A rotatable thruster aircraft includes a fixed wing; rotatable thruster assemblies, each including first and second thrusters that provide rotation via differential thrust; and vertical lift thrusters, optionally connected via an elongated member; and an aircraft control unit, including a processor, a non-transitory memory, an input/output component, and a power manager that controls specific power applied to the thrusters.
Rotatable thruster aircraft with separate lift thrusters
02.08.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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