Abstract: A gliding yaw bearing system for use in a wind turbine includes a first bearing assembly configured for being attached to a tower of the wind turbine, a second beating assembly configured for being attached to a nacelle of the wind turbine. An upwind section of the second bearing assembly is different from a downwind section of the second bearing assembly. A wind turbine utilizing the gliding yaw bearing system is also encompassed herein.

Abstract: In a first aspect, a method for removing a gliding pad of a gliding yaw bearing of a wind turbine is provided. The method comprises selecting a gliding pad to be removed, rotating a nacelle to a removal position and removing the selected gliding pad. In a further aspect, a gliding yaw bearing for a wind turbine is provided. The gliding yaw bearing comprises a first bearing component configured to be coupled to a tower of a wind turbine and a second bearing component configured to be coupled to a nacelle of a wind turbine. The first bearing component is configured to rotate with respect to the second bearing component. The gliding yaw bearing further comprises one or more axial gliding pads arranged between the first and the second bearing components. In yet a further aspect, a wind turbine comprising examples of yaw bearings according to any of the examples herein disclosed is provided.

Abstract: A gliding yaw bearing system (20) for use in a wind turbine comprising a first bearing assembly configured for being attached to a tower (2) of the wind turbine, a second bearing assembly configured for being attached to a nacelle (4) of the wind turbine, an upwind section of the second bearing assembly is different from a downwind section of the second bearing assembly. Wind turbines, specifically direct drive wind turbines, comprising gliding yaw bearings are also disclosed.

Abstract: In a first aspect, a method for removing a gliding pad of a gliding yaw bearing of a wind turbine is provided. The method comprises selecting a gliding pad to be removed, rotating a nacelle to a removal position and removing the selected gliding pad. In a further aspect, a gliding yaw bearing for a wind turbine is provided. The gliding yaw bearing comprises a first bearing component configured to be coupled to a tower of a wind turbine and a second bearing component configured to be coupled to a nacelle of a wind turbine. The first bearing component is configured to rotate with respect to the second bearing component. The gliding yaw bearing further comprises one or more axial gliding pads arranged between the first and the second bearing components. In yet a further aspect, a wind turbine comprising examples of yaw bearings according to any of the examples herein disclosed is provided.

Abstract: A blade pitch system for a wind turbine comprising a motor coupled to a central reduction gearing, wherein a rotatable output of the central reduction gearing is fixed to a mobile link that in use is joined to the blade and allows rotation of the blade around its longitudinal axis and a static part of the central reduction gearing or the motor is fixed to a static link that in use is joined to a wind turbine hub, wherein the system further comprises one or more flexible couplings to couple the central reduction gearing or the motor and the static or the mobile link such that torque about a blade longitudinal axis is transmitted between the blade and the reduction gearing while substantially limiting the transmission of other loads.

Abstract: A blade pitch system for a wind turbine comprising a motor coupled to a central reduction gearing, wherein a rotatable output of the central reduction gearing is fixed to a mobile link that in use is joined to the blade and allows rotation of the blade around its longitudinal axis and a static part of the central reduction gearing or the motor is fixed to a static link that in use is joined to a wind turbine hub, wherein the system further comprises one or more flexible couplings to couple the central reduction gearing or the motor and the static or the mobile link such that torque about a blade longitudinal axis is transmitted between the blade and the reduction gearing while substantially limiting the transmission of other loads.