Vertical take off and landing aircraft has lift and propulsion producing rotors, whose axes are not coaxial, and a control pod and main coupling unit linked by control lines via carrying pipes to rotor couplings

摘要

VTOL aircraft has at least two rotor, drive and tank units (1, 6), at least a main coupling unit (8) to which a control pod is connected and at least two pipe carriers (7) that have one end connected to a connection coupling of a rotor, drive and tank unit and one end connected to the main coupling unit. Hydraulic, electrical, pneumatic, and or optical control channels link the control pod to the rotor couplings via the pipe carriers.