Aircraft capable of vertical takeoff

An aircraft, comprising:

• a bearing structure;
• the bearing structure having at least one central fuselage and two pylons, each pylon situated laterally at a distance from the fuselage;
• a wing structure;
• at least four hub rotors;
• at least one thrust drive;
• each of the hub rotors fastened to the bearing structure, having a propeller having two propeller blades, and configured to produce, through rotation of the propeller, an upward drive force acting in a vertical direction for the aircraft;
• the thrust drive configured to produce a thrust force acting in a horizontal direction on the bearing structure;
• each pylon having at least two hub rotors;
• each hub rotor configured to arrest a respective propeller blade of a respective hub rotor in an arrested position relative to a respective pylon;
• and
• the respective propeller blade of each hub rotor not extending, in the arrested position, beyond an outer dimension of the respective pylon,
• wherein each propeller is situated in the respective pylon in such a way that each propeller is enclosed by the respective pylon on at least two opposite sides when in a non-arrested position.