CPC B64C 29/0025 (2013.01) [B64C 5/02 (2013.01); B64C 5/06 (2013.01); B64C 5/10 (2013.01); B64C 9/00 (2013.01); B64C 13/04 (2013.01); B64C 27/08 (2013.01); B64D 27/24 (2013.01); B64D 41/00 (2013.01)] | 11 Claims |
1. An aircraft (1) comprising:
an electrically driven, vertical take-off and landing, multicopter, including a multiplicity of rotors (2.1-2.9) arranged in a substantially common rotor plane (R),
a tail unit (6), protruding downward with respect to the rotor plane (R) and located below the rotor plane (R), in a rear region of the aircraft (1) with respect to a forward flying direction (FR), and
the tail unit (6) comprises two vertical stabilizers (6.1, 6.2) that extend downward from support arms (3.1, 3.2) that each support at least one of the rotors, a tailplane (6.3) connected between the two vertical stabilizers (6.1, 6.2), and the tailplane (6.3) is located below the support arms.
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