The present invention relates to a braking system for a wind turbine, and in particular, to a brake having a “fail safe” spring mechanism and an electromechanical actuator providing an assist to the spring mechanism during dynamic braking.
The primary braking system for most modern wind turbines is the aerodynamic braking system, which essentially consists in turning the rotor blades about 90 degrees along their longitudinal axis (in the case of a pitch controlled turbine or an active stall controlled turbine), or in turning the rotor blade tips 90 degrees (in the case of a stall controlled turbine).
A mechanical brake is used as a backup system for the aerodynamic braking system, and as a parking brake, once the turbine is stopped in the case of a stall controlled turbine. The mechanical brakes typically comprise two hydraulically actuated calipers that engage a disk on the shaft that connects gearbox and generator. In case an emergency, braking of the wind turbine is needed, the mechanical brake is activated simultaneously to the aerodynamic brakes.
More recently, electromechanical brakes have been used in place of the hydraulic brakes. In electromechanical brakes, an electric device generates the necessary energy once braking action is required. Some of the advantages of electromechanical brakes compared to hydraulic systems is that they are easy to install, require minimal maintenance, and are cleaner to operate in that no hydraulic oil is required.
At least one embodiment of the invention provides a brake comprising a caliper; brake linings associated with the caliper; at least one spring that forces the brake linings toward each other; an electromechanical actuator capable of forcing the brake linings away from each other against the spring force when actuated in a first direction and also capable of forcing the brake linings toward each other in combination with the spring force when actuated in a second direction opposite the first direction.
Embodiments of this invention will now be described in further detail with reference to the accompanying drawing, in which:
Referring now to
The pusher plate 50 is acted upon by at least one compression spring 60. The compression spring 60 causes the pusher plate 50 to move toward the disc 30 to engage the brake 10 by creating a clamping load on the linings 22 and the disc 30.
During operation, the brake 10 is disengaged by the electromechanical actuator 40 which retracts the pusher plate 50 away from the disc 30 and compresses the spring 60. In a stopping situation, the actuator 40 can move the pusher plate 50 toward the disc 30 to allow the compression spring 60 to extend and provide a clamping force to stop or slow the disc 30. If additional clamping force is required, the actuator 40 can move the pusher plate 50 to assist the spring 60. Accordingly, the brake 10 provides a hybrid passive and active brake system by providing the “Fail safe” of the spring 60 and using the electromechanical force of the actuator 40 to increase the clamping force beyond the spring force. In the same manner, the clamping force can be controlled by incrementing the motor and using an encoder or strain gauge to provide a closed loop control of the braking. Use of an encoder also allows the brake 10 to compensate for the decrease in spring force caused by lining wear and provides the actual wear and lining thickness.
During an electrical power failure, the springs will clamp on the disc at 100% spring force. Since the motor is not energized, the brake system will not be at full torque rating. This reduction in clamping force is beneficial and extends the life of the wind turbine gearbox. The fail safe spring clamping load of the brake will be sufficient for parking brake torque requirements. Parking brake torque requirements are less than dynamic braking torque requirements.
In one embodiment of the invention as best shown in
The brake 10 can use the same gearbox mounting location, brake bracket, floating brake/rod system as the current existing hydraulic brakes making the brake 10 retrofittable into existing wind turbines.
In the embodiment shown, the ball screw 46 is a high efficiency ball screw, which allows the use of inexpensive dowel pins to be used to prevent rotation of the pusher plate 50 instead of expensive splines. In the embodiment shown, the gear system is a two-stage 25:1 planetary gear which, along with the high efficiency ball screw, allows for smaller motor torque requirement. The smaller motor shown in the embodiment utilizes low amperage and voltage which allows for an uninterruptable power supple to be used.
Although not shown, the brake can utilize two latches or bolts to release the brake. It is also contemplated that the actuator can be used for the yaw brake in addition to application as the high speed shaft brake. This is beneficial for economy of scale, inventory and maintenance.
The brake 10 replaces existing hydraulic brakes used in the Wind Turbine Market. The clamping load of the brake is produced by a compact gearbox drive train and springs. The compact gearbox drive train is a co-axial design and includes a motor, planetary gears and ball screw. It provides the primary source for controlling the brake clamping load. The springs supplement the braking clamp load and also provide fail safe operation during power failure. The supplemental clamping force from the springs during braking allows the electromechanical actuator to be minimized with a smaller motor, gearbox and ball screw. The smaller components minimizes the physical size of the brake system and allows the co-axial design of the components which is more cost efficient.
Referring now to
Although the principles, embodiments and operation of the present invention have been described in detail herein, this is not to be construed as being limited to the particular illustrative forms disclosed. They will thus become apparent to those skilled in the art that various modifications of the embodiments herein can be made without departing from the spirit or scope of the invention. Accordingly, the scope and content of the present invention are to be defined only by the terms of the appended claims.
The present application claims the benefit of the filing date of U.S. Provisional Application Ser. No. 61/168,955; filed Apr. 14, 2009, the disclosure of which is expressly incorporated herein by reference.
Number | Date | Country | |
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61168955 | Apr 2009 | US |