发明名称 Method and apparatus for cooling high temperature ceramic turbine blade portions
摘要 An array of skewed cooling air conduits are embedded within a ceramic turbine blade for cooling an upper blade surface by producing a cool air film thereon, and by removing heat through conduction. The conduits provide a large bonding surface area in the ceramic, and are recessed to prevent clogging by the ceramic and to prevent direct contact with the hot gas stream at the upper blade surface.
申请公布号 US5039562(A) 申请公布日期 1991.08.13
申请号 US19900527929 申请日期 1990.05.23
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE 发明人 LIANG, GEORGE P.
分类号 F01D5/18;F01D5/28 主分类号 F01D5/18
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