发明名称 FAN CASE
摘要 A fan case for use in a gas turbine engine of an aircraft includes an outer shroud and a liner extending along the outer shroud. The fan case provides a protective band that blocks fan blades from being thrown out of the fan case in case of a blade-off event in which a fan blade is released during operation of the gas turbine engine.
申请公布号 US2015354408(A1) 申请公布日期 2015.12.10
申请号 US201514701124 申请日期 2015.04.30
申请人 Rolls-Royce Corporation 发明人 Snyder Burke J.
分类号 F01D25/24 主分类号 F01D25/24
代理机构 代理人
主权项 1. A fan case adapted to extend around blades of a fan rotor included in a gas turbine engine, the fan case comprising an annular outer shroud arranged to extend around a central axis of the fan case, the annular outer shroud having an outer surface facing away from the central axis and an inner surface facing toward the central axis and a liner segment coupled to the inner surface of the annular outer shroud, the liner segment including an inner radial surface, an outer radial surface spaced apart radially from the inner radial surface, and a head surface extending between and interconnecting the inner and outer radial surfaces, wherein the head surface intersects a first ray extending from the central axis to the annular outer shroud.
地址 Indianapolis IN US