发明名称 |
Wheel accelerator for aircraft landing gear - uses structure acting on wheel periphery to accelerate it to landing peripheral velocity |
摘要 |
A structure (21) having different resistance values (CW1) according to the relative position of slipstream attach during the landing approach, generates a resulting air force (L). This acts as a peripheral force on the wheel. Thus the peripheral force is accelerated to a peripheral velocity (a), corresp. to the latter rolling motion during landing. USE/ADVANTAGE - The accelerator is intended for aircraft landing approach for preventing excessive type abrasion during landing, and for reducing the ground contact impact.
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申请公布号 |
DE4230918(A1) |
申请公布日期 |
1994.03.17 |
申请号 |
DE19924230918 |
申请日期 |
1992.09.16 |
申请人 |
METZGER, MARCUS, 7570 BADEN-BADEN, DE |
发明人 |
METZGER, MARCUS, 7570 BADEN-BADEN, DE |
分类号 |
B64C25/40;(IPC1-7):B64C25/40 |
主分类号 |
B64C25/40 |
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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