Aircraft with double-fuselage tandem wing vertical take-off and landing layout

The patent of the invention discloses an aircraft with a double-fuselage tandem wing vertical take-off and landing layout, and particularly relates to the technical field of aviation aircrafts. The aircraft with a double-fuselage tandem wing vertical take-off and landing layout comprises two fuselages which are arranged at an interval, and an engine is arranged on each fuselage; a front tandem type wing and a rear tandem type wing which are distributed at an interval are arranged on the two fuselages; an electric tilting rotor wing arranged at one end of the front tandem type wing is also symmetrically arranged on each fuselage; a generator is connected between each electric tilting rotor wing and each engine, the generators are electrically connected with the engines, the rear tandem typewing is provided with a first lift fan located between the two fuselages and a sliding flow rudder located below the first lift fan, and each fuselage is provided with a vertical fin located at one end of the rear tandem typ