发明名称 Wing Rotary
摘要 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.
申请公布号 US2007034733(A1) 申请公布日期 2007.02.15
申请号 US20060380539 申请日期 2006.04.27
申请人 IKESHIRO TATSUO 发明人 IKESHIRO TATSUO
分类号 B64C29/00;B64C39/00 主分类号 B64C29/00
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