The invention relates to wind turbines and in particular to regulation and adjustment of the rotor blades of a wind turbine for modifying the aerodynamic properties of the rotor blades.
Rotor blades of wind turbines are mounted with their longitudinal axis extending transversely to the axis of the drive shaft and the hub of the wind turbine. The pitch of the rotor blades may be adjusted by rotating the rotor blades about their longitudinal axis, whereby their individual aerodynamic properties and performance are modified and the overall performance of the wind turbine is adapted to the actual conditions such as wind speed and load.
Rotor blades of wind turbines may also have movable parts such as one or more flaps along their trailing edge. Such movable parts may be moved individually to further modify and improve the aerodynamic properties of the rotor blade. Such movable parts can be actuated to move by means of an actuator situated within the blade near the movable part or preferably in the hub or in the root of the blade, i.e. near the hub, or possibly in the nacelle of a wind turbine.
Electrically conductive objects such as metal components in or at a rotor blade may potentially attract lightning and lightning strokes can be destroying and should be avoided. This applies in particular to actuating rods, shafts and wires but also to electrical cables and conductors.
The invention provides a rotor blade for a wind turbine addressing this situation. The rotor blade comprises a rotor blade body with a root for connecting the rotor blade to a hub of a wind turbine, a tip, a longitudinal axis extending between the root and the tip, a leading edge and a trailing edge. The rotor blade has a movable part and motion transmitting means for connecting to an actuator and transmitting motion from the actuator to the movable part, and the motion transmitting means is electrically non-conductive, whereby the risk of lightning stroke accidents is reduced.
The motion transmitting means is preferably connectable to the actuator being outside the blade body whereby the motion transmitting means does not introduce electrically conductive parts into the rotor blade.
The movable part can be a flap at the trailing edge of the rotor blade, and the motion transmitting means may comprise a shaft for transmitting linear and/or rotary motion for activating the one or more flaps. The motion transmitting means of the rotor blade can comprise a composite material such as a glass fibre or carbon fibre reinforced material which are particular suitable for use in rotor blades. The rotor blade can further comprise a spring arranged so as to load the movable part towards a neutral position, whereby it is ensured that the flaps will assume the neutral position should the actuating mechanism fail. Further, a clutch is preferably arranged between the actuator and each flap.
In
In
The shaft 13 can be hollow or solid and it is electrically non-conductive or at least of low conductivity. Suitable materials for the shaft 13 include glass or carbon fibre enforced composite materials. Also other components such as the rocker arm 16, the push rod 17 and the actuation arm 18 can advantageously be made of an electrically non-conductive material.
In
In the shown embodiment the shaft is a rotary shaft that can transmit rotary motion. In cases where a linear motion is needed the shaft may be a push rod or a wire capable of transmitting push and/or pull forces. In order to ensure proper functioning of the mechanism and correct positioning of the flaps feedback from position or force sensors can be used in a closed loop control system.
In
Number | Date | Country | Kind |
---|---|---|---|
PA 2009 00708 | Jun 2009 | DK | national |
This application claims priority under 35 U.S.C.§119(a) to DK Application No. PA 2009 00708, filed Jun. 8, 2009. This application also claims the benefit of U.S. Provisional Application No. 61/184,882, filed Jun. 8, 2009. Each of these applications is incorporated by reference herein in its entirety.
Number | Date | Country | |
---|---|---|---|
61184882 | Jun 2009 | US |