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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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