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A rotor hub and method to dampen a force exerted on a rotor hub by a rotor blade during flight. The rotor hub including a central member rotatably coupled to a rotor mast, a blade grip rigidly attached to a blade and movably coupled to the central member, and an adjustable damper operably associated

A rotor hub and method to dampen a force exerted on a rotor hub by a rotor blade during flight. The rotor hub including a central member rotatably coupled to a rotor mast, a blade grip rigidly attached to a blade and movably coupled to the central member, and an adjustable damper operably associated with the blade grip. The method includes damping the force exerted on the rotor hub with the adjustable damper and selectively adjusting the adjustable damper between a first spring rate and a second spring rate.

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1. A rotor hub, comprising: a central member rotatably coupled to a rotor mast;a blade grip movably coupled to the central member; andan adjustable damper operably associated with the blade grip;a blade strap configured to movably attach the blade grip to the central member, the blade strap forms an

1. A rotor hub, comprising: a central member rotatably coupled to a rotor mast;a blade grip movably coupled to the central member; andan adjustable damper operably associated with the blade grip;a blade strap configured to movably attach the blade grip to the central member, the blade strap forms an opening that receives the adjustable damper;a bearing disposed within the opening of the blade strap and attached to the adjustable damper;wherein the force exerted by the rotor blade passes through the bearing and damped with the adjustable damper;wherein the blade grip exerts a force on the central member during flight; andwherein the adjustable damper is adjusted between a first spring rate and a second spring rate to dampen the force exerted on the central member. 2. The rotor hub of claim 1, further comprising: a flapping hinge rigidly attached to and disposed within the opening of the blade strap;wherein the flapping hinge pivotally secures the blade grip to the central member via the blade strap. 3. The rotor hub of claim 1, further comprising: a bracket rigidly attached to the blade grip and securely attached to the bearing; anda pitch horn rigidly attached to the bracket;wherein the bracket attaches the blade grip to the blade strap. 4. The rotor hub of claim 1, the adjustable damper comprising: a piston movably disposed within a fluidly sealed housing, the piston having: a post that extend through an opening of the housing and attaches to the bearing;a first fluid reservoir disposed within the housing;a second fluid reservoir disposed within the housing;a first passage extending the length of the piston and in fluid communication with both the first fluid reservoir and the second fluid reservoir; anda switchable valve in fluid communication with the first passage;wherein fluid passes through the first passage when the switchable valve is in an opened position, and fluid is restricted from passing through the first passage when the switchable valve is in a closed position. 5. The rotor hub of claim 4, further comprising: an elastomeric seal secured to and disposed between an outer surface of the piston and an inner surface of the housing. 6. The rotor hub of claim 4, the adjustable damper further comprising: a second passage extending the length of the piston and in continuous fluid communication with both the first fluid reservoir and the second fluid reservoir. 7. A rotor hub, comprising: a central member rotatably coupled to a rotor mast;a blade grip attached to the central member;a blade strap movably coupled to the central member and securely coupled to the blade grip, the blade strap forming an opening;an adjustable damper disposed within the opening of the blade strap, the adjustable damper having a piston disposed within a housing; anda bearing disposed within the opening of the blade strap and attached to a post of the piston of the adjustable damper;wherein the blade grip movably couples to the central member via the blade strap;wherein during flight the blade exerts a force on the rotor hub that passes through the bearing and is damped with the adjustable damper; andwherein the adjustable damper is adjusted during flight to dampen changes in the force exerted on the rotor hub. 8. The rotor hub of claim 7, the adjustable damper comprising: a first fluid reservoir disposed within the housing;a second fluid reservoir disposed within the housing;a first passage extending the length of the piston and in fluid communication with both the first fluid reservoir and the second fluid reservoir; anda switchable valve in fluid communication with the first passage;wherein fluid passes through the first passage when the switchable valve is in an opened position, and fluid is restricted from passing through the first passage when the switchable valve is in a closed position. 9. The rotor hub of claim 8, further comprising: an elastomeric seal secured between an outer surface of the piston and an inner surface of the housing;wherein the elastomeric seal elastically attaches the piston to the housing. 10. The rotor hub of claim 9, wherein: when the flow of fluid through the first passage is permitted, movement of the piston is resisted by a shear force required to cause shear deflection of the elastomeric seal; andwhen the flow of fluid through the first passage is restricted, movement of the piston is resisted by a fluid force required to cause bulging deflection of the elastomeric seal. 11. The rotor hub of claim 8, the adjustable damper further comprising: a second passage extending the length of the piston and in continuous fluid communication with both the first fluid reservoir and the second fluid reservoir. 12. The rotor hub of claim 8, wherein the switchable valve is autonomously operated between the opened position and the closed position. 13. The rotor hub of claim 8, wherein the switchable valve is a rotary valve. 14. The rotor hub of claim 7, wherein the rotor hub is a soft in-plane rotor hub.