A fixed-wing aircraft includes a load element, which is coupled to a fuselage of the fixed-wing aircraft; and an actuator device, by which a position of the load element can be varied in relation to the fuselage during a flight of the fixed-wing aircraft in order to displace a center of gravity of the fixed-wing aircraft by the load element.
FIXED-WING AIRCRAFT AND METHOD FOR OPERATING A FIXED-WING AIRCRAFT
29.03.2018
Patent
Elektronische Ressource
Englisch
FIXED-WING AIRCRAFT AND METHOD FOR OPERATING A FIXED-WING AIRCRAFT
Europäisches Patentamt | 2020
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