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.
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
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