发明名称 Titanium MMC fanshaft with superalloy end attachment
摘要 A first hollow titanium MMC driveshaft portion is diffusion bonded to a third portion which in turn is fastened to a second superalloy portion via circumferentially positioned pins which are tightly fitted within aligned holed formed in the second and third driveshaft portions. The first, second and third portions are concentric with respect to the driveshaft centerline, and the pins are retained by means of a concentric retaining cylinder.
申请公布号 US5277661(A) 申请公布日期 1994.01.11
申请号 US19920842932 申请日期 1992.02.27
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE 发明人 MAK, STEPHEN W.;STEGEMILLER, HEIDI J.
分类号 F01D5/02;F16C3/02;(IPC1-7):F16C3/00;B63H1/26;B41J19/32 主分类号 F01D5/02
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