| 摘要 |
<p>An aircraft for vertical take-off and landing. The aircraft comprises a first wing, a second wing and a fuselage. The first wing comprises a first longitudinal wing axis and the second wing comprises a second longitudinal wing axis. The first wing extends along the first longitudinal wing axis and the second wing extends along the second longitudinal wing axis from the fuselage. The first wing is tiltable with a first rotational direction around the first longitudinal wing axis and the second wing is tiltable with a second rotational direction around the second longitudinal wing axis. In a fixed-wing flight mode, the wings do not rotate around a second axis. In a hover flight mode, the wings are tilted around the longitudinal wing axis with respect to its orientation in the fixed-wing flight mode and that the wing rotates around the second axis.</p> |
