发明名称 Compressor rotor heat shield
摘要 A heat shield for a rotor in a turbine engine is provided. The heat shield includes a main body having a first pair of recesses. The first pair of recesses is adapted to fit around a portion of one or more rotor blades or between two axially adjacent rotor wheels. The first pair of recesses limits axial and radial movement of the heat shield by interaction with the rotor blades or by interaction with the two axially adjacent rotor wheels. The first pair of recesses engage axially adjacent rotor blades or the axially adjacent rotor wheels. The heat shield protects the rotor from hot gas.
申请公布号 US9441639(B2) 申请公布日期 2016.09.13
申请号 US201313892414 申请日期 2013.05.13
申请人 General Electric Company 发明人 Hafner Matthew Troy
分类号 F04D29/58;F04D29/32 主分类号 F04D29/58
代理机构 代理人 Pemrick James W.;Cusick Ernest G.;Landgraff Frank A.
主权项 1. A heat shield for a rotor in a turbine engine, the heat shield comprising: a main body having a first pair of recesses, the first pair of recesses adapted to fit around a portion of one or more rotor blades, the first pair of recesses limiting axial and radial movement of the heat shield by interaction with the rotor blades, the first pair of recesses engaging axially adjacent rotor blades; and wherein the heat shield protects the rotor from hot gas, and the heat shield is retained on the rotor by engagement or connection to a rotor blade and without connection of the heat shield to a rotor wheel.
地址 Schenectady NY US