Abstract: The invention relates to an aircraft (1), preferably an unmanned aircraft (UAV), drone, or Unmanned Aerial System (UAS), comprising a rigid wing (2) which enables aerodynamic horizontal flight, and at least four rotors (4, 4?) which are driven by means of controllable electric motors (5) and which can be pivoted between a vertical starting position and a horizontal flight position by means of a pivoting mechanism (7), wherein all electric motors (5) and rotors (4) are arranged on the wing (2).
Type:
Application
Filed:
May 31, 2013
Publication date:
May 21, 2015
Applicant:
LOGO-TEAM UG (HAFTUNGSBESCHRANKT)
Inventors:
Florian Seibel, Michael Wohlfahrt, Michael Kriegel