CN219954793U - Full sky imager adjusts structure - Google Patents
Full sky imager adjusts structure Download PDFInfo
- Publication number
- CN219954793U CN219954793U CN202321139852.XU CN202321139852U CN219954793U CN 219954793 U CN219954793 U CN 219954793U CN 202321139852 U CN202321139852 U CN 202321139852U CN 219954793 U CN219954793 U CN 219954793U
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- sky imager
- threaded rod
- vertical
- plate
- sky
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- 238000009434 installation Methods 0.000 claims abstract description 23
- 230000000149 penetrating effect Effects 0.000 claims description 5
- 238000010030 laminating Methods 0.000 claims description 2
- 239000000758 substrate Substances 0.000 abstract description 4
- 238000013461 design Methods 0.000 description 5
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000003384 imaging method Methods 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
Abstract
The utility model discloses an all-sky imager adjusting structure, which comprises a substrate, wherein an installing plate is fixed at the edge of the bottom end of the substrate; the bottom surface of the top plate is fixedly connected with the top end of the vertical threaded rod, and the top plate is rotatably provided with a horizontal threaded rod through a bearing seat at one end; the limiting bottom groove is formed in the inner wall of the limiting bottom groove and is attached to the bottom end of the positioning bolt, the limiting bottom groove is formed in the top surface of the top plate, the positioning nut is installed at the top end of the positioning bolt, the supporting rod is rotatably installed on the side of the top plate, and the top end of the supporting rod is rotatably connected with one end of the bottom surface of the full-sky imager body. This all-sky imager adjusts structure, through novel installation adjusting structure, make all-sky imager can be in stable use under the installation environment of difference, and can be according to the difference of installation environment, convenient adjustment and the installation height of fixed all-sky imager, the levelness of the all-sky imager of adjustment that can also be convenient guarantees that all-sky imager can be quick stable installation use.
Description
Technical Field
The utility model relates to the technical field of all-sky imagers, in particular to an adjusting structure of an all-sky imager.
Background
The full-sky imager is a continuous automatic monitoring instrument of full sky cloud quantity in daytime, is a full-automatic full-color sky imaging system, provides real-time processing and displays the sky state in daytime, can realize continuous automatic monitoring of the full sky cloud quantity in daytime, has higher space-time resolution, and has more accurate cloud quantity calculation results. The solar energy tracking system mainly comprises an imaging part, a solar tracking device and an environment protection system.
The existing installation and adjustment structure of the full-sky imager is simple in design, and is only a simple bracket and a metal plate provided with a threaded installation hole, and because the installation is carried out by using the bracket and the metal plate, when the installation plane of the full-sky imager is uneven, the full-sky imager is inconvenient to adjust to a horizontal state by using by the simple installation structure. It is desirable to design an all-sky imager adjustment structure that addresses the above-described issues.
Disclosure of Invention
The utility model aims to provide an all-sky imager adjusting structure so as to solve at least one technical problem in the background technology.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
an all-sky imager adjustment structure, comprising:
the base plate is fixed with a mounting plate at the edge of the bottom end of the base plate, a mounting window is formed in the mounting plate in a penetrating mode, a vertical adjusting sleeve is rotatably arranged at the top of the base plate in a penetrating mode through a bearing seat, and a vertical threaded rod is arranged in the center of the vertical adjusting sleeve;
the bottom surface of the top plate is fixedly connected with the top end of the vertical threaded rod, a horizontal threaded rod is rotatably arranged at one end of the top plate through a bearing seat, a movable plate is arranged on the horizontal threaded rod, a vertical hole is formed in the center of the movable plate, and a positioning bolt is arranged in the vertical hole in a penetrating manner;
the limiting bottom groove is formed in the inner wall of the limiting bottom groove and is attached to the bottom end of the positioning bolt, the limiting bottom groove is formed in the top surface of the top plate, the positioning nut is installed at the top end of the positioning bolt, the supporting rod is rotatably installed on the side of the top plate, and the top end of the supporting rod is rotatably connected with one end of the bottom surface of the full-sky imager body.
Preferably, the mounting plates are symmetrically distributed at two ends of the bottom surface of the substrate, the front view of the mounting plates is L-shaped, and the vertical part and the horizontal part of the mounting plates are provided with mounting windows.
Preferably, the vertical adjusting sleeve and the vertical threaded rod are symmetrically distributed about the center of the top plate, the vertical adjusting sleeve and the vertical threaded rod are in threaded connection, and the vertical adjusting sleeve is in a 'straight' shape in front view.
Preferably, the horizontal threaded rod is in threaded connection with the movable plate, and the horizontal threaded rod is symmetrically distributed about the center of the movable plate.
Preferably, the middle part of the positioning bolt is tightly attached to the inner wall of the vertical hole, the bottom end of the positioning bolt is attached to the central inner wall of the limiting bottom groove, and the side view cross section of the limiting bottom groove is shaped like a Chinese character 'ji'.
Preferably, the supporting rods are symmetrically distributed about the center of the full-sky imager body, and the supporting rods are obliquely arranged at 45 degrees.
Preferably, a bottom shaft is mounted on the other side of the bottom end of the all-sky imager body, and the bottom shaft is rotatably connected with the top surface of the top plate.
Compared with the prior art, the utility model has the beneficial effects that:
through the novel installation adjusting structure, the all-sky imager can be stably used in different installation environments, the installation height of the all-sky imager can be conveniently adjusted and fixed according to the different installation environments, the levelness of the all-sky imager can be conveniently adjusted, and the rapid and stable installation and use of the all-sky imager are ensured;
1. according to the utility model, the whole device is suspended and fixed or supported and fixed by matching the mounting plate and the mounting window with bolts, the vertical threaded rod is driven by the rotating vertical adjusting sleeve to vertically move with the top plate and the full-sky imager body, so that the use height of the full-sky imager body can be conveniently and quickly adjusted, and the use height of the full-sky imager body is quickly fixed by utilizing thread self-locking;
2. according to the utility model, the horizontal threaded rod is rotated in the forward direction or the reverse direction, so that the horizontal threaded rod drives the movable plate to horizontally move along the limiting bottom groove by utilizing the threaded connection relation, the supporting rod is pushed to be rotated and erected or rotated to be put down, the full-sky imager body is driven to rotate clockwise or anticlockwise by taking the bottom shaft as the center, the inclination angle of the full-sky imager body is changed, the full-sky imager is suitable for mounting surfaces with different inclination angles, and the full-sky imager body can be ensured to be used stably and horizontally.
Drawings
Fig. 1 is a schematic diagram of the front view structure of the present utility model.
Fig. 2 is a schematic side view of the present utility model.
Fig. 3 is a schematic cross-sectional elevation view of the present utility model.
Fig. 4 is a schematic side sectional view of the present utility model.
In the figure: 1. a substrate; 2. a mounting plate; 3. installing a window; 4. a vertical adjustment sleeve; 5. a vertical threaded rod; 6. a top plate; 7. a horizontal threaded rod; 8. a movable plate; 9. a vertical hole; 10. positioning bolts; 11. a limiting bottom groove; 12. positioning a nut; 13. a support rod; 14. a full sky imager body; 15. a bottom shaft.
Detailed Description
The utility model is further described in connection with the following detailed description, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the utility model easy to understand.
In the description of the present utility model, it should be noted that the directions or positional relationships indicated by the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", etc. are based on the directions or positional relationships shown in the drawings, are merely for convenience of describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific direction, be configured and operated in the specific direction, and thus should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "provided," "connected," and the like are to be construed broadly, and may be fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-4, an embodiment of the present utility model is provided:
an all-sky imager adjustment structure, comprising:
the base plate 1, the mounting plate 2 is fixed on the edge of the bottom end of the base plate 1, the mounting plate 2 is penetrated and provided with mounting windows 3, the mounting plate 2 is symmetrically distributed at two ends of the bottom surface of the base plate 1, the front view of the mounting plate 2 is L-shaped, the mounting windows 3 are respectively arranged at the vertical part and the horizontal part of the mounting plate 2, and the orientation of the mounting windows 3 with different calibers can be turned according to different mounting environments during mounting by the structural design, so that the mounting windows 3 with different calibers are favorably used for bolt mounting, the top of the base plate 1 is penetrated and rotatably provided with a vertical adjusting sleeve 4 through a bearing seat, and the center of the vertical adjusting sleeve 4 is provided with a vertical threaded rod 5;
the top plate 6, the top end of the top plate 6 is fixedly connected with the top end of the vertical threaded rod 5, the vertical adjusting sleeve 4 and the vertical threaded rod 5 are symmetrically distributed around the center of the top plate 6, the vertical adjusting sleeve 4 and the vertical threaded rod 5 are in threaded connection, the vertical adjusting sleeve 4 is in a 'right-hand' shape, the vertical adjusting sleeve 4 can be conveniently operated, the vertical adjusting sleeve 4 can drive the vertical threaded rod 5 to stably vertically move along with the top plate 6 by utilizing a threaded connection relationship when rotating, the top plate 6 is rotatably provided with the horizontal threaded rod 7 through one end through a bearing seat, the movable plate 8 is arranged on the horizontal threaded rod 7, the vertical hole 9 is formed in the center of the movable plate 8, and the positioning bolt 10 is arranged in the vertical hole 9 in a penetrating manner;
spacing kerve 11, spacing kerve 11 inner wall and positioning bolt 10 bottom laminating, spacing kerve 11 is offered on roof 6 top surface, positioning nut 12 is installed on positioning bolt 10 top, roof 6 limit side swivelling joint has bracing piece 13, bracing piece 13 top and full sky imager body 14 bottom surface one end swivelling joint, when twisting horizontal threaded rod 7 and rotating, horizontal threaded rod 7 can promote fly leaf 8 and carry out displacement adjustment through positioning bolt 10 and spacing kerve 11 on roof 6, so be favorable to the fly leaf 8 to promote the imager body 14 through bracing piece 13 and carry out angular adjustment this time.
In one embodiment, the horizontal threaded rod 7 is in threaded connection with the movable plate 8, the horizontal threaded rod 7 is distributed symmetrically about the center of the movable plate 8, and the above structural design enables the movable plate 8 to be stably driven to be attached to the surface of the top plate 6 for horizontal sliding displacement by utilizing the threaded connection relationship when the horizontal threaded rod 7 rotates.
In one preferred embodiment, the middle part of the positioning bolt 10 is tightly attached to the inner wall of the vertical hole 9, the bottom end of the positioning bolt 10 is attached to the central inner wall of the limiting bottom groove 11, the side view cross section of the limiting bottom groove 11 is in a shape of a letter "Chinese character 'ji', the above structural design can prevent the bottom end of the positioning bolt 10 from slipping off the limiting bottom groove 11, and the movable plate 8 can stably move horizontally with the positioning bolt 10, and the positioning nut 12 can stably position the movable plate 8 when extruding the movable plate 8.
In one embodiment, the supporting rods 13 are symmetrically distributed about the center of the full-sky imager body 14, and the supporting rods 13 are obliquely arranged at 45 degrees, so that the supporting rods 13 are rotated, erected and rotated to be the same in magnitude, and the supporting rods 13 can push and pull the full-sky imager body 14 to rotate clockwise or anticlockwise in the same magnitude.
In one preferred embodiment, the bottom shaft 15 is mounted on the other side of the bottom end of the all-sky imager body 14, and the bottom shaft 15 is rotatably connected with the top surface of the top plate 6, so that the all-sky imager body 14 can stably rotate around the bottom shaft 15 to adjust the use angle.
The working principle of the utility model is as follows: when the device is used, firstly, according to the installation environment of the full-sky imager body 14, a horizontal or vertical installation window 3 in fig. 3 is selected to be used, bolts penetrate through the installation window 3, the whole device is fixed on a vertical installation surface or a horizontal installation surface, then, the symmetrically distributed vertical adjustment sleeves 4 in fig. 3 are screwed simultaneously, the vertical adjustment sleeves 4 rotate to drive the vertical threaded rods 5 to vertically move upwards with the top plates 6 and the full-sky imager body 14 until the height of the full-sky imager body 14 is proper, the rotation of the vertical adjustment sleeves 4 is stopped, and the heights of the top plates 6 of the vertical threaded rods 5 and the full-sky imager body 14 are fixed by utilizing thread self-locking;
many times, the mounting surface to which the mounting plate 2 is connected is not standard vertical or horizontal, at this time, the positioning nut 12 in fig. 3 needs to be screwed up, the positioning nut 12 no longer extrudes the movable plate 8 to fix with the top plate 6, and meanwhile, the horizontal threaded rod 7 is used for driving the movable plate 8 in fig. 3 to move horizontally left or right along the limiting bottom groove 11 by using the threaded connection relation with the positioning bolt 10, the movable plate 8 pushes the supporting rod 13 to rotate up or rotate in the moving process, the supporting rod 13 pushes the whole-sky imager body 14 to rotate anticlockwise or clockwise around the bottom shaft 15 in the rotating process, and is matched with the level meter to measure, until the whole-sky imager body 14 is adjusted to be horizontal, the rotation of the horizontal threaded rod 7 is stopped and the downward rotation of the positioning nut 12 is reset, the horizontal threaded rod 7 and the movable plate 8 are matched with the threaded self-locking of the threads of the positioning nut 12, the movable plate 8 and the supporting rod 13 are stably fixed, the whole-sky imager body 14 is stably supported and positioned, and the whole-sky imager body 14 is ensured to be stably used horizontally.
The foregoing is merely exemplary embodiments of the present utility model, and specific structures and features that are well known in the art are not described in detail herein. It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present utility model may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (7)
1. An all-sky imager adjustment structure, characterized in that it includes:
the device comprises a base plate (1), wherein an installation plate (2) is fixed at the edge of the bottom end of the base plate (1), an installation window (3) is penetrated and formed in the installation plate (2), a vertical adjusting sleeve (4) is penetrated and rotatably installed at the top of the base plate (1) through a bearing seat, and a vertical threaded rod (5) is installed at the center of the vertical adjusting sleeve (4);
the top plate (6), the bottom surface of the top plate (6) is fixedly connected with the top end of the vertical threaded rod (5), the top plate (6) is rotatably provided with a horizontal threaded rod (7) through a bearing seat at one end, a movable plate (8) is arranged on the horizontal threaded rod (7), a vertical hole (9) is formed in the center of the movable plate (8), and a positioning bolt (10) is arranged in the vertical hole (9) in a penetrating manner;
spacing kerve (11), spacing kerve (11) inner wall and positioning bolt (10) bottom laminating, spacing kerve (11) are seted up on roof (6) top surface, positioning nut (12) are installed on positioning bolt (10) top, roof (6) limit side rotation installs bracing piece (13), bracing piece (13) top and full sky imager body (14) bottom surface one end swivelling joint.
2. The all-sky imager adjustment structure of claim 1, wherein: the mounting plates (2) are symmetrically distributed at two ends of the bottom surface of the base plate (1), the front view of the mounting plates (2) is L-shaped, and mounting windows (3) are formed in the vertical part and the horizontal part of the mounting plates (2).
3. The all-sky imager adjustment structure of claim 1, wherein: the vertical adjusting sleeve (4) and the vertical threaded rod (5) are symmetrically distributed about the center of the top plate (6), the vertical adjusting sleeve (4) and the vertical threaded rod (5) are in threaded connection, and the vertical adjusting sleeve (4) is in a right-looking shape.
4. The all-sky imager adjustment structure of claim 1, wherein: the horizontal threaded rod (7) is in threaded connection with the movable plate (8), and the horizontal threaded rod (7) is distributed symmetrically about the center of the movable plate (8).
5. The all-sky imager adjustment structure of claim 1, wherein: the middle part of the positioning bolt (10) is tightly attached to the inner wall of the vertical hole (9), the bottom end of the positioning bolt (10) is attached to the central inner wall of the limiting bottom groove (11), and the side view section of the limiting bottom groove (11) is shaped like a Chinese character 'ji'.
6. The all-sky imager adjustment structure of claim 1, wherein: the supporting rods (13) are distributed symmetrically about the center of the full-sky imager body (14), and the supporting rods (13) are obliquely arranged at 45 degrees.
7. The all-sky imager adjustment structure of claim 1, wherein: the bottom shaft (15) is arranged on the other side of the bottom end of the full-sky imager body (14), and the bottom shaft (15) is rotationally connected with the top surface of the top plate (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321139852.XU CN219954793U (en) | 2023-05-12 | 2023-05-12 | Full sky imager adjusts structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321139852.XU CN219954793U (en) | 2023-05-12 | 2023-05-12 | Full sky imager adjusts structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219954793U true CN219954793U (en) | 2023-11-03 |
Family
ID=88537104
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321139852.XU Active CN219954793U (en) | 2023-05-12 | 2023-05-12 | Full sky imager adjusts structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219954793U (en) |
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2023
- 2023-05-12 CN CN202321139852.XU patent/CN219954793U/en active Active
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