The present disclosure relates to a heliostat, and more particularly to a joint therefor. Current heliostats may have a relatively limited range of motion both in azimuth as well as in elevation. The relatively limited range of motion may require configuration changes for best operation at different field positions and at different latitudes. This may result in the use of different heliostat configurations in different fields or even in different parts of the same field to focus the sun's energy on the receiver.
The relatively limited range of motion may also require some heliostats to reposition themselves 180 degrees at specific times during the day to continue tracking the sun. This action typically requires approximately 15 minutes during which the sun's energy is not captured.
A heliostat according to an exemplary aspect of the present disclosure includes a joint with a range of motion in both elevation and azimuth of more than 90 degrees.
A heliostat according to an exemplary aspect of the present disclosure includes a pedestal which defines a longitudinal axis, the pedestal defines a first radius. A first link is movably mounted to the pedestal about a first axis. A second link movably mounted to the first link about a second axis, the second axis displaced from the longitudinal centerline by at least the first radius.
A heliostat according to an exemplary aspect of the present disclosure includes a joint having a first member and a second member, wherein the first member has an axis of rotation that is skew to an axis of rotation of the second member, wherein the axis of the first member is offset a first distance from the axis of the second member, and wherein the second member has a radial length about the second axis at least approximately ½ of the first distance.
Various features will become apparent to those skilled in the art from the following detailed description of the disclosed non-limiting embodiment. The drawings that accompany the detailed description can be briefly described as follows:
Referring to
Referring to
Referring to
The joint 42 generally includes a first link 50 and a second link 52. The first link 50 includes a first arcuate arm 54 with end pivots 54A, 54B and a second arcuate arm 56 with end pivots 56A, 56B. The end pivots 54A, 54B, as illustrated define an initial elevation axis B and the end pivots 56A, 56B defines an initial azimuthal axis C (also illustrated in
The second link 52 includes an arcuate arm 58 with end pivots 58A, 58B (
The first link 50 is movably mounted to the pedestal 40 about axis B. The second link 52 is movably mounted to the first link 50 about axis C. That is, axis C is offset by at least the column radius r1 relative to the longitudinal centerline A by axis B to achieve a significant freedom of motion. The second link 52 positions the heliostat array 46 at least an additional radius r1 from axis C to provide essentially unrestricted azimuth and elevation motion of the heliostat array 46 relative to the pedestal 40. By using the elevational axis B to achieve the offset, the joint 42 provides a significant range of motion in both elevation and azimuth. In one non-limiting embodiment, the range of motion is more than 90 degrees and typically approximately 180 degrees in both elevation and azimuth. It should be understood that the heliostat array 46 may be mounted asymmetrically as desired to optimize load and other operating characteristics and requirements.
Through the unique combination of kinematics, a full range of smooth and continuous motion with no singularity conditions is achieved. The range of motion avoids any unique non-sun gathering maneuvers.
Referring to
The drive system 70 adjusts the heliostat array 46 relative to the pedestal 40 to provide articulation to utilize the range of motion provide by the joint 42. The joint 42 essentially provides one point g in space for the heliostat array 46. By defining the two other points e, f as represented by the mounts 74A, 74B the definition and orientation of the heliostat array 46 plane is established. In this manner, there is no singularity point and no need to significantly realign the azimuth to continue tracking the sun. Instead, sun tracking is accomplished in a smooth and continuous manner.
Each of the drive rod 72A, 72B are attached to the mounts 74A, 74B through joints 78A, 78B such as a ball-joint or U-joint to provide a universal connection therebetween. The mounts 74A, 74B support the respective joints 78A, 78B to permit rotation and articulation of the respective drive rod 72A, 72B to position the heliostat array 46.
Referring to
The wrist rotator 88 is mounted to the forearm 84 through the rotational bearing 86 such that the wrist rotator 88 may rotate about the forearm 84 (illustrated schematically by axis F and arrow F). The rotational bearing 86 may essentially include a sleeve which permits rotation F.
The wrist rotator 88 includes a turntable 96 which permits rotation (illustrated by arrow W) of the drive motor 90 and thus the drive rod 72A about an axis W (also illustrated in
The shoulder 80, arm 82 and forearm 84 provide an offset to provide full motion and avoid overextension of the drive rod 72A, 72B. The arm 82 and forearm 84 may each be of a length which is at least equivalent to the radius r1. The arm 82 and forearm 84 may alternatively be of a longer or shorter length dependant in part on whether more or less than a 180 degree range of motion is to be provided. The drive rods 72A, 72B may be maintained in tension when extended and only experience compressive loading when at reduced extension.
The joint 42 facilitates an extended operational range for the heliostat 26 with a robust drive system 70 for effective control and actuation of heliostat 26. Unique maneuvers are avoided and relatively uncomplicated and reliable hardware supports the heliostat array 46.
It should be understood that like reference numerals identify corresponding or similar elements throughout the several drawings. It should also be understood that although a particular component arrangement is disclosed in the illustrated embodiment, other arrangements will benefit herefrom.
Although particular step sequences are shown, described, and claimed, it should be understood that steps may be performed in any order, separated or combined unless otherwise indicated and will still benefit from the present disclosure.
The foregoing description is exemplary rather than defined by the limitations within. Various non-limiting embodiments are disclosed herein, however, one of ordinary skill in the art would recognize that various modifications and variations in light of the above teachings will fall within the scope of the appended claims. It is therefore to be understood that within the scope of the appended claims, the disclosure may be practiced other than as specifically described. For that reason the appended claims should be studied to determine true scope and content.
The present disclosure claims priority to U.S. Provisional Patent Disclosure Ser. No. 61/089,843, filed Aug. 18, 2008.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/US2009/054124 | 8/18/2009 | WO | 00 | 12/29/2010 |
Number | Date | Country | |
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61089843 | Aug 2008 | US |