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
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