DC Field | Value | Language |
---|---|---|
dc.contributor.author | Har, Dongsoo | ko |
dc.contributor.author | Moraes, Celso | ko |
dc.contributor.author | Kum, Dongsuk | ko |
dc.date.accessioned | 2019-09-23T05:20:14Z | - |
dc.date.available | 2019-09-23T05:20:14Z | - |
dc.date.issued | 2019-08-06 | - |
dc.identifier.uri | http://hdl.handle.net/10203/267631 | - |
dc.description.abstract | 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. | - |
dc.title | Aircraft capable of vertical take-off and landing, vertical and horizontal flight and on-air energy generation | - |
dc.title.alternative | 수직 테이크오프와 착륙, 수직의 및 수평 비행 및 방송중 에너지 생산의 가능한 항공기 | - |
dc.type | Patent | - |
dc.type.rims | PAT | - |
dc.contributor.localauthor | Har, Dongsoo | - |
dc.contributor.localauthor | Kum, Dongsuk | - |
dc.contributor.nonIdAuthor | Moraes, Celso | - |
dc.contributor.assignee | KAIST | - |
dc.identifier.iprsType | 특허 | - |
dc.identifier.patentApplicationNumber | 15391700 | - |
dc.identifier.patentRegistrationNumber | 10370082 | - |
dc.date.application | 2016-12-27 | - |
dc.date.registration | 2019-08-06 | - |
dc.publisher.country | US | - |
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