METHOD OF IMPROVING A STABILITY SPEED OF A TILTROTOR AIRCRAFT

A method of increasing a stability speed of a tiltrotor aircraft includes pivoting a rotor assembly having at least three rotor blades 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 in...

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Bibliographische Detailangaben
Hauptverfasser: STAMPS, Frank, CHOI, Jouyoung Jason
Format: Patent
Sprache:eng
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Zusammenfassung:A method of increasing a stability speed of a tiltrotor aircraft includes pivoting a rotor assembly having at least three rotor blades 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.