Aircraft

The invention relates to an aircraft, which is an electric driven, vertical take-off and landing multi-rotor helicopter (1), preferably a manned and/or load-carrying multi-rotor helicopter. A plurality of rotors are arranged substantially on a same rotor plane (R), and a tail wing group (6) projecting upward or downward with respect to the rotor plane (R) is arranged above or below the rotor plane(R), preferably in the rear region of the aircraft (1) with respect to the forward flight direction. 本发明涉及一种飞行器，其形式为电动驱动的、垂直起降的、优选载人和/或载重的多旋翼直升机(1)，在所述飞行器中，多个旋翼大致设置在同一旋翼平面(R)上，其中，在所述旋翼平面(R)的上方或下方设置相对于所述旋翼平面(R)向上或向下伸出的尾翼组(6)，所述尾翼组优选相对于前进飞行方向设置在所述飞行器(1)的后部区域中。