A rotor system (200, 300, 400, 500) is provided in one example embodiment and may include a first pair of rotor blades (210, 310, 410, 510) comprising a first pitch (P1) and a first diameter (D1); and a second pair of rotor blades (220, 320, 420, 520) comprising a second pitch (P2) and a second diameter (D2) wherein the first pitch (P1) of the first pair of rotor blades (210, 310, 410, 510) and the second pitch (P2) of the second pair of rotor blades (220, 320, 420, 520)are different.
MULTI-BLADE ROTOR SYSTEM
MEHRSCHAUFELROTORSYSTEM
SYSTÈME DE ROTOR À PALES MULTIPLES
30.06.2021
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2017
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