发明名称 HYBRID ROTOR DISK ASSEMBLY FOR A GAS TURBINE ENGINE
摘要 A rotor disk assembly for a gas turbine engine includes a rotor hub defined about an axis of rotation, the rotor hub includes a blade mount section with a first radial flange having a multiple of first apertures and a second radial flange with a multiple of second apertures.
申请公布号 US2012301306(A1) 申请公布日期 2012.11.29
申请号 US201113116199 申请日期 2011.05.26
申请人 ALVANOS IOANNIS;SUCIU GABRIEL L.;DYE CHRISTOPHER M.;LEVASSEUR GLENN 发明人 ALVANOS IOANNIS;SUCIU GABRIEL L.;DYE CHRISTOPHER M.;LEVASSEUR GLENN
分类号 F01D5/30 主分类号 F01D5/30
代理机构 代理人
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