发明名称 APPARATUS AND METHOD OF BALANCING A SHAFT OF AN AIRCRAFT ENGINE
摘要 <p>An apparatus for balancing a shaft(12) of an assembled aircraft engine(10) using a mounting plate (20) and standard fasteners(33). The mounting plate(20), which can be accessed from the front of the assembled engine, provides mounting means for the nose cone assembly (18) and balancing means by the addition of balancing weights through fasteners (33). The mounting plate (20) comprises a first group of holes (32) ans a second group of holes (34) to accommodate the fasteners (33).</p>
申请公布号 WO2005100941(A1) 申请公布日期 2005.10.27
申请号 WO2005CA00551 申请日期 2005.04.12
申请人 PRATT & WHITNEY CANADA CORP.;ROCKARTS, SEAN ANDRE;BARNETT, BARRY 发明人 ROCKARTS, SEAN ANDRE;BARNETT, BARRY
分类号 F01D5/02;F02C7/20;F16F15/22;F16F15/32;F16F15/34;G01M1/32;H02K5/16;H02K7/08;(IPC1-7):G01M1/32 主分类号 F01D5/02
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