Aircraft capable of vertical take-off and landing, vertical and horizontal flight and on-air energy generation수직 테이크오프와 착륙, 수직의 및 수평 비행 및 방송중 에너지 생산의 가능한 항공기

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An aircraft includes: a fuselage having opposing leading and trailing extremities along a vertical axis; a fixed wing airframe having opposed at least two main wings connected to the fuselage and extending on a horizontal axis; at least two electric coplanar main wing motors respectively attached to the main wings; a duct frame attach to the trailing extremity of the fuselage; at least two horizontal stabilizers connected to the duct frame and extending on the horizontal axis; an electric tail motor fitted an inner side of the duct frame; multiple battery packs installed inside the fuselage and suitable for supply power to the main wing motors and the tail motor; and support beams suitable for connecting the duct frame to the fuselage.
Assignee
KAIST
Country
US (United States)
Issue Date
2019-08-06
Application Date
2016-12-27
Application Number
15391700
Registration Date
2019-08-06
Registration Number
10370082
URI
http://hdl.handle.net/10203/267631
Appears in Collection
GT-Patent(특허)
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