发明名称 |
NON-FRANGIBLE WHEEL |
摘要 |
<p>NON-FRANGIBLE WHEEL An improved aircraft wheel configuration obviates the hazard of wheel failure during take-off and landing situations when tire deflation occurs and the wheel accepts full loading on its flanges, The wheel is configured to provide a differential flange height between the inboard and outboard flanges such that the total load applied to the wheel is distributed equally between the flanges. Alternatively, and/or in addition the flanges are restructured to provide an increased section modulus and the inboard flange is designed to provide a wider contact surface.</p> |
申请公布号 |
CA1124279(A) |
申请公布日期 |
1982.05.25 |
申请号 |
CA19800350196 |
申请日期 |
1980.04.18 |
申请人 |
GOODYEAR AEROSPACE CORPORATION |
发明人 |
KIRK, RICHARD L.;BERGER, ROBERT E.;BAIRD, ROY W. |
分类号 |
B60B25/02;B60B21/04;B60B25/10;B64C25/34;(IPC1-7):60B21/00 |
主分类号 |
B60B25/02 |
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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