This application claims priority to Japanese Patent Application No. 2011-115395 filed on May 24, 2011, the contents of which are hereby incorporated by reference into the present application. The present invention relates to a solar concentrating system using a heliostat.
A system utilizing sunlight is a one of the systems for obtaining electrical energy or thermal energy. Some types of systems utilizing sunlight comprise a solar concentrating system that concentrates the sunlight at one point in order to utilize the sunlight efficiently. A device called a heliostat is known for concentrating the sunlight at one point. The heliostat comprises a mirror reflector (usually a moderately concave mirror), and an actuator for adjusting a direction of the mirror reflector.
The heliostat adjusts the direction of the mirror reflector in synchronism with movement of the sun so that reflected light is constantly concentrated at a receiver disposed at one predetermined point (target point). The direction of the mirror reflector must be controlled precisely to constantly direct the reflected light toward the receiver. Unlike a photovoltaic system in which a solar panel may be generally directed toward the sun, the heliostat requires high precision control. Discussion of the control performance of heliostats is introduced in non-patent document 1: “PERFORMANCE OF SOLAR CONCENTRATOR CONTROL SYSTEM”, Kenneth W. Stone, Charles W. Lopez, Proceedings of Joint Solar Engineering Conference, ASME 1994.
As introduced in non-patent document 1, the direction of the mirror reflector (azimuth and inclination angle) is basically determined based on the solar position (azimuth and inclination angle). That is, the direction of the mirror reflector is adjusted, based on the solar position, so that the reflected light is directed toward the receiver. However, there is a possibility that, if the wind is strong, the mirror reflector may be tilted by the wind pressure, and the reflected light will deviate from the receiver. Concentration efficiency falls drastically if the reflected light deviates even slightly from the receiver. The present invention provides a solar concentrating system having a mechanism that corrects a deviation of the direction of the reflected light caused by wind pressure.
A solar concentrating system taught in the present specification comprises a heliostat and a controller. As described above, the heliostat has an actuator that adjusts a direction of a mirror reflector. The actuator may typically be a motor. The controller is configured to output a target angle command to the actuator. The system taught in the present specification further comprises an anemometer, and the controller is configured to determine the target angle command based on a solar position, and on a wind direction and a wind speed measured by the anemometer.
More specifically, the target angle command determined by the controller is composed of a target angle first element determined from the solar position, and a target angle second element determined based on the wind direction and the wind speed. The target angle first element is determined so that reflected light is directed toward a predetermined target position (the position of a receiver). The target angle second element corresponds to an estimated value of a twist angle, caused by wind pressure, from an output shaft of the actuator to a support shaft of the mirror reflector. The existence of this target angle second element corrects the deviation of the direction of the reflected light caused by the wind pressure. Moreover, since the actuator and the support shaft of the mirror reflector are connected via a reduction gear, the “twist angle” may be also equivalent to a twist angle between an input shaft and an output shaft of the reduction gear.
The technique taught in the present specification is suitable for a system that does not directly measure the direction of the mirror reflector. More specifically, the technique taught in the present specification is effective in case the controller has an open loop control system that does not give feedback concerning the angle of the output shaft of the actuator or the angle of the mirror reflector, or in case the controller has a feedback control system that controls the actuator so that a deviation between the target angle and the rotation angle of the output shaft of the actuator becomes zero. In the system taught in the present specification, instead of directly measuring the direction of the mirror reflector and giving feedback, the target angle second element compensates for the inclination angle of the mirror reflector caused by the wind pressure.
In
The system 100 further comprises a solar tracking sensor 6 that measures a solar position (azimuth and inclination angle), an anemometer 4 that measures the wind direction and the wind speed of wind flowing near the system 100, and a controller 10 configured to control the heliostats 2.
A motor 23 and a reduction gear 25 are incorporated into each heliostat 2, and the direction of a mirror reflector 26 can be adjusted by the motor 23 and the reduction gear 25. The controller 10 acquires the solar position from sensor data of the solar tracking sensor 6, and controls the direction of the mirror reflector 26 so that reflected light of the sunlight reaches the receiver 9. Specifically, the controller 10 calculates a target angle of the mirror reflector from the solar position and the position of the receiver 9, and outputs that angle to a driver of the motor 23 as a command value (target angle command). Moreover, the mirror reflector 26 curves so as to have a slightly concave surface, such that the reflected light is focused at the position of the receiver 9.
Further, the controller 10 acquires data of the wind direction and the wind speed of the wind flowing near the system 100 from sensor data of the anemometer 4 and, based on that data, corrects the target angle command calculated based on the sensor data of the solar tracking sensor 6. A correction value is determined so as to have a size to compensate for an angle by which the mirror reflector 26 is tilted by wind pressure. The controller 10 calculates the target angle command including the correction value for each of the plurality of heliostats, and sends each target angle command to a driver of the motor of each heliostat. Moreover, each heliostat 2 comprises a driving mechanism for the two axes of the azimuth and inclination angle, and a target angle command is also calculated for each axis. However, for simplifying the explanation below, the description will be given assuming one drive shaft axis of the mirror reflector.
In
First, the configuration of the heliostat 2 will be described with reference to
As described above, the sensor data of the angle sensor 24 indicates the rotation angle of the output shaft of the motor 23. This angle is sent to a converter 21. In the converter 21, the rotation angle of the output shaft of the motor 23 is converted to an angle of the mirror reflector 26 and is output. The output of the converter 21 is used for feedback control of the motor 23 as an estimated angle of the mirror reflector.
The motor 23 is driven by a driver 22. The driver 22 receives the angle command from the controller 10, and drives the motor 23 in accordance with the angle command. Moreover, specifically, the motor 23 is current-controlled (i.e., torque-controlled) by the driver 22. It is noted that details are omitted in
The controller 10 will be described. The controller 10 acquires the sensor data of the solar tracking sensor 6, and a first calculating unit 34 calculates a mirror reflector angle (the target angle first element Ar1) so that the reflected light is directed toward the receiver 9. A calculation for calculating the angle of the mirror reflector from the solar position and the position of the receiver 9 is also implemented in a conventional concentrating system, and consequently a detailed description is omitted.
Further, based on the sensor data of the anemometer 4, a second calculating unit 32 of the controller 10 calculates a compensation value (the target angle second element Ar2) that compensates for the inclination angle of the mirror reflector caused by wind pressure. The target angle second element Ar2 will be described specifically later. The target angle first element Ar1 and the second element Ar2 are added, becoming the target angle command value Ar. Within the controller 10, the difference between the target angle command value Ar and an estimated angle of the mirror reflector based on the sensor data of the angle sensor 24 is sent to the driver 22. Consequently, the controller 10 controls the heliostat 2 so that the angle of the mirror reflector 26 matches the target angle command Ar. The motor 23 stops at an angle equivalent to the estimated angle (As1+As2) of the mirror reflector. Below, angle As1 represents the actual angle of the mirror reflector corresponding to the target angle first element Ar1, and angle As2 represents the actual angle corresponding to the target angle second element Ar2.
The compensation value (the target angle second element A2), which compensates for the inclination angle of the mirror reflector caused by the wind direction and the wind speed, will be described. Now, if there is no wind, the angle of the mirror reflector 26 can be expressed by the value obtained by multiplying the reduction ratio of the reduction gear 25 by the rotation angle of the motor output shaft 23a. At this time, the current angle As of the mirror reflector 26 is equal to the target angle Ar. Further, since the sensor data of the anemometer 4 is zero, the target angle second element Ar2 is zero. That is, if there is no wind, the target angle command Ar output by the controller 10 is Ar1, and the actual angle of the mirror reflector also becomes a value corresponding to the target angle first element Ar1, i.e., it becomes the angle As1. If the actual angle of the mirror reflector is As1, the reflected light is directed accurately toward the receiver 9.
Since the mirror reflector is a huge flat plate, considerable force is generated when subjected to wind. Below, this force is called wind load F. Upon receiving this wind load F, twisting occurs between the output shaft of the motor (the input shaft of the reduction gear) and the support shaft of the mirror reflector (the output shaft of the reduction gear). Consequently, a deviation occurs between the actual angle and the estimated angle of the mirror reflector that is based on the sensor data of the angle sensor 24 which measures the angle of the output shaft 23a of the motor 23. The target angle second element Ar2 compensates for this deviation.
One example of the calculation process of the target angle second element Ar2 will be described with reference to
[Eq. 1]
F=Cw×q×Aw (Eq. 1)
Here, coefficient Cw is a coefficient of the wind force, and Cw=1.2 in case the pressure receiving surface (the surface of the mirror reflector) is a rectangle. Variable Aw is the area of the pressure receiving surface. As shown in
[Eq. 2]
q=0.6×V2×E×I (Eq. 2)
In (Eq. 2), E is an environment variable, and I is an application variable. Eq. 1 and Eq. 2 are described in detail in the Japanese Industrial Standard (JIS). The coefficient of wind force Cw, environment variable E, and application variable I are also defined by the JIS. For details, refer to “JIS C 8955”.
As shown in
[Eq. 3]
M=F×d×cos(Ta) (Eq. 3)
The support shaft 27 is twisted by this moment M. Now, letting K be the torsional rigidity between the output shaft 23a of the motor (the input shaft of the reduction gear) and the support shaft of the mirror reflector 27 (the output shaft of the reduction gear), twist angle As2 (the inclination angle of the mirror reflector) due to the wind pressure is expressed as M=K×As2. As a result, the inclination angle Ar2 of the mirror reflector due to the wind pressure can be expressed by the following formula (Eq. 4).
The angle Ar2 obtained in (Eq. 4) is equivalent to the target angle second element. As shown in (Eq. 2), the wind speed V is included in the design velocity pressure q. Further, the angle Ta formed by the plane of the mirror reflector 26 and the wind direction is equal to the wind direction. The wind speed V and the wind direction Ta are measured by the anemometer 4.
The second calculating unit 32 of
As described above, by adjusting the angle of the mirror reflector by means of the target angle command value that includes the compensation value (the target angle second element) which offsets the inclination angle of the mirror reflector due to the wind pressure, the reflected light can be directed accurately toward the receiver 9 even in wind.
Points to keep in mind for the system 100 of the embodiment will be mentioned. In the system 100 of the embodiment, feedback control of the rotation angle of the output shaft of the motor was adopted. In case the performance of the motor driver is sufficiently high, an open loop control for the rotation angle of the output shaft of the motor may be adopted.
Further, in the embodiment, the solar tracking sensor was used to obtain the solar position. Instead, the solar position may be obtained by calculating from GPS data (latitude, longitude, date and time).
Further, the target angle command output by the controller 10 may include a third element in addition to the target angle first element Ar1 and second element Ar2. Here, the target angle third element is determined so as to have a size to compensate for the inclination angle of the mirror reflector caused by the weight of the mirror reflector.
The torsional rigidity K between the output shaft 23a of the motor (the input shaft of the reduction gear) and the support shaft 27 of the mirror reflector (the output shaft of the reduction gear) may be obtained in advance by experiments, etc.
While specific examples of the present invention have been described above in detail, these examples are merely illustrative and place no limitation on the scope of the claims. The technology described in the claims also encompasses various changes and modifications to the specific examples described above. The technical elements explained in the present description or drawings provide technical utility either independently or through various combinations. The present invention is not limited to the combinations described at the time the claims are filed. Further, the purpose of the examples illustrated by the present description or drawings is to satisfy multiple objectives simultaneously, and satisfying any one of those objectives gives technical utility to the present invention.
Number | Date | Country | Kind |
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2011-115395 | May 2011 | JP | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/JP2012/060325 | 4/17/2012 | WO | 00 | 11/17/2013 |