| 摘要 |
The invention concerns an aircraft with vertical take-off and landing having a passenger cabin (3) remaining horizontal whatever the angle of inclination of the aircraft, characterised in that the support stands (69), (70), (71) and (72) in contact with the ground are supported each by a beam bearing a change-over flap (77), (78), (79) and (80) pivoting about an axis perpendicular to the aircraft axis and located in the vertical extension of the beam, the aircraft being vertical. |
