发明名称 |
Gas turbine engine synchronizing ring bumper |
摘要 |
<p>A gas turbine engine (10) includes a synchronizing ring (34). A cradle (78) includes an integrally formed anti-rotation feature (82). The cradle (78) is secured to the synchronizing ring (34) and located relative thereto with the anti-rotation feature (82). A bumper (80) is slidably supported within the cradle (78). In one example, a bushing (48) is provided within a hole (90) in the bumper (80). A fastener (92) is inserted into the hole (90) and a bushing (48) to secure the bumper (80) to the synchronizing ring (34).</p> |
申请公布号 |
EP2481892(A2) |
申请公布日期 |
2012.08.01 |
申请号 |
EP20120153325 |
申请日期 |
2012.01.31 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
GASMEN, EUGENE C.;WIECKO, STANLEY |
分类号 |
F01D17/16;F01D25/24;F02C9/20 |
主分类号 |
F01D17/16 |
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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