System for contactless displacement measurement of a blade root of a wind turbine
A system for measuring displacements of a blade root of a rotor blade of a wind turbine includes a hub, and a rotor blade coupled to the hub by a pitch bearing. The system further comprises a reference plane and at least one displacement sensor. The reference plane is configured to move with the rotor blade as the rotor blade moves relative to the hub while the displacement sensor is fixed to the hub and the displacement sensor is configured to detect a displacement of the reference plane relative to the hub without physical contact. Alternatively, the reference plane has a fixed position with respect to the hub while the displacement sensor is fixed to the rotor blade and the displacement sensor is configured to detect a displacement of the reference plane relative to the rotor blade without physical contact.
1. A system of a wind turbine, the system comprising:
a hub, the hub comprising a non-rotating component of a pitch bearing;
a rotor blade comprising a blade root, the blade root comprising a blade root end and a rotating ring component of the pitch bearing affixed to the blade root end;
a plurality of non-contact displacement sensors operably facing the rotor blade and fixed directly or indirectly to the hub;
a respective reference plane associated with each of the plurality of non-contact displacement sensors, the respective reference planes defined by the rotor blade or a component that moves with the rotor blade as the rotor blade moves relative to the hub;
wherein each of the plurality of non-contact displacement sensors detects relative movement between the respective reference plane and the hub without being physically connected to the component defining the respective reference plane; and
wherein the plurality of displacement sensors are mounted opposite to and facing their respective reference plane.
2. The system of claim 1 , further comprising a controller communicatively coupled to the plurality of displacement sensors, the controller configured to determine loads exerted on the rotor blade based on displacement of the blade root indicated by signals received from the plurality of displacement sensors.
3. The system of claim 2 , further comprising a pitch adjustment mechanism communicatively coupled with the controller, the pitch adjustment mechanism comprising a pinion gear engaged with the rotating ring component of the pitch bearing to adjust a pitch angle of the rotor blade by rotating the rotor blade around a longitudinal axis of the rotor blade, wherein the controller is configured to adjust the pitch angle of the rotor blade in dependence of the determined loads.
4. The system of claim 2 , further comprising a communication path configured to transfer the signals received from the plurality of displacement sensors to the controller without transferring the signals from the rotor blade to the hub.
5. The system of claim 1 , wherein the plurality of displacement sensors are configured to detect displacement of their respective reference plane in one or more different directions.
6. The system of claim 1 , wherein the plurality of displacement sensors are located within an interior of the hub.
7. The system of claim 1 , wherein the plurality of displacement sensors are arranged around a longitudinal axis of the rotor blade at a uniform distance from each other.
8. The system of claim 1 , wherein each of the respective reference planes is defined by one of: a surface of the blade root end, or a surface of the rotating ring component, or a component separate from the associated displacement sensor attached to the blade root end, or a component separate from the associated displacement sensor attached to the rotating ring component.
9. The system of claim 1 , wherein each of the plurality of displacement sensors is fixed directly to the hub, or is fixed on a component attached to the hub.