发明名称 Turbomachinery shaft insert
摘要 An insert for a hollow rotatable shaft on the end of which an impeller is mounted, the insert having a first cylindrical portion receivable within the end of the shaft. The insert includes a radially extending portion adjacent the end of the shaft having an annular wall including radially inner and outer surfaces for engaging tightly similar surfaces in a recess formed in the impeller to provide inner and outer pilot surfaces. The insert also includes a tubular extension which is received within a bore in the impeller, the tubular extension having spaced longitudinally extending slits for permitting the extension together with radially extending hook-like tongues thereon to be received within radial slots in the bore of the impeller to lock the impeller to the insert.
申请公布号 US4890946(A) 申请公布日期 1990.01.02
申请号 US19890358028 申请日期 1989.05.26
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE UNITED STATES NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 VON PRAGENAU, GEORGE L.
分类号 F01D5/02;F16D1/06 主分类号 F01D5/02
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