WO2014134754A1 - 太阳能模块的支撑构件组 - Google Patents

太阳能模块的支撑构件组 Download PDF

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Publication number
WO2014134754A1
WO2014134754A1 PCT/CN2013/000270 CN2013000270W WO2014134754A1 WO 2014134754 A1 WO2014134754 A1 WO 2014134754A1 CN 2013000270 W CN2013000270 W CN 2013000270W WO 2014134754 A1 WO2014134754 A1 WO 2014134754A1
Authority
WO
WIPO (PCT)
Prior art keywords
wing
web
frame member
solar module
bearing plate
Prior art date
Application number
PCT/CN2013/000270
Other languages
English (en)
French (fr)
Inventor
管浩鸿
颜同义
黄任伟
Original Assignee
友达光电股份有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 友达光电股份有限公司 filed Critical 友达光电股份有限公司
Priority to DE112013006791.9T priority Critical patent/DE112013006791B4/de
Publication of WO2014134754A1 publication Critical patent/WO2014134754A1/zh

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24—HEATING; RANGES; VENTILATING
    • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S25/00—Arrangement of stationary mountings or supports for solar heat collector modules
    • F24S25/60—Fixation means, e.g. fasteners, specially adapted for supporting solar heat collector modules
    • F24S25/63—Fixation means, e.g. fasteners, specially adapted for supporting solar heat collector modules for fixing modules or their peripheral frames to supporting elements
    • F24S25/632—Side connectors; Base connectors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24—HEATING; RANGES; VENTILATING
    • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S25/00—Arrangement of stationary mountings or supports for solar heat collector modules
    • F24S25/10—Arrangement of stationary mountings or supports for solar heat collector modules extending in directions away from a supporting surface
    • F24S25/11—Arrangement of stationary mountings or supports for solar heat collector modules extending in directions away from a supporting surface using shaped bodies, e.g. concrete elements, foamed elements or moulded box-like elements
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/40—Solar thermal energy, e.g. solar towers
    • Y02E10/47—Mountings or tracking
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/50—Photovoltaic [PV] energy

Definitions

  • the present invention relates to a support member set for a solar module. Background technique
  • solar modules are mostly erected outdoors by support members to greet the sun. Since the solar module and the support member group are systems that are placed outdoors for a long time, they must be able to withstand various harsh environmental conditions. For example, when the solar module and the support member group are erected in a windy area, the solar module and the support member group must have sufficient wind pressure withstand capability. Moreover, if the solar module and the support member group are placed in a snowy area, the solar module and the support member group must have sufficient snow pressure bearing capacity.
  • One aspect of the present invention is to provide a support member set for a solar module to address the difficulties mentioned in the prior art.
  • a support member group of a solar module includes a frame member, a pillar, a connecting member, a first member, and a second member.
  • the frame member includes a first wing, a second wing and a first web.
  • the second wing is disposed substantially parallel to the first wing.
  • the first web joins the first wing and the second wing such that the first wing, the second wing and the first web together define a receiving groove for receiving the solar module.
  • a post for supporting the frame member, and the post has an end surface facing the frame member, the end surface being divided into a first half and a second half, the first half being closer to the frame member than the second half The central axis.
  • the connecting member is for connecting the pillar and the frame member, and the connecting member includes the bearing plate and the fixing plate.
  • the end surfaces of the frame member and the strut abut against the opposite surfaces of the bearing plates, respectively.
  • the retaining plate is attached substantially perpendicularly to the bottom surface of the bearing plate for securing the connecting member to the post.
  • the first component is used to join and fix the fixing plate and the pillar.
  • the second component is used to join and secure the frame member and the bearing plate.
  • the bearing plate has a through hole therein.
  • Frame structure The member also has a through hole therein, and the through hole of the frame member is a long hole.
  • the second member passes through the through hole of the bearing plate and the through hole of the frame member.
  • the support member set of the solar module further includes an insulating coating, and the insulating coating is plated on the surface of the frame member.
  • the connecting member may include a screwing member that is disposed on the frame member to couple with the second member to fix the frame member and the connecting member, and the screw member breaks the insulating coating to directly contact the frame member.
  • the frame member further includes a third flap and a second web.
  • the third wing is disposed substantially parallel to the second wing, and the third wing is located below the second wing for abutting against the bearing plate of the connecting member.
  • the second web is parallel and connected to the first web and is used to connect the second wing to the third wing.
  • the third wing has a first wing that extends in a generally identical direction in a direction generally perpendicular to the second web. The second component is used to join and secure the first wing and the bearing plate.
  • the frame member further includes a third flap and a second web.
  • the third wing is disposed substantially parallel to the second wing, and the third wing is located below the second wing for abutting against the bearing plate of the connecting member.
  • the second web is parallel and connected to the first web and is used to connect the second wing to the third wing.
  • the third wing has a first wing and a second wing.
  • the first wing and the second wing extend in a substantially uniform direction in a direction generally perpendicular to the second web.
  • the second wing portion and the first wing portion extend in opposite directions in a direction substantially perpendicular to the second web.
  • the second component is used to join and secure the second wing and the bearing plate.
  • the frame member further includes a fourth flap and a third web.
  • the fourth wing is coupled to the second web, substantially parallel to the third wing, and above the second wing of the third wing.
  • the second component is further coupled to the fourth wing.
  • the third web connects the fourth wing and the second wing of the third wing such that at least a portion of the second web, the second wing of the third wing, the third web and the fourth wing form a common Hollow frame strip.
  • the vertical height of the second wing portion of the fourth to third wing plates is smaller than the vertical height of the first wing portion of the second to third wing plates.
  • the vertical height of the second wing portion of the fourth to third wing plates is substantially equal to the vertical height of the first wing portion of the second to third wing plates.
  • a support member group of a solar module includes a frame member, a pillar, and a connecting member.
  • the frame member includes a first wing, a second wing, and a first web.
  • the second wing is disposed substantially parallel to the first wing.
  • the first web connects the first wing to the second wing, such that the first wing
  • the plate, the second wing and the first web jointly define a receiving groove for receiving the solar module.
  • the struts are for supporting the frame member, and the struts have end surfaces facing the frame members, the end surfaces having opposing inner and outer edges. The inner edge is closer to the central axis of the frame member than the outer edge, and the outer edge is closer to the vertical projection position of the first web on the plane of the end surface than the inner edge.
  • a connecting member is used to connect the pillar to the frame member.
  • the connecting member includes a bearing plate, a fixing plate, a first member, and a second member.
  • the end surfaces of the frame member and the strut abut against the opposite surfaces of the bearing plates, respectively.
  • the fixing plate is attached substantially perpendicularly to the bottom surface of the bearing plate for fixing the connecting member to the pillar.
  • the first component is used to join and secure the fixed plate and the post.
  • the second component is used to join and secure the frame member and the abutment plate.
  • the bearing plate has a through hole therein.
  • the frame member also has a through hole therein, and the through hole of the frame member is a long hole.
  • the second member passes through the through hole of the bearing plate and the through hole of the frame member.
  • the support member set of the solar module further includes an insulating coating, and the insulating coating is plated on the surface of the frame member.
  • the connecting member may include a screwing member that is disposed on the frame member to couple with the second member to fix the frame member and the connecting member, and the screw member breaks the insulating coating to directly contact the frame member.
  • the frame member further includes a third flap and a second web.
  • the third wing is disposed substantially parallel to the second wing, and the third wing is located below the second wing for abutting against the bearing plate of the connecting member.
  • the second web is parallel and connected to the first web and is used to connect the second wing to the third wing.
  • the third wing has a first wing that extends in a generally identical direction in a direction generally perpendicular to the second web. The second component is used to join and secure the first wing and the bearing plate.
  • the frame member further includes a third flap and a second web.
  • the third wing is disposed substantially parallel to the second wing, and the third wing is located below the second wing for abutting against the bearing plate of the connecting member.
  • the second web is parallel and connected to the first web and is used to connect the second wing to the third wing.
  • the third wing has a first wing and a second wing.
  • the first wing and the second wing extend in a substantially uniform direction in a direction generally perpendicular to the second web.
  • the second wing portion and the first wing portion extend in opposite directions in a direction substantially perpendicular to the second web.
  • the second component is used to join and secure the second wing and the bearing plate.
  • the frame member further includes a fourth wing and a third belly Board.
  • the fourth wing is coupled to the second web, substantially parallel to the third wing, and above the second wing of the third wing.
  • the second component is further coupled to the fourth wing.
  • the third web connects the fourth wing and the second wing of the third wing such that at least a portion of the second web, the second wing of the third wing, the third web and the fourth wing form a common Hollow frame strip.
  • the vertical height of the second wing portion of the fourth to third wing plates is smaller than the vertical height of the first wing portion of the second to third wing plates.
  • the vertical height of the second wing portion of the fourth to third wing plates is substantially equal to the vertical height of the first wing portion of the second to third wing plates.
  • the connecting member includes a third member, and the frame member has a through hole therein, and the pillar has a fixing hole therein.
  • the third member passes through the through hole of the frame member and extends into the fixing hole of the post, thereby joining and fixing the frame member and the pillar.
  • FIG. 1 is a perspective view of a support member group in accordance with a first embodiment of the present invention.
  • FIG. 2 is a top plan view of the support member set of FIG. 1.
  • Figure 3 is a cross-sectional view along line 3 of Figure 2.
  • Figure 4 is a side elevational view of portion 4 of Figure 1.
  • Figure 5 is an enlarged view of a portion 5 of Figure 2.
  • FIG. 6 is a partial cross-sectional view showing a support member group according to another embodiment of the present invention, the cross-sectional area of which is indicated by a portion 6 of FIG.
  • Figure 7 is a cross-sectional view showing a support member group according to a second embodiment of the present invention, the cross-sectional position of which is the same as that of Figure 3.
  • Figure 8 is a cross-sectional view showing a support member group according to a third embodiment of the present invention, the cross-sectional position of which is the same as that of Figure 3.
  • Figure 9 is a cross-sectional view showing a support member group according to a fourth embodiment of the present invention, the cross-sectional position of which is the same as that of Figure 3.
  • Figure 10 is a cross-sectional view showing a support member group according to a fifth embodiment of the present invention, the cross-sectional position of which is the same as that of Figure 3.
  • frame member 111 first wing
  • HI fourth wing to, three wing: vertical height of the wing
  • H2 second wing to, three wing: - vertical height of the wing
  • the error or range of the index value is generally within twenty percent, preferably within ten percent, and more preferably Within five percent.
  • the numerical values mentioned are regarded as approximations, that is, as “about”, “about” or The error or range represented by “roughly”.
  • a support member set of a solar module includes a frame member 110, a post 120 and a connecting member 130.
  • the frame member 110 is used to frame the solar module therein.
  • the pillar 120 stands on the ground.
  • the connecting member 130 is used to connect the strut 120 with the frame member 110.
  • the number of the pillars 120 and the connecting members 130 is four, which are respectively attached to the four corners of the frame member 110. Further, the struts 120 on the side of the frame member 110 (for example, the front side) are shorter than the struts 120 on the other side (for example, the rear side) of the frame member 110, thereby causing the frame member 110 to be inclined by a predetermined angle with respect to the ground.
  • the solar module installed therein greets the sunlight. It should be understood that the number and size of the struts 120 and the connecting members 130 are merely illustrative, and are not intended to limit the present invention. Those skilled in the art should elastically select the struts 120 and the connecting members 130 according to actual needs. Implementation.
  • FIG 3 is a cross-sectional view along line 3 of Figure 2.
  • Figure 4 is a side elevational view of portion 4 of Figure 1. as the picture shows.
  • the frame member 110 includes a first flap 111, a second flap 112 and a first web 113.
  • the second flap 112 is disposed substantially parallel to the first flap 111 and the second flap 112 is located below the first flap 111.
  • the first web 113 connects the first flap 111 and the second flap 112 such that the first flap 111, the second flap 112 and the first web 113 together define a receiving groove G for receiving the solar module.
  • the post 120 is for supporting the frame member 110, and the post 120 has an end surface 122 facing the frame member 110.
  • the end surface 122 is divided into a first half I and a second half II, and the first half I is The second half II is closer to the central axis of the frame member 110.
  • the vertical projection position of the first web 113 on the end surface 122 falls on the second half II.
  • the end surface 122 described above has opposing inner and outer edges 121, 123, which are closer to the central axis of the frame member 110 than the outer edge 123.
  • the vertical projection position of the first web 113 on the plane in which the end surface 122 is located is relatively farther from the inner edge 121 and closer to the outer edge 123.
  • the outer edge 123 is closer to the vertical projection position of the first web 113 on the plane of the end surface 122 than the inner edge 121.
  • the axial force of the strut 120 will be sufficient to support the frame member 110 and the solar module to reduce the risk of permanent deformation of the strut 120 or the connecting member 130.
  • the axial force of the strut 120 can be sufficiently used to support the frame member 110 and the solar module, the overall system's ability to withstand wind pressure or snow pressure also increases.
  • the vertical projection position of the first web 113 on the plane in which the end surface 122 is located It can overlap with the outer edge 123.
  • this does not limit the present invention, and those skilled in the art should flexibly select the position of the first web 113 as needed.
  • the above connecting member 130 includes a bearing plate 131, a fixing plate 132, a first member 133 and a second member 134.
  • the frame member 110 and the end surface 122 of the strut 120 abut against opposite surfaces of the bearing plate 131, respectively.
  • the fixing plate 132 is attached substantially perpendicularly to the bottom surface of the bearing plate 131 for fixing the connecting member 130 to the stay 120.
  • the post 120 has a side surface 125 that abuts the end surface 122.
  • the fixed plate 132 is opposed to the side surface 125 of the post 120.
  • the first member 133 is for joining and fixing the fixing plate 132 and the stay 120.
  • the second member 134 is for joining and fixing the frame member 110 and the bearing plate 131.
  • the number of the fixing plates 132 described above is two, for example, the fixing plate 132a and the fixing plate
  • the 132bo fixing plate 132a, the fixing plate 132b and the partial bearing plate 131 interposed therebetween define a substantially U-shaped (:, or ⁇ -shaped) cross-sectional shape to constrain the pillar 120 to the fixing plate 132a and the fixing.
  • the first member 133 is for joining and fixing the fixing plate 132a, the post 120 and the fixing plate 132b to surely fix the relative positions of the strut 120 and the connecting member 130.
  • the first component 133 can be a bolt, a latch, or other suitable component.
  • the frame member 110 may further include a third flap 114 and a second web 115.
  • the third wing 114 is disposed substantially parallel to the second wing 112 and below the second wing 112 for abutting against the bearing plate 131 of the connecting member 130.
  • the second web 115 is parallel to the first web 113 and connected to the junction with the second flap 112, and the second web 115 connects the second flap 112 with the third flap 114.
  • the third wing 114 has a first wing portion 114a and a second wing portion 114b.
  • the first wing portion 114a and the second wing plate 112 extend in substantially the same direction and in a direction substantially perpendicular to the second web 115, i.e., toward the interior of the frame member 110.
  • the second wing portion 114b and the second wing 112 extend in opposite directions in a direction substantially perpendicular to the second web 115, i.e., toward the exterior of the frame member 110.
  • the junction of the third wing 114 and the second web 115 is the junction of the first wing portion 114a and the second wing portion 114b, and the first wing portion 114a and the second wing portion 114b are the second web 115
  • the joint is intended to extend in the opposite direction.
  • the frame member 110 of the present embodiment may further include a fourth wing 116 and a third web 117.
  • the fourth flap 116 is coupled to the second web 115, the fourth flap 116 is disposed substantially parallel to the third flap 114, and the fourth flap 116 is positioned above the second wing portion 114b of the third flap 114.
  • the third web 117 connects the fourth wing 116 with the second wing 114b of the third wing 114 such that at least a portion of the second web 115, the second wing portion 114b of the third wing 114, and the third web 117 and the fourth wing 116 together form a hollow frame strip.
  • the first wing 111, the second wing 112, the third wing 114, and the fourth wing 116 of the aforementioned frame member 110 The members are generally horizontal, and the first web 113, the second web 115, and the third web 117 are substantially perpendicular members.
  • the vertical height HI of the second wing portion 114b of the fourth wing plate 116 to the third wing plate 114 is smaller than the vertical height H2 of the first wing portion 114a of the second wing plate 112 to the third wing plate 114.
  • this does not limit the present invention, and those skilled in the art should flexibly select the relative positions of the fourth flap 116 and the second flap 112 as needed.
  • the manufacturer may choose to provide the reinforcing ribs 118 between the second flap 112 and the first wing portion 114a of the third flap 114. It should be understood that such a reinforcing rib 118 is not an essential component, and if the strength of the frame member 110 is sufficient, the reinforcing rib 118 may alternatively be omitted.
  • the vertical projection positions of the second web 115 and the reinforcing rib 118 on the plane where the end surface 122 is located are both at the end.
  • the above-described second web 115 falls on the second half II at a vertical projection position on the end surface 122. That is, the outer edge 123 is closer to the vertical projection position of the second web 115 on the end surface 122 than the inner edge 121.
  • the vertical projection position of the reinforcing rib 118 described above on the end surface 122 falls on the first half I. That is, the inner edge 121 is closer to the vertical projection position of the reinforcing rib 118 on the end surface 122 than the outer edge 123.
  • the second wing portion 114b and the fourth wing plate 116 of the bearing plate 131 and the third wing plate 114 have a through hole THa, a through hole THb and a through hole THc therein, respectively.
  • the second member 134 passes through the through hole THa, the through hole THb and the through hole THc, thereby connecting and fixing the second wing portion 114b and the fourth wing plate 116 of the bearing plate 131 and the third wing plate 114 to be fixed.
  • the second component 134 described above can be a bolt, a latch or other suitable component.
  • Figure 5 is an enlarged view of a portion 5 of Figure 2.
  • the through hole (e.g., through hole THc) of the frame member 110 may be a long hole.
  • the frame member 110 and the connecting member 130, which are provided with the solar module may not be aligned due to uneven ground.
  • the through hole of the frame member 110 for example, the through hole THc
  • the through hole THc is a long hole, a part of the tolerance range can be generated, and the assembly can be smoothly completed.
  • the second member 134 is a bolt
  • the connecting member 130 of the present embodiment may further include a first nut fixing wing 136, a second nut fixing wing 137 and a nut fixing web.
  • the first nut fixing wing 136 is connected to the fixing plate 132b.
  • the second nut fixing wing 137 is separated from the first nut fixing wing 136 for the bolt (i.e., the second member 134) to pass therethrough.
  • the nut fixing web 138 connects the bearing plate 131 and the second nut fixing wing 137 such that the first nut fixing wing 136, the second nut fixing wing 137, the nut fixing web 138, the partial bearing plate 131 and a part of the fixing plate 132b collectively defines a nut housing space N.
  • the nut 135 is housed in the nut accommodating space N.
  • the bolt i.e., the second member 134) is locked in the nut 135 through the space between the first nut fixing wing 136 and the second nut fixing wing 137.
  • the bolt is attached to the nut 135 (ie, the second part) 134) It is also impossible to displace in the vertical direction, so that the fourth wing 116 can be selected without the need for a nut to save the assembly process. Further, since the weight of the solar module and the frame member 110 is extremely heavy, even if no nut is fixed to the fourth flap 116, the frame member 110 is not easily detached from the bolt (i.e., the second member 134).
  • the assembler may also choose to retrofit the nut 135 to the fourth wing 116 or to mount the nut 135 under the bearing plate 131 and the fourth wing 116.
  • the nut 135 is modified on the fourth wing 116 (i.e., only the nut 135 is mounted on the fourth wing 116, the nut is not mounted under the bearing plate 131), or the second component 134 is a latch.
  • the connecting member 130 does not need to have the first nut fixing wing 136, the second nut fixing wing 137 and the nut fixing web 138.
  • any of the frame member 110 and the connecting member 130 is sufficient to tap the thread, the manufacturer may also choose to tap the frame member 110 and/or the connecting member 130 and directly bolt (ie, The second component 134) is locked in the thread without the need to provide a nut 135.
  • the second component 134 is locked in the thread without the need to provide a nut 135.
  • the support member group may further include an insulating plating layer 140 which is plated on the surface of the frame member 110 (for example, the surfaces of the fourth flap 116 and the third web 117:). Since the solar module generates electricity when illuminated by light, the presence of the insulating coating 140 prevents the power generated by the solar module from electrically injuring the assembler through the frame member 110.
  • the above insulating plating layer 140 may be, for example, an anodic film.
  • the connecting member 130 may include a screwing member that is disposed on the frame member 110 to be coupled with the second member 134 to fix the frame member 110 and the connecting member 130, and the screw member may be broken.
  • the plating layer 140 is in direct contact with the frame member 110.
  • the nut 135 can be screwed onto the fourth wing 116 with the second component 134, and the nut 135 will break the insulating coating. 140, and directly contacts the fourth wing 116.
  • a conductive path is formed between the connecting member 130 and the frame member 110, and the solar module is grounded through the frame member 110, the connecting member 130, and the pillar.
  • Figure 6 illustrates the destruction of the insulating coating 140 with the nut 135, this does not limit the invention.
  • the insulating coating 140 may also be destroyed by a bolt head or gasket.
  • Those skilled in the art should flexibly select their implementation according to actual needs.
  • the material of the frame member 110 may be metal, such as: aluminum alloy, steel, stainless steel or any combination of the above.
  • the method of manufacturing the frame member 110 may be forging, casting, or any combination of the above.
  • the frame members 110 may also be selected to be strip-shaped in the form of aluminum extrusion, and then assembled into the frame members 110. Structurally, the first flap 111, the second flap 112, the first web 113, the third flap 114, the second web 115, the fourth flap 116, and the third web 117 are reinforced and reinforced.
  • the ribs 118 are integrally formed components.
  • the material of the connecting member 130 described above may be a metal such as aluminum alloy, steel, stainless steel or any combination thereof.
  • the method of manufacturing the connecting member 130 may be forging, casting, or any combination of the above.
  • the bearing plate 131, the fixing plate 132, the first nut fixing wing 136, the second nut fixing wing 137 and the nut fixing web 138 are integrally formed components, and the first member 133 and the second member 134 are integrally formed. It is a separate component with nut 135 (if any).
  • the material of the above-mentioned pillars 120 may be metal, such as aluminum alloy, steel, stainless steel or any combination thereof.
  • the method of manufacturing the struts 120 can be forging, casting, or any combination of the above.
  • Figure 7 is a cross-sectional view showing a support member group according to a second embodiment of the present invention, the cross-sectional position of which is the same as that of Figure 3.
  • the difference between the present embodiment and the first embodiment is that: in the present embodiment, the vertical height HI of the second wing portion 114b of the fourth wing plate 116 to the third wing plate 114 is substantially equal to the second wing plate 112 to the first The vertical height H2 of the first wing portion 114a of the three-wing plate 114.
  • the other related structures and material details are the same as those of the first embodiment, and thus the description thereof will not be repeated.
  • Figure 8 is a cross-sectional view showing a support member group according to a third embodiment of the present invention, the cross-sectional position of which is the same as that of Figure 3.
  • the present embodiment is different from the first embodiment in that the frame member 110 of the present embodiment omits the fourth flap 116 and the third web 117, so that the second member 134 passes through the through hole THa and the through hole only together.
  • THb thereby connecting and fixing the bearing plate 131 and the second wing portion 114b of the third wing 114, The relative position of the frame member 110 and the connecting member 130 can be fixed.
  • Other related structural and material details are the same as those of the first embodiment, and thus the description thereof will not be repeated.
  • Fourth embodiment is different from the first embodiment in that the frame member 110 of the present embodiment omits the fourth flap 116 and the third web 117, so that the second member 134 passes through the through hole THa and the through hole only together.
  • THb thereby connecting and fixing the bearing plate 131 and the
  • Figure 9 is a cross-sectional view showing a support member group according to a fourth embodiment of the present invention, the cross-sectional position of which is the same as that of Figure 3.
  • the present embodiment is different from the first embodiment in that the frame member 110 of the present embodiment omits the fourth wing portion 116, the third web 117, and the second wing portion 114b of the third flap 114.
  • the through hole THa is modified to the first wing portion 114a of the third wing 114, and the through hole THb, the second member 134, the nut 135, the first nut fixing wing 136, and the second nut fixing wing are provided.
  • the 137 and nut fixing web 138 are modified on the other side of the connecting member 130 such that the through hole THb is opposed to the through hole THa.
  • the second member 134 passes through the through hole THa and the through hole THb, thereby connecting and fixing the first wing portion 114a of the bearing plate 131 and the third wing 114 to fix the frame member 110 and The relative position of the connecting member 130.
  • Other related structural and material details are the same as those of the first embodiment, and thus the description thereof will not be repeated.
  • Figure 10 is a cross-sectional view showing a support member group according to a fifth embodiment of the present invention, the cross-sectional position of which is the same as that of Figure 3.
  • the present embodiment is different from the first embodiment in that the connecting member 130 of the present embodiment includes only the third member 139, and the through hole THb is modified in the first wing portion 114a of the third flap 114 and is located in the second belly. Between the plate 115 and the reinforcing rib 118, the post 120 has a fixing hole SH therein.
  • the third member 139 passes through the through hole THb and protrudes into the fixing hole SH, thereby joining and fixing the frame member 110 and the stay 120, and therefore, the third flap 114 of the frame member 110 directly abuts On the end surface 122 of the post 120, and the second web 115 (i.e., the vertical projection of the first web 113) extends against the second half II of the end surface 122.
  • the third component 139 described above can be a stud, a latch, or any combination of the above. As for other related structures and material details, they are the same as the first embodiment, and therefore will not be repeated.
  • Embodiments of the present invention will be disclosed hereinafter to explain the support member group of the above embodiment, and it is indeed possible to provide the required performance. It should be understood that in the following description, the parameters already mentioned in the above embodiments will not be repeated, and only need to be further defined to supplement them.
  • the support member group of the first embodiment is mainly employed, and in this embodiment, Nuts are mounted on the bearing plate 131 and on the fourth wing 116.
  • the frame member is made of aluminum alloy (AL5052H32 or AL6063T5), and the bearing plate 131, the fixing plate 132, the first nut fixing wing 136, the second nut fixing wing 137 and the nut fixing web 138 are integrally formed of aluminum alloy (AL5052H32 or AL6063T5), a first member 133, second member 134 and the nut 135 are made of stainless steel (SUS304) o elasticity coefficient of the material, yield strength and fracture strength as shown in table 1 below. Table 1 Elastic coefficient, lodging strength and breaking strength of each material
  • the axial force of the pillar can be sufficiently used to support the frame member and the solar module module to reduce the pillar or the connecting member. The risk of permanent deformation.
  • the axial force of the strut is sufficient to support the frame member and the solar module module, the overall system's ability to withstand wind or snow pressure is also increased.

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Abstract

一种太阳能模块的支撑构件组，包含框架构件（110）、支柱（120）与连接构件（130），框架构件（110）包含第一翼板（111）、第二翼板（112）与第一腹板（113），第二翼板（112）相对于第一翼板（111）实质平行设置，第一腹板（113）连接第一翼板（111）与第二翼板（112），使得第一翼板（111）、第二翼板（112）与第一腹板（113）共同定义容置槽（G），借此容置太阳能模块，支柱（120）用以支撑框架构件（110），且此支柱（120）具有面对框架构件（110）的端表面（122），此端表面（122）区分为第一半部（I）与第二半部（II），上述的第一半部（I）较第二半部（II）更靠近框架构件（110）的中轴线（C），第一腹板（113）在端表面（122）上的垂直投影位置落在第二半部（II），连接构件（130）用以连接支柱（120）与框架构件（110）。

Description

太阳能模块的支撑构件组 技术领域
本发明是有关于一种太阳能模块的支撑构件组。 背景技术
一般而言，太阳能模块大多是通过支撑构件组架设于户外，以迎接太阳光。 由于太阳能模块与支撑构件组是长期放置于户外的系统，因此必须要能够承受 各种恶劣的环境条件。举例来说， 当太阳能模块与支撑构件组架设在风大的区 域， 太阳能模块与支撑构件组就必须具备足够的风压承受能力。又， 若太阳能 模块与支撑构件组架设在会下雪的区域，太阳能模块与支撑构件组就必须具备 足够的雪压承受能力。
然而， 由于现有的支撑构件组大多强调快速拆装的能力， 而没有足够的压 力承受能力， 因此在恶劣的环境条件下承受风压及雪压时，往往会因为支撑能 力不足而有永久变形的风险， 严重时甚至会让太阳能模块掉落。 发明公开
本发明的一技术态样是在提供一种太阳能模块的支撑构件组，用以解决以 上先前技术所提到的困难。
根据本发明一实施方式， 一种太阳能模块的支撑构件组包含框架构件、支 柱、 连接构件、 第一部件与第二部件。 框架构件包含第一翼板、 第二翼板与第 一腹板。第二翼板相对于第一翼板实质平行设置。第一腹板连接第一翼板与第 二翼板， 使得第一翼板、第二翼板与第一腹板共同定义容置槽， 借此容置太阳 能模块。支柱用以支撑框架构件， 且此支柱具有面对框架构件的端表面， 此端 表面区分为第一半部与第二半部，上述的第一半部较第二半部更靠近框架构件 的中轴线。第一腹板在端表面上的垂直投影位置落在第二半部。连接构件用以 连接支柱与框架构件， 且此连接构件包含承靠板与固定板。框架构件与支柱的 端表面分别抵接承靠板的相对两表面。固定板大致垂直地连接于承靠板的底表 面， 用来使连接构件固定于支柱。第一部件用以连结并固定固定板与支柱。第 二部件用以连结并固定框架构件与承靠板。
在本发明一或多个实施方式中， 上述的承靠板具有贯穿孔于其中。框架构 件亦具有贯穿孔于其中， 此框架构件的贯穿孔为长孔。第二部件穿过承靠板的 贯穿孔与框架构件的贯穿孔。
在本发明一或多个实施方式中，上述的太阳能模块的支撑构件组更包含绝 缘镀层， 此绝缘镀层镀于框架构件的表面。连接构件可包含螺合构件， 此螺合 构件设置于框架构件上， 以与第二部件连结而固定框架构件与连接构件， 且此 螺合构件破坏绝缘镀层， 而直接接触框架构件。
在本发明一或多个实施方式中，上述的框架构件更包含第三翼板与第二腹 板。第三翼板相对于第二翼板实质平行设置，且此第三翼板位于第二翼板下方， 用以抵靠于连接构件的承靠板。第二腹板与第一腹板平行并相连， 并用以连接 第二翼板与第三翼板。第三翼板具有第一翼部， 此第一翼部与第二翼板朝大致 相同的方向沿大致垂直于第二腹板的方向延伸。第二部件用以连结并固定第一 翼部与承靠板。
在本发明一或多个实施方式中，上述的框架构件更包含第三翼板与第二腹 板。第三翼板相对于第二翼板实质平行设置，且此第三翼板位于第二翼板下方， 用以抵靠于连接构件的承靠板。第二腹板与第一腹板平行并相连， 并用以连接 第二翼板与第三翼板。第三翼板具有第一翼部与第二翼部。第一翼部与第二翼 板朝大致相同的方向沿大致垂直于第二腹板的方向延伸。第二翼部与第一翼部 朝相反的方向沿大致垂直于第二腹板的方向延伸。第二部件用以连结并固定第 二翼部与承靠板。
在本发明一或多个实施方式中，上述的框架构件更包含第四翼板与第三腹 板。第四翼板连接第二腹板， 相对于第三翼板实质平行设置， 且位于第三翼板 的第二翼部上方。第二部件更连结于第四翼板。第三腹板连接第四翼板与第三 翼板的第二翼部， 使得至少部分的第二腹板、第三翼板的第二翼部、 第三腹板 与第四翼板共同构成中空框条。
在本发明一或多个实施方式中，上述的第四翼板至第三翼板的第二翼部的 垂直高度， 小于第二翼板至第三翼板的第一翼部的垂直高度。
在本发明一或多个实施方式中，上述的第四翼板至第三翼板的第二翼部的 垂直高度， 大致等于第二翼板至第三翼板的第一翼部的垂直高度。
根据本发明另一实施方式， 一种太阳能模块的支撑构件组包含框架构件、 支柱与连接构件。框架构件包含第一翼板、第二翼板与第一腹板。第二翼板相 对于第一翼板实质平行设置。第一腹板连接第一翼板与第二翼板， 使得第一翼 板、第二翼板与第一腹板共同定义容置槽， 借此容置太阳能模块。支柱用以支 撑框架构件， 且此支柱具有面对框架构件的端表面， 此端表面具有相对的内侧 边缘与外侧边缘。 内侧边缘较外侧边缘更靠近框架构件的中轴线， 且外侧边缘 较内侧边缘更靠近第一腹板在端表面所在的平面上的垂直投影位置。连接构件 用以连接支柱与框架构件。
在本发明一或多个实施方式中， 上述的连接构件包含承靠板、 固定板、第 一部件与第二部件。 框架构件与支柱的端表面分别抵接承靠板的相对两表面。 固定板大致垂直地连接于承靠板的底表面，用来使连接构件固定于支柱。第一 部件用以连结并固定固定板与支柱。第二部件用以连结并固定框架构件与承靠 板。
在本发明一或多个实施方式中， 上述的承靠板具有贯穿孔于其中。框架构 件亦具有贯穿孔于其中， 此框架构件的贯穿孔为长孔。第二部件穿过承靠板的 贯穿孔与框架构件的贯穿孔。
在本发明一或多个实施方式中，上述的太阳能模块的支撑构件组更包含绝 缘镀层， 此绝缘镀层镀于框架构件的表面。连接构件可包含螺合构件， 此螺合 构件设置于框架构件上， 以与第二部件连结而固定框架构件与连接构件， 且此 螺合构件破坏绝缘镀层， 而直接接触框架构件。
在本发明一或多个实施方式中，上述的框架构件更包含第三翼板与第二腹 板。第三翼板相对于第二翼板实质平行设置，且此第三翼板位于第二翼板下方， 用以抵靠于连接构件的承靠板。第二腹板与第一腹板平行并相连， 并用以连接 第二翼板与第三翼板。第三翼板具有第一翼部， 此第一翼部与第二翼板朝大致 相同的方向沿大致垂直于第二腹板的方向延伸。第二部件用以连结并固定第一 翼部与承靠板。
在本发明一或多个实施方式中，上述的框架构件更包含第三翼板与第二腹 板。第三翼板相对于第二翼板实质平行设置，且此第三翼板位于第二翼板下方， 用以抵靠于连接构件的承靠板。第二腹板与第一腹板平行并相连， 并用以连接 第二翼板与第三翼板。第三翼板具有第一翼部与第二翼部。第一翼部与第二翼 板朝大致相同的方向沿大致垂直于第二腹板的方向延伸。第二翼部与第一翼部 朝相反的方向沿大致垂直于第二腹板的方向延伸。第二部件用以连结并固定第 二翼部与承靠板。
在本发明一或多个实施方式中，上述的框架构件更包含第四翼板与第三腹 板。第四翼板连接第二腹板， 相对于第三翼板实质平行设置， 且位于第三翼板 的第二翼部上方。第二部件更连结于第四翼板。第三腹板连接第四翼板与第三 翼板的第二翼部， 使得至少部分的第二腹板、第三翼板的第二翼部、 第三腹板 与第四翼板共同构成中空框条。
在本发明一或多个实施方式中，上述的第四翼板至第三翼板的第二翼部的 垂直高度， 小于第二翼板至第三翼板的第一翼部的垂直高度。
在本发明一或多个实施方式中，上述的第四翼板至第三翼板的第二翼部的 垂直高度， 大致等于第二翼板至第三翼板的第一翼部的垂直高度。
在本发明一或多个实施方式中， 上述的连接构件包含第三部件， 框架构件 具有贯穿孔于其中，支柱具有固定孔于其中。第三部件穿过框架构件的贯穿孔， 而伸入支柱的固定孔中， 借此连结并固定框架构件与支柱。 附图简要说明
图 1绘示依照本发明第一实施方式的支撑构件组的立体图。
图 2绘示图 1的支撑构件组的俯视图。
图 3绘示沿图 2的线段 3的剖面图。
图 4绘示图 1的局部 4的侧视图。
图 5绘示图 2的局部 5的放大图。
图 6绘示依照本发明另一实施方式的支撑构件组的局部剖面图，其剖面区 域如图 3的局部 6所标示。
图 7绘示依照本发明第二实施方式的支撑构件组的剖面图，其剖面位置与 图 3相同。
图 8绘示依照本发明第三实施方式的支撑构件组的剖面图，其剖面位置与 图 3相同。
图 9绘示依照本发明第四实施方式的支撑构件组的剖面图，其剖面位置与 图 3相同。
图 10绘示依照本发明第五实施方式的支撑构件组的剖面图， 其剖面位置 与图 3相同。
其中， 附图标记：
110： 框架构件 111 : 第一翼板
112： 第二翼板 113 : 第一腹板 114： 114a
114b 第二翼部 115
116 第四翼板 117
118 加强肋板 120 支柱
121 内侧边缘 122 端表面
123 外侧边缘 125 侧表面
130 连接构件 131
132 固定板 132a 固定板
132b 固定板 133 第一部件
134 第二部件 135 螺母
136 第一螺母固定翼 137 第二螺母固定翼
138 螺母固定腹板
3： 4： 局部
5： 局部 6： 局部
C: 中轴线 G: 容置槽
HI : 第四翼板至，三翼板的: .翼部的垂直高度
H2: 第二翼板至，三翼板的: -翼部的垂直高度
N: 螺母容置空间 THa: 贯穿孔
THb: 贯穿孔 THc: 贯穿孔
SH: 固定孔 I： 第一半部
II： 第二半部 实现本发明的最佳方式
以下将以附图揭露本发明的多个实施方式， 为明确说明起见， 许多实务上 的细节将在以下叙述中一并说明。然而， 应了解到， 这些实务上的细节不应用 以限制本发明。 也就是说， 在本发明部分实施方式中， 这些实务上的细节是非 必要的。此外， 为简化附图起见， 一些公知惯用的结构与元件在附图中将以简 单示意的方式绘示。
关于本文中所使用的 "约"、 "大约"或 "大致"， 一般是指数值的误差或 范围于百分之二十以内，较好地是于百分之十以内，更佳地是于百分之五以内。 文中若无明确说明， 所提及的数值皆视为近似值， 即具有如 "约"、 "大约"或 "大致"所表示的误差或范围。
第一实施方式
图 1绘示依照本发明第一实施方式的支撑构件组的立体图。 图 2绘示图 1的 支撑构件组的俯视图。如图 1、 2所示， 一种太阳能模块的支撑构件组包含框架 构件 110、支柱 120与连接构件 130。框架构件 110用以将太阳能模块框设于其中。 支柱 120站立于地面上。 连接构件 130用以连接支柱 120与框架构件 110。
在本实施方式中， 支柱 120与连接构件 130的数量均为 4个， 其分别安装于 框架构件 110的四个角落。此外， 位于框架构件 110—侧 (例如： 前侧)的支柱 120 较位于框架构件 110另一侧 (例如：后侧)的支柱 120短，借此让框架构件 110相较 于地面倾斜一预定角度，使得安装于其中的太阳能模块迎接太阳光。应了解到， 以上所举的支柱 120与连接构件 130的数量与尺寸关均仅为例示，而非用以限制 本发明， 本领域技术人员， 应视实际需要， 弹性选择支柱 120与连接构件 130 的实施方式。
图 3绘示沿图 2的线段 3的剖面图。图 4绘示图 1的局部 4的侧视图。如图所示。 框架构件 110包含第一翼板 111、 第二翼板 112与第一腹板 113。 第二翼板 112相 对于第一翼板 111实质平行设置， 且此第二翼板 112位于第一翼板 111下方。 第 一腹板 113连接第一翼板 111与第二翼板 112， 使得第一翼板 111、 第二翼板 112 与第一腹板 113共同定义容置槽 G， 借此容置太阳能模块。 支柱 120用以支撑框 架构件 110， 且此支柱 120具有面对框架构件 110的端表面 122， 此端表面 122区 分为第一半部 I与第二半部 II， 上述的第一半部 I较第二半部 II更靠近框架构件 110的中轴线 。 第一腹板 113在端表面 122上的垂直投影位置落在第二半部 II。 或者说， 上述的端表面 122具有相对的内侧边缘 121与外侧边缘 123， 内侧边缘 121较外侧边缘 123更靠近框架构件 110的中轴线 。 第一腹板 113在端表面 122 所在的平面上的垂直投影位置较远离内侧边缘 121， 并较靠近外侧边缘 123。亦 SP ,外侧边缘 123较内侧边缘 121更靠近第一腹板 113在端表面 122所在的平面上 的垂直投影位置。
在此设计中， 当框架构件 110将太阳能模块框设于其中时， 支柱 120的轴向 力将可充分地用来支撑框架构件 110与太阳能模块，以减少支柱 120或连接构件 130永久变形的风险。此外， 也因为支柱 120的轴向力可充分地用来支撑框架构 件 110与太阳能模块， 因此整体系统承受风压或雪压的能力也会上升。
在本实施方式中，第一腹板 113在端表面 122所在的平面上的垂直投影位置 可与外侧边缘 123重叠。 但此并不限制本发明， 本领域技术人员， 应视实际需 要， 弹性选择第一腹板 113的位置。
请继续参考图 3、 4。 上述的连接构件 130包含承靠板 131、 固定板 132、 第 一部件 133与第二部件 134。 框架构件 110与支柱 120的端表面 122分别抵接承靠 板 131的相对两表面。 固定板 132大致垂直地连接于承靠板 131的底表面， 用来 使连接构件 130固定于支柱 120。 支柱 120具有侧表面 125， 此侧表面 125与端表 面 122相邻接。 固定板 132与支柱 120的侧表面 125相对。 第一部件 133用以连结 并固定固定板 132与支柱 120。第二部件 134用以连结并固定框架构件 110与承靠 板 131。
具体而言， 上述的固定板 132的数量为 2个， 例如： 固定板 132a与固定板
132bo 固定板 132a、 固定板 132b与介于两者间的部分承靠板 131共同定义一大 致呈倒 U形 (：或， π形)的剖面形状， 以将支柱 120拘束于固定板 132a与固定板 132b之间。 第一部件 133用以连结并固定固定板 132a、 支柱 120与固定板 132b， 以确实固定支柱 120与连接构件 130的相对位置。在本实施方式中，第一部件 133 可为螺栓、 插销或其他适合的部件。
在本实施方式中， 框架构件 110更可包含第三翼板 114与第二腹板 115。 第 三翼板 114相对于第二翼板 112实质平行设置， 且位于第二翼板 112下方， 用以 抵靠于连接构件 130的承靠板 131。第二腹板 115与第一腹板 113平行并相连于与 第二翼板 112的连接处， 且第二腹板 115连接第二翼板 112与第三翼板 114。第三 翼板 114具有第一翼部 114a与第二翼部 114b。 第一翼部 114a与第二翼板 112朝大 致相同的方向且沿大致垂直于第二腹板 115的方向延伸，亦即朝向框架构件 110 的内部延伸。 第二翼部 114b与第二翼板 112朝相反的方向沿大致垂直于第二腹 板 115的方向延伸， 亦即朝向框架构件 110的外部延伸。 第三翼板 114与第二腹 板 115的连接处即为第一翼部 114a与第二翼部 114b的连接处， 而第一翼部 114a 与第二翼部 114b以第二腹板 115的连接处为准朝相反方向延伸。
此外， 本实施方式的框架构件 110更可包含第四翼板 116与第三腹板 117。 第四翼板 116连接第二腹板 115， 第四翼板 116相对于第三翼板 114实质平行设 置， 且第四翼板 116位于第三翼板 114的第二翼部 114b上方。 第三腹板 117连接 第四翼板 116与第三翼板 114的第二翼部 114b， 使得至少部分的第二腹板 115、 第三翼板 114的第二翼部 114b、第三腹板 117与第四翼板 116共同构成中空框条。 前述框架构件 110的第一翼板 111、 第二翼板 112、 第三翼板 114与第四翼板 116 大致呈水平的构件， 而第一腹板 113、 第二腹板 115与第三腹板 117大致呈垂直 的构件。
在本实施方式中，第四翼板 116至第三翼板 114的第二翼部 114b的垂直高度 HI , 小于第二翼板 112至第三翼板 114的第一翼部 114a的垂直高度 H2。 但此并 不限制本发明， 本领域技术人员， 应视实际需要， 弹性选择第四翼板 116与第 二翼板 112的相对位置。
另外， 在本实施方式中， 为了强化框架构件 110抗弯曲的能力， 制造者可 选择在第二翼板 112与第三翼板 114的第一翼部 114a之间设置加强肋板 118。 应 了解到， 此一加强肋板 118并非必要元件， 若框架构件 110的强度足够， 加强肋 板 118也可以选择省略不设置。
在本实施方式中，为了确实利用支柱 120的轴向力来支撑框架构件 110与太 阳能模块， 第二腹板 115与加强肋板 118在端表面 122所在的平面上的垂直投影 位置均落在端表面 122上。 更具体地说， 上述的第二腹板 115在端表面 122上的 垂直投影位置落在第二半部 II上。 亦即， 外侧边缘 123较内侧边缘 121更靠近第 二腹板 115在端表面 122上的垂直投影位置。 上述的加强肋板 118在端表面 122 上的垂直投影位置落在第一半部 I上。 亦即， 内侧边缘 121较外侧边缘 123更靠 近加强肋板 118在端表面 122上的垂直投影位置。
在本实施方式中，承靠板 131、第三翼板 114的第二翼部 114b与第四翼板 116 分别具有贯穿孔 THa、 贯穿孔 THb与贯穿孔 THc于其中。第二部件 134—并穿过 贯穿孔 THa、 贯穿孔 THb与贯穿孔 THc， 借此连结并固定承靠板 131、 第三翼板 114的第二翼部 114b与第四翼板 116， 以固定框架构件 110与连接构件 130的相对 位置。 上述的第二部件 134可为螺栓、 插销或其他适合的部件。
图 5绘示图 2的局部 5的放大图。 如图所示， 在本实施方式中， 框架构件 110 的贯穿孔 (例如： 贯穿孔 THc)可为长孔。 在组装时， 框设有太阳能模块的框架 构件 110与连接构件 130可能会因为地面不平而无法对位。 此时若框架构件 110 的贯穿孔 (例如： 贯穿孔 THc)为长孔， 就可以产生一部分的公差容许范围， 让 组装顺利完成。
回到图 3、 4。 在第二部件 134为螺栓的实施方式中， 若承靠板 131、 第三翼 板 114的第二翼部 114b与第四翼板 116的肉厚太薄而无法攻螺纹，则组装者可选 择以螺母 135来固定螺栓 (亦即， 第二部件 134)。 更具体地说， 本实施方式的连 接构件 130更可包含第一螺母固定翼 136、 第二螺母固定翼 137与螺母固定腹板 138o 第一螺母固定翼 136连接固定板 132b。 第二螺母固定翼 137与第一螺母固 定翼 136分开以供螺栓 (亦即， 第二部件 134)穿过。 螺母固定腹板 138连接承靠 板 131与第二螺母固定翼 137， 使得第一螺母固定翼 136、 第二螺母固定翼 137、 螺母固定腹板 138、部分的承靠板 131与部分的固定板 132b共同定义螺母容置空 间N。螺母 135容置于螺母容置空间 N中。螺栓 (亦即， 第二部件 134)穿过第一螺 母固定翼 136与第二螺母固定翼 137之间的空间而锁附于螺母 135中。
在本实施方式中， 由于螺母 135受第一螺母固定翼 136与第二螺母固定翼 137的拘束而无法于垂直方向上位移，连带使得锁附于螺母 135中的螺栓 (亦即， 第二部件 134)也无法于垂直方向上位移， 因此第四翼板 116上可选择不用再上 螺母， 以节省组装工序。 此外， 由于太阳能模块与框架构件 110的重量极重， 因此纵使第四翼板 116上没有螺母固定， 框架构件 110也不容易脱离螺栓 (亦即， 第二部件 134)。
当然， 组装者也可以选择将螺母 135改装在第四翼板 116上， 或者在承靠板 131下及第四翼板 116上均安装螺母 135。此外，在将螺母 135改装在第四翼板 116 上 (亦即， 仅第四翼板 116上安装有螺母 135， 承靠板 131下则没有安装螺母：)， 或第二部件 134为插销的实施方式中，连接构件 130也不需要具有第一螺母固定 翼 136、 第二螺母固定翼 137与螺母固定腹板 138。 另外， 若框架构件 110与连接 构件 130中的任一者的肉厚足够攻螺纹， 则制造者也可以选择在框架构件 110 及 /或连接构件 130中攻螺纹，并直接将螺栓 (亦即，第二部件 134)锁附于螺纹中， 而不需要设置螺母 135。本领域技术人员， 应视实际需要弹性选择连接构件 130 的实施方式。
图 6绘示依照本发明另一实施方式的支撑构件组的局部剖面图， 其剖面区 域如图 3的局部 6所标示。在本实施方式中， 支撑构件组更可包含绝缘镀层 140， 此绝缘镀层 140镀于框架构件 110的表面 (：例如第四翼板 116与第三腹板 117的表 面：)。 由于太阳能模块照到光线就会发电， 因此绝缘镀层 140的存在可避免太阳 能模块所产生的电力透过框架构件 110而电伤组装者。上述的绝缘镀层 140例如 可为阳极膜。
在本实施方式中， 连接构件 130可包含螺合构件， 此螺合构件设置于框架 构件 110上， 以与第二部件 134连结而固定框架构件 110与连接构件 130， 且此螺 合构件会破坏绝缘镀层 140， 而直接接触框架构件 110。 举例来说， 在图 6中， 螺母 135可与第二部件 134螺合于第四翼板 116上， 且螺母 135会破坏绝缘镀层 140， 而直接接触第四翼板 116。 如此一来， 连接构件 130与框架构件 110之间就 会产生导电通道，让太阳能模块透过框架构件 110、连接构件 130与支柱而接地。
应了解到， 虽然图 6绘示以螺母 135来破坏绝缘镀层 140， 但此并不限制本 发明。在本发明一或多个实施方式中， 亦可以选择以螺栓头或垫圈来破坏绝缘 镀层 140。 本领域技术人员应视实际需要， 弹性选择其实施方式。
在以上实施方式中， 框架构件 110的材质可为金属， 例如： 铝合金、 钢、 不锈钢或上述的任意组合。 框架构件 110的制造方法可为锻造、 铸造或上述的 任意组合。 当然， 如果材质或形状许可， 框架构件 110也可以选择先以铝挤成 型的方式制造成条状材后， 再将这些条状材组装成框架构件 110。 从结构上来 看， 上述的第一翼板 111、 第二翼板 112、 第一腹板 113、 第三翼板 114、 第二腹 板 115、 第四翼板 116、 第三腹板 117与加强肋板 118为一体成型的元件。
此外， 上述的连接构件 130的材质可为金属， 例如： 铝合金、 钢、 不锈钢 或上述的任意组合。 连接构件 130的制造方法可为锻造、 铸造或上述的任意组 合。 从结构上来看， 上述的承靠板 131、 固定板 132、 第一螺母固定翼 136、 第 二螺母固定翼 137与螺母固定腹板 138为一体成型的元件， 第一部件 133、 第二 部件 134与螺母 135(如果有:)则为独立的元件。
再者， 上述的支柱 120的材质可为金属， 例如： 铝合金、 钢、 不锈钢或上 述的任意组合。 支柱 120的制造方法可为锻造、 铸造或上述的任意组合。 第二实施方式
图 7绘示依照本发明第二实施方式的支撑构件组的剖面图， 其剖面位置与 图 3相同。 本实施方式与第一实施方式的不同点在于： 在本实施方式中， 第四 翼板 116至第三翼板 114的第二翼部 114b的垂直高度 HI， 大致等于第二翼板 112 至第三翼板 114的第一翼部 114a的垂直高度 H2。 至于其他相关的结构与材质细 节， 均与第一实施方式相同， 因此不再重复赘述。 第三实施方式
图 8绘示依照本发明第三实施方式的支撑构件组的剖面图， 其剖面位置与 图 3相同。 本实施方式与第一实施方式的不同点在于： 本实施方式的框架构件 110省略了第四翼板 116与第三腹板 117， 因此第二部件 134仅一并穿过贯穿孔 THa与贯穿孔 THb，借此连结并固定承靠板 131与第三翼板 114的第二翼部 114b， 即可固定框架构件 110与连接构件 130的相对位置。至于其他相关的结构与材质 细节， 均与第一实施方式相同， 因此不再重复赘述。 第四实施方式
图 9绘示依照本发明第四实施方式的支撑构件组的剖面图， 其剖面位置与 图 3相同。 本实施方式与第一实施方式的不同点在于： 本实施方式的框架构件 110省略了第四翼板 116、 第三腹板 117与第三翼板 114的第二翼部 114b。 此外， 本实施方式将贯穿孔 THa改设在第三翼板 114的第一翼部 114a， 并将贯穿孔 THb、 第二部件 134、 螺母 135、 第一螺母固定翼 136、 第二螺母固定翼 137与螺 母固定腹板 138改设在连接构件 130的另一侧， 使得贯穿孔 THb与贯穿孔 THa相 对。在本实施方式中， 第二部件 134—并穿过贯穿孔 THa与贯穿孔 THb， 借此连 结并固定承靠板 131与第三翼板 114的第一翼部 114a， 以固定框架构件 110与连 接构件 130的相对位置。 至于其他相关的结构与材质细节， 均与第一实施方式 相同， 因此不再重复赘述。 第五实施方式
图 10绘示依照本发明第五实施方式的支撑构件组的剖面图，其剖面位置与 图 3相同。 本实施方式与第一实施方式的不同点在于： 本实施方式的连接构件 130仅包含第三部件 139， 贯穿孔 THb改设在第三翼板 114的第一翼部 114a， 且 位于第二腹板 115与加强肋板 118之间， 支柱 120具有固定孔 SH于其中。 在本实 施方式中， 第三部件 139穿过贯穿孔 THb, 而伸入固定孔 SH中， 借此连结并固 定框架构件 110与支柱 120， 因此， 框架构件 110的第三翼板 114直接抵靠于支柱 120的端表面 122上， 且第二腹板 115(亦即第一腹板 113的垂直投影：)延伸抵靠在 端表面 122的第二半部 II上。 上述的第三部件 139可为螺柱、 插销或上述的任意 组合。至于其他相关的结构与材质细节， 均与第一实施方式相同， 因此不再重 复赘述。 以下将揭露本发明的实施例， 借此说明上述实施方式的支撑构件组， 确实 能够提供所需要的性能。应了解到， 在以下叙述中， 已经在上述实施方式中提 到的参数将不再重复赘述， 仅就需进一歩界定者加以补充。
在以下实施例中， 主要采用第一实施方式的支撑构件组， 在本实施例中， 在承靠板 131下及第四翼板 116上均安装有螺母。 框架构件的材质为铝合金 (AL5052H32或 AL6063T5), 承靠板 131、 固定板 132、 第一螺母固定翼 136、 第 二螺母固定翼 137与螺母固定腹板 138为一体成型的铝合金 (AL5052H32或 AL6063T5) , 第一部件 133、 第二部件 134与螺母 135的材质均为不锈钢 (SUS304)o 上述材质的弹性系数、 降伏强度与断裂强度列于以下表一。 表一 各材质的弹性系数、 降伏强度与断裂强度
Figure imgf000014_0001
在以上条件下， 模拟太阳能模块的正面承受 5400 Pa的均匀压力， 结果显 示支撑构件组的各元件均无断裂的风险， 确实能够承受 5400 Pa的均匀压力。 工业应用性
本发明的太阳能模块的支撑构件组，当框架构件将太阳能模组模块框设于 其中时， 支柱的轴向力将可充分地用来支撑框架构件与太阳能模组模块， 以减 少支柱或连接构件永久变形的风险。此外， 也因为支柱的轴向力可充分地用来 支撑框架构件与太阳能模组模块，因此整体系统承受风压或雪压的能力也会上 升。

Claims

权 利 要 求 书
1. 一种太阳能模块的支撑构件组， 包含：
一框架 件， 包含： 一第二翼板， 相对于该第一翼板实质平行设置； 以及
一第一腹板， 连接该第一翼板与该第二翼板， 使得该第一翼板、 该第二翼 板与该第一腹板共同定义一容置槽， 借此容置一太阳能模块；
一支柱， 用以支撑该框架构件， 该支柱具有面对该框架构件的一端表面， 该端表面区分为一第一半部与一第二半部，该第一半部较该第二半部更靠近该 框架构件的中轴线，其中该第一腹板在该端表面上的垂直投影位置落在该第二 半部；
一连接构件， 用以连接该支柱与该框架构件， 其中该连接构件包含： 一承靠板，该框架构件与该支柱的该端表面分别抵接该承靠板的相对两表 面； 以及
至少一固定板， 大致垂直地连接于该承靠板的一底表面， 用来使该连接构 件固定于该支柱；
一第一部件， 用以连结并固定该固定板与该支柱； 以及
一第二部件， 用以连结并固定该框架构件与该承靠板。
2. 如权利要求 1所述的太阳能模块的支撑构件组， 该承靠板具有至少一贯 穿孔于其中， 该框架构件亦具有至少一贯穿孔于其中， 该框架构件的该贯穿孔 为长孔， 该第二部件穿过该承靠板的该贯穿孔与该框架构件的该贯穿孔。
3. 如权利要求 2所述的太阳能模块的支撑构件组， 更包含：
一绝缘镀层， 镀于该框架构件的表面， 其中该连接构件包含一螺合构件， 该螺合构件设置于该框架构件上，以与该第二部件连结而固定该框架构件与该 连接构件， 且该螺合构件破坏该绝缘镀层， 而直接接触该框架构件。
4. 如权利要求 1所述的太阳能模块的支撑构件组， 该框架构件更包含： 一第三翼板， 相对于该第二翼板实质平行设置， 且位于该第二翼板下方， 用以抵靠于该连接构件的该承靠板； 以及
一第二腹板， 与该第一腹板平行并相连， 并用以连接该第二翼板与该第三 其中该第三翼板具有一第一翼部，该第一翼部与该第二翼板朝大致相同的 方向沿大致垂直于该第二腹板的方向延伸，
其中该第二部件用以连结并固定该第一翼部与该承靠板。
5. 如权利要求 1所述的太阳能模块的支撑构件组， 该框架构件更包含： 一第三翼板， 相对于该第二翼板实质平行设置， 且位于该第二翼板下方， 用以抵靠于该连接构件的该承靠板； 以及
一第二腹板， 与该第一腹板平行并相连， 并用以连接该第二翼板与该第三 翼板，
其中该第三翼板具有一第一翼部与一第二翼部，该第一翼部与该第二翼板 朝大致相同的方向沿大致垂直于该第二腹板的方向延伸，该第二翼部与该第一 翼部朝相反的方向沿大致垂直于该第二腹板的方向延伸，
其中该第二部件用以连结并固定该第二翼部与该承靠板。
6. 如权利要求 5所述的太阳能模块的支撑构件组， 该框架构件更包含： 一第四翼板， 连接该第二腹板， 相对于该第三翼板实质平行设置， 且位于 该第三翼板的该第二翼部上方， 且该第二部件更连结于该第四翼板； 以及
一第三腹板， 连接该第四翼板与该第三翼板的该第二翼部， 使得至少部分 的该第二腹板、该第三翼板的该第二翼部、该第三腹板与该第四翼板共同构成 一中空框条。
7. 如权利要求 6所述的太阳能模块的支撑构件组， 该第四翼板至该第三翼 板的该第二翼部的垂直高度，小于该第二翼板至该第三翼板的该第一翼部的垂 直高度。
8. 如权利要求 6所述的太阳能模块的支撑构件组， 该第四翼板至该第三翼 板的该第二翼部的垂直高度，大致等于该第二翼板至该第三翼板的该第一翼部 的垂直高度。
9. 一种太阳能模块的支撑构件组， 包含：
一框架 件， 包含： 一第二翼板， 相对于该第一翼板实质平行设置； 以及
一第一腹板， 连接该第一翼板与该第二翼板， 使得该第一翼板、 该第二翼 板与该第一腹板共同定义一容置槽， 借此容置一太阳能模块；
一支柱， 用以支撑该框架构件， 该支柱具有面对该框架构件的一端表面， 该端表面具有相对的一内侧边缘与一外侧边缘，该内侧边缘较该外侧边缘更靠 近该框架构件的中轴线，且该外侧边缘较该内侧边缘更靠近该第一腹板在该端 表面所在的平面上的垂直投影位置； 以及
一连接构件， 用以连接该支柱与该框架构件。
10. 如权利要求 9所述的太阳能模块的支撑构件组， 该连接构件包含： 一承靠板，该框架构件与该支柱的该端表面分别抵接该承靠板的相对两表 面；
至少一固定板， 大致垂直地连接于该承靠板的一底表面， 用来使该连接构 件固定于该支柱；
一第一部件， 用以连结并固定该固定板与该支柱； 以及
一第二部件， 用以连结并固定该框架构件与该承靠板。
11. 如权利要求 10所述的太阳能模块的支撑构件组， 该承靠板具有至少一 贯穿孔于其中， 该框架构件亦具有至少一贯穿孔于其中， 该框架构件的该贯穿 孔为长孔， 该第二部件穿过该承靠板的该贯穿孔与该框架构件的该贯穿孔。
12. 如权利要求 11所述的太阳能模块的支撑构件组， 更包含：
一绝缘镀层， 镀于该框架构件的表面， 其中该连接构件包含一螺合构件， 该螺合构件设置于该框架构件上，以与该第二部件连结而固定该框架构件与该 连接构件， 且该螺合构件破坏该绝缘镀层， 而直接接触该框架构件。
13. 如权利要求 10所述的太阳能模块的支撑构件组， 该框架构件更包含： 一第三翼板， 相对于该第二翼板实质平行设置， 且位于该第二翼板下方， 用以抵靠于该连接构件的该承靠板； 以及
一第二腹板， 与该第一腹板平行并相连， 并用以连接该第二翼板与该第三 翼板，
其中该第三翼板具有一第一翼部，该第一翼部与该第二翼板朝大致相同的 方向沿大致垂直于该第二腹板的方向延伸，
其中该第二部件用以连结并固定该第一翼部与该承靠板。
14. 如权利要求 10所述的太阳能模块的支撑构件组， 该框架构件更包含： 一第三翼板， 相对于该第二翼板实质平行设置， 且位于该第二翼板下方， 用以抵靠于该连接构件的该承靠板； 以及
一第二腹板， 与该第一腹板平行并相连， 并用以连接该第二翼板与该第三 其中该第三翼板具有一第一翼部与一第二翼部，该第一翼部与该第二翼板 朝大致相同的方向沿大致垂直于该第二腹板的方向延伸，该第二翼部与该第一 翼部朝相反的方向沿大致垂直于该第二腹板的方向延伸，
其中该第二部件用以连结并固定该第二翼部与该承靠板。
15. 如权利要求 14所述的太阳能模块的支撑构件组， 该框架构件更包含： 一第四翼板， 连接该第二腹板， 相对于该第三翼板实质平行设置， 且位于 该第三翼板的该第二翼部上方， 且该第二部件更连结于该第四翼板； 以及 一第三腹板， 连接该第四翼板与该第三翼板的该第二翼部， 使得至少部分 的该第二腹板、该第三翼板的该第二翼部、该第三腹板与该第四翼板共同构成 一中空框条。
16. 如权利要求 15所述的太阳能模块的支撑构件组， 该第四翼板至该第三 翼板的该第二翼部的垂直高度，小于该第二翼板至该第三翼板的该第一翼部的 垂直高度。
17. 如权利要求 15所述的太阳能模块的支撑构件组， 该第四翼板至该第三 翼板的该第二翼部的垂直高度，大致等于该第二翼板至该第三翼板的该第一翼 部的垂直高度。
18. 如权利要求 9所述的太阳能模块的支撑构件组， 该连接构件包含一第 三部件， 该框架构件具有一贯穿孔于其中， 该支柱具有一固定孔于其中， 该第 三部件穿过该框架构件的该贯穿孔， 而伸入该支柱的该固定孔中，借此连结并 固定该框架构件与该支柱。
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