A series of convertible aircrafts (1, 1') with a core (100) with an airframe (2) defining a first axis (Y) is described; a first, a second, a third, a fourth, a fifth and a sixth rotor (20a, 20b, 21a, 21b, 22a, 22b) which are rotatable about respective first, second, third, fourth, fifth and sixth axis (B, C, D, E, F, G), and operable independently of each other so as to generate respectively a first, a second, a third, a fourth, a fifth and a sixth thrust value (T1, T2, T3, T4, T5, T6) independent of each other; the core (100) comprises an electric power source (81) and electric motors (72a, 72b, 73a, 73b, 74a, 74b) which are connected to said first, second, third, fourth, fifth and sixth rotor (20a, 20b, 21a, 21b, 22a, 22b); each aircraft (1, 1') of the series comprises a module (110, 120, 130, 140) associated with a respective architecture and interfaced with said core (100).
SERIES OF CONVERTIBLE AIRCRAFTS CAPABLE OF HOVERING AND METHOD FOR CONFIGURING A CONVERTIBLE AIRCRAFT CAPABLE OF HOVERING
EINE REIHE VON UMWANDELBAREN LUFTFAHRZEUGEN MIT FÄHIGKEIT ZUM SCHWEBEN UND VERFAHREN ZUR KONFIGURIERUNG EINES UMWANDELBAREN LUFTFAHRZEUGS MIT FÄHIGKEIT ZUM FLIEGEN
SÉRIE D'AÉRONEFS CONVERTIBLES CAPABLES DE VOL STATIONNAIRE ET PROCÉDÉ DE CONFIGURATION D'UN AÉRONEF CONVERTIBLE CAPABLE DE VOL STATIONNAIRE
2023-07-26
Patent
Electronic Resource
English
European Patent Office | 2023
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