CN208154332U - A kind of durable type solar energy aeronautical light device - Google Patents
A kind of durable type solar energy aeronautical light device Download PDFInfo
- Publication number
- CN208154332U CN208154332U CN201820632077.4U CN201820632077U CN208154332U CN 208154332 U CN208154332 U CN 208154332U CN 201820632077 U CN201820632077 U CN 201820632077U CN 208154332 U CN208154332 U CN 208154332U
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- China
- Prior art keywords
- lamp holder
- lamp
- fixed
- chamber
- solar energy
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- Legal status (The legal status 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 status listed.)
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Abstract
The utility model discloses a kind of durable type solar energy aeronautical light devices, it is related to aeronautical light technical field, including lamp holder, lamp holder outer wall surrounding is respectively arranged with the solar panel of a certain angle, solar panel is connected with the battery pack being fixed on inboard wall of lamp holder, there are two ventilation openings for setting in lamp holder inner bottom surface, fan assembly is provided in ventilation opening, lamp holder bottom centre is connected with support base, lamp holder surrounding inner wall is fixed with controller and pressure limiting device, lamp holder top is connected with light body, the light body includes the support rod for connecting lamp holder, the chamber seat that support rod top is fixed with, fixed lamp chamber above chamber seat, fixed illumination region above lamp chamber, illumination region includes lampshade and the identical LED lamp panel of multiple structures, each LED lamp panel bottom is connected with the temperature sensor being fixed on inside lamp chamber;The utility model has the advantages that safety and stability and long service life.
Description
Technical field
The utility model relates to aeronautical light technical fields, fill more particularly to a kind of durable type solar energy aeronautical light
It sets.
Background technique
In the development process of aviation industry, increasingly due to high-altitude facility such as squarer, high-rise, beacon etc.
More, for aviation safety, they are all the barriers potentially dangerous to aviation in a way, and aeronautical light is as one
The red safety lamp that kind is always on or flashes, can effectively indicate high-altitude barrier, be the critical facility of aircraft navigation.For aviation
The usage amount of lamps and lanterns is more and more, more and more stronger for the electric power dependence of highly energy-consuming, how to be to mention using aviation condition
For aeronautical light electric energy it is enough provide safeguard, and increase aeronautical light service life and quality, be this field researcher research
Direction.
LED light in general aeronautical light be easy in the operating condition it is heating up, when temperature is higher than 70 DEG C or more, LED
Lamp bead will receive badly damaged, cause light decay, influence the illumination effect of aeronautical light, or even failure can not shine, existing aviation
All it is single led lamp in lamp illumination region, after LED lamp bead damage, the timely disassembling, assembling and replacing of staff is needed, due to aeronautical light
Dismounting belongs to high altitude operation, staff can not real time operation then there is security risk when aeronautical light failure;It is existing too
The lamp holder of positive energy aeronautical light is all sealing, has electric energy storage device, control circuit and various devices inside lamp holder, these devices are general
It can continue working, cause aeronautical light internal temperature excessively high, so that entire aeronautical light is easy to break down, reduce solar energy boat
The service life of empty lamp.
Utility model content
The purpose of this utility model is that:Cause mainly for solving existing solar energy aeronautical light since temperature is excessively high using
Service life too low problem, the utility model provide a kind of durable type solar energy aeronautical light device.
The utility model specifically uses following technical scheme to achieve the goals above:
A kind of durable type solar energy aeronautical light device, including lamp holder, lamp holder outer wall surrounding are respectively arranged with certain angle
The solar panel of degree, solar panel are connected with the battery pack being fixed on inboard wall of lamp holder, have in lamp holder inner bottom surface
Two ventilation openings are provided with fan assembly in ventilation opening, and lamp holder bottom centre is connected with support base, and lamp holder surrounding inner wall is fixed
There are controller and pressure limiting device, lamp holder top is connected with light body, and the light body includes the support rod for connecting lamp holder, branch
The chamber seat that strut top is fixed with, fixed lamp chamber above chamber seat, fixed illumination region above lamp chamber, illumination region include lampshade and
The identical LED lamp panel of multiple structures, each LED lamp panel bottom is connected with the temperature sensor being fixed on inside lamp chamber.
Further, fan assembly includes the Liang Ge support plate mechanism being separately fixed on the inner wall of lamp holder two sides, two branch
Fagging mechanism is respectively fixed with a head-down rotary electric machine, and it is logical at one that one of rotary electric machine lower part is connected with setting
Enter fan in air port, another rotary electric machine lower part, which is connected with to be arranged in another ventilation opening, goes out fan.
Further, lamp chamber surrounding encirclement is provided with heat dissipating layer.
Further, inboard wall of lamp holder is provided with wireless remote control module.
Further, battery pack includes battery and reserve battery, and battery is lithium battery, and reserve battery is MnZn electricity
Pond.
Further, chamber seat surrounding is provided with a ultrasonic insects expelling device.
Further, lampshade uses acrylate cydariform Fresnel lens, and outer cover of lamp holder is cast using aluminium alloy.
The beneficial effects of the utility model are as follows:
1, the illumination region of the utility model is provided with multiple LED lamp panels, only one general LED lamp panel shines, as the LED
When the temperature sensor of lamp plate detects that temperature is greater than 75 DEG C, the power supply circuit that controller controls the LED lamp panel is disconnected and is controlled
Other LED light start to shine, this greatly reduces the probability of damage of entire illumination region lamp, allow the service life of entire aeronautical light
Increase, reduces security risk, two LED lamp panels also can be set while glistening, this makes aeronautical light working environment range wider.
2, the fan assembly structure of the utility model is simple, and blower fan does not work generally with exhaust fan, since there are two
Ventilation opening, entire lamp holder heating rate is very slow, after the temperature sensor inside lamp holder detects that temperature reaches warning value, control
Device control blower fan and exhaust fan processed enter work, allow entire lamp holder to cool down rapidly, reduce various equipment and electricity inside lamp holder
The damage on road further allows the service life of entire aeronautical light to increase;Since fan assembly is arranged in lamp holder bottom, effectively prevent
Rainwater is stopped and has entered lamp holder, various equipment and circuit is allowed inside lamp holder to be corroded probability reduction.
3, the electric energy storage device of the utility model uses lithium battery, for traditional lead storage battery, is recycled
Service life is high, and it is not necessary that power unit is safeguarded and replaced at any time, battery pack is additionally provided with reserve battery, when solar electric power supply system event
When barrier, reserve battery access circuit is powered, and is guaranteed that aeronautical light can be always on, be further reduced security risk and increase
The service life of aeronautical light.
4, the lampholder shell of the utility model is cast using aluminium alloy, and good heat conduction effect, there are also one layer for lamp chamber surrounding
Heat dissipating layer makes entire aeronautical light heat dissipation effect and antiageing effect more preferably, and the ultrasonic mosquito dispeller being arranged on chamber seat can also have
Effect prevents mosquito from causing aviation lamp wiring weak.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model;
Fig. 2 is the structural schematic diagram of light body;
Appended drawing reference:1- light body, 1.1- chamber seat, 1.1.1- ultrasonic insects expelling device, 1.2- lamp chamber, 1.2.1- heat dissipation
Layer, 1.3- illumination region, 1.3.1-LED lamp plate, 1.3.2- lampshade, 1.4- temperature sensor, 2- support rod, 3- lamp holder, 3.1- wind
Fan device, 3.1.1- rotary electric machine, 3.1.2- support plate mechanism, 3.1.3- blower fan, 3.1.4- exhaust fan, 3.2- battery pack,
3.2.1- battery, 3.2.2- reserve battery, 3.3- controller, 3.4- pressure limiting device, 3.5- temperature sensing device, 3.6- is wireless
Remote control module, 3.7- ventilation opening, 4- device of solar generating, 5- support base.
Specific embodiment
In order to which those skilled in the art better understand the utility model, with reference to the accompanying drawing with following embodiment to this
Utility model is described in further detail.
Embodiment 1
As shown in Fig. 1 to 2, the present embodiment provides a kind of durable type solar energy aeronautical light device, including lamp holder 3, outside lamp holder 3
Wall surrounding is respectively arranged with the solar panel of a certain angle, and solar panel, which is connected with, is fixed on 3 inner wall of lamp holder
On battery pack 3.2 be provided with fan assembly 3.1, lamp in ventilation opening 3.7 there are two ventilation opening 3.7 in 3 inner bottom surface of lamp holder
3 bottom centre of seat are connected with support base 5, and 3 surrounding inner wall of lamp holder is fixed with controller 3.3 and pressure limiting device 3.4, on lamp holder 3
Portion is connected with light body 1, and the light body 1 includes the support rod 2 of connection lamp holder 3, the chamber seat that 2 top of support rod is fixed with
1.1, the 1.1 fixed lamp chamber 1.2 in top of chamber seat, the 1.2 fixed illumination region 1.3 in top of lamp chamber, illumination region 1.3 includes lampshade
1.3.2 the identical LED lamp panel 1.3.1 with multiple structures, the bottom each LED lamp panel 1.3.1 are connected with one and are fixed on lamp chamber
Temperature sensor 1.4 inside 1.2.
Embodiment 2
This implementation is to be further optimized on the basis of embodiment 1, specifically:
Fan device includes the Liang Ge support plate mechanism 3.1.2 being separately fixed on 3 two sides inner wall of lamp holder, two support triggers
Structure 3.1.2 is respectively fixed with a head-down rotary electric machine 3.1.1, and the lower part one of rotary electric machine 3.1.1, which is connected with, to be set
It sets and enters fan in a ventilation opening 3.7, the lower part another rotary electric machine 3.1.1, which is connected with, to be arranged in another ventilation opening
Go out fan in 3.7.
Blower fan 3.1.3 and exhaust fan 3.1.4 does not work generally, since there are two ventilation openings 3.7,3 liters of entire lamp holders
Warm speed is very slow, and after the temperature sensor 1.4 inside lamp holder 3 detects that temperature reaches warning value, the control of controller 3.3 is inhaled
Fan 3.1.3 and exhaust fan 3.1.4 enter work, and entire lamp holder 3 is allowed to cool down rapidly.
Embodiment 3
The present embodiment is to be further optimized on the basis of embodiment 1, specifically:
The encirclement of 1.2 surrounding of lamp chamber is provided with heat dissipating layer 1.2.1, and 3 inner wall of lamp holder is provided with wireless remote control module 3.6, battery
Group 3.2 includes battery 3.2.1 and reserve battery 3.2.2, and battery 3.2.1 is lithium battery, and reserve battery 3.2.2 is MnZn electricity
Pond, 1.1 surrounding of chamber seat are provided with a ultrasonic insects expelling device 1.1.1, and lampshade 1.3.2 is saturating using acrylate cydariform Fresnel
Mirror, 3 shell of lamp holder are cast using aluminium alloy.
The above, the only preferred embodiment of the utility model, are not intended to limit the utility model, the utility model
Scope of patent protection be subject to claims, it is equivalent made by all specifications and accompanying drawing content with the utility model
Structure change similarly should be included in the protection scope of the utility model.
Claims (7)
1. a kind of durable type solar energy aeronautical light device, including lamp holder (3), which is characterized in that lamp holder (3) outer wall surrounding is set respectively
It is equipped with the solar panel of a certain angle, solar panel is connected with the battery pack being fixed on lamp holder (3) inner wall
(3.2), there are two ventilation opening (3.7), ventilation opening (3.7) is interior to be provided with fan assembly for setting in lamp holder (3) inner bottom surface
(3.1), lamp holder (3) bottom centre is connected with support base (5), and lamp holder (3) surrounding inner wall is fixed with controller (3.3) and pressure limiting
Device (3.4), lamp holder (3) top are connected with light body (1), and the light body (1) includes the support rod of connection lamp holder (3)
(2), the chamber seat (1.1) that support rod (2) top is fixed with, the fixed lamp chamber (1.2) in chamber seat (1.1) top, lamp chamber (1.2) top
Fixed illumination region (1.3), illumination region (1.3) include lampshade (1.3.2) and the identical LED lamp panel of multiple structures (1.3.1), often
A LED lamp panel (1.3.1) bottom is all connected with one and is fixed on the internal temperature sensor (1.4) of lamp chamber (1.2).
2. a kind of durable type solar energy aeronautical light device according to claim 1, which is characterized in that the fan assembly
It (3.1) include the Liang Ge support plate mechanism (3.1.2) being separately fixed on the inner wall of lamp holder (3) two sides, Liang Ge support plate mechanism
(3.1.2) is respectively fixed with a head-down rotary electric machine (3.1.1), the one of rotary electric machine lower part (3.1.1) connection
There is the blower fan (3.1.3) being arranged in a ventilation opening (3.7), another lower part rotary electric machine (3.1.1) is connected with setting
Exhaust fan (3.1.4) in another ventilation opening (3.7) is provided with a temperature sensing at arm center in lamp holder (3) upper casing
Device (1.4).
3. a kind of durable type solar energy aeronautical light device according to claim 1, which is characterized in that the LED lamp panel
(1.3.1) is two, and the encirclement of lamp chamber (1.2) surrounding is provided with heat dissipating layer (1.2.1).
4. a kind of durable type solar energy aeronautical light device according to claim 1, which is characterized in that in the lamp holder (3)
Wireless remote control module (3.6) are provided on wall.
5. a kind of durable type solar energy aeronautical light device according to claim 1, which is characterized in that the battery pack
It (3.2) include battery (3.2.1) and reserve battery (3.2.2), battery (3.2.1) is lithium battery, reserve battery (3.2.2)
For manganese-zinc battery.
6. a kind of durable type solar energy aeronautical light device according to claim 1, which is characterized in that the chamber seat (1.1)
A ultrasonic insects expelling device (1.1.1) is provided in surrounding.
7. a kind of durable type solar energy aeronautical light device according to claim 1, which is characterized in that the lampshade
(1.3.2) uses acrylate cydariform Fresnel lens, and lamp holder (3) shell is cast using aluminium alloy.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201820632077.4U CN208154332U (en) | 2018-04-28 | 2018-04-28 | A kind of durable type solar energy aeronautical light device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820632077.4U CN208154332U (en) | 2018-04-28 | 2018-04-28 | A kind of durable type solar energy aeronautical light device |
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Publication Number | Publication Date |
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CN208154332U true CN208154332U (en) | 2018-11-27 |
Family
ID=64376595
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CN201820632077.4U Expired - Fee Related CN208154332U (en) | 2018-04-28 | 2018-04-28 | A kind of durable type solar energy aeronautical light device |
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CN (1) | CN208154332U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110645554A (en) * | 2019-10-12 | 2020-01-03 | 广州领尚灯具有限公司 | High-watt-rate quick cooling device for illuminating lamp |
-
2018
- 2018-04-28 CN CN201820632077.4U patent/CN208154332U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110645554A (en) * | 2019-10-12 | 2020-01-03 | 广州领尚灯具有限公司 | High-watt-rate quick cooling device for illuminating lamp |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181127 Termination date: 20200428 |