发明名称 Mounting system for a gas turbine engine
摘要 A mounting system for a gas turbine engine includes a mounting linkage assembly and a tangential link positioned generally transverse to the mounting linkage assembly. The mounting linkage assembly reacts at least a thrust load. The tangential link reacts at least a vertical load, a side load, and a torque load of the gas turbine engine.
申请公布号 US8167237(B2) 申请公布日期 2012.05.01
申请号 US20080052769 申请日期 2008.03.21
申请人 SUCIU GABRIEL L.;MERRY BRIAN D.;FRANKLIN DAVID W. J.;DYE CHRISTOPHER M.;UNITED TECHNOLOGIES CORPORATION 发明人 SUCIU GABRIEL L.;MERRY BRIAN D.;FRANKLIN DAVID W. J.;DYE CHRISTOPHER M.
分类号 B64D27/02 主分类号 B64D27/02
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