| 发明名称 |
Mounting system for a gas turbine engine |
| 摘要 |
A mounting system (56) for a gas turbine engine (10) includes a thrust ring (62) and a linkage assembly (64). The linkage assembly (64) is at least partially received by the thrust ring (62). The linkage assembly (64) reacts at least a side load and a thrust load communicated from the thrust ring (62). |
| 申请公布号 |
EP2080879(B1) |
申请公布日期 |
2016.05.18 |
| 申请号 |
EP20090250067 |
申请日期 |
2009.01.12 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SUCIU, GABRIEL L.;MARX, JON A.;MERRY, BRIAN D.;DYE, CHRISTOPHER |
| 分类号 |
F02C7/20;B64D27/18;B64D27/26;B64D29/06 |
主分类号 |
F02C7/20 |
| 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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