发明名称 THERMAL PLUG FOR TURBINE BUCKET SHANK CAVITY AND RELATED METHOD
摘要 A turbine rotor disk includes a row of buckets secured about a radially outer periphery of the rotor disk, each bucket having an airfoil, a platform, a shank and a mounting portion, the mounting portion received in a radial slot formed in the rotor disk such that adjacent buckets in adjacent radial slots are separated by a rotor disk post located between adjacent mounting portions and a shank cavity between adjacent shanks, radially outward of the rotor disk post and radially inward of adjacent platforms. The shank cavity is substantially filled with at least one discrete thermal plug.
申请公布号 US2013108446(A1) 申请公布日期 2013.05.02
申请号 US201113283764 申请日期 2011.10.28
申请人 BUTKIEWICZ JEFFREY JOHN;GENERAL ELECTRIC COMPANY 发明人 BUTKIEWICZ JEFFREY JOHN
分类号 F01D5/08;B23P15/04;F01D5/02 主分类号 F01D5/08
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