 |
FIELD: manufacturing technology.SUBSTANCE: cooled working perforated turbine blade shell comprises a perforated with small diameter cooling holes curved shape. Middle line of each of cooling holes is located in plane of vane along blade and normal to surface contour of blade profile.EFFECT: higher cooling efficiency of turbine blade and higher reliability and service life.1 cl, 4 dwg |
| 申请公布号 |
RU2582539(C1) |
申请公布日期 |
2016.04.27 |
| 申请号 |
RU20150119120 |
申请日期 |
2015.05.20 |
| 申请人 |
FEDERALNOE GOSUDARSTVENNOE BJUDZHETNOE OBRAZOVATELNOE UCHREZHDENIE VYSSHEGO PROFESSIONALNOGO OBRAZOVANIJA "UFIMSKIJ GOSUDARSTVENNYJ AVIATSIONNYJ TEKHNICHESKIJ UNIVERSITET" |
发明人 |
GISHVAROV ANAS SAIDOVICH;TRUSHIN VLADIMIR ALEKSEEVICH |
| 分类号 |
F01D5/18 |
主分类号 |
F01D5/18 |
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