The applicant of this disclosure has developed a truss-based foundation system for supporting single-axis trackers, fixed-tilt solar arrays and other structures. Known commercially as EARTH TRUSS, this system relies on a pair of adjacent legs that form a truss with the ground. In a typical configuration, each leg consists of a below ground portion called a screw anchor driven partially into the ground, and an upper leg section that is sleeved over a coupler at the upper end of each anchor. The free ends of each upper leg section are joined together with a so-called truss cap or adapter that unifies these components into a complete foundation structure. In the current form of the EARTH TRUSS, crimps are used to secure overlapping portions of the upper leg sections to their respective screw anchors and to connectors on the truss cap.
Until the EARTH TRUSS system emerged on the market, tracker makers designed their systems to be supported by generic H-pile foundations. H-piles are standard wide flange galvanized steel beams such as W6×9 s, W6×12 s, or combinations of these driven at a plum orientation. These beams are driven into the ground with an impacting or vibratory pile driver in repeated North-South oriented rows across the intended array site. Some tracker makers specify the same foundation for each supported component (e.g., bearing, motors, etc.) whereas others may require lower, taller, and/or heavier foundations at certain points in the array depending on the loads that must be resisted at those points. For example, motor piles and those around the permitter of the array often experience larger top-of-pile loads than internal bearing piles that experience relatively lower forces. With H-piles, variances for particular foundations are relatively easy to accomplish by simply adjusting the size of the beam, the driving depth, and/or the reveal height (i.e., the length remaining above-ground after driving). Such variations are more difficult to accommodate with same-sized truss foundations. However, in order for EARTH TRUSS to be competitive with H-piles, a solution is needed for these non-standard foundation case that relies on substantially the same components and the same installation machine and work flows.
Taking for example, the Horizon NX tracker from Array Technologies, Inc. (ATI) of Albuquerque, N. Mex., in that tracker, one foundation in each row supports a so-called center structure. The center structure is where torque is transferred to the torque tube. For every megawatt or so of tracker, one row has a motorized center structure that applies torque directly to the torque tube above it. The motorized center structure has an output shaft that runs to the non-motorized or passive center structure of the next adjacent row. At that center structure, torque is transferred to a local drive gear but is also output to another drive shaft so that it can be translated to the next adjacent row and so-on and, so-forth. This mechanical linkage continues across all rows supported by the drive motor to enable a single motor to turn multiple rows at once. Universal joint connections between the drive shafts and center structures are used to take up variances in terrain.
Typically, the foundation that supports the center structure must be stronger than other foundations in the row that merely support the torque tube bearings due to the additional forces experienced at the foundation supporting the motor. Also, this foundation typically must be lower to the ground to leave room between the torque tube and the foundation for the center structure. To account for these non-standard cases while minimizing the use of non-standard components used in other foundations, various embodiments of this disclosure provide a foundation for supporting motorized and non-motorized center structures for a connected row tracker system such as the ATI Horizon NX tracker.
The following description is intended to convey a thorough understanding of the embodiments described by providing a number of specific embodiments and details involving A-frame-shaped truss foundations used to support single-axis solar trackers. It should be appreciated, however, that the present invention is not limited to these specific embodiments and details, which are exemplary only. It is further understood that one possessing ordinary skill in the art in light of known systems and methods, would appreciate the use of the invention for its intended purpose.
Turning now to the drawing figures,
As discussed in the background section, the applicant of this disclosure has developed a novel foundation for supporting single-axis trackers and other devices known commercially as EARTH TRUSS. This foundation consists of a pair of adjacent driven screw anchors, an upper bearing support or so-called truss cap, and a pair of upper leg sections that interconnect the truss cap to the driven screw anchors. In order to utilize the same or similar components and the same or similar installation machine and installation work flows, various embodiments of the invention provide a variant of the EARTH TRUSS foundation adapted to resist forces experienced at the motorized and non-motorized center structures in the ATI tracker system.
One example of this foundation is shown in
As shown in the figures, center structure support 30 is an elongated structure with main body 32, support portions 33 and open distal ends 34 for receiving clamp assemblies 36. As shown in the figure, the ATI center structure sits on center structure support 30 at the approximate middle, extending transverse to the long axis of support 30, resting on and attached to opposing support portions 33. Bolts, hucks or other fasteners may be used to secure the center structure to support 30. As discussed in greater detail herein, one or more bolts or other fasteners extend through distal ends 34 and clamp assemblies 36 to lock legs 20 and center support structure 30 together.
Turning now to
To accept the geometry of driving coupler 20, various embodiments provide a two-piece clamp assembly 36 that has reciprocal voids shaped and dimensioned to receive the coupler with a clamped rather than crimped connection. This is seen, for example in
Assembly of the system described in the context of
Typically, though not necessarily, screw anchors are driven so as to maintain perpendicularity to the intended rotational axis of the tracker, which, in the case of the ATI tracker shown and discussed herein, is the torque tube itself. In various embodiments, the reveal height, which is the difference between the length of the anchor and the embedment depth, will be set to result in the center structure bearings being at the same height as the other bearings in the same row when the center structure is placed the center structure support. In various embodiments, the so-called truss driver machine that drives the screw anchors into underlying ground on the array site will compute the required embedment depth based on the screw anchor length, minimum embedment depth for that site and the intended height of the tracker's rotational axis, which in this case, is the torque tube, among other factors.
Once the pair of adjacent screw anchors have been driven, next, in step 205, clamps are placed around the driving coupler at the upper end of each screw anchor. The clamps may be manually held in place until one end of the center structure support is slid around them, and this process may be repeated for the second end. One or more bolts or other fasteners may be loosely passed through the slots in the center structure support and the clamp halves to keep the assembly from falling apart while positional adjustments are made. Then, at step 210, using a jig, laser alignment or other techniques, the center structure may be oriented at the precise height and level necessary to achieve alignment with other bearings in the row. For example, a laser target or other device may be attached to the center structure support to enable proper orientation of the support relative to the truss legs and clamp before locking them in place. Finally, at step 215 one or more bolts or other fasteners passing through the clamp halves and the center structure support are torqued down to the specified torque to preserve the orientation of the center structure support.
It should be appreciated that the specific geometry of the driving coupler is exemplary only. The concept is to take the geometry of this structure, which may be optimized for one or more different purposes and to adapt it to a geometric shape or other shape, in this case, a rectangular box, which can be supported with more conventional surface on surface mechanical fitment. Other coupler shapes are possible as long as the two clamp haves have reciprocal voids that enable them to capture coupler when clamped around it while providing flat external surfaces that can be received in the flanged openings of the center structure support. Also, it should be appreciated that although the single-axis tracker from ATI is shown in these figures, that the various embodiments of the invention may be used to support other tracker system as well.
The embodiments of the present inventions are not to be limited in scope by the specific embodiments described herein. Indeed, various modifications of the embodiments of the present inventions, in addition to those described herein, will be apparent to those of ordinary skill in the art from the foregoing description and accompanying drawings. Thus, such modifications are intended to fall within the scope of the following appended claims. Further, although some of the embodiments of the present invention have been described herein in the context of a particular implementation in a particular environment for a particular purpose, those of ordinary skill in the art will recognize that its usefulness is not limited thereto and that the embodiments of the present inventions can be beneficially implemented in any number of environments for any number of purposes. Accordingly, the claims set forth below should be construed in view of the full breath and spirit of the embodiments of the present inventions as disclosed herein.
This claims priority to U.S. provisional patent application No. 63/105,756 filed on Oct. 26, 2020, titled “TRUSS FOUNDATIONS FOR SOLAR TRACKER CENTER STRUCTURES”, the disclosure of which is hereby incorporated by reference in its entirety.
Number | Date | Country | |
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63105756 | Oct 2020 | US |