发明名称 STRUCTURAL GUIDE VANE CIRCUMFERENTIAL LOAD BEARING SHEAR PIN
摘要 A turbofan engine structural guide vane is mounted to a forward bulkhead of a core engine case structure at an inner end and to a fan case at an outer end. A plurality of shear pins extend from the aft portion of the structural guide vane into a corresponding plurality of openings defined in the bulkhead for bearing circumferential loads.
申请公布号 WO2014062220(A1) 申请公布日期 2014.04.24
申请号 WO2013US30318 申请日期 2013.03.12
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 REINHARDT, GREGORY, E.;REMBISH, PAUL, THOMAS;CONNER, STEVEN, L.;HYATT, THOMAS, B.;FEIGLESON, STEVEN, J.;KLINETOB, CARL, BRIAN
分类号 F02K3/00;B64D27/10;F02C3/00;F02C7/06;F02K99/00 主分类号 F02K3/00
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