Title:
AIRCRAFT TIRE AND RIM HAVING BLADE LIKE WINDMILL TO REDUCE FRICTION, SHOCK OR THE LIKE BETWEEN TIRE AND RUNWAY WHEN AIRCRAFT IS LANDING
Document Type and Number:
Japanese Patent JP2004058978
Kind Code:
A
Abstract:
To reduce the weight of an aircraft, to lessen the wear of a tire, and to prolong the service life of the tire.
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.
Inventors:
Urasato, Yukitaka
Application Number:
JP2002000255833
Publication Date:
February 26, 2004
Filing Date:
July 29, 2002
Export Citation:
Assignee:
URASATO YUKITAKA
International Classes:
B64C25/40; B64C25/00; (IPC1-7): B64C25/40
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