A method of increasing a stability speed of a tiltrotor aircraft (10) includes pivoting a rotor assembly (23, 25) having at least three rotor blades (27) from a first position for operating the tiltrotor aircraft in a helicopter mode to a second position for operating the tiltrotor aircraft in an airplane mode, and increasing a stiffness of the rotor assembly when the rotor assembly is in the second position.
METHOD OF INCREASING A STABILITY SPEED OF A TILTROTOR AIRCRAFT
VERFAHREN ZUR ERHÖUNG DER STABILITÄTSGESCHWINDIGKEIT EINES KIPPROTORFLUGZEUGS
PROCÉDÉ D'AUGMENTATION D'UNE VITESSE DE STABILITÉ D'UN AÉRONEF À ROTORS BASCULANTS
15.06.2022
Patent
Elektronische Ressource
Englisch
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