| 摘要 |
<p>The present invention relates to an aircraft comprising a fuselage (100) comprising a fuselage axis (101), a first wing arrangement (110) and a second wing arrangement (120). The first wing arrangement (110) is mounted to the fuselage (100) such that the first wing arrangement (110) is tiltable around a first rotary wing axis (111) of the first wing arrangement (110) and such that the first wing arrangement (110) is rotatable around the fuselage axis (101). The first wing arrangement (110) is adapted in such a way that, in a fixed-wing flight mode, the first wing arrangement (110) do not rotate around the fuselage axis (101). The first wing arrangement (110) is further adapted in such a way that, in a hover flight mode, the first wing arrangement (110) is tilted around the respective first rotary wing axis (111) with respect to its orientation in the fixed-wing flight mode and that the first wing arrangement (110) rotates around the fuselage axis (101). The aircraft further comprises an extendible lift increasing system which is arranged to the first wing arrangement (110) for selectively amending a lift area of the first wing arrangement (110) in the fixed-wing flight mode and the hover flight mode.</p> |
