发明名称 AERODYNAMICALLY ROTATABLE AIRCRAFT WHEEL
摘要 PROBLEM TO BE SOLVED: To alleviate shocks upon landing, prevent uneven tire abrasion, improve safeness and ensure energy and resource saving by preliminarily rotating the wheels of an aircraft that is about to be landed. SOLUTION: For its rotation especially requiring no power and posing no adverse effects on aircraft flight, a wheel uses an airflow in flight. The tire groove is devised accordingly. The tire or wheel is mounted on its sidewalls with projections or fins for generating torque by means of air force. The upper half of the wheel is mounted with a cover that causes air force acting on the lower half to rotate the wheel. The three methods may be used in a combination.
申请公布号 JP2001146199(A) 申请公布日期 2001.05.29
申请号 JP19990370752 申请日期 1999.11.19
申请人 SATO TAKUJI 发明人 SATO TAKUJI
分类号 B64C25/40;(IPC1-7):B64C25/40 主分类号 B64C25/40
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