发明名称 TRACK FAIRING ASSEMBLY FOR A TURBINE ENGINE NACELLE
摘要 The present disclosure relates generally to an aerodynamic track fairing assembly used on an engine nacelle, the track fairing assembly positionable on the aft section of the engine nacelle, the aerodynamic track fairing assembly including an upper section extending toward an aft end of the aft section of the engine nacelle, a bottom section extending toward the aft end of the aft section of the engine nacelle, the bottom section affixed to the upper section to form a track cavity therebetween, and a fairing fitting disposed within the track cavity and affixed to the bottom section.
申请公布号 US2016237856(A1) 申请公布日期 2016.08.18
申请号 US201514621456 申请日期 2015.02.13
申请人 United Technologies Corporation 发明人 Sidelkovskiy Dmitriy B.;Zysman Steven H.;Malecki Robert E.
分类号 F01D25/28;F01D25/24 主分类号 F01D25/28
代理机构 代理人
主权项 1. A turbine engine nacelle including an aft section comprising: an aerodynamic track fairing assembly positionable on the aft section of the nacelle, the aerodynamic track fairing comprising: an upper section extending toward an aft end of the aft section of the nacelle, the upper portion including an upper portion end;a bottom section extending toward the aft end of the aft section of the nacelle, the bottom section including a bottom section end, and a bottom section interior surface;wherein the upper section end is affixed to bottom section end to form a track cavity between the upper section and the bottom section;a fairing fitting disposed within the track cavity and affixed to the bottom section interior surface.
地址 Farmington CT US
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