FIELD: mechanical engineering; gas turbines. SUBSTANCE: proposed cooled ceramet blade of gas turbine has shaped ceramet envelope, metal carrying rod with flange on periphery and shank in root, and metal screen-deflector with "button" semi-spherical bosses arranged in clearance between ceramet envelope and carrying rod. Shank of carrying rod is made in form of "thread" lock enclosed from disk side by heat shielding ceramic linings. EFFECT: facilitated assembling and disassembling of ceramic blade. 14 cl, 4 dwg
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---|---|---|---|
QUASIADIABATIC CERAMIC NOZZLE ASSEMBLY OF HIGH- TEMPERATURE GAS TURBINE (VERSIONS) | 1999 |
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Authors
Dates
2003-05-10—Published
1999-01-10—Filed