发明名称 AIRCRAFT TIRE AND RIM HAVING BLADE LIKE WINDMILL TO REDUCE FRICTION, SHOCK OR THE LIKE BETWEEN TIRE AND RUNWAY WHEN AIRCRAFT IS LANDING
摘要 PROBLEM TO BE SOLVED: To reduce the weight of an aircraft, to lessen the wear of a tire, and to prolong the service life of the tire. SOLUTION: Blades of a semi-spherical shape or an adequate shape which are rotated under the wind are fitted to a tire, a rim or both of an aircraft. The tire and the rim are fitted to the aircraft, in which wheels are rotated by the effect with the outside air when the aircraft lowers its landing gear, and rotated at considerably high speed when the aircraft is landing to reduce the friction and shocks when the aircraft lands. COPYRIGHT: (C)2004,JPO
申请公布号 JP2004058978(A) 申请公布日期 2004.02.26
申请号 JP20020255833 申请日期 2002.07.29
申请人 URASATO YUKITAKA 发明人 URASATO YUKITAKA
分类号 B64C25/40;(IPC1-7):B64C25/40 主分类号 B64C25/40
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