CN208074840U - A kind of swinging durable type solar energy aeronautical light - Google Patents
A kind of swinging durable type solar energy aeronautical light Download PDFInfo
- Publication number
- CN208074840U CN208074840U CN201820632096.7U CN201820632096U CN208074840U CN 208074840 U CN208074840 U CN 208074840U CN 201820632096 U CN201820632096 U CN 201820632096U CN 208074840 U CN208074840 U CN 208074840U
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- CN
- China
- Prior art keywords
- supporting rod
- fixed
- swivel becket
- lamp holder
- swinging
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Abstract
The utility model discloses a kind of swinging durable type solar energy aeronautical lights,It is related to aeronautical light technical field,Including lamp holder,Lamp holder lower casing inner wall is disposed with battery pack from left to right,Voltage limiter and controller,Lamp holder upper casing outer wall is provided with supporting rod,The device of solar generating that can be rotated around supporting rod is provided on supporting rod anchor ring,Device of solar generating includes the swivel becket A being fixed on supporting rod,It is provided with supporting pad below swivel becket A,It is connected with rotary electric machine device below supporting pad,It is fixed on swivel becket A anchor rings that there are one telescopic devices,The telescopic device other end is connected with solar panel,It is connected with the holding set being set on supporting rod above swivel becket A,Set top is kept to be connected with the swivel becket B being fixed on supporting rod,The bindiny mechanism of connection solar panel is fixed on swivel becket B anchor rings,Supporting rod top is connected with light body；The utility model has the advantages that efficient power supply system, safety and stability and with long service life.
Description
Technical field
The utility model is related to aeronautical light technical fields, more particularly to a kind of swinging durable type solar energy aviation
Lamp.
Background technology
In the evolution 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 flickers, 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 carry 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.In recent years, the utilization of the exploitation with developed countries such as America and Europes to low-carbon, the energy-saving and environmental protection energy, solar energy is more filled
Point, technology is also more ripe, is powered for aeronautical light using solar energy, simplifies the setting to power cord in installation process, for section
About conventional energy resource, conservation of nature environment, promotion sustainable economic development have particularly important meaning.
The solar panel of general solar energy aeronautical light all many, but it cannot be guaranteed that at any time perpendicular to sunlight
Solar energy is absorbed, this causes sexual valence relatively low, and general electric energy storage device uses traditional lead-acid accumulator, this accumulator longevity
Order it is low need periodic maintenance and replacement, waste manpower and materials.LED light in aeronautical light is easy fever and rises in the operating condition
Temperature, when temperature is higher than 70 DEG C or more, LED lamp bead can be seriously damaged, causes light decay, influences the illumination effect of aeronautical light,
Even failure can not shine, and existing aeronautical light is generally single led lamp, after LED lamp panel is damaged, needs staff timely
Disassembling, assembling and replacing, since the dismounting of aeronautical light belongs to working at height, staff can not real time operation, when aeronautical light fails, then
There are security risks.
Utility model content
The purpose of this utility model is that：It is absorbed and storage solar energy efficiency mainly for solving existing solar energy aeronautical light
Problem low, service life is short, the utility model provide a kind of swinging durable type solar energy aeronautical light.
The utility model specifically uses following technical scheme to achieve the goals above：
A kind of swinging durable type solar energy aeronautical light, including lamp holder, lamp holder lower casing inner wall are disposed with from left to right
Battery pack, voltage limiter and controller, battery pack include accumulator, and lamp holder upper casing inner wall is provided with wireless remote control module, on lamp holder
It is provided with supporting rod at shell outer wall center, the device of solar generating that can be rotated around supporting rod is provided on supporting rod anchor ring, too
Positive energy power generator includes coordinating to be connected with to be arranged below the swivel becket A that supporting rod rotates, swivel becket A on supporting rod to exist
Lamp holder upper casing outer wall can be connected with the rotation for being fixed on lamp holder upper casing inner wall with the supporting pad of swivel becket A rotations, supporting pad lower section
Electric machine, fixed there are one telescopic device on swivel becket A anchor rings, the telescopic device other end is connected with solar panel, turns
It is connected with above rotating ring A and is set in rotatable holding set on supporting rod, keeping set top to be connected with cooperation can on supporting rod
The bindiny mechanism of connection solar panel is fixed with around the swivel becket B of supporting rod rotation, on swivel becket B anchor rings, on supporting rod
Portion is connected with light body.
Further, telescopic device includes telescopic rod, and telescopic rod epimere is fixed with limited block, and telescopic rod bottom, which is fixed on, to be turned
On rotating ring A anchor rings and inside is fixed with the long regulating mechanism of bar, is provided with gyrator at the top of telescopic rod, gyrator is connected with revolution
Slide block mechanism, rotary slider mechanism are combined with the sliding rail for being fixed on Solar panel backside, and bindiny mechanism passes through rotation
Pair is connected to solar panel edge.
Further, light body includes the chamber seat coordinated with supporting rod, and the fixed lamp chamber in chamber seat top, lamp chamber top is admittedly
Determine illumination region, illumination region includes lampshade and the identical LED lamp panel of two groups of structures, and two groups of LED lamp panel bottoms are connected separately with one
A temperature sensor being fixed on inside lamp chamber.
Further, lamp holder upper casing inner wall is provided with wireless remote control module.
Further, battery pack includes accumulator and reserve battery, and accumulator is ferric phosphate lithium cell, and reserve battery is manganese
Zinc battery.
Further, there are one ultrasonic insects expelling devices for the setting of chamber seat surrounding.
Further, lamp chamber surrounding encirclement is provided with heat dissipating layer, and lampholder shell is formed using aluminium alloy compression casting and bottom
It is provided with heat sink.
The beneficial effects of the utility model are as follows：
1, the utility model controls rotary electric machine device by controller and is rotated around supporting rod by device of solar generating, together
When control device control lever length regulating device be adjusted at any time by the angle of solar panel, ensure solar panel begin
Eventually to receive sunlight closest to vertical state, and energy is stored using accumulator, realizes and utmostly utilize the energy, carry
High energy utilization rate, has saved the energy, and device of solar generating is only provided with one piece of solar panel, cost-effective, into
One step has saved cost.
2, the electric energy storage device of the utility model uses lithium iron phosphate storage battery, for traditional lead accumulator,
Service life cycle is high, efficiently solves the problems, such as that lead accumulator service life is short, without being safeguarded at any time to power unit and more
It changes, greatly reduces the maintenance cost of battery, battery pack is additionally provided with reserve battery, standby when solar electric power supply system failure
Circuit is accessed with battery to be powered, and ensures that aeronautical light can be always on, this design reduces security risks.
3, the illumination region of the utility model is provided with multiple LED lamp panels, and general only there are one LED lamp panels to shine, as the LED
When the temperature sensor of lamp plate detects that temperature is more than 75 DEG C, the circuit that controller controls the LED lamp panel disconnects and controls other
LED light start to shine, it reduce the probability of damage of entire illumination region lamp, and the service life of entire aeronautical light is allowed to increase, into
One step reduces security risk.
4, the utility model is formed using aluminium alloy compression casting due to lamp holder shell, and heat sink is arranged at good heat conduction effect, lamp holder bottom,
Lamp chamber surrounding also has one layer of heat dissipating layer, makes entire aeronautical light heat dissipation effect and antiageing effect more preferably, and what is be arranged on chamber seat is super
Sound wave device for expelling mosquitos, which also can effectively prevent mosquito, causes aviation lamp wiring weak.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the structural schematic diagram of light body；
Fig. 3 is the structural schematic diagram of device of solar generating；
Reference numeral：1- light bodies, 1.1- chamber seats, 1.1.1- ultrasonic insects expelling devices, 1.2- lamp chambers, 1.2.1- heat dissipations
Layer, 1.3- illumination regions, 1.3.1-LED lamp plates, 1.3.2- lampshades, 1.4- temperature sensors, 2- device of solar generating, 2.1- turn
Rotating ring A, 2.2- supporting pad, 2.3- rotary electric machine devices, 2.4- telescopic devices, 2.4.1- telescopic rods, 2.4.2- limited blocks,
2.4.3- the long regulating mechanism of bar, 2.4.4- gyrators, 2.4.5- rotary sliders mechanism, 2.4.6- sliding rails, 2.5- keep set,
2.6- swivel beckets B, 2.7- bindiny mechanisms, 2.8- solar panels, 3- lamp holders, 3.1- battery packs, 3.1.1- accumulators,
3.1.2- reserve battery, 3.2- wireless remote control modules, 3.3- voltage limiters, 3.4- controllers, 3.5- heat sinks, 4- supporting rods.
Specific implementation mode
In order to which those skilled in the art are better understood from the utility model, below in conjunction with the accompanying drawings with following embodiment to this
Utility model is described in further detail.
Embodiment 1
As shown in Figure 1, the present embodiment provides a kind of swinging durable type solar energy aeronautical light, including lamp holder 3, under lamp holder 3
Shell inner wall is disposed with battery pack 3.1, voltage limiter 3.3 and controller 3.4 from left to right, and battery pack 3.1 includes accumulator
3.1.1,3 upper casing inner wall of lamp holder is provided with wireless remote control module 3.2, and lamp holder is provided with supporting rod 4 at 3 upper casing outer wall center, branch
The device of solar generating 2 that can be rotated around supporting rod 4 is provided on 4 anchor ring of strut, device of solar generating 2 includes that cooperation is being propped up
Be connected with below the swivel becket A2.1 that can be rotated around supporting rod 4 on strut 4, swivel becket A2.1 setting 3 upper casing outer wall of lamp holder can
With the supporting pad 2.2 of swivel becket A2.1 rotations, 2.2 lower section of supporting pad is connected with the rotary electric machine for being fixed on 3 upper casing inner wall of lamp holder
Device 2.3, fixed there are one telescopic device 2.4 on swivel becket A2.1 anchor rings, 2.4 other end of telescopic device is connected with solar-electricity
Pond plate 2.8, the tops swivel becket A2.1, which are connected with, is set in rotatable holding set 2.5 on supporting rod 4, and 2.5 top of set is kept to connect
It is connected to the swivel becket B2.6 that cooperation can rotate on supporting rod 4 around supporting rod 4, the connection sun is fixed on swivel becket B2.6 anchor rings
The bindiny mechanism 2.7 of energy solar panel 2.8,4 top of supporting rod is connected with light body 1.
Embodiment 2
As shown in Fig. 1 to 3, this implementation is further optimized on the basis of embodiment 1, specifically：
Telescopic device 2.4 includes telescopic rod 2.4.1, and telescopic rod 2.4.1 epimeres are fixed with limited block 2.4.2, telescopic rod
2.4.1 bottom is fixed on swivel becket A2.1 anchor rings and inside is fixed with the long regulating mechanism 2.4.3 of bar, the tops telescopic rod 2.4.1
Portion is provided with gyrator 2.4.4, and gyrator 2.4.4 is connected with rotary slider mechanism 2.4.5, rotary slider mechanism 2.4.5 cooperations
There are the sliding rail 2.4.6 for being fixed on 2.8 back side of solar panel, bindiny mechanism 2.7 to be connected to solar energy by revolute pair
2.8 edge of solar panel.
3 upper casing inner wall of lamp holder is provided with wireless remote control module 3.2.
Battery pack 3.1 includes accumulator 3.1.1 and reserve battery 3.1.2, and accumulator 3.1.1 is ferric phosphate lithium cell, standby
It is manganese-zinc battery with battery 3.1.2.
Abnormal signal can be sent to master control room by wireless remote control module 3.2, and wireless remote control module 3.2 also can be by controller
3.4 operation informations are sent to master control room, and the signal that master control room is sent out is fed back to controller 3.4 to be adjusted in real time
Control.
Embodiment 3
As shown in Fig. 1 to 3, the present embodiment is further optimized on the basis of embodiment 1, specifically：
Light body 1 includes the chamber seat 1.1 coordinated with supporting rod 4, the 1.1 fixed lamp chamber 1.2 in top of chamber seat, lamp chamber 1.2
The fixed illumination region 1.3 in top, illumination region 1.3 include lampshade 1.3.2 and two groups of structures identical LED lamp panel 1.3.1, two groups
The bottoms LED lamp panel 1.3.1 are separately connected that there are one be fixed on temperature sensor 1.4 inside lamp chamber 1.2.
There are one ultrasonic insects expelling device 1.1.1 for the setting of 1.1 surrounding of chamber seat.
The encirclement of 1.2 surrounding of lamp chamber is provided with heat dissipating layer 1.2.1, and 3 shell of lamp holder is formed using aluminium alloy compression casting and bottom
It is provided with heat sink 3.5.
Illumination region 1.3 is provided with multiple LED lamp panel 1.3.1, and general only there are one LED lamp panel 1.3.1 to shine, as the LED
When the temperature sensor 1.4 of lamp plate 1.3.1 detects that temperature is more than 75 DEG C, controller 3.4 controls the electricity of LED lamp panel 1.3.1
Road, which disconnects and controls other LED lamp panel 1.3.1, to be started to shine.
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 every specification and accompanying drawing content with the utility model
Structure change similarly should be included in the scope of protection of the utility model.
Claims (7)
1. a kind of swinging durable type solar energy aeronautical light, including lamp holder, which is characterized in that lamp holder (3) lower casing inner wall from a left side to
The right side is disposed with battery pack (3.1), voltage limiter (3.3) and controller (3.4), and battery pack (3.1) includes accumulator
(3.1.1) is provided with supporting rod (4) at lamp holder (3) upper casing outer wall center, and being fixed on supporting rod (4) anchor ring can be around supporting rod
(4) device of solar generating (2) rotated, device of solar generating (2) can be around supporting rods on supporting rod (4) including being fixed on
(4) the swivel becket A (2.1) rotated, be connected with below swivel becket A (2.1) setting lamp holder (3) upper casing outer wall can be with swivel becket A
(2.1) supporting pad (2.2) rotated, supporting pad (2.2) lower section are connected with the rotary electric machine dress for being fixed on lamp holder (3) upper casing inner wall
It sets (2.3), fixed there are one telescopic device (2.4) on swivel becket A (2.1) anchor ring, telescopic device (2.4) other end is connected with too
Positive energy solar panel (2.8), the tops swivel becket A (2.1) are connected with the guarantor that is set in and can be rotated around supporting rod (4) on supporting rod (4)
Set (2.5) is held, keeps being connected with the swivel becket B that is fixed on and can rotate around supporting rod (4) on supporting rod (4) above set (2.5)
(2.6), the bindiny mechanism (2.7) of connection solar panel (2.8), supporting rod (4) are fixed on swivel becket B (2.6) anchor ring
Top is connected with light body (1).
2. a kind of swinging durable type solar energy aeronautical light according to claim 1, which is characterized in that the light body
(1) include the chamber seat (1.1) coordinated with supporting rod (4), 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 (1.3.1) of two structures, often
A LED lamp panel (1.3.1) bottom is fixed on the internal temperature sensor (1.4) of lamp chamber (1.2) there are one all connecting.
3. a kind of swinging durable type solar energy aeronautical light according to claim 1, which is characterized in that the telescopic device
(2.4) include telescopic rod (2.4.1), telescopic rod (2.4.1) epimere is fixed with limited block (2.4.2), the bottom telescopic rod (2.4.1)
It is fixed on swivel becket A (2.1) anchor ring and inside is fixed with the long regulating mechanism of bar (2.4.3), set at the top of telescopic rod (2.4.1)
It is equipped with gyrator (2.4.4), gyrator (2.4.4) is connected with rotary slider mechanism (2.4.5), rotary slider mechanism (2.4.5)
It is combined with the sliding rail (2.4.6) for being fixed on solar panel (2.8) back side, bindiny mechanism (2.7) is connected by revolute pair
It is connected on solar panel (2.8) edge.
4. a kind of swinging durable type solar energy aeronautical light according to claim 1, which is characterized in that the lamp holder (3)
Upper casing inner wall is provided with wireless remote control module (3.2).
5. according to a kind of swinging durable type solar energy aeronautical light any one of in claims 1 to 3, feature exists
In the battery pack (3.1) includes accumulator (3.1.1) and reserve battery (3.1.2), and accumulator (3.1.1) is LiFePO4
Battery, reserve battery (3.1.2) are manganese-zinc battery.
6. a kind of swinging durable type solar energy aeronautical light according to claim 2, which is characterized in that chamber seat (1.1) four
There are one ultrasonic insects expelling devices (1.1.1) for setting on week.
7. a kind of swinging durable type solar energy aeronautical light according to claim 2, which is characterized in that lamp chamber (1.2) four
Week surrounds and is provided with heat dissipating layer (1.2.1), and lamp holder (3) shell is formed using aluminium alloy compression casting and bottom is provided with heat sink
(3.5)。
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820632096.7U CN208074840U (en) | 2018-04-28 | 2018-04-28 | A kind of swinging durable type solar energy aeronautical light |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820632096.7U CN208074840U (en) | 2018-04-28 | 2018-04-28 | A kind of swinging durable type solar energy aeronautical light |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208074840U true CN208074840U (en) | 2018-11-09 |
Family
ID=64045172
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820632096.7U Expired - Fee Related CN208074840U (en) | 2018-04-28 | 2018-04-28 | A kind of swinging durable type solar energy aeronautical light |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208074840U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20220012146A (en) * | 2020-07-22 | 2022-02-03 | 주식회사 신성일렉스 | System of solar type - obstacle light having battery cooling function |
-
2018
- 2018-04-28 CN CN201820632096.7U patent/CN208074840U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20220012146A (en) * | 2020-07-22 | 2022-02-03 | 주식회사 신성일렉스 | System of solar type - obstacle light having battery cooling function |
| KR102366924B1 (en) * | 2020-07-22 | 2022-02-24 | 주식회사 신성일렉스 | System of solar type - obstacle light having battery cooling function |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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: 20181109 Termination date: 20200428 |