| 摘要 |
The invention relates to an aircraft with vertical take-off and landing, in particular, to an aircraft with hybrid or electric drive, intended to be used for air transport of passengers and freights without requiring landing runways. According to the invention, the aircraft has a fuselage (2) and extensible wings (3) located on either side of the fuselage (2); it has a cabin (4) of an aerodynamic shape extending laterally and backwards, respectively, with two spars (5) provided therebetween with a gap (6), as well as a modular propelling system (7) consisting of two multiple propellers (8) mounted on the cabin (4), located in front of the wings (3), on either side of the fuselage (2), and one multiple propeller (9) located within the said gap (6), mounted between the two said spars (5). |
