发明名称 Blade assembly with preloaded bearing assembly
摘要 A bearing assembly (30) is supported in a blade assembly such as a propeller (10), turbine or fan assembly and a blade assembly for a structure or craft having a hub having at least one blade opening (16), a blade (14) having an outer sleeve (18) received within the blade opening (16), and at least one preloaded bearing assembly (30) provided between the outer sleeve (18) and the hub (12) and where the at least one preloaded bearing assembly (30) is preloaded by means of a wedge assembly, allows the blade (14) to rotate within the hub (12) and is subject to the effects of rotational centrifugal force acting on the blade (14).
申请公布号 GB2542546(A) 申请公布日期 2017.03.22
申请号 GB20170001666 申请日期 2014.07.07
申请人 GE Aviation Systems Limited 发明人 Michael Fedor Towkan;Daryl John Burford;Stephen John Bowen Parker
分类号 B64C11/06 主分类号 B64C11/06
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