发明名称 SPINNER FOR A GAS TURBINE ENGINE
摘要 A spinner for use in a gas turbine engine includes a body and an aft ring coupled to the body. The body is symmetrically formed by filament winding around a central axis. The aft ring includes a band coupled to the body and a plurality of fairings that extend outward in a radial direction from the band away from the central axis.
申请公布号 US2016010459(A1) 申请公布日期 2016.01.14
申请号 US201514635412 申请日期 2015.03.02
申请人 Rolls-Royce Corporation 发明人 Romanowski Erin M.;Engebretsen Eric W.;Scott Matthew A.
分类号 F01D5/12;F02C3/04 主分类号 F01D5/12
代理机构 代理人
主权项 1. A spinner for use in a gas turbine engine comprising a filament-wound body formed substantially symmetrically around a central axis, the body including a side wall having a diameter that increases along the central axis from a forward side of the body to an aft side of the body, and an aft ring including a band that overlaps the side wall along the aft side of the body and a plurality of fairings that extend outward in a radial direction from the band away from the central axis.
地址 Indianapolis IN US