发明名称 AIRCRAFT WHEEL BEARING ARRANGEMENT
摘要 A bearing arrangement for an aircraft landing gear wheel is provided that effectively supports the wheel on an axle while maximizing internal wheel volume available for mounting non- engine drive means used to power the wheel and/or brakes or other structures within the maximized wheel volume. The bearing arrangement is preferably employed with a two-part aircraft wheel mounted on a landing gear axle and includes bearing structures located only on wheel sections adjacent to the axle. A specifically configured cantilevered joint portion of inboard and outboard wheel sections supports weight and loads bearing structures, eliminating the need for and space required by a high speed bearing. Stiffness necessary for strength and structural integrity is provided by the materials selected to form the wheel sections.
申请公布号 WO2013186635(A3) 申请公布日期 2014.05.08
申请号 WO2013IB01905 申请日期 2013.05.01
申请人 BOREALIS TECHNICAL LIMITED 发明人 PERKINS, SCOTT
分类号 B60B19/06;B60B37/10;B64C25/40 主分类号 B60B19/06
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