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AssigneesBeihang University, Tianmushan Laboratory
InventorsLongfei ZHAO, Zongxia JIAO, Wuyao JIANG, Jingfeng XIE, Jinhao LOU, Haishan HUANG, Xufei YAN, Zhaotong CHEN, Jixiang LIANG, Pengfei KANG
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The present disclosure discloses a tri-wing hybrid vertical take-off and landing aircraft, including a tilting body fuselage, a front wing assembly, a middle wing assembly, and a rear wing assembly. The front, middle, and rear wing assemblies are sequentially arranged along the longitudinal direction of the tilting body fuselage. The front, middle, and rear wing assemblies are provided in pairs, symmetrically arranged on both sides of the tilting body fuselage. Specifically, the front wing assembly includes a front wing body, a first power unit, and a first pontoon mechanism. The front wing body is fixedly connected to the tilting body fuselage, and the first pontoon mechanism is mounted below the front wing body. The first power unit is mounted on the front wing body and, in a parked state, is in a tilted position to provide the moment required for tilting the fuselage upward. The present disclosure enables easier lifting during the take-off phase.
A tri-wing hybrid vertical take-off and landing aircraft, comprising:
Dependencies are inferred from the claim text.