发明名称 NOSECAP
摘要 The present disclosure relates generally to a nosecap for a gas turbine engine. The nosecap may be injection molded in an embodiment. The nosecap may have bolt holes surrounded by bolt pockets that are asymmetric about a plane passing through a geometric center of the nosecap and passing through and dividing the bolt hole in an embodiment.
申请公布号 US2016273451(A1) 申请公布日期 2016.09.22
申请号 US201415032517 申请日期 2014.10.15
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Kling Colin J.;Brown Charles W.
分类号 F02C7/04 主分类号 F02C7/04
代理机构 代理人
主权项 1. A nosecap for a gas turbine engine, the nosecap comprising: an injection molded body having a forward surface and an aft surface separated by an edge.
地址 Farmington CT US