CN206677503U - Solar energy wing plate linearity installation and debugging platform - Google Patents
Solar energy wing plate linearity installation and debugging platform Download PDFInfo
- Publication number
- CN206677503U CN206677503U CN201720430527.7U CN201720430527U CN206677503U CN 206677503 U CN206677503 U CN 206677503U CN 201720430527 U CN201720430527 U CN 201720430527U CN 206677503 U CN206677503 U CN 206677503U
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- wing plate
- installation
- solar energy
- platform body
- planer
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Abstract
The utility model belongs to solar energy optical-thermal support manufacture installing area, more particularly to a kind of solar energy wing plate linearity installation and debugging platform.Including platform body, spacing stopper and planer-type positioning tool；The spacing stopper can fix solar bracket crossbeam and installed in the both ends of platform body, the platform body is provided with graduation mark, the planer-type positioning tool can linear slide be arranged on platform body on, the glide direction of planer-type positioning tool is consistent with graduation mark direction.Can solve the problems, such as solar bracket crossbeam upper flange installation after overall linearity, improve be arranged on wing plate on radian eyeglass entirety focal point uniformity, so as to improve Heat-collecting effect.Dismount simple and convenient transport.
Description
Technical field
The utility model belongs to solar energy optical-thermal support manufacture installing area, more particularly to a kind of solar energy wing plate linearity
Installation and debugging platform.
Background technology
Solar energy heating support starts to apply in solar heat collection heating field at present, thermal-arrest support mainly by column,
Solar bracket crossbeam, radian reflex reflector lens and thermal-collecting tube are formed, and are interconnected with underground heat exchange system, realize heat exchange by water
After heating, into municipal heating pipe network, reach and meet resident's heating demand, existing solar energy heating support manufacture and technology are because of this
Body defective workmanship, linearity reduces after solar bracket crossbeam galvanizing, the wing plate integrated straight installed on solar bracket crossbeam
Dimension disunity, the radian reflective mirror entirety for causing to install on wing plate cause scattering not optically focused not in unified flatness, so as to
Failing fully to focus on causes thermal-collecting tube can not be warming up to design temperature, causes not realizing that hot water heating is asked using solar energy optical-thermal
Topic.
Utility model content
For in the prior art the defects of, the utility model provides a kind of solar energy wing plate linearity installation and debugging platform,
Can solve the problems, such as solar bracket crossbeam upper flange installation after overall linearity, improve be arranged on wing plate on radian eyeglass it is whole
Body focal point uniformity, so as to improve Heat-collecting effect.Dismount simple and convenient transport.
A kind of solar energy wing plate linearity installation and debugging platform provided by the utility model, including platform body, limiting block
Head and planer-type positioning tool；The spacing stopper can fix solar bracket crossbeam and be arranged on the both ends of platform body,
The platform body is provided with graduation mark, and line direction of the graduation mark along two spacing stoppers arranges that graduation mark can be measured
The distance between two adjacent vanes on solar bracket crossbeam, the planer-type positioning tool can linear slide be arranged on platform
On body, gantry positioning tool can slidably reciprocate along the line of the spacing stopper in both ends, the glide direction of planer-type positioning tool
Consistent with graduation mark direction, graduation mark can be used for calculating the displacement of planer-type positioning tool；Work is positioned by planer-type
Fill to the wing plate installed on solar bracket crossbeam positional punch one by one, it is ensured that on solar bracket crossbeam after whole wing plates installations
On the same line, planer-type positioning tool can ensure that no matter whether overall fixed hole position position is consistent on wing plate, can reach
After wing plate whole installation on the same line.
Further, the platform body is provided with chute, and the planer-type positioning tool lower end is provided with can be in chute
The sliding block of slip, planer-type positioning tool can in platform body along graduation mark linear slide, ensure that adjacent wing plate away from
From accuracy.
Further, the platform body is cuboid.
Further, the spacing stopper is two, and the distance of two spacing stoppers is less than the length of solar bracket crossbeam.
Further, two spacing stoppers are located at start position and the final position of graduation mark, start position respectively
Scale be zero.
Further, the positive stop is provided with to the spacing hole of fixed solar bracket crossbeam, solar bracket
The end of crossbeam is arranged in spacing hole.
Further, the spacing stopper is bolted on platform body.
The beneficial effects of the utility model are：Realized and be fixed on solar bracket crossbeam by planer-type positioning tool
All wing plates on the same line, for postorder cambered surface eyeglass installation after reflective intersection point provide guarantee on the same line.
The manufacturing process can not consider solar bracket crossbeam problem on deformation caused by galvanizing simultaneously, while be the big rule of standardization
Molding makes installation solar energy heating support and provides technical guarantee.Need to debug reflection angle problem one by one after thoroughly having prevented installation,
Human and material resources, financial resources are saved.
Brief description of the drawings
, below will be right in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
The required accompanying drawing used is briefly described in embodiment or description of the prior art.In all of the figs, it is similar
Element or part are typically identified by similar reference.In accompanying drawing, each element or part might not be according to the ratios of reality
Draw.
Fig. 1 is structural representation of the present utility model.
In accompanying drawing：1 represents platform body；2 represent spacing stopper；3 represent planer-type positioning tool；4 solar brackets are horizontal
Beam；5 statement wing plates.
Embodiment
As shown in Figure 1, the utility model provides a kind of solar energy wing plate linearity installation and debugging platform, including cuboid is put down
1, two spacing stopper 2 of playscript with stage directions body and planer-type positioning tool 3；Spacing stopper 2 is located at the both ends of platform body 1 respectively, spacing
Spacing hole in stopper 2 is used for fixing solar bracket crossbeam 4, and spacing stopper 2 is bolted on platform body 1.Institute
State platform body 1 and be provided with chute, the lower end of planer-type positioning tool 3 is provided with the sliding block that can be slided in chute, planer-type
Positioning tool 3 can linear slide be arranged on platform body 1 on, the glide direction of planer-type positioning tool 3 and graduation mark direction
Unanimously.
The platform body 1 is provided with graduation mark, graduation mark can accurately calculate the slip of planer-type positioning tool 3 away from
From two spacing stoppers 2 are separately mounted to start position and the final position of graduation mark.
Application method of the present utility model is as follows, between solar bracket crossbeam 4 is fixed on into two spacing stoppers 2, then
Wing plate 5 is installed on solar bracket crossbeam 4, slided by planer-type positioning tool 3 on platform body 1 to wing plate 5 one by one
Positional punch, planer-type positioning tool 3 can ensure that no matter whether overall fixed hole position position is consistent on wing plate 5, can reach the wing
After 5 whole installations of plate on the same line, connected, solved by length identical connecting rod between two adjacent vanes 5
Linearity is reduced after the galvanizing of solar bracket crossbeam 4, and the 5 overall linearity of wing plate installed on solar bracket crossbeam 4 is not united
One the problem of.
Finally it should be noted that：Various embodiments above is only to illustrate the technical solution of the utility model, rather than it is limited
System；Although the utility model is described in detail with reference to foregoing embodiments, one of ordinary skill in the art should
Understand：It can still modify to the technical scheme described in foregoing embodiments, either to which part or whole
Technical characteristic carries out equivalent substitution；And these modifications or replacement, the essence of appropriate technical solution is departed from this practicality newly
The scope of each embodiment technical scheme of type, it all should cover among claim of the present utility model and the scope of specification.
Claims (7)
- A kind of 1. solar energy wing plate linearity installation and debugging platform, it is characterised in that：Including platform body, spacing stopper and gantry Formula positioning tool；The spacing stopper can fix solar bracket crossbeam and installed in the both ends of platform body, the platform Body is provided with graduation mark, the planer-type positioning tool can linear slide be arranged on platform body, planer-type positioning work The glide direction of dress is consistent with graduation mark direction.
- 2. solar energy wing plate linearity installation and debugging platform according to claim 1, it is characterised in that：The platform body Chute is provided with, the planer-type positioning tool lower end is provided with the sliding block that can be slided in chute.
- 3. solar energy wing plate linearity installation and debugging platform according to claim 1, it is characterised in that：The platform body For cuboid.
- 4. solar energy wing plate linearity installation and debugging platform according to claim 1, it is characterised in that：The spacing stopper For two.
- 5. solar energy wing plate linearity installation and debugging platform according to claim 4, it is characterised in that：Two described spacing Stopper is located at start position and the final position of graduation mark respectively.
- 6. solar energy wing plate linearity installation and debugging platform according to claim 1, it is characterised in that：The positive stop It is provided with to the spacing hole of fixed solar bracket crossbeam.
- 7. solar energy wing plate linearity installation and debugging platform according to claim 1, it is characterised in that：The spacing stopper It is bolted on platform body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720430527.7U CN206677503U (en) | 2017-04-21 | 2017-04-21 | Solar energy wing plate linearity installation and debugging platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720430527.7U CN206677503U (en) | 2017-04-21 | 2017-04-21 | Solar energy wing plate linearity installation and debugging platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206677503U true CN206677503U (en) | 2017-11-28 |
Family
ID=60403053
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720430527.7U Active CN206677503U (en) | 2017-04-21 | 2017-04-21 | Solar energy wing plate linearity installation and debugging platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206677503U (en) |
-
2017
- 2017-04-21 CN CN201720430527.7U patent/CN206677503U/en active Active
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