发明名称 Ceramic matrix composite rotor module for a gas turbine engine, corresponding turbine assembly and method of assembling
摘要 A rotor (62) module for a gas turbine engine (20) including a multiple of ceramic matrix composite (CMC) airfoil rows (74A,74B,74C) which extend from a common CMC drum (66). A corresponding turbine assembly and a method of assembling are also provided.
申请公布号 EP2570608(A2) 申请公布日期 2013.03.20
申请号 EP20120169252 申请日期 2012.05.24
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SUCIU, GABRIEL L.;ALVANOS, IOANNIS;MERRY, BRIAN D.
分类号 F01D5/28;C04B35/80;F01D5/34;F01D11/00 主分类号 F01D5/28
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