A fixed-wing aircraft (110) comprises a load element (112), which is coupled to a fuselage (111) of the fixed-wing aircraft (110); and an actuator device (120), by means of which a position (71, 72) of the load element (112) can be varied in relation to the fuselage (111) during a flight of the fixed-wing aircraft (110) in order to displace a centre of gravity of the fixed-wing aircraft (110) by means of the load element (112).
FIXED-WING AIRCRAFT AND METHOD FOR OPERATING A FIXED-WING AIRCRAFT
STARRFLÜGELFLUGZEUG UND VERFAHREN ZUM BETRIEB EINES STARRFLÜGELFLUGZEUGS
AÉRONEF À VOILURE FIXE ET PROCÉDÉ DE FONCTIONNEMENT D'UN AÉRONEF À VOILURE FIXE
2020-08-19
Patent
Elektronische Ressource
Englisch
FIXED-WING AIRCRAFT AND METHOD FOR OPERATING A FIXED-WING AIRCRAFT
Europäisches Patentamt | 2018
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