发明名称 Metallic-Coated Polymer Thrust Reverser Cascades
摘要 A thrust reverser cascade for a gas turbine engine is disclosed. The thrust reverser cascade may comprise a plurality of turning vanes. One or more of the turning vanes may comprise a core formed from a polymer and a metallic coating applied to at least a portion of an outer surface of the core. The metallic coating may comprise nickel or a nickel alloy.
申请公布号 US2015285184(A1) 申请公布日期 2015.10.08
申请号 US201414459930 申请日期 2014.08.14
申请人 United Technologies Corporation 发明人 Sawyers-Abbott Nigel David
分类号 F02K1/70;B29D99/00;B29C71/00 主分类号 F02K1/70
代理机构 代理人
主权项 1. A thrust reverser cascade for a gas turbine engine, comprising: a plurality of turning vanes, at least one of the plurality of turning vanes comprising a core formed from at least one polymer, andat least one metallic coating applied to at least a portion of an outer surface of the core.
地址 Hartford CT US