Title:
WING ROTORY
Document Type and Number:
WIPO Patent Application WO/2005/039974
Kind Code:
A1
Abstract:
VTOL aircraft capable of being freely navigated on the land, on the water, and in the air, wherein since the entire part of a rotor installed so as to surround a body is rotated to generate a lift, a high-output engine and a runway are not required and, if the forward thereof is open, a vertical take-off and landing from a home garden and a building rooftop is allowed, basically a shaft is fitted to vanes to form the rotor, a plurality of rotor shafts are connected to each other and rotated in routes on both sides of the body to generate the lift when the vanes move forward through the upper part of route walls and to decrease the lift when the vanes move backward through the lower part thereof, and when a large amount of cargo is transported, aircraft of the same type are laterally connected to each other for extension to immediately cope with a requirement at site.
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Inventors:
IKESHIRO TATSUO (JP)
Application Number:
PCT/JP2003/013735
Publication Date:
May 06, 2005
Filing Date:
October 27, 2003
Export Citation:
Assignee:
IKESHIRO TATSUO (JP)
International Classes:
B64C29/00; B64C39/00; (IPC1-7): B64C29/00; B64C39/00
Domestic Patent References:
| WO1979000945A1 | 1979-11-15 |
Foreign References:
| US1839556A | 1932-01-05 | |||
| JPS5327997A | 1978-03-15 |
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