COOLED MOVING OR NOZZLE BLADE OF GAS TURBINE Russian patent published in 2000 - IPC

Abstract RU 2151303 C1

FIELD: mechanical engineering; gas turbines. SUBSTANCE: cooled moving or nozzle blade of gas turbine has at least one cooling channel 15 inside blade 1. Wavy inner partition 11 is part of wall of cooling channel 15. EFFECT: increased service life improved reliability of blade. 11 cl, 7 dwg

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RU 2 151 303 C1

Authors

Bregman V.M.

Dates

2000-06-20—Published

1996-03-14—Filed