Patent Application
20100232964
The present invention relates generally to the field of wind turbines, and, more particularly, to an improved wind turbine having a plurality of electro-hydraulic actuators mounted on the rotatable hub of the turbine for independently controlling the pitch of a like plurality of blades.
Wind turbines are, of course, known. In recent years, many of the problems of having a wind turbine supply power synchronously to an electrical grid have been addressed and overcome.
Wind turbines today are relatively sophisticated. They are typically mounted on a tower, and have plurality of blades (normally three) mounted on a hub for rotation about a horizontal axis relative to a nacelle. The nacelle may be aimed into the direction of the oncoming wind. Each of the blades is typically of variable pitch, and the pitch of each blade may be controlled independently of the others. These blades are typically arranged at 120° intervals. When one blade is pointing aiming downwardly toward the 6 o'clock position, the wind proximate the ground is typically less than the speed of the wind moving over the other two blades. Hence, the pitch of each blade is controlled independently of one another with the goal trying to normalize (i.e., keep reasonably constant) the rotational speed of the hub from ground effects, gusts, etc.
Heretofore, wind turbines have been characterized as being of the electrical-type or of the hydraulic-type. In either case, the generator is typically mounted in the nacelle. Control signals and power are supplied up through the tower, and to a pitch-controlling mechanism. In both cases, this pitch-controlling mechanism has been heretofore mounted in the nacelle, and this necessitates a type of slip ring joint between the nacelle and the rotatable hub. In addition, this arrangement has been accompanied by the use of a large bull gear, and with various hoses within the hub. The life expectancy of such an arrangement has been as short as about four years due to excessive wear on the bull gear caused principally by variations in the speed of the wind.
Accordingly, it would be generally desirable to provide an improved wind turbine in which the pitch-controlling electro-hydraulic actuator is mounted within the hub, rather then on the nacelle.
With parenthetical reference to the corresponding parts, portions or surfaces of the disclosed embodiment, merely for purposes of illustration and not by way of limitation, the present invention provides an improvement for use in a wind turbine (20) having a plurality of variable-pitch blades (24) mounted on a hub (23) for rotation relative to a nacelle (22).
The improvement broadly includes: a electro-hydraulic actuator (25) for controlling the pitch of one of the blades, the actuator including: a motor (26) adapted to be supplied with a current; a pump (27) driven by the motor and arranged to provide a hydraulic output as a function of the current supplied to the motor; and a hydraulic actuator (28) operatively arranged to selectively vary the pitch of the associated blade as a function of the hydraulic output of the pump; and wherein the motor, pump and actuator are physically arranged within the hub of the wind turbine.
In one form, the wind turbine has three of the variable-pitch blades (24) mounted on the hub, and wherein one of the electro-hydraulic actuators (25) is provided for each of the blades.
The motor may be a d.c. brushless motor.
The pump may be a fixed displacement pump.
In the preferred embodiment, the polarity of the hydraulic output from the pump is a function of the polarity of the current supplied to the motor.
The actuator may have a piston (30) slidably mounted within a cylinder (31) and sealingly separating a first chamber (35) on one side of the piston from a second chamber (36) on the other side of the piston, and wherein a rod (32) is mounted on the piston and extends through chamber (35) and penetrates and end wall of the cylinder such that the piston has unequal-area surfaces facing into the chambers. The improved actuator may further include a hydraulic reservoir (41) and an anti-cavitation valve (57) operatively arranged between the tank and the actuator such that hydraulic fluid will flow from the reservoir to the chamber facing the larger-area piston face when such chamber is expanding, and will flow to the reservoir from the chamber facing the larger-area piston face when such chamber is contracting.
The hydraulic reservoir may be pressurized.
The anti-cavitation valve may operate automatically as a function of the polarity of the hydraulic output of the pump.
The improvement may further include a pressure relief valve (48, 52) operatively arranged to limit the maximum pressure of the pump hydraulic output.
The pump may have a high-pressure side and a low-pressure side, and a case drain.
A bypass valve (54) may be positioned selectively operable to communicate the high- and low-pressure sides.
The case drain (40) may communicate with the reservoir through a filter.
The improvement may further include a restricted orifice (56) in series with the bypass valve.
The improvement may further include: a source (62) of pressurized hydraulic fluid communicating via a conduit (63) with the chamber into which the small-area piston surface faces, and a normally-open solenoid valve (64) arranged in the conduit, and wherein the solenoid valve is arranged to be opened in the event of a power failure to permit hydraulic fluid to flow from the source through the conduit and into the chamber into which the small-area piston surface faces to cause such chamber to expand and to urge the piston to move toward a position relative to the cylinder at which the blade is feathered.
The improvement may further include blocking valves (59, 60) operatively arranged to selectively isolate the pump from the small- and large-area actuator chambers.
Power and/or control signals to the motor are preferably supplied form the nacelle to the hub through a contactless rotary transformer. Examples of these are shown and described in U.S. Pat. Nos. 5,608,771, 6,813,316 and 5,572,178, the aggregated disclosures of which are hereby incorporated by reference.
Accordingly, the general object of the invention is to provide an improved electro-hydraulic actuator for use in a wind turbine to control the pitch of one of a plurality of variable-pitch blades thereon.
Another object is to provide an improved electro-hydraulic actuator for use in a wind turbine, wherein the major components of the actuator are mountable on the rotating hub and not on the nacelle.
Another object is to provide an improved actuator for use in a wind turbine, and wherein the actuator contains a fail-safe mechanism for urging the associated blade to move toward a feathered position in the event of a power failure or interruption.
These and other objects and advantages will become apparent from the foregoing and ongoing written specification, the drawings and the appended claims.
At the outset, it should be clearly understood that like reference numerals are intended to identify the same structural elements, portions or surfaces consistently throughout the several drawing figures, as such elements, portions or surfaces may be further described or explained by the entire written specification, of which this detailed description is an integral part. Unless otherwise indicated, the drawings are intended to be read (e.g., cross-hatching, arrangement of parts, proportion, degree, etc.) together with the specification, and are to be considered a portion of the entire written description of this invention. As used in the following description, the terms “horizontal”, “vertical”, “left”, “right”, “up” and “down”, as well as adjectival and adverbial derivatives thereof (e.g., “horizontally”, “rightwardly”, “upwardly”, etc.), simply refer to the orientation of the illustrated structure as the particular drawing figure faces the reader. Similarly, the terms “inwardly” and “outwardly” generally refer to the orientation of a surface relative to its axis of elongation, or axis of rotation, as appropriate.
Referring now to the drawings, and more particularly to
Heretofore, the mechanism for controlling the pitch of the blades was mounted on the nacelle, and control was transferred to the hub by means of a bull gear. In the present invention, however, the electro-hydraulic actuators are mounted within the hub, and the bull gear can be eliminated altogether.
Referring now to
In the preferred embodiment, the motor is a brushless D.C. motor that is supplied with a current from the nacelle via a contactless rotary transformer (not shown). When the supplied current is of one polarity, the motor will rotate in one direction. When the supplied current supplied is of the opposite polarity, the motor will rotate in the opposite direction.
Pump 27 is preferably a fixed displacement pump, and is connected to the motor by means of a shaft 29.
The actuator 28 is shown as having a piston 30 slidably mounted within a cylinder 31. A rod 32 as its left end mounted on the piston, and penetrates the cylinder right end wall. An eye 33 is mounted on the right end of rod 32. Another eye 34 is shown as being mounted on the cylinder left end wall. The piston is slidably mounted within the cylinder, and sealingly separates a leftward chamber 35 from a rightward chamber 36. The entire circular vertical end surface of piston 30 faces into left chamber 35. However, an annular vertical surface of the piston faces rightwardly into right chamber 36. The entire electro-hydraulic actuator is mounted within the rotatable hub of the wind turbine. Eye 34 is mounted to the rotatable hub, and eye 33 is mounted to a lever arm (not shown) connected to control the pitch of the associated blade.
One side of pump 27 communicates with actuator left chamber 35 via a conduit 38, and the opposite side of pump 27 communicates with actuator right chamber 36 via a conduit 39. A drain conduit 40 communicates a portion of the pump flow with a reservoir 41 via a filter 42 and a check valve 43. More particularly, conduit 40 extends between the case drain and the filter, conduit 44 communicates the filter 42 with check valve 43, and conduit 45 communicates check valve 43 with another conduit 46 communicating with the reservoir or tank 41. This tank is shown as having a diaphragm, and is gas pressurized to a pressure of about 90-250 psi.
Conduit 38 communicates with tank 41 via a conduit 47 which includes a high-pressure relief valve 48, connected conduits 49, 50 and 46. Conduit 39 communicates with tank 41 via conduit 51 which contains another high-pressure relief valve 52, and connected conduits 49, 50 and 46. The function of pressure relief valves 48, 52 is to provide a relief for an over pressure condition depending on the polarity of the pump operation. Conduit 38 also communicates with conduit 39 via a conduit 53, a bypass solenoid 54, and a conduit 55 containing a restricted orifice 56.
Conduits 38 and 39 also communicate with one another via a conduit 54, an anti-cavitation valve 55, and a conduit 56. Solenoid-operated bypass valves 57, 60 are positioned in conduit 38, 39, respectively. The anti-cavitation valve 57 is a type of inverse shuttle valve that samples the pressure of the fluid in conduits 38, 39, and moves automatically in response to the pressure differential therebetween. The function of anti-cavitation valve 57 is to accommodate the volumetric changes between opposed actuator chambers 35, 36. In other words, when piston moves leftwardly within the cylinder, the volume of fluid removed from collapsing left chamber 35 will be greater than the volume of fluid supplied to expanding right chamber 36. The anti-cavitation valve functions to permit the excess or differential fluid to flow through conduits 46, 49, 50 to the reservoir. Conversely, when the actuator piston moves rightwardly relative to the cylinder, a differential amount of fluid may flow from reservoir 41 through conduit 46 and the anti-cavitation valve into the expanding left actuator chamber.
A charge fitting 61 communicates with conduit 39 to allow fluid to be added to the system. A fail-safe accumulator 62 communicates with conduit 39 via a conduit 63 containing a normally-opened solenoid valve 64.
When the wind turbine is first started, bypass valves 59, 60 are closed, and fluid is first pumped into accumulator 62 to charge and pressurize this accumulator to about 3,000 psi. Thereafter, valves 59, 60 are opened to permit fluid to flow to the actuator.
The function of the fail-safe accumulator 62 is to provide a source of pressurized hydraulic fluid to the system in the event of a loss of power to the motor. In the event of a power failure, fail-safe accumulator 62 will provide a source of pressurized hydraulic fluid to displace the actuator rod leftwardly toward a feathered positioned of the blade.
A commercial form of the apparatus is depicted in
Referring now to
The present invention expressly contemplates that many changes and modifications may be made. In the improved wind turbine, an electro-hydraulic actuator is provided for each blade so that the pitch of the various blades can be controlled independently of one another. While it is presently preferred to use a D.C. brushless motor, other types of motors may be used as well. Similarly, while the fixed-displacement pump is presently preferred, other types of pumps might possibly be substituted therefore.
The actuator might, of course, have a rod penetrating both cylinder end walls. However, this would like interfere with the nose of the hub. Nevertheless, if arrangement could be accommodated, there would be no need for the anti-cavitation valve since the volume of the expanding chamber would equal the volume of the collapsing chamber.
If desired, the motor controller and the power stage can be incorporated directly into the improved hub-mounted electro-hydraulic actuator.
Therefore, while the presently-preferred form of the improvement has been shown and described, and several modifications thereof discussed, persons skilled in this art will readily appreciate that various additional changes and modifications may be made without departing from the spirit of the invention, as defined and differentiated by the following claims.
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/US2007/023681 | 11/9/2007 | WO | 00 | 5/7/2010 |
