METHOD OF IMPROVING A STABILITY SPEED OF A TILTROTOR AIRCRAFT
First Claim
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1. A method of increasing a stability speed of a tiltrotor aircraft, the method comprising:
- pivoting a rotor assembly of the tiltrotor aircraft 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, wherein the rotor assembly comprises at least four rotor blades.
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Abstract
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.
1 Citation
20 Claims
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1. A method of increasing a stability speed of a tiltrotor aircraft, the method comprising:
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pivoting a rotor assembly of the tiltrotor aircraft 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, wherein the rotor assembly comprises at least four rotor blades. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13)
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14. A method of increasing a stability speed of a tiltrotor aircraft, the method comprising:
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pivoting a rotor assembly of the tiltrotor aircraft 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, the rotor assembly comprising at least four rotor blades; and moving, during flight, flap centers of each of the at least four rotor blades radially outward from a mast of the rotor assembly to lower a delta-3 of the rotor assembly when the rotor assembly is in the second position. - View Dependent Claims (15, 16, 17, 18, 19, 20)
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Specification