WO2014161107A1 - 太阳能模块的支架与应用其的太阳能系统 - Google Patents

太阳能模块的支架与应用其的太阳能系统 Download PDF

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Publication number
WO2014161107A1
WO2014161107A1 PCT/CN2013/000404 CN2013000404W WO2014161107A1 WO 2014161107 A1 WO2014161107 A1 WO 2014161107A1 CN 2013000404 W CN2013000404 W CN 2013000404W WO 2014161107 A1 WO2014161107 A1 WO 2014161107A1
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WO
WIPO (PCT)
Prior art keywords
carrier
frame
solar
fixing member
support
Prior art date
Application number
PCT/CN2013/000404
Other languages
English (en)
French (fr)
Inventor
邱丝绣
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
Publication of WO2014161107A1 publication Critical patent/WO2014161107A1/zh

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Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S20/00—Supporting structures for PV modules
    • H02S20/20—Supporting structures directly fixed to an immovable object
    • H02S20/22—Supporting structures directly fixed to an immovable object specially adapted for buildings
    • H02S20/23—Supporting structures directly fixed to an immovable object specially adapted for buildings specially adapted for roof structures
    • 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
    • F24S25/20—Peripheral frames for modules
    • 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
    • F24S25/61—Fixation means, e.g. fasteners, specially adapted for supporting solar heat collector modules for fixing to the ground or to building structures
    • 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
    • F24S25/67—Fixation means, e.g. fasteners, specially adapted for supporting solar heat collector modules for coupling adjacent modules or their peripheral frames
    • 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
    • F24S2025/6006—Fixation means, e.g. fasteners, specially adapted for supporting solar heat collector modules by using threaded elements, e.g. stud bolts
    • 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
    • Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
    • Y02B10/00—Integration of renewable energy sources in buildings
    • Y02B10/10—Photovoltaic [PV]
    • 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 solar energy system, and more particularly to a support for a solar module. Background technique
  • an embodiment of the present invention provides a bracket for a solar module for supporting at least one solar module, the solar module having a frame.
  • the support of the solar module comprises a fixing member, a carrier and a locking member.
  • the fixture includes a top portion and an extension connected to and perpendicular to the sides of the top portion, and a central portion of the top portion has a recessed portion.
  • the carrier includes a bearing portion for supporting the frame thereon, and has a plurality of first perforations, wherein the extension portion is for passing through the second perforation and the first perforation of the frame, and the frame is clamped to the fixing member and Between the carriers.
  • the locking element locks the fixing member to the carrier.
  • the recessed portion of the fixing member has a first opening
  • the carrier has a second opening for the locking member to pass through the first opening and the second opening to lock the fixing member and the carrier .
  • the top of the fixing member has two bearing portions on both sides of the recessed portion for clamping the frame between the bearing portion of the fixing member and the bearing portion of the carrier.
  • the first through hole and the second through hole may be oblong holes.
  • the number of extensions may be two, and the number of first perforations of the carrier is two, for fixing the frames of the two sets of solar modules.
  • each of the extensions may be four, and the number of first perforations of the carrier is four, for fixing the frame of the four sets of solar modules.
  • each of the extensions of the solar module further includes a plurality of bumps disposed at the ends of the extensions.
  • the carrier further includes a limiting portion standing upright on a side of the bearing portion and a plurality of protrusions disposed on the bearing portion.
  • the bracket of the solar module further includes a support frame, wherein the support frame includes a base, a joint portion, and a triangular connection portion connecting the base and the joint portion, wherein the bearer portion is fixed by the lock member combination.
  • the support frame further includes support ribs disposed on the triangular connection portion and parallel to the base.
  • the support frame further includes reinforcing ribs, and the reinforcing ribs are disposed on the triangular connecting portion, wherein the angle between the reinforcing ribs and the base is between 30 degrees and 65 degrees.
  • the solar module contains a solar panel and a frame.
  • the frame is used to secure the solar panel therein.
  • the frame includes a holding portion, a protruding portion, and a connecting portion for holding the solar panel.
  • the protrusion is located outside the frame relative to the solar panel and has a plurality of first perforations.
  • the connecting portion connects the holding portion and the protruding portion.
  • the fixture includes a top portion and an extension connected to and perpendicular to the sides of the top portion, and a central portion of the top portion has a recessed portion.
  • the carrier includes a bearing portion for supporting the frame thereon, and has a plurality of second through holes, wherein the extending portion is configured to pass through the first through hole and the second through hole, and the frame is sandwiched between the fixing member and the carrier between.
  • the locking element locks the fixing member to the carrier.
  • the recessed portion of the fixing member has a first opening
  • the carrier has a second opening for the locking member to pass through the first opening and the second opening to lock the fixing member and the carrier .
  • the top of the fixing member has two bearing portions on both sides of the recessed portion for clamping the frame between the bearing portion of the fixing member and the bearing portion of the carrier.
  • the first perforation is an oblong hole.
  • the number of extensions may be two, and the number of second perforations of the carrier is two, for fixing the frames of the two sets of solar modules.
  • the number of extensions may be four, and the number of second perforations of the carrier is four for securing the frame of the four sets of solar modules.
  • each of the extensions of the solar module includes a plurality of bumps disposed at the ends of the extensions.
  • the carrier further includes a limiting portion standing upright on a side of the bearing portion and a plurality of The bump is disposed on the bearing portion.
  • the bracket of the solar module further includes a support frame, wherein the support frame includes a base, a joint portion, and a triangular connection portion connecting the base and the joint portion, wherein the bearer portion is fixed by the lock member combination.
  • the support frame further includes support ribs disposed on the triangular connection portion and parallel to the base.
  • the support frame further includes reinforcing ribs, and the reinforcing ribs are disposed on the triangular connecting portion, wherein the angle between the reinforcing ribs and the base is between 30 degrees and 65 degrees.
  • the bracket of the solar module provided by the invention is used to simplify the assembly process of the solar system, thereby improving the assembly efficiency of the solar module.
  • FIG. 1A and 1B are respectively a partial perspective view and an exploded view of an assembly of a solar module of the present invention
  • Figure 2 is a cross-sectional view of the frame of Figure 1B;
  • FIG 3 is a perspective view of the fixing member of Figure 1B;
  • Figure 4 is a perspective view of the carrier of Figure 1B;
  • FIG. 5 is a partial cross-sectional view showing the assembled embodiment of the solar module of the present invention.
  • 6A and 6B are respectively a partial perspective view and an exploded view of another embodiment of the bracket of the solar module of the present invention.
  • 7A and 7B are a partial plan view and a partial bottom view, respectively, showing another embodiment of the bracket of the solar module of the present invention.
  • Figure 8 is a perspective view of the fixing member of Figure 7A;
  • Figure 9 is a perspective view of the carrier of Figure 7A;
  • 10A and 10B are a partial plan view and a partial bottom view, respectively, showing still another embodiment of the bracket of the solar module of the present invention.
  • Depression section 161 Support rib
  • first opening 200 solar panel
  • A-A, B-B line segment
  • Solar system 100 includes a solar module and a bracket to support the solar module.
  • the solar module includes a solar panel and a frame 110.
  • the bracket of the solar module includes a fixture 120, a carrier 130, and a locking component 140.
  • the frame 110 includes a grip portion 112 for holding the solar panel, a projection portion 114, and a joint portion 116 connecting the grip portion 112 and the projection portion 114.
  • the projection 114 extends outwardly from the lower edge of the connecting portion 116, and at least one end of the projection 114 has a first through hole 118.
  • the fixture 120 includes a top portion 122 and an extension 124 that is coupled and perpendicular to the sides of the top portion 122.
  • the two extending portions 124 can respectively pass through the two first through holes 118 of the adjacent two protrusions 114 of the two frames 110 to connect and fix the plurality of frames 110 through the fixing member 120.
  • the two frames 110 each have a protrusion 114, and one end of the protrusion 114 is provided
  • the first through hole 118 when the two frames 110 are close, the two first through holes 118 are also adjacent to each other.
  • the extension 124 of the fixture 120 can pass through the adjacent two first perforations 118 such that the fixture 120 connects the two frames 110 as a bridge structure.
  • the carrier 130 has a second through hole 132 corresponding to the first through hole 118.
  • the extending portion 124 of the fixing member 120 further passes through the second through hole 132, so that the protruding portion 114 is held between the fixing member 120 and the carrier 130, that is, The upper surface of the protrusion 114 abuts against the lower surface of the fixture 120, and the lower surface of the protrusion 114 abuts the upper surface of the carrier 130.
  • the first through hole 118 and the second through hole 132 may be oblong holes.
  • the aforementioned circular hole may be a rectangular opening and formed by forming a round chamfer at a corner thereof.
  • the top portion 122 of the fixture 120 has a first opening 126 and the carrier member 130 includes a second opening 134 corresponding to the first opening 126.
  • the adjacent two frames 110 are not in direct contact with each other to maintain a certain interval g, and the positions of the first opening 126 and the second opening 134 are overlapped at the interval ⁇
  • the locking element 140 includes a stud 142 and a nut 144.
  • the studs 142 are used to pass through the first opening 126 and the second opening 134, and the nut 144 is used to be locked to the stud 142 to fix the stud 142, the fixing member 120, and the carrier 130. More specifically, after the stud 142 passes through the first opening 126 and the second opening 134, the nut 144 is screwed from the two ends of the stud 142 to the two nuts 144 respectively against the fixing member 120 and the carrier 130.
  • the fixing member 120 and the carrier 130 are fixed between the two nuts 144, and the protruding portion 114 of the frame 110 is sandwiched between the fixing member 120 and the carrier 130.
  • the foregoing locking element 140 can be used to lock the fixing member 120 and the bearing member 130.
  • the stud 142 can also be locked in a metal roof, an asphalt roof, etc.
  • the roof structure allows the solar system 100 to be directly attached to the roof.
  • Fig. 2 is a cross-sectional view of the frame 110 of Fig. 1B taken along line A-A.
  • the frame 110 includes a holding portion 112 for holding the solar panel 200, a protruding portion 114, and a connecting portion 116 connecting the holding portion 112 and the protruding portion 114.
  • the gripping portion 112 is located at the upper edge of the connecting portion 116 and has an opening toward the inside of the frame 110 for holding the solar panel 200, and the protruding portion 114 extends outward from the lower edge of the connecting portion 116. After assembly, the solar panel 200 and the projections 114 extend toward opposite sides of the connecting portion 116, respectively.
  • the material of the frame 110 may be a metal, preferably a light weight aluminum.
  • the distance d between the first through hole 118 (see FIG. 1B) and the edge of the protruding portion 114 ranges from 10 mm to 20 mm. Wherein the distance between the first perforation 118 and the end edge of the protrusion 114 is greater than 10 mm to ensure that the first perforation 118 is not too close to the edge of the frame 110, and the fixing member 120 is prevented from fixing the support frame 110 after a period of time due to too little material, first The possibility of deformation of the perforations 118. And because the fixing member 120 passes through the first through hole 118, it will be solid at the same time. When two adjacent frames 110 are defined, when the distance d between the first end 118 and the edge of the protrusion 114 or the edge of the frame 110 is less than 20 mm, the material of the fixing member 120 can be saved, and the material cost can be reduced.
  • FIG. 3 is a perspective view of the fixing member 120 of FIG. 1B.
  • the fixture 120 includes a top portion 122 and an extension 124 that is joined and perpendicular to the sides of the top portion 122.
  • the number of extensions 124 is two.
  • the top portion 122 of the fixing member 120 includes a recessed portion 121 and a bearing portion 128.
  • the bearing portion 128 is connected to both sides of the recessed portion 121, and the recessed portion 121 is recessed relative to the bearing portion 128.
  • the first opening 126 is disposed in the recessed portion 121. .
  • the recessed section 121 has two inclined portions 123 and a lowering portion 125, and the two inclined portions 123 are connected to the descending portion 125 and the two bearing portions 128, respectively.
  • the position of the descending portion 125 can shorten the distance between the fixing member 120 and the carrier member 130.
  • the design of the fixing member 120 and the stud 142 is fixed and fixed when the bearing member 130, the frame 110, and the fixing member 120 are coupled by the locking member 140 to reduce the distance between the supporting member 130 and the fixing member 120.
  • the lower end of the lower portion 125 is in contact with the adjacent frame 110 to generate a reverse force to reduce the influence of the pressing force generated when the stud 142 is fixed on the fixing member 120.
  • the height difference h between the bearing section 128 and the descending portion 125 is 5 mm to 10 mm. If the height difference h is lower than this range, the function of lowering the height cannot be achieved because the step difference is too small. If the height difference h is larger than this range, an excessive step is generated to increase the possibility of deformation of the fixing member 120.
  • the width w1 of the inclined portion 123 is about 5 mm to 10 mm. If the width w1 of the inclined portion 123 is smaller than this range, the inclined portion 123 is excessively inclined, and there is a possibility that stress concentration may occur in the inclined portion 123. If the width w1 of the inclined portion 123 is larger than this range, material is wasted and increased and adjacent The distance between the frames 110.
  • the width w2 of the descending portion 125 is about 25 mm to 35 mm.
  • the width w2 of the descending portion 125 must at least allow the stud 142 to pass through.
  • the width w2 of the lower portion 125 need not be too wide to save material and reduce the distance between adjacent frames 110.
  • the interval g in Fig. 1A is approximately 2wl+w2.
  • the fixing member 120 further includes a plurality of bumps 150 disposed on the outer surface of the extending portion 124.
  • the bumps 150 may be a plurality of V-shaped ribs as shown in this embodiment, or any other shape of bumps.
  • the function of the bump 150 is to rub the surface of the frame 110 by the bump 150 when the extending portion 124 passes through the first through hole 118 of the frame 110 to break the anodized layer (: insulating layer:) on the surface of the frame 110 to reach the ground. efficacy.
  • the bumps 150 can also make the bond between the fixing member 120 and the frame 110 more stable.
  • FIG. 4 is a perspective view of the carrier 130 of FIG. 1B.
  • the carrier 130 includes a bearing portion 136 and a limiting portion 138 standing upright on the bearing portion 136.
  • the limiting portion 138 is erected One end of the bearing portion 136 is such that the side cross section of the carrier 130 has an approximately L-shaped configuration.
  • Both the second through hole 132 and the second opening 134 are located on the bearing portion 136.
  • the abutment portion 136 serves to provide a supporting force for the support frame 110 after the assembly is completed.
  • the limiting portion 138 can be used to position the frame 110.
  • the carrier 130 more selectively includes a plurality of bumps 150.
  • the bump 150 may be disposed on the bearing portion 136.
  • the bump 150 on the carrier 130 can rub the surface of the frame 110 to break the anodized layer (: insulating layer:) on the surface of the frame 110 to reach the ground. efficacy.
  • the bumps 150 can also provide additional friction so that the bond between the frame 110 and the carrier 130 is more stable.
  • FIG. 5 a partial cross-sectional view along line B-B of an embodiment of the solar energy system of FIG. 1A is shown.
  • the edges of the projections 114 of the adjacent two frames are held between the fixture 120 and the carrier 130.
  • the locking member 140 locks the fixing member 120 and the carrier member 130 to further fix the protruding portion 114 interposed therebetween.
  • the distance between the bearing portion 128 of the fixing member 120 and the carrier member 130 is about the thickness of the protruding portion 114 of the frame, but is not limited, and the spacing thereof may be slightly smaller than the thickness of the protruding portion 114.
  • the length of the extending portion 124 of the fixing member 120 is preferably greater than the thickness of the protruding portion 114 and the thickness of the carrier member 130, so that the extending portion 124 protrudes from the carrier member 130 to effectively position the fixing member 120 and the carrier member 130.
  • FIG. 6A and 6B there are shown a partial perspective view and an exploded view, respectively, of another embodiment of the solar energy system of the present invention.
  • the solar system 100 further includes a support frame 160 in addition to the fixing member 120 for fixing the frame 110, the carrier member 130, and the locking member 140.
  • the solar system 100 having the support frame 160 can be applied to a roof having an inclined angle.
  • the support frame 160 includes a base 162, a joint portion 164, and a triangular joint portion 166 that connects the base 162 and the joint portion 164.
  • the joint portion 164 has a third opening 168 therein, and the locking member 140 further passes through the third opening 168 to fix the bearing portion 136 of the carrier 130 to the joint portion 164.
  • the base 162 and the joint portion 164 are located on the same side of the triangular connecting portion 166, respectively connected to the two vertices of the triangular connecting portion 166 and disposed approximately parallel, wherein the base 162 is substantially parallel and connected to the bottom edge of the triangular connecting portion 166.
  • the triangular connecting portion 166 can strengthen the pulling force between the base 162 and the joint portion 164 and strengthen the structural strength of the support frame 160. In addition, the triangular connecting portion 166 can disperse the stress when the solar module is depressed by the larger base portion. , to prevent the support base 160 from being deformed by external force.
  • the support frame 160 further includes a support rib 161 disposed in the triangular connection portion 166, and the support rib 161 is parallel to the base 162.
  • the support rib 161 can be used to reinforce the structural strength of the triangular joint 166. This prevents the triangular joint 166 from being deformed by the gravity of the solar panel.
  • the position of the support rib 161 is a position to receive a large force, and therefore, the thickness of the support rib 161 may be slightly larger than the thickness of other portions in the support base 160 to strengthen the supporting force of the support rib 161.
  • the support frame 160 further includes a reinforcing rib 163.
  • the reinforcing rib 163 is disposed in the triangular connecting portion 166.
  • the angle ⁇ between the reinforcing rib 163 and the pedestal 162 is between 30 degrees and 65 degrees.
  • the support frame 160 is applied to the installation of the inclined roof, that is, after the solar system 100 is installed, the bracket will be parallel to the roof but inclined to the surface, and the downforce of the solar panel will be approximately the same as the reinforcing rib 163. Parallel (depending on the angle of inclination of the roof and the angle ⁇ between the reinforcing rib 163 and the base 162).
  • the function of the reinforcing ribs 163 is to support the downward pressure of the solar panel to ensure that the support frame 160 is not deformed by gravity.
  • a screw hole 165 may be further disposed on the base 162 of the support frame 160.
  • the solar system 100 may further include another locking component 140' for passing through the screw hole 165 of the base 162, and then locking the support frame 160 to a fixture such as a cement block or a roof.
  • the foregoing solar energy system 100 fixes the frame 110 in groups of two, but if the design of the fixing member 120 and the carrier 130 is changed, the frame 110 can also be fixed by four groups to further save material cost.
  • the details are as follows.
  • FIGS 7A and 7B there are shown a partial top view and a partial bottom view, respectively, of another embodiment of a solar energy system in accordance with the present invention. It should be noted that the bracket in the solar system 100' is used to fix the four frames 110, but two of the frames 110 are hidden in a plan view to show the features of the embodiment.
  • the fixing member 120' in the embodiment includes four extending portions 124
  • the carrier member 130' also includes four second through holes 132.
  • the extending portion 124 of the fixing member 120' passes through the first through hole (not shown) on the frame 110 and the second through hole 132 on the carrier 130', and the extending portion 124 protrudes from The second perforation 132 is effective to position the fixture 120' and the carrier 130'.
  • the locking element 140 then passes through the first opening 126 of the fixing member 120 ′ and the second opening 134 of the carrier 130 ′ to fix the two, and the protruding portion 114 of the frame 110 is sandwiched between the fixing member 120 ′ and the carrier 130 . 'between.
  • the fixture 120' includes a top portion 122 and an extension 124 disposed on either side of the top portion 122 and perpendicular to the top portion 122, wherein the number of extension portions 124 is four.
  • the top portion 122 includes a bearing portion 128 and a recessed portion 121, and the first opening 126 is located at the center of the recessed portion 121.
  • a bump 150 is more selectively disposed on the extending portion 124.
  • the carrier 130' includes four second through holes 132 and a second opening 134, wherein the second opening 134 is located on the carrier 130' Slightly at the center.
  • the carrier 130' includes a bearing portion 136.
  • a bump 150 may be selectively disposed on the bearing portion 136.
  • FIG. 10A and 10B there are shown a partial top view and a partial bottom view, respectively, of yet another embodiment of the solar energy system of the present invention.
  • the solar system 100' further includes a support frame 160, and the locking member 140 is fixed to the support frame 160 after passing through the fixing member 120' and the carrier member 130'.
  • the bracket of the solar module provided by the invention is used to simplify the assembly process of the solar system, thereby improving the assembly efficiency of the solar module.

Abstract

提供一种太阳能模块的支架与应用其的太阳能系统，用以支持至少一太阳能模块。太阳能模块（100）具有框架（110）。太阳能模块（100）的支架包含有固定件（120）、承载件（130）以及锁固元件（140）。固定件（120）包含顶部（122）以及连接并垂直于顶部（122）两侧的延伸部（124），且顶部（122）的中央具有一凹陷段（121）。承载件（130）包含一承靠部（136）用以使框架（110）承靠于其上，具有多个第一穿孔（118），延伸部（124）用于穿过支架（110）的第二穿孔（132）与第一穿孔（118），而使框架（110）夹设于该固定件（120）与承载件（130）之间。锁固元件（140）用于锁固固定件于承载件（130）。

Description

太阳能模块的支架与应用其的太阳能系统 技术领域
本发明是有关于一种太阳能系统， 特别是有关于一种太阳能模块的支架。 背景技术
近几年来， 由于世界各地的原油存量逐年的减少， 能源问题已成为全球注 目的焦点。为了解决能源耗竭的危机， 各种替代能源的发展与利用实为当务之 急。 随着环保意识抬头， 加上太阳能具有零污染、 以及取之不尽用之不竭的优 点， 太阳能已成为相关领域中最受瞩目的焦点。 因此， 在日照充足的位置， 例 如建筑物屋顶、 广场等等， 愈来愈常见到太阳能面板的装设。
太阳能模块多需要搭接在支架上， 以固定于建筑物屋顶， 而如何简化太阳 能模块的架设时所需要的工具以及歩骤，便成为提升太阳能模块组装效率的重 要因素。 发明公开
为了解决公知技术中的问题，本发明的一实施例提供了一种太阳能模块的 支架， 用于支持至少一太阳能模块， 太阳能模块具有一框架。太阳能模块的支 架包含有固定件、承载件以及锁固元件。固定件包含顶部以及连接并垂直于顶 部两侧的延伸部， 且顶部的中央具有一凹陷段。承载件包含一承靠部用以使框 架承靠于其上， 具有多个第一穿孔， 其中延伸部用于穿过框架的第二穿孔与第 一穿孔，而使框架夹设于固定件与承载件之间。锁固元件锁固固定件于承载件。
于一或多个实施例中， 固定件的凹陷段具有第一开口， 承载件具有第二开 口， 用以使锁固元件穿设于第一开口与第二开口而锁固固定件与承载件。
于一或多个实施例中， 固定件的顶部另具有两承靠段位于凹陷段的两侧， 用于使框架夹设于固定件的承靠段与承载件的承靠部之间。
于一或多个实施例中， 第一穿孔与第二穿孔可以为长圆孔。
于一或多个实施例中， 延伸部的数量可以为二， 且承载件的第一穿孔数量 为二， 用于固定两组太阳能模块的框架。
于一或多个实施例中， 延伸部的数量可以为四， 且承载件的第一穿孔数量 为四， 用于固定四组太阳能模块的框架。 于一或多个实施例中，太阳能模块的支架每一延伸部更包含多个凸块， 设 置于延伸部的端部。
于一或多个实施例中，承载件另包含直立于承靠部侧边的限位部以及多个 凸块设置于承靠部。
于一或多个实施例中，太阳能模块的支架更包含支撑架， 其中支撑架包含 基座、 结合部、 以及连接基座与结合部的三角形连接部， 其中承靠部通过锁固 元件固定于结合部。
于一或多个实施例中，支撑架更包含支撑肋，支撑肋设置于三角形连接部， 并平行于基座。
于一或多个实施例中，支撑架更包含补强肋，补强肋设置于三角形连接部， 其中补强肋与基座之间的夹角介于 30度至 65度之间。
本发明的另一实施例为一种太阳能系统， 包含太阳能模块、 固定件、 承载 件以及锁固元件。太阳能模块包含太阳能面板与一框架。框架用以固定太阳能 面板于其中。其中框架包含用以挟持太阳能面板的挟持部、 突出部， 以及连接 部。突出部位于框架相对于太阳能面板的外侧， 且具有多个第一穿孔。连接部 连接挟持部与突出部。 固定件包含顶部以及连接并垂直于顶部两侧的延伸部， 且顶部的中央具有一凹陷段。承载件包含一承靠部用以使框架承靠于其上， 具 有多个第二穿孔， 其中延伸部用于穿过第一穿孔与第二穿孔， 而使框架夹设于 固定件与承载件之间。 锁固元件锁固固定件于承载件。
于一或多个实施例中， 固定件的凹陷段具有第一开口， 承载件具有第二开 口， 用以使锁固元件穿设于第一开口与第二开口而锁固固定件与承载件。
于一或多个实施例中， 固定件的顶部另具有两承靠段位于凹陷段的两侧， 用于使框架夹设于固定件的承靠段与承载件的承靠部之间。
于一或多个实施例中， 第一穿孔为长圆孔。
于一或多个实施例中， 延伸部的数量可以为二， 且承载件的第二穿孔数量 为二， 用于固定两组太阳能模块的框架。
于一或多个实施例中， 延伸部的数量可以为四， 且承载件的第二穿孔数量 为四， 用于固定四组太阳能模块的框架。
于一或多个实施例中，太阳能模块的支架每一延伸部更包含多个凸块， 设 置于延伸部的端部。
于一或多个实施例中，承载件另包含直立于承靠部侧边的限位部以及多个 凸块设置于承靠部。
于一或多个实施例中，太阳能模块的支架更包含支撑架， 其中支撑架包含 基座、 结合部、 以及连接基座与结合部的三角形连接部， 其中承靠部通过锁固 元件固定于结合部。
于一或多个实施例中，支撑架更包含支撑肋，支撑肋设置于三角形连接部， 并平行于基座。
于一或多个实施例中，支撑架更包含补强肋，补强肋设置于三角形连接部， 其中补强肋与基座之间的夹角介于 30度至 65度之间。
使用本发明所提供的太阳能模块的支架， 用以简化太阳能系统的组装歩 骤， 从而提升太阳能模块组装效率。 附图简要说明
图 1A与图 1B分别绘示本发明的太阳能模块的支架一实施例组装完成的 局部立体视图以及爆炸图；
图 2绘示图 1B中的框架的剖面图；
图 3绘示图 1B中的固定件的立体视图；
图 4绘示图 1B中的承载件的立体视图；
图 5 绘示本发明的太阳能模块的支架一实施例组装完成的局部剖面示意 图；
图 6A与图 6B分别绘示本发明的太阳能模块的支架另一实施例的局部立 体视图与爆炸图；
图 7A与图 7B分别绘示本发明中的太阳能模块的支架另一实施例的局部 俯视图与局部仰视图；
图 8绘示图 7A中的固定件的立体视图；
图 9绘示图 7A中的承载件的立体视图；
图 10A与图 10B分别绘示本发明的太阳能模块的支架再一实施例的局部 俯视图与局部仰视图。
其中， 附图标记：
100、 100'： 太阳能系统 136: 承靠部
110： 框架 138: 限位部
112： 挟持部 140、 140'： 锁固元件 114： 突出部 142： 螺柱
116： 连接部 144： 螺帽
118： 第一穿孔 150： 凸块
120、 120'： 固定件 160： 支撑架
121： 凹陷段 161： 支撑肋
122： 顶部 162： 基座
123： 倾斜部 163： 补强肋
124： 延伸部 164： 结合部
125： 下降部 166： 三角形连接部
126： 第一开口 200： 太阳能面板
128： 承靠段 d: 间距
130、 130'： 承载件 g: 间隔
h: 高度差
wl、 w2: 宽度
A-A、 B-B: 线段 实现本发明的最佳方式
以下将以附图及详细说明清楚说明本发明的精神，任何本领域技术人员在 了解本发明的较佳实施例后， 当可由本发明所教示的技术， 加以改变及修饰， 其并不脱离本发明的精神与范围。
参照图 1A与图 IB, 其分别绘示本发明的太阳能系统一实施例组装完成的 局部立体视图以及爆炸图。 太阳能系统 100包含有太阳能模块以及用以支持太 阳能模块的支架。 太阳能模块包含有太阳能面板以及框架 110。 太阳能模块的 支架包含有固定件 120、 承载件 130， 以及锁固元件 140。框架 110包含有用以挟 持太阳能面板的挟持部 112， 突出部 114、 以及连接挟持部 112与突出部 114的连 接部 116。 突出部 114从连接部 116的下缘起向外延伸， 突出部 114的至少一端具 有第一穿孔 118。
固定件 120包含有顶部 122以及连接并垂直于顶部 122两侧的延伸部 124。两 延伸部 124可分别穿过两框架 110的相邻两突出部 114的两第一穿孔 118， 以透过 固定件 120连接并固定多个框架 110。
更具体地说， 两个框架 110分别具有突出部 114， 突出部 114的一端设置有 第一穿孔 118， 当两个框架 110靠近时， 两第一穿孔 118亦彼此相邻。 固定件 120 的延伸部 124可穿过相邻的两第一穿孔 118， 使得固定件 120作为跨桥结构而连 接两个框架 110。
承载件 130则具有对应于第一穿孔 118的第二穿孔 132，固定件 120的延伸部 124更穿过第二穿孔 132，使得突出部 114被挟持在固定件 120与承载件 130之间， 即突出部 114的上表面抵触固定件 120的下表面， 而突出部 114的下表面抵触承 载件 130的上表面。 第一穿孔 118与第二穿孔 132可以为长圆孔。 其中前述的长 圆孔可以为矩形开口， 并在其转角处形成圆形倒角制作而成。
固定件 120的顶部 122具有第一开口 126，承载件 130则包含有对应于第一开 口 126的第二开口 134。 相邻的两框架 110之间不直接接触而保持有一定的间隔 g， 第一开口 126与第二开口 134的位置便是重叠于此间隔^
锁固元件 140包含有螺柱 142以及螺帽 144。 螺柱 142用于穿过第一开口 126 与第二开口 134， 螺帽 144用来锁合于螺柱 142上， 以固定螺柱 142、 固定件 120 以及承载件 130。 更具体地说， 当螺柱 142穿过第一开口 126与第二开口 134后， 螺帽 144分别自螺柱 142的两端旋入至两螺帽 144分别抵触固定件 120与承载件 130， 以将固定件 120与承载件 130固定于两螺帽 144之间， 而框架 110的突出部 114则被夹设于固定件 120与承载件 130之间。
如此一来， 便可以实现快速且便利地组装太阳能系统 100的功效。
前述的锁固元件 140除了可以用于锁固固定件 120与承载件 130之外， 通过 增加螺柱 142的长度，亦可以将螺柱 142进一歩地锁固于如金属屋顶、沥青材质 屋顶等屋顶结构， 使得太阳能系统 100直接固定于屋顶上。
同时参照图 1B与图 2，其中图 2绘示图 1B中的框架 110沿线段 A-A的剖面图。 框架 110包含有用以挟持太阳能面板 200的挟持部 112， 突出部 114、 以及连接挟 持部 112与突出部 114的连接部 116。 挟持部 112位于连接部 116的上缘并具有向 框架 110内侧的开口用以挟持太阳能面板 200，而突出部 114从连接部 116的下缘 起向外延伸。 组装后， 太阳能面板 200与突出部 114分别朝向连接部 116的相对 两侧延伸。 框架 110的材料可以为金属， 较佳地为重量较轻的铝。
第一穿孔 118(见图 1B)与突出部 114端缘的间距 d范围为 10mm~20mm。其中 第一穿孔 118与突出部 114端缘之间距大于 10mm可确保第一穿孔 118不会太靠 近框架 110边缘， 而避免固定件 120固定支撑框架 110—段时间后发生因材料太 少， 第一穿孔 118变形的可能性。 又因固定件 120穿过第一穿孔 118后会同时固 定两个邻近的框架 110， 当第一穿孔 118与突出部 114端缘或框架 110边缘的间距 d小于 20mm则可以节省固定件 120的材料， 降低材料成本。
同时参照图 1B与图 3， 其中图 3绘示图 1B中的固定件 120的立体视图。 固定 件 120包含有顶部 122以及连接并垂直于顶部 122两侧的延伸部 124， 延伸部 124 的数量为二。固定件 120的顶部 122包含有凹陷段 121以及承靠段 128，承靠段 128 连接于凹陷段 121两侧， 且凹陷段 121相对于承靠段 128凹陷，第一开口 126设置 于凹陷段 121。更具体地说， 凹陷段 121有两倾斜部 123与一下降部 125， 两倾斜 部 123分别连接下降部 125以及两承靠段 128。
如此一来， 固定件 120结合框架 110与承载件 130后， 下降部 125的位置可缩 短固定件 120与承载件 130之间的间距。此种设计可以使得承载件 130、框架 110、 固定件 120通过锁固元件 140结合后， 减少因承载件 130与固定件 120间距较大， 而使固定件 120与螺柱 142在固定时与固定后承受较大的作用力而变形弯曲的 情形。下降部 125下侧两端与邻近框架 110碰触可产生反向作用力， 以减少螺柱 142固定时所产生的下压作用力对于固定件 120的影响。
承靠段 128与下降部 125之间的高度差 h为 5mm~10mm。若是高度差 h低于此 范围， 则会因为过小的段差无法达到降低高度的功能， 若是高度差 h大于此范 围， 则会产生过大的段差而增加固定件 120变形的可能性。 倾斜部 123的宽度 wl约为 5mm~10mm。 倾斜部 123的宽度 wl若是小于此范围， 则使倾斜部 123过 于倾斜而可能在倾斜部 123产生应力集中的可能性， 倾斜部 123的宽度 wl若是 大于此范围， 则会浪费材料并增加与邻近框架 110之间的距离。下降部 125的宽 度 w2约为 25mm~35mm。下降部 125的宽度 w2至少须可容许螺柱 142穿过。而下 降部 125的宽度 w2无需过宽则是为了节省材料并减少邻近两框架 110之间的距 离。 其中图 1A中之间隔 g大致为 2wl+w2。
固定件 120上更选择性地包含有多个凸块 150， 凸块 150设置于延伸部 124 的外表面。 凸块 150可以为如本实施例所示的多个 V形凸肋， 或是其他任意形 状的凸块。 凸块 150的作用在于当延伸部 124穿过框架 110的第一穿孔 118时， 通 过凸块 150摩擦框架 110表面， 以破坏框架 110表面的阳极处理层 (：绝缘层：)，而达 到接地的功效。 此外， 凸块 150亦可以使得固定件 120与框体 110之间的结合更 为稳固。
同时参照图 1B与图 4， 其中图 4绘示图 1B中的承载件 130的立体视图。 承载 件 130包含有承靠部 136以及直立于承靠部 136的限位部 138。 限位部 138直立于 承靠部 136的一端，使得承载件 130的侧剖面具有近似于 L形结构。第二穿孔 132 与第二开口 134均位于承靠部 136上。 承靠部 136用以在组装完成之后提供支撑 框架 110的支撑力。 限位部 138则可用以定位框架 110。
同样地， 承载件 130更可选择性地包含有多个凸块 150。 凸块 150可以设置 于承靠部 136上。 当框架 110固定于固定件 120与承载件 130之间时， 承载件 130 上的凸块 150可以摩擦框架 110表面， 以破坏框架 110表面的阳极处理层 (：绝缘 层：)， 而达到接地的功效。 此外， 凸块 150亦可以提供额外的摩擦力， 使得框体 110与承载件 130之间的结合更为稳固。
参照图 5， 其绘示图 1A的太阳能系统一实施例组装完成后沿 B-B线段的局 部剖面示意图。 相邻两框架的突出部 114边缘会被挟持在固定件 120与承载件 130之间。锁固元件 140锁固固定件 120与承载件 130， 以进一歩固定夹设于其间 的突出部 114。
固定件 120的承靠段 128与承载件 130之间的间距约为框架的突出部 114的 厚度， 但不限定， 其间距亦可略小于突出部 114的厚度。 而固定件 120的延伸部 124的长度较佳为大于突出部 114与承载件 130的厚度总合，使得延伸部 124凸出 于承载件 130， 以有效地定位固定件 120与承载件 130。
参照图 6A与图 6B , 其分别绘示本发明的太阳能系统另一实施例的局部立 体视图与爆炸图。 本实施例与前一实施例的差别在于， 太阳能系统 100除了前 述的用以固定框架 110的固定件 120、承载件 130以及锁固元件 140之外， 更包含 有支撑架 160。
具有支撑架 160的太阳能系统 100可以适用于具有倾斜角度的屋顶。支撑架 160包含有基座 162、 结合部 164以及连接基座 162与结合部 164的三角形连接部 166。 其中结合部 164上具有第三开口 168， 锁固元件 140更穿过第三开口 168以 将承载件 130的承靠部 136固定于结合部 164上。 基座 162与结合部 164位于三角 形连接部 166的同一侧，分别连接于三角形连接部 166的两个顶点且约略平行设 置， 其中基座 162与三角形连接部 166的底边实质平行且连接。
三角形连接部 166可以加强基座 162与结合部 164之间的牵制力并强化支撑 架 160的结构强度， 除此之外， 三角形连接部 166通过较大的基部可以分散太阳 能模块下压时的应力， 避免支撑座 160因外力挤压而变形。
支撑架 160更包含有支撑肋 161， 支撑肋 161设置于三角形连接部 166内， 支 撑肋 161平行于基座 162。 支撑肋 161可用以强化三角形连接部 166的结构强度， 以避免三角形连接部 166因为太阳能面板的重力挤压而变形。支撑肋 161的位置 为承受较大作用力的位置， 因此， 支撑肋 161的厚度可以略大于支撑座 160内其 他部分的厚度， 以强化支撑肋 161的支撑力。
支撑架 160更包含有补强肋 163。补强肋 163设置于三角形连接部 166内。其 中补强肋 163与基座 162之间的夹角 Θ介于 30度至 65度之间。如前所述， 支撑架 160应用于斜屋顶的安装， 亦即当太阳能系统 100安装完成之后， 支架会平行于 屋顶但是倾斜于地表，此时太阳能面板的下压力将会约略与补强肋 163平行 (视 屋顶的倾斜角度以及补强肋 163与基座 162之间的夹角 Θ而定)。补强肋 163的作 用便是在于支撑太阳能面板的下压力，以确保支撑架 160不因重力挤压而变形。
支撑架 160的基座 162上可更设置有螺丝孔 165。太阳能系统 100更可包含有 另一锁固元件 140'， 用以穿过基座 162的螺丝孔 165之后， 再将支撑架 160锁固 于如水泥块或屋顶等固定物上。
前述的太阳能系统 100为将框架 110两两一组的进行固定，但是若是经由改 变固定件 120与承载件 130的设计， 框架 110亦可以被四个一组的固定， 以进一 歩节省材料成本， 详细说明如以下实施例。
参照图 7A与图 7B , 其分别绘示本发明中的太阳能系统另一实施例的局部 俯视图与局部仰视图。 需说明的是， 本太阳能系统 100'中的支架用以固定四个 框架 110，但是于俯视图中其中两个框架 110予以隐藏，以表现本实施例的特征。
本实施例与前述实施例的差别在于， 本实施例中的固定件 120'包含有四个 延伸部 124， 而承载件 130'上亦包含有四个第二穿孔 132。 待框架 110就定位之 后， 固定件 120'的延伸部 124分别穿过框架 110上的第一穿孔 (图中未绘示)以及 承载件 130'上的第二穿孔 132， 延伸部 124并突出于第二穿孔 132以有效定位固 定件 120'以及承载件 130'。 锁固元件 140再穿过固定件 120'的第一开口 126与承 载件 130'的第二开口 134以固定两者， 并使框架 110的突出部 114夹设于固定件 120'与承载件 130'之间。
参照图 8， 其绘示图 7A中的固定件 120'的立体视图。 固定件 120'包含有顶 部 122以及设置于顶部 122两侧并垂直于顶部 122的延伸部 124， 其中延伸部 124 的数量为四。顶部 122包含有承靠段 128以及凹陷段 121， 第一开口 126位于凹陷 段 121的中央。 延伸部 124上更可选择性地设置有凸块 150。
参照图 9， 其绘示图 7A中的承载件 130'的立体视图。 承载件 130'上包含有 四个第二穿孔 132与一个第二开口 134， 其中第二开口 134位于承载件 130'的约 略中央处。 承载件 130'包含有承靠部 136。 承靠部 136上可以选择性地设置有凸 块 150。
再参照图 10A与图 10B , 其分别绘示本发明的太阳能系统再一实施例的局 部俯视图与局部仰视图。 本实施例与前一实施例的差别在于， 太阳能系统 100' 更包含有支撑架 160， 锁固元件 140穿过固定件 120'与承载件 130'之后固定于支 撑架 160上。
虽然本发明已以实施例揭露如上， 然其并非用以限定本发明， 任何本领域 技术人员， 在不脱离本发明的精神和范围内， 当可作各种的更动与润饰， 因此 本发明的保护范围当以权利要求书为准。 工业应用性
使用本发明所提供的太阳能模块的支架， 用以简化太阳能系统的组装歩 骤， 从而提升太阳能模块组装效率。

Claims

权 利 要 求 书
1.一种太阳能模块的支架， 其特征在于， 用于支持至少一太阳能模块， 该 太阳能模块具有一框架， 该支架包含：
一固定件， 包含一顶部以及连接并垂直于该顶部两侧的多个延伸部， 且该 顶部的中央具有一凹陷段；
一承载件， 包含一承靠部用以使该框架承靠于其上， 具有多个第一穿孔， 其中这些延伸部用于穿过该框架的多个第二穿孔与这些第一穿孔，而使该框架 夹设于该固定件与该承载件之间； 以及
一锁固元件， 用于锁固该固定件于该承载件。
2.如权利要求 1所述的太阳能模块的支架， 其特征在于， 该固定件的该凹 陷段具有一第一开口， 该承载件具有一第二开口， 用以使该锁固元件穿设于该 第一开口与该第二开口而锁固该固定件与该承载件。
3. 如权利要求 1所述的太阳能模块的支架， 其特征在于， 该固定件的该顶 部另具有两承靠段位于该凹陷段的两侧，用于使该框架夹设于该固定件的该承 靠段与该承载件的该承靠部之间。
4. 如权利要求 1所述的太阳能模块的支架， 其特征在于， 这些第一穿孔为 长圆孔。
5. 如权利要求 1所述的太阳能模块的支架， 其特征在于， 这些延伸部的数 量为两个， 且该承载件的这些第一穿孔数量为两个，用于固定两组太阳能模块 的框架。
6. 如权利要求 1所述的太阳能模块的支架， 其特征在于， 这些延伸部的数 量为四个， 且该承载件的这些第一穿孔数量为四个，用于固定四组太阳能模块 的框架。
7. 如权利要求 1所述的太阳能模块的支架， 其特征在于， 每一这些延伸部 更包含多个凸块， 设置于这些延伸部的端部。
8. 如权利要求 1所述的太阳能模块的支架， 其特征在于， 该承载件另包含 直立于该承靠部侧边的一限位部以及多个凸块设置于该承靠部。
9. 如权利要求 1所述的太阳能模块的支架，其特征在于，还包含一支撑架， 其中该支撑架包含一基座、一结合部、 以及连接该基座与该结合部的一个三角 形连接部， 其中该承靠部通过该锁固元件固定于该结合部。
10. 如权利要求 9所述的太阳能模块的支架， 其特征在于， 该支撑架更包 含一支撑肋， 设置于该三角形连接部内， 并平行于该基座。
11. 如权利要求 9所述的太阳能模块的支架， 其特征在于， 该支撑架更包 含一补强肋， 设置于该三角形连接部内， 其中该补强肋与该基座之间的夹角介 于 30度至 65度之间。
12. 一种太阳能系统， 其特征在于， 包含：
至少一太阳能模块，包含一太阳能面板与一框架， 该框架用以固定该太阳 能面板于其中， 其中该框架包含：
一挟持部， 用以挟持该太阳能面板；
一突出部， 位于该框架相对于该太阳能板的外侧， 且具有多个第一穿孔； 以及
一连接部， 连接该挟持部与该突出部；
一固定件， 包含一顶部以及连接并垂直于该顶部两侧的多个延伸部， 且该 顶部的中央具有一凹陷段；
一承载件， 包含一承靠部用以使该框架承靠于其上， 具有对应于这些第一 穿孔的多个第二穿孔， 其中这些延伸部分别用于穿过该第一穿孔与该第二穿 孔， 而使该突出部夹设于该固定件与该承载件之间； 以及
一锁固元件， 用于锁固该固定件于该承载件。
13.如权利要求 12所述的太阳能系统， 其特征在于， 该固定件的该凹陷段 具有一第一开口， 该承载件具有一第二开口，用以使该锁固元件穿设于该第一 开口与该第二开口而锁固该固定件与该承载件。
14. 如权利要求 12所述的太阳能系统， 其特征在于， 该固定件的该顶部另 具有两承靠段位于该凹陷段的两侧，用于使该框架的该突出部夹设于该固定件 的该承靠段与该承载件的该承靠部之间。
15. 如权利要求 12所述的太阳能系统， 其特征在于， 这些第一穿孔与这些 第二穿孔为长圆孔， 这些延伸部的延伸长度大于该突出部的厚度。
16. 如权利要求 12所述的太阳能系统， 其特征在于， 这些延伸部的数量为 两个， 且该承载件的这些第二穿孔数量为两个，用于固定两组太阳能模块的框 架。
17. 如权利要求 12所述的太阳能系统， 其特征在于， 这些框架与这些延伸 部的数量为四个， 且该承载件的这些第二穿孔数量为四个，用于固定四组太阳 能模块的框架。
18. 如权利要求 12所述的太阳能系统， 其特征在于， 还包含一支撑架， 其 中该支撑架包含一基座、一结合部、 以及连接该基座与该结合部的一个三角形 连接部， 其中该承靠部通过该锁固元件固定于该结合部。
19. 如权利要求 18所述的太阳能系统， 其特征在于， 该支撑架更包含一支 撑肋， 设置于该三角形连接部内， 并平行于该基座。
20. 如权利要求 18所述的太阳能系统， 其特征在于， 该支撑架更包含一补 强肋， 设置于该三角形连接部内， 其中该补强肋与该基座之间的夹角介于 30 度至 65度之间。
PCT/CN2013/000404 2013-04-01 2013-04-07 太阳能模块的支架与应用其的太阳能系统 WO2014161107A1 (zh)

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