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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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