CN218153956U - Adjustable aviation obstruction beacon - Google Patents
Adjustable aviation obstruction beacon Download PDFInfo
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- CN218153956U CN218153956U CN202222150671.9U CN202222150671U CN218153956U CN 218153956 U CN218153956 U CN 218153956U CN 202222150671 U CN202222150671 U CN 202222150671U CN 218153956 U CN218153956 U CN 218153956U
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Abstract
The utility model provides an adjustable aviation obstruction beacon, the solar panel angularly adjustable of installing on it to can increase the illumination volume on it, improve the generating efficiency, guarantee the actual operation effect of lamps and lanterns. It includes the lamps and lanterns support, the lamps and lanterns body is installed to the front end at lamps and lanterns support top, the solar panel that the power supply was used is installed to the rear end at lamps and lanterns support top, its characterized in that: the solar lamp comprises a solar panel, and is characterized in that an arc-shaped support is installed at the lower end of the solar panel, the bottom of the arc-shaped support extends into the lamp support and is movably connected inside the lamp support, and an adjusting mechanism which is connected with the arc-shaped support in a power mode is installed inside the lamp support and can adjust the angle of the arc-shaped support.
Description
Technical Field
The utility model relates to an aviation obstruction beacon technical field specifically is an adjustable aviation obstruction beacon.
Background
High-rise structures such as chimneys, cooling towers, communication microwave antenna towers and the like in the thermal power plant need to be provided with building barrier lamps according to the requirements of local aviation and traffic management departments.
Because aviation obstruction light is installed when the building top, the surperficial sunray received of lamps and lanterns is sufficient, consequently is necessary to install solar power system additional to the realization is as the power supply of aviation obstruction light through solar energy power generation, however because solar panel on the present aviation obstruction light is mostly the fixed bolster, consequently leads to the generating efficiency lower, influences the actual operation effect of lamps and lanterns.
SUMMERY OF THE UTILITY MODEL
The solar panel that uses to current aviation obstruction beacon adopts the fixed bolster installation, consequently leads to the generating efficiency lower, influences the problem of the actual motion effect of lamps and lanterns, the utility model provides an adjustable aviation obstruction beacon, the solar panel angularly adjustable of installing on it to can increase the illumination volume on it, improve the generating efficiency, guarantee the actual motion effect of lamps and lanterns.
The technical scheme is as follows: the utility model provides an adjustable aviation obstruction beacon, its includes the lamps and lanterns support, the lamps and lanterns body is installed to the front end at lamps and lanterns support top, the solar panel that the power supply was used is installed to the rear end at lamps and lanterns support top, its characterized in that: the solar lamp comprises a solar panel, and is characterized in that an arc-shaped support is installed at the lower end of the solar panel, the bottom of the arc-shaped support extends into the lamp support and is movably connected inside the lamp support, and an adjusting mechanism which is connected with the arc-shaped support in a power mode is installed inside the lamp support and can adjust the angle of the arc-shaped support.
It is further characterized in that: the adjusting mechanism comprises an adjusting motor, a power shaft of the adjusting motor is provided with a driving gear, and a rack meshed with the driving gear is arranged outside the arc-shaped support;
the solar tracking lamp comprises a lamp support, a storage battery, a controller and a regulating motor, wherein the lamp support is internally provided with a partition plate, the regulating motor is arranged at the upper end of the partition plate, the lower end of the partition plate is provided with the storage battery and the controller, the solar tracker is also arranged outside the lamp support, and the controller is respectively in electric control connection with the regulating motor, the storage battery, the solar tracker and a lamp body;
the controller is a TMS320F2806 type DSP, the solar tracker is an LDR type sensor, and the storage battery is NP100-12.
After having adopted above-mentioned structure, because solar panel is installed at the top of lamps and lanterns support, this solar panel passes through arc support and swing joint to can adjust the angle of arc support through adjustment mechanism, thereby can adjust the angle of solar panel above that, with the illumination volume that increases above that, improve the generating efficiency, guarantee the actual operation effect of lamps and lanterns body.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic structural view of the interior of the lamp body of the present invention;
fig. 3 is a control flow chart of the controller, the adjusting motor, the storage battery, the solar tracker and the lamp body of the present invention.
Detailed Description
As shown in fig. 1 and 2, an adjustable aviation obstruction beacon, including lamps and lanterns support 4, lamps and lanterns body 1 is installed to the front end at 4 tops of lamps and lanterns support, the rear end at 4 tops of lamps and lanterns support is installed and is being had the solar panel 2 of 1 power supplies of lamps and lanterns body, arc support 3 is installed to solar panel 2's lower extreme, the inside swing joint of lamps and lanterns support 4 is stretched into to the bottom of this arc support 3, the internally mounted of lamps and lanterns support 4 has the adjustment mechanism who is connected with 3 power of arc support, can adjust the angle of arc support 3 through this adjustment mechanism, thereby adjust the angle of solar panel 2 above that. Specifically, the adjusting mechanism comprises an adjusting motor 12, a driving gear 10 is sleeved on a power shaft of the adjusting motor 12, a rack 9 meshed with the driving gear 10 is arranged outside the arc-shaped support 3, the arc angle range of the rack 9 is 30 to 90 degrees, and the range corresponds to the solar altitude angle variation range in different latitude areas. The adjusting motor 12 is started, and the rack 9 is driven to rotate through the driving gear 10, so that the angle of the solar panel 2 on the adjusting motor can be adjusted, the illumination intensity of light received by the solar panel 2 is increased, the power generation efficiency is improved, and the operation effect of the lamp body 1 is ensured.
Further, a partition plate 8 is installed inside the lamp support 4, the adjusting motor 12 is installed at the upper end of the partition plate 8, a storage battery 6 and a controller 7 are installed at the lower end of the partition plate 8, the solar tracker 5 is further installed outside the lamp support 4, the controller 7 is respectively connected with the adjusting motor 12, the storage battery 6, the solar tracker 5 and the lamp body 1 in an electric control mode, the controller can be a TMS320F2806 type DSP, the solar tracker 5 can be an LDR type sensor, the storage battery 6 can be NP100-12, according to the solar rays monitored by the solar tracker 5, the controller 7 controls the motor 13 to rotate, the driving gear 10 is driven to rotate, the arc-shaped support 3 is driven to rotate, the inclination angle of the solar panel 2 is adjusted, the power generation efficiency is improved, meanwhile, the storage battery 6 serves as an energy storage element, and standby electric energy can be provided for the lamp body 1.
The above description is only for the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope of the present invention should be covered within the protection scope of the present invention. Therefore, the protection scope of the present invention shall be subject to the protection scope of the claims.
Claims (4)
1. The utility model provides an adjustable aviation obstruction beacon, its includes the lamps and lanterns support, the lamps and lanterns body is installed to the front end at lamps and lanterns support top, the solar panel that the power supply was used is installed to the rear end at lamps and lanterns support top, its characterized in that: the solar lamp comprises a solar panel, an arc-shaped support, a lamp support and an adjusting mechanism, wherein the lower end of the solar panel is provided with the arc-shaped support, the bottom of the arc-shaped support extends into the lamp support and is movably connected inside the lamp support, the lamp support is internally provided with the adjusting mechanism which is in power connection with the arc-shaped support, and the angle of the arc-shaped support can be adjusted by the adjusting mechanism.
2. An adjustable aircraft obstruction light according to claim 1, wherein: the adjusting mechanism comprises an adjusting motor, a driving gear is mounted on a power shaft of the adjusting motor, and a rack meshed with the driving gear is arranged outside the arc-shaped support.
3. An adjustable aircraft obstruction light according to claim 2, wherein: the solar lamp comprises a lamp support and is characterized in that a partition plate is arranged inside the lamp support, an adjusting motor is arranged at the upper end of the partition plate, a storage battery and a controller are arranged at the lower end of the partition plate, a solar tracker is further arranged outside the lamp support, and the controller is in electric control connection with the adjusting motor, the storage battery, the solar tracker and the lamp body respectively.
4. An adjustable aviation obstruction light as recited in claim 3, wherein: the controller is a TMS320F2806 type DSP, the solar tracker is an LDR type sensor, and the storage battery is NP100-12.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222150671.9U CN218153956U (en) | 2022-08-16 | 2022-08-16 | Adjustable aviation obstruction beacon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222150671.9U CN218153956U (en) | 2022-08-16 | 2022-08-16 | Adjustable aviation obstruction beacon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218153956U true CN218153956U (en) | 2022-12-27 |
Family
ID=84550670
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222150671.9U Active CN218153956U (en) | 2022-08-16 | 2022-08-16 | Adjustable aviation obstruction beacon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218153956U (en) |
-
2022
- 2022-08-16 CN CN202222150671.9U patent/CN218153956U/en active Active
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