CN220249902U - Low-power consumption aviation obstruction light - Google Patents
Low-power consumption aviation obstruction light Download PDFInfo
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- CN220249902U CN220249902U CN202321919991.4U CN202321919991U CN220249902U CN 220249902 U CN220249902 U CN 220249902U CN 202321919991 U CN202321919991 U CN 202321919991U CN 220249902 U CN220249902 U CN 220249902U
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- photovoltaic module
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- aviation obstruction
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- power consumption
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- 238000009434 installation Methods 0.000 claims abstract description 40
- 238000003466 welding Methods 0.000 claims description 5
- 241000309551 Arthraxon hispidus Species 0.000 description 8
- 230000004888 barrier function Effects 0.000 description 8
- 230000009471 action Effects 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
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- Non-Portable Lighting Devices Or Systems Thereof (AREA)
Abstract
The application provides a low-power consumption aviation obstruction lamp, including installation component, installation component's upper surface is equipped with lighting component, one side of lighting component is equipped with photovoltaic module, one side that installation component is close to photovoltaic module is equipped with the column spinner, one side that photovoltaic module is located the column spinner is equipped with the spliced pole, the spliced pole connects soon with the column spinner, relate to aviation obstruction lamp technical field, wherein, be equipped with column spinner and rotation axis at installation component's upper surface, be equipped with the spliced pole at photovoltaic module's lower surface, when installation photovoltaic module, with the spliced pole and the column spinner mutual contact that photovoltaic module was lost, and rotate the column spinner, be connected with the spliced pole under the rotation of column spinner, thereby can convenient and fast with photovoltaic module and installation component interconnect.
Description
Technical Field
The utility model relates to the technical field of aviation obstruction lights, in particular to a low-power consumption aviation obstruction light.
Background
The aviation obstruction lights are arranged on high-rise buildings with the tops higher than the ground by more than 45 meters according to the national standard. In order to distinguish the general-purpose illuminating lamp from the normal illuminating lamp, the aviation obstruction light is not always on, but is shiny, the low-light-intensity aviation obstruction light is always on, the medium-light-intensity aviation obstruction light and the high-light-intensity aviation obstruction light are shiny, and the shiny frequency is not lower than 20 times per minute and not higher than 70 times per minute. The aviation obstruction lights are used for displaying the outline of the structure, so that an aircraft operator can judge the height and the outline of the obstruction, and a warning effect is achieved.
The photovoltaic module is generally installed to current aviation obstruction beacon, carries out electric power through photovoltaic module, can reduce the consumption, but when installing photovoltaic module, need adopt bolt and nut with photovoltaic module's four corners and bottom plate interconnect, the connection step is loaded down with trivial details and inconvenient.
Disclosure of Invention
In order to overcome current aviation obstruction light and connect step loaded down with trivial details and the inconvenient problem of installation when the installation, this application embodiment provides a low-power consumption aviation obstruction light, be equipped with column spinner and rotation axis at the upper surface of installation component, be equipped with the spliced pole at the lower surface of photovoltaic module, when installation photovoltaic module, with the spliced pole that photovoltaic module was lost singly with the column spinner mutual contact to rotate the column spinner, be connected with the spliced pole under the rotation of column spinner, thereby can convenient and fast with photovoltaic module and installation component interconnect.
The technical scheme adopted by the embodiment of the application for solving the technical problems is as follows:
the utility model provides a low-power consumption aviation obstruction light, includes the installation component, the upper surface of installation component is equipped with lighting component, lighting component is spot welding with the connected mode of installation component, one side of installation component is equipped with the connecting plate, and the inside bolt that is equipped with of connecting plate, one side of lighting component is equipped with photovoltaic component, one side that installation component is close to photovoltaic component is equipped with the column spinner, photovoltaic component is located one side of column spinner and is equipped with the spliced pole, the spliced pole is connected with the column spinner spin, corresponds the spliced pole of photovoltaic component lower surface and the column spinner of installation component upper surface each other, then rotates the column spinner, makes spliced pole and column spinner spin connect each other under pivoted column spinner effect, can be quick connect photovoltaic component and installation component closely.
Preferably, the lighting assembly comprises a control box shell, the side wall of the control box shell close to the photovoltaic assembly is provided with a binding post, one side of the binding post is provided with a wiring hole, the wiring hole penetrates through a power line, the problem that the control box shell enters into a water source is avoided, the upper surface of the control box shell is provided with a connecting seat, the upper surface of the connecting seat is provided with a barrier lamp main body, and the barrier lamp main body flashes to achieve the reminding effect.
Preferably, the photovoltaic module comprises a solar cell panel, the junction of solar cell panel and spliced pole is equipped with universal joint head, the inside of universal joint head is equipped with the round pin axle, and round pin axle and spliced pole are pegged graft and are connected, make spliced pole and universal joint head connect closely under the effect of round pin axle like this, and when spliced pole and column interconnect, can change photovoltaic module's inclination through universal joint head, the inside solar cell panel's of photovoltaic module effect is with light energy conversion electric energy down, transmit inside the control box shell, then supply power for the barrier lamp main part, reach the purpose of low-power consumption, the effect that the scintillation of barrier lamp main part reaches the warning like this can.
Preferably, the installation component includes the bottom plate, the crossing department of bottom plate and column spinner is equipped with the rotation axis, and the one end and the bottom plate spot welding of rotation axis are connected, and the other end and the column spinner swivelling joint of rotation axis.
The embodiment of the application has the advantages that:
1. according to the utility model, the rotary column and the rotary shaft are arranged on the upper surface of the installation component, the connecting column is arranged on the lower surface of the photovoltaic component, when the photovoltaic component is installed, the connecting column of the photovoltaic component is contacted with the rotary column, the rotary column is rotated and connected with the connecting column under the rotation of the rotary column, so that the photovoltaic component and the installation component can be connected with each other conveniently and rapidly.
2. According to the utility model, the universal connectors are arranged on the connecting columns and the solar panel connecting columns, so that the inclination angle of the photovoltaic module can be adjusted through the universal connectors when the connecting columns and the rotating columns are connected with each other.
3. According to the utility model, the binding post is arranged on one side of the control box shell, and the opening of the binding post is positioned at the bottom end, so that rainwater can be prevented from entering the control box shell.
Drawings
The utility model will be further described with reference to the drawings and examples.
FIG. 1 is a schematic diagram of the overall structure of a low-power aviation obstruction lamp of the utility model;
FIG. 2 is a schematic view of the overall structure of the lighting assembly of the present utility model;
FIG. 3 is a schematic view of the overall structure of the mounting assembly of the present utility model;
fig. 4 is a schematic side view of a photovoltaic module according to the present utility model.
The main reference numerals illustrate:
1. a lighting assembly; 11. a control box housing; 12. binding posts; 13. a connecting seat; 14. an obstruction light body; 2. a mounting assembly; 21. a bottom plate; 22. a spin column; 23. a rotation shaft; 3. a photovoltaic module; 31. a solar cell panel; 32. a universal joint; 33. and (5) connecting the columns.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and fully with reference to the accompanying drawings, in which it is evident that the embodiments described are only some, but not all embodiments of the utility model. 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. In addition, hereinafter, for convenience of description, references to "upper", "lower", "left", "right" are equal to directions of upper, lower, left, right, etc. of the drawing itself, and the references to "first", "second", etc. are to be distinguished in description, and have no other special meaning.
The technical scheme in the embodiment of the application aims to solve the problems, and the overall thought is as follows:
examples
The embodiment provides a specific structure of low-power consumption aviation obstruction light, as shown in fig. 1-4, including installation component 2, the upper surface of installation component 2 is equipped with lighting component 1, lighting component 1 is spot welding with the connected mode of installation component 2, one side of installation component 2 is equipped with the connecting plate, and the inside bolt that is equipped with of connecting plate, one side of lighting component 1 is equipped with photovoltaic module 3, one side that installation component 2 is close to photovoltaic module 3 is equipped with column 22, photovoltaic module 3 is located one side of column 22 and is equipped with spliced pole 33, spliced pole 33 connects with column 22 soon, the spliced pole 33 of the lower surface of photovoltaic module 3 corresponds each other with column 22 of installation component 3 upper surface, then rotate column 22, make spliced pole 33 and column 22 mutually spin under pivoted column 22 effect, can be quick connect closely photovoltaic module 3 and installation component 2.
By adopting the technical scheme:
the connecting column 33 on the lower surface of the photovoltaic module 3 and the rotating column 22 on the upper surface of the installation module 3 correspond to each other, then the rotating column 22 is rotated, the connecting column 33 and the rotating column 22 are mutually screwed under the action of the rotating column 22, and the photovoltaic module 3 and the installation module 2 can be quickly and tightly connected.
The lighting assembly 1 comprises a control box shell 11, a wiring hole is formed in one side of the control box shell 11, which is close to the side wall of the photovoltaic assembly 3, and a wiring hole penetrates through a power line, the problem that the control box shell 11 enters a water source is avoided, a connecting seat 13 is arranged on the upper surface of the control box shell 11, a barrier lamp main body 14 is arranged on the upper surface of the connecting seat 13, and the barrier lamp main body 14 flashes to achieve the reminding effect.
By adopting the technical scheme:
the lateral wall that control box shell 11 is close to photovoltaic module 3 is equipped with terminal 12, and the wiring hole has been seted up to one side of terminal 12, and the inside power cord that runs through of wiring hole has avoided control box shell 11 to get into the problem of water source.
The photovoltaic module 3 includes solar cell panel 31, the junction of solar cell panel 31 and spliced pole 33 is equipped with universal joint head 32, the inside of universal joint head 32 is equipped with the round pin axle, and round pin axle and spliced pole 33 are pegged graft and are connected, make spliced pole 33 and universal joint head 32 connect closely like this under the effect of round pin axle, and when spliced pole 33 and column 22 interconnect, can change the inclination of photovoltaic module 3 through universal joint head 32, the inside solar cell panel 31 of photovoltaic module 3 is under the effect with light energy conversion electric energy, inside the control box shell 11 is transmitted, then supply power for obstacle lamp main part 14, reach the purpose of low-power consumption, obstacle lamp main part 14 twinkle like this reach the effect of reminding can.
By adopting the technical scheme:
the universal joint 32 is provided to the connection column 33 and the solar cell panel 31, so that the inclination angle of the photovoltaic module 3 can be adjusted by the universal joint 32 when the connection column 33 and the rotation column 22 are connected to each other.
The mounting assembly 2 comprises a bottom plate 21, a rotating shaft 23 is arranged at the intersection of the bottom plate 21 and a rotating column 22, one end of the rotating shaft 23 is in spot welding connection with the bottom plate 21, and the other end of the rotating shaft 23 is in rotating connection with the rotating column 22.
By adopting the technical scheme:
the rotating column 22 is rotated, the rotating shaft 23 at the bottom end of the rotating column 22 can prevent the rotating column 22 from generating friction with the bottom plate 21, and therefore the connecting column 33 and the rotating column 22 are mutually screwed under the action of the rotating column 22, and the photovoltaic module 3 and the installation module 2 can be quickly and tightly connected.
Working principle: during installation, take out installation component 2, install installation component 2 in suitable position department, then take out lighting assembly 1, with lighting assembly 1 and installation component 2 interconnect, afterwards take out photovoltaic module 3, run through terminal 12 inside with control box shell 11 interconnect with the power cord, then correspond each other the spliced pole 33 of photovoltaic module 3 lower surface and the column 22 of installation component 3 upper surface, then rotate column 22, make spliced pole 33 and column 22 connect soon each other under pivoted column 22 effect, can be quick connect photovoltaic module 3 with installation component 2 closely.
Then, under the action of the solar cell panel 31 in the photovoltaic module 3, light energy is converted into electric energy and is transmitted into the control box shell 11, and then the barrier lamp body 14 is powered to achieve the purpose of low power consumption, so that the barrier lamp body 14 flashes to achieve the reminding effect.
And the universal joint 32 is arranged on the connecting column 33 and the solar panel 31, so that the inclination angle of the photovoltaic module 3 can be adjusted by the universal joint 32 when the connecting column 33 and the rotating column 22 are connected with each other.
Finally, it should be noted that: it is apparent that the above examples are only illustrative of the present utility model and are not limiting of the embodiments. Other variations or modifications of the above teachings will be apparent to those of ordinary skill in the art. It is not necessary here nor is it exhaustive of all embodiments. And obvious variations or modifications thereof are contemplated as falling within the scope of the present utility model.
Claims (6)
1. The utility model provides a low-power consumption aviation obstruction light, its characterized in that, including installation component (2), the upper surface of installation component (2) is equipped with lighting component (1), one side of lighting component (1) is equipped with photovoltaic module (3), one side that installation component (2) is close to photovoltaic module (3) is equipped with column spinner (22), one side that photovoltaic module (3) are located column spinner (22) is equipped with spliced pole (33), spliced pole (33) connect soon with column spinner (22).
2. A low-power aviation obstruction light according to claim 1, wherein the lighting assembly (1) comprises a control box housing (11), a connecting seat (13) is arranged on the upper surface of the control box housing (11), and an obstruction light main body (14) is arranged on the upper surface of the connecting seat (13).
3. The low-power consumption aviation obstruction light according to claim 2, wherein the side wall of the control box shell (11) close to the photovoltaic module (3) is provided with a wiring terminal (12), and one side of the wiring terminal (12) is provided with a wiring hole.
4. The low-power consumption aviation obstruction light according to claim 1, wherein the photovoltaic module (3) comprises a solar panel (31), a universal connector (32) is arranged at the joint of the solar panel (31) and the connecting column (33), a pin shaft is arranged in the universal connector (32), and the pin shaft is connected with the connecting column (33) in a plugging manner.
5. A low-power consumption aviation obstruction light according to claim 1, wherein the mounting assembly (2) comprises a base plate (21), the intersection of the base plate (21) and a rotating column (22) being provided with a rotation axis (23).
6. The low-power consumption aviation obstruction light according to claim 1, wherein the lighting assembly (1) and the mounting assembly (2) are connected in a spot welding mode, a connecting plate is arranged on one side of the mounting assembly (2), and bolts are arranged inside the connecting plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321919991.4U CN220249902U (en) | 2023-07-20 | 2023-07-20 | Low-power consumption aviation obstruction light |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321919991.4U CN220249902U (en) | 2023-07-20 | 2023-07-20 | Low-power consumption aviation obstruction light |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220249902U true CN220249902U (en) | 2023-12-26 |
Family
ID=89267532
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321919991.4U Active CN220249902U (en) | 2023-07-20 | 2023-07-20 | Low-power consumption aviation obstruction light |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220249902U (en) |
-
2023
- 2023-07-20 CN CN202321919991.4U patent/CN220249902U/en active Active
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