发明名称 FAN ROTOR WITH INTEGRATED PLATFORM ATTACHMENT
摘要 A fan rotor, for an aircraft engine, including at least one blade root attachment lug, each blade root attachment lug including an attachment lug surface, wherein at least one cavity is disposed on each attachment lug surface.
申请公布号 EP3058180(A2) 申请公布日期 2016.08.24
申请号 EP20140863712 申请日期 2014.09.05
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 HUBBERT, COREY L.;TOMEO, PETER V.
分类号 F01D5/30;F02K3/06 主分类号 F01D5/30
代理机构 代理人
主权项
地址