An aircraft is provided and includes an airframe, a blade disk, which is rotatable relative to the airframe, including a plurality of rotor blades, a rotor shaft disposed to drive rotation of the blade disk relative to the airframe and a pitching of each of the rotor blades about corresponding pitch axes and a rotor assembly configured to form couplings by which each of the rotor blades is coupled to the rotor shaft. The rotor assembly includes a composite laminate arranged to resolve loading associated with the couplings in-plane of the composite laminate.
AIRCRAFT ROTOR ASSEMBLY WITH COMPOSITE LAMINATE
FLUGZEUGROTORBAUGRUPPE MIT VERBUNDLAMINAT
ENSEMBLE ROTOR D'AÉRONEF DOTÉ DE STRATIFIÉ COMPOSITE
2017-04-26
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |