This application claims priority to and the benefit of Indian Patent Application No. 202141017660, entitled “BEARING ASSEMBLY FOR TRACKER ASSEMBLY AND METHODS OF MAKING AND USING THE SAME,” by Akhilesan SASIDHARAN et al., filed Apr. 16, 2021, which is assigned to the current assignee hereof and incorporated herein by reference in its entirety.
The following disclosure relates to bearing assemblies for tracker assemblies with exemplary uses in renewable energy structures.
Tracking assemblies are typically used in radar, light shelf, antennas, solar panels, automobiles and other applications which require continuous rotary motion. One common example of tracker assembly used in the industry is solar trackers for use with renewable energy source assemblies. Solar trackers conventionally include a mounting means to mount solar panels. The mounting means of the solar tracker is designed to change its orientation of the solar panels so as to reflect the sun's position to maximize efficiency. Further, ground preparation to accommodate for surface undulations for mounting tracking assemblies remains a diligent and costly step in maximizing solar panel efficiency. Therefore, as the industries surrounding renewable energy sources and tracker assemblies continue to mature, improvements in the components responsible for ensuring power generation will be demanded to improve efficiency, provide lower maintenance, increase deployment potential, and lower the cost of installation.
The present disclosure may be better understood, and its numerous features and advantages made apparent to those skilled in the art by referencing the accompanying drawings.
The use of the same reference symbols in different drawings indicates similar or identical items.
The following description in combination with the figures is provided to assist in understanding the teachings disclosed herein. The following discussion will focus on specific implementations and embodiments of the teachings. This focus is provided to assist in describing the teachings and should not be interpreted as a limitation on the scope or applicability of the teachings. However, other embodiments can be used based on the teachings as disclosed in this application.
The terms “comprises,” “comprising,” “includes,” “including,” “has,” “having” or any other variation thereof, are intended to cover a non-exclusive inclusion. For example, a method, article, or apparatus that comprises a list of features is not necessarily limited only to those features but may include other features not expressly listed or inherent to such method, article, or apparatus. Further, unless expressly stated to the contrary, “or” refers to an inclusive-or and not to an exclusive-or. For example, a condition A or B is satisfied by any one of the following: A is true (or present) and B is false (or not present), A is false (or not present) and B is true (or present), and both A and B are true (or present).
Also, the use of “a” or “an” is employed to describe elements and components described herein. This is done merely for convenience and to give a general sense of the scope of the invention. This description should be read to include one, at least one, or the singular as also including the plural, or vice versa, unless it is clear that it is meant otherwise. For example, when a single embodiment is described herein, more than one embodiment may be used in place of a single embodiment. Similarly, where more than one embodiment is described herein, a single embodiment may be substituted for that more than one embodiment.
Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The materials, methods, and examples are illustrative only and not intended to be limiting. To the extent not described herein, many details regarding specific materials and processing acts are conventional and may be found in textbooks and other sources within the bearing and bearing assembly arts.
The power generation structure 100 can further include tracker assembly 104 including a bearing assembly 115 attached to the base 103, and in particular, directly attached to the support beam 108, and configured to move a rail 118 operably connected to the bearing assembly 115. The bearing assembly 115 as described herein may refer to a movable interface between at least two components, where one of the components is designed to move relative to the other component. Types of movement can include simple translation (along one axis), compound translation (along two or more axes), simple rotation (around one axis) compound rotation (around two or more axes), and a combination thereof. The tracker assembly 104 can further include a drive mechanism 116 that may include a motor, which aids movement of the bearing assembly 115 and the rail 118. In particular, the drive mechanism 116 can be programmed such that it changes the position of the rail 118, and thus, the position of photovoltaic (solar) panels 101 that may be attached to the rail 118, such that the panels 101 can follow the position of the sun in the sky for efficient collection and/or direction of radiant beams of energy from the sun. As will be appreciated, movement of the rail 118 can facilitate movement of portions of the structure 100, and in particular, panels 101 that are attached to the rail 118 via support structures 102. For example, the rail 118 may be adapted to rotatably support the panels 101 about a rotational axis. As illustrated, the structure 100 can include an array of panels 101 attached to a single base 103. According to one embodiment, the panels 101 can be energy conversion structures, such as solar panels, configured to convert radiant energy of the sun into electrical power. In another embodiment, the panels 101 of the article can be reflectors, such as mirrors, designed to re-direct the radiant energy of the sun to nearby energy conversion structures, such as solar panels.
While not illustrated, the structure 100 can include other bearing assemblies, such as between the foundation 107 and the support beam 108 for rotation of the support beam 108 relative to the foundation 107. Moreover, it will be appreciated that other energy conversion structures can utilize a bearing assembly 115, and particularly components disclosed herein within the bearing assembly 115. For example, another suitable energy conversion structure can include a wind turbine, which may include a plurality of propellers (or vanes) extending from a central structure, wherein the turbines must be allowed to rotate for the generation of electrical power, and thus, may utilize components disclosed herein at a bearing assembly within the structure.
Still referring to
As shown in
The fastener 256 may allow for rotation of the adjustable housing portion 250B relative to the fixed housing portion 250A. In this way, the bearing assembly of
As shown in
In an embodiment therein, the adaptor, rail, housing, or any components mentioned herein (or any components thereof) may at least partially include a metal. According to certain embodiments, the metal may include iron, copper, titanium, tin, aluminum, alloys thereof, or may be another type of metal. In a number of embodiments, the adaptor, rail, housing, or any components mentioned herein (or any components thereof) may include a polymer. In an embodiment, the adaptor, rail, and or housing (or any components thereof) may be made a plastic polymer. The plastic polymer may be selected from the group including a polyketone, a polyaramid, a polyphenylene sulfide, a polyethersulfone, a polypheylene sulfone, a polyamideimide, ultra high molecular weight polyethylene, a fluoropolymer, a polybenzimidazole, a polyacetal, polybutylene terephthalate (PBT), polypropylene (PP), polycarbonate (PC), Acrylonitrile butadiene styrene (ABS), polyethylene terephthalate (PET), a polyimide (PI), polyetherimide, polyetheretherketone (PEEK), polyethylene (PE), a polysulfone, a polyamide (PA), polyphenylene oxide, polyphenylene sulfide (PPS), a polyurethane, a polyester, a liquid crystal polymer (LCP), or any combination thereof. The plastic polymer may be a thermoplastic or thermosetting polymer. In an embodiment therein, the adaptor, rail, and or housing (or any components thereof) may also includes glass filler, silica, clay mica, kaolin or other synthetic fillers. In an embodiment therein, the adaptor, rail, and or housing (or any components thereof) may be constructed by at least one of a chamfering, turning, reaming, forging, extruding, molding, sintering, rolling, or casting, injection molding, or 3-D printing. The adaptor, rail, housing, or any components mentioned herein (or any components thereof) of embodiments herein can utilize one or more combinations of features, including particular materials, thicknesses of the material, dimensions of the component, and certain mechanical properties (e.g., stiffness), and chemical inertness that are desired in the industry.
As stated above, in a number of embodiments, a material strip may be mounted, affixed, or otherwise disposed against the exterior surface of the adaptor (first adaptor member and/or second adaptor member). Further, as stated above, in a number of embodiments, a material strip may be mounted, affixed, or otherwise disposed against the interior surface of the housing (first housing member and/or second housing member). For purposes of illustration,
In a number of embodiments, the low friction layer 504 may further include fillers, including glass fibers, carbon fibers, silicon, PEEK, aromatic polyester, carbon particles, bronze, fluoropolymers, thermoplastic fillers, aluminum oxide, polyamidimide (PAI), PPS, polyphenylene sulfone (PPSO2), LCP, aromatic polyesters, molybdenum disulfide, tungsten disulfide, graphite, grapheme, expanded graphite, boron nitrade, talc, calcium fluoride, or any combination thereof. Additionally, the filler can include alumina, silica, titanium dioxide, calcium fluoride, boron nitride, mica, Wollastonite, silicon carbide, silicon nitride, zirconia, carbon black, pigments, or any combination thereof. Fillers can be in the form of beads, fibers, powder, mesh, or any combination thereof. The fillers may be at least 10 wt % based on the total weight of the low friction layer, such as at least 15 wt %, 20 wt %, 25 wt % or even 30 wt %.
Still referring to
The adhesive layer 521 may include any known adhesive material common to the ring arts including, but not limited to, fluoropolymers, epoxy resins, polyimide resins, polyether/polyamide copolymers, ethylene vinyl acetates, ethylene tetrafluoroethylene (ETFE), ETFE copolymer, perfluoroalkoxy (PFA), or any combination thereof.
Additionally, the adhesive can include at least one functional group selected from —C═O, —C—O—R, —COH, —COOH, —COOR, —CF2═CF—OR, or any combination thereof, where R is a cyclic or linear organic group containing between 1 and 20 carbon atoms. Additionally, the adhesive can include a copolymer.
Filler particles (functional and/or nonfunctional) may be added in to the adhesive layer 521 such as carbon fillers, carbon fibers, carbon particles, graphite, metallic fillers such as bronze, aluminum, and other metals and their alloys, metal oxide fillers, metal coated carbon fillers, metal coated polymer fillers, or any combination thereof.
In an embodiment, the hot melt adhesive can have a melting temperature of not greater than 250° C., such as not greater than 220° C. In another embodiment, the adhesive may break down above 200° C., such as above 220° C. In further embodiments, the melting temperature of the hot melt adhesive can be higher than 250° C. or even higher than 300° C.
The substrate 519 may be coated with corrosion protection layers 514 and 505 including corrosion protection material to prevent corrosion of the material strip 5003 prior to processing. Additionally, a corrosion protection layer 518 can be applied over layer 514. Layers 514 and 505 can include corrosion protection materials including a phosphate of zinc, iron, manganese, or any combination thereof, or a nano-ceramic layer. Further, layers 514 and 505 can include corrosion protection materials including functional silanes, nano-scaled silane based primers, hydrolyzed silanes, organosilane adhesion promoters, solvent/water based silane primers, chlorinated polyolefins, pas sivated surfaces, commercially available zinc (mechanical/galvanic) or zinc-nickel coatings, or any combination thereof. Layer 518 can include functional silanes, nano-scaled silane based primers, hydrolyzed silanes, organosilane adhesion promoters, solvent/water based silane primers. Corrosion protection layers 514, 505, and 518 can be removed or retained during processing.
As stated above, the material strip 5003 may further include a corrosion resistant coating 525. The corrosion resistant coating 525 can include an adhesion promoter layer 527 and an epoxy layer 529. The adhesion promoter layer 527 can include corrosion protection materials including phosphate of zinc, iron, manganese, tin, or any combination thereof, or a nano-ceramic layer. The adhesion promoter layer 527 can include corrosion protection materials including functional silanes, nano-scaled silane based layers, hydrolyzed silanes, organosilane adhesion promoters, solvent/water based silane primers, chlorinated polyolefins, passivated surfaces, commercially available zinc (mechanical/galvanic) or Zinc-Nickel coatings, or any combination thereof. The adhesion promoter layer 527 can be applied by spray coating, e-coating, dip spin coating, electrostatic coating, flow coating, roll coating, knife coating, coil coating, or the like.
The epoxy layer 529 can be corrosion protection materials including a thermal cured epoxy, a UV cured epoxy, an IR cured epoxy, an electron beam cured epoxy, a radiation cured epoxy, or an air cured epoxy. Further, the epoxy layer 529 can include corrosion protection materials including polyglycidylether, diglycidylether, bisphenol A, bisphenol F, oxirane, oxacyclopropane, ethylenoxide, 1,2-epoxypropane, 2-methyloxirane, 9,10-epoxy-9,10-dihydroanthracene, or any combination thereof. The epoxy layer 529 can further include a hardening agent. The hardening agent can include amines, acid anhydrides, phenol novolac hardeners such as phenol novolac poly[N-(4-hydroxyphenyl)maleimide] (PHPMI), resole phenol formaldehydes, fatty amine compounds, polycarbonic anhydrides, polyacrylate, isocyanates, encapsulated polyisocyanates, boron trifluoride amine complexes, chromic-based hardeners such as chromium, polyamides, or any combination thereof. Generally, acid anhydrides can conform to the formula R—C═O—O—C═O—R′ where R can be CXHYXZAU as described above. Amines can include aliphatic amines such as monoethylamine, diethylenetriamine, triethylenetetraamine, and the like, alicyclic amines, aromatic amines such as cyclic aliphatic amines, cyclo aliphatic amines, amidoamines, polyamides, dicyandiamides, imidazole derivatives, and the like, or any combination thereof. Generally, amines can be primary amines, secondary amines, or tertiary amines conforming to the formula R1R2R3N where R can be CXHYXZAU as described above. In an embodiment, the epoxy layer 529 can include fillers to improve the conductivity, such as carbon fillers, carbon fibers, carbon particles, graphite, metallic fillers such as bronze, aluminum, and other metals and their alloys, metal oxide fillers, metal coated carbon fillers, metal coated polymer fillers, or any combination thereof. The conductive fillers can allow current to pass through the epoxy coating and can increase the conductivity of the material strip as compared to a material strip without conductive fillers. In an embodiment, the epoxy layer 529 can be applied by spray coating, e-coating, dip spin coating, electrostatic coating, flow coating, roll coating, knife coating, coil coating, or the like. Additionally, the epoxy layer 529 can be cured, such as by thermal curing, UV curing, IR curing, electron beam curing, irradiation curing, or any combination thereof. Preferably, the curing can be accomplished without increasing the temperature of the component above the breakdown temperature of any of the low friction layer 504, the adhesive layer 521, the substrate 519, or the adhesion promoter layer 527. Accordingly, the epoxy may be cured below about 250° C., even below about 200° C.
In an embodiment, under step 412 of
In other embodiments, under step 412 of
In an embodiment, the low friction layer 504 or any layers can be glued to the substrate 519 using the melt adhesive layer 521 to form a laminate. In an embodiment, any of the intervening or outstanding layers on the material strip 5000, 5001, 5002, 5003, may form the laminate. The laminate can be cut into strips or blanks that can be formed into the material strip. The cutting of the laminate may include use of a stamp, press, punch, saw, or may be machined in a different way. The material strip may then be formed by stamp, press, punch, saw, rolling, flanging, deep-drawing, or may be machined in a different way to fit the shape of the adaptor or housing as described above. In particular embodiment, the material strip 5000 may be molded directly to one of the adaptor or the housing. In another embodiment, the material strip 5000 may be molded to the adaptor or housing as a layer on the component, resulting in a layered structure similar to
The bearing assemblies of the tracker assemblies of the embodiments herein can demonstrate improved operations and characteristics over conventional bearing assemblies of the tracker assemblies. For example, in one embodiment, the bearing assemblies of embodiments herein demonstrate improved resistance to corrosion and weathering. Further, bearing assemblies of embodiments herein demonstrate improved stick-slip performance properties due to the material strip, which are an improvement over conventional bearing members. Further, the housing may allow for swinging the adapter and rail, allowing for compensation of axial misalignments between multiple bearing assemblies and/or tracker assemblies that may compensate for ground/land undulations or misalignment. Therefore, bearing assemblies of the tracker assemblies of the embodiments herein may improve efficiency, provide lower maintenance, lower the cost of installation, and therefore, increase potential deployment of tracker assemblies and/or renewable energy structures.
Many different aspects and embodiments are possible. Some of those aspects and embodiments are described below. After reading this specification, skilled artisans will appreciate that those aspects and embodiments are only illustrative and do not limit the scope of the present invention. Embodiments may be in accordance with any one or more of the embodiments as listed below.
Embodiment 1: A bearing assembly of a power generation structure comprising: an adapter fixed to and rotatable with a rail; and a housing adapted to support the adapter and the rail; wherein the housing comprises a fixed housing portion attached to a support beam, and an adjustable housing portion attached to the adapter and rail, wherein a low friction material is present at an interface between an exterior surface of adaptor and an interior surface of the adjustable housing portion, wherein the adjustable housing portion is capable of self-aligning adjustment of at least a portion of the adapter and rail out of alignment with a central axis of the support beam.
Embodiment 2: A bearing assembly of a power generation structure comprising: an adapter fixed to and rotatable with a rail; and a housing adapted to support the adapter and the rail; wherein the housing comprises a fixed housing portion attached to a support beam, and an adjustable housing portion attached to the adapter and rail, wherein a low friction material is present at an interface between an exterior surface of adaptor and an interior surface of the adjustable housing portion, wherein the adjustable housing portion is capable of self-aligning adjustment of at least a portion of the adapter and rail out of alignment with a central axis of the support beam.
Embodiment 3: A bearing assembly of a power generation structure comprising: an adapter; and a housing comprising a fixed housing portion attached to a support beam, and an adjustable housing portion attached to the adapter, wherein a low friction material is present at an interface between an exterior surface of adaptor and an interior surface of the adjustable housing portion, wherein the adjustable housing portion is capable of adjusting at least a portion of the adapter out of alignment with a central axis of the support beam at an angle, α, of at least −60° and not greater than +60°.
Embodiment 4: A tracker assembly of a power generation structure comprising: a support beam having a central axis; a rail adapted to rotate about a rotational axis; and a bearing assembly operatively attached to the support beam and the rail, the bearing assembly comprising: an adapter fixed to and rotatable with the rail; and a housing adapted to support the adapter and the rail; wherein the housing comprises a fixed housing portion attached to the support beam, and an adjustable housing portion attached to the adapter and rail, wherein a low friction material is present at an interface between an exterior surface of adaptor and an interior surface of the adjustable housing portion, wherein the adjustable housing portion is capable of self-aligning adjustment of at least a portion of the adapter and rail out of alignment with the central axis of the support beam.
Embodiment 5: The bearing assembly or tracker assembly according to any of the preceding embodiments, wherein the adaptor has an interior surface for engaging a rail, wherein the interior surface has a cross-sectional shape that is non-circular.
Embodiment 6: The bearing assembly or tracker assembly according to any of the preceding embodiments, wherein an exterior surface of the rail has a cross-sectional shape that is non-circular.
Embodiment 7: The bearing assembly or tracker assembly according to embodiment 6, wherein the non-circular cross section of the interior surface of the adaptor is complementary to the non-circular cross section of the exterior surface of the rail so as to fix the two components.
Embodiment 8: The bearing assembly or tracker assembly according to any of the preceding embodiments, wherein the adjustable housing portion comprises a first housing member and a second housing member adapted to function as a clamp around the adaptor.
Embodiment 9: The bearing assembly or tracker assembly according to any of the preceding embodiments, wherein the low friction material is fixed to an exterior surface of the adapter.
Embodiment 10: The bearing assembly or tracker assembly according to any of the preceding embodiments, wherein the low friction material is fixed to an interior surface of the adjustable housing portion.
Embodiment 11: The bearing assembly or tracker assembly according to any of the preceding embodiments, wherein the low friction material comprises a material strip and wherein an exterior surface of the adapter comprises a groove adapted to accommodate the material strip.
Embodiment 12: The bearing assembly or tracker assembly according to any of the preceding embodiments, wherein the low friction material is preformed according to the shape of the adapter.
Embodiment 13: The bearing assembly or tracker assembly according to any of the preceding embodiments, wherein the low friction material comprises a thermoplastic polymer.
Embodiment 14: The bearing assembly or tracker assembly according to any of the preceding embodiments, wherein the low friction material comprises a fluoropolymer.
Embodiment 15: The bearing assembly or tracker assembly according to any of the preceding embodiments, further comprising a fastener for rotationally fastening the fixed housing portion to the adjustable housing portion.
Embodiment 16: The bearing assembly or tracker assembly according to embodiment 15, wherein the fastener comprises at least one of screws, bolts, clamps, clasps, clips, latches, pins, rivets, ties, or nails.
Embodiment 17: The bearing assembly or tracker assembly according to any of the preceding embodiments, further comprising a beam fastener for fastening the fixed housing portion to the support beam.
Embodiment 18: The bearing assembly or tracker assembly according to embodiment 17, wherein the fastener comprises at least one of screws, bolts, clamps, clasps, clips, latches, pins, rivets, ties, or nails.
Embodiment 19: The bearing assembly or tracker assembly according to any of the preceding embodiments, wherein the fixed housing portion is uniform with the support beam.
Embodiment 20: The bearing assembly or tracker assembly according to any of the preceding embodiments, wherein the fixed housing portion comprises a framed hood.
Embodiment 21: The bearing assembly or tracker assembly according to any of the preceding embodiments, wherein the rail is adapted to rotatably support a photovoltaic panel.
Note that not all of the features described above are required, that a region of a specific feature may not be required, and that one or more features may be provided in addition to those described. Still further, the order in which features are described is not necessarily the order in which the features are installed.
Certain features are, for clarity, described herein in the context of separate embodiments, may also be provided in combination in a single embodiment. Conversely, various features that are, for brevity, described in the context of a single embodiment, may also be provided separately or in any subcombinations.
Benefits, other advantages, and solutions to problems have been described above with regard to specific embodiments, however, the benefits, advantages, solutions to problems, and any feature(s) that may cause any benefit, advantage, or solution to occur or become more pronounced are not to be construed as a critical, required, or essential feature of any or all the claims.
The specification and illustrations of the embodiments described herein are intended to provide a general understanding of the structure of the various embodiments. The specification and illustrations are not intended to serve as an exhaustive and comprehensive description of all of the elements and features of assembly and systems that use the structures or methods described herein. Separate embodiments may also be provided in combination in a single embodiment, and conversely, various features that are, for brevity, described in the context of a single embodiment, may also be provided separately or in any subcombination. Further, reference to values stated in ranges includes each and every value within that range. Many other embodiments may be apparent to skilled artisans only after reading this specification. Other embodiments may be used and derived from the disclosure, such that a structural substitution, logical substitution, or any change may be made without departing from the scope of the disclosure. Accordingly, the disclosure is to be regarded as illustrative rather than restrictive.
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