发明名称 |
ENGINE MOUNTING SYSTEM |
摘要 |
A mounting system for a gas turbine engine includes a low pressure turbine section, a first bearing, a mid-turbine frame, and a rear mount. The first bearing supports at least a portion of the low pressure turbine section. The mid-turbine frame supports the first bearing. The rear mount is connected to the mid-turbine frame and is configured to react loads from the gas turbine engine. |
申请公布号 |
EP2969758(A4) |
申请公布日期 |
2016.11.23 |
申请号 |
EP20140779843 |
申请日期 |
2014.03.11 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SUCIU, GABRIEL L.;MERRY, BRIAN D. |
分类号 |
B64D27/10;F01D15/02;F02C7/20 |
主分类号 |
B64D27/10 |
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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