CN207729452U - Solar energy aviation obstruction beacon - Google Patents
Solar energy aviation obstruction beacon Download PDFInfo
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- CN207729452U CN207729452U CN201721920589.2U CN201721920589U CN207729452U CN 207729452 U CN207729452 U CN 207729452U CN 201721920589 U CN201721920589 U CN 201721920589U CN 207729452 U CN207729452 U CN 207729452U
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- lamp body
- sensor
- control device
- aviation obstruction
- solar energy
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- 230000036413 temperature sense Effects 0.000 claims abstract description 35
- 239000005341 toughened glass Substances 0.000 claims description 12
- 230000001939 inductive effect Effects 0.000 claims description 7
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 4
- 239000004917 carbon fiber Substances 0.000 claims description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 4
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 5
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- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
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- 229910052799 carbon Inorganic materials 0.000 description 1
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- 238000006243 chemical reaction Methods 0.000 description 1
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- 238000005485 electric heating Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
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- 229910052724 xenon Inorganic materials 0.000 description 1
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- Circuit Arrangement For Electric Light Sources In General (AREA)
Abstract
The utility model is suitable for aviation obstruction beacon technical field, provides a kind of solar energy aviation obstruction beacon, including：Lamp body base, lamp body, solar panel and control device, lamp body are arranged in the top of lamp body base, and lamp body base is arranged in the top of control device, and solar panel is arranged in the side of control device；Solar energy aviation obstruction beacon further includes photoinduction sensor, temperature sense sensor and heater strip, and photoinduction sensor and temperature sense sensor are arranged on lamp body base, and heater strip is arranged in lamp body and on solar panel；The input terminal of control device is connect with photoinduction sensor and temperature sense sensor, and the output end of control device is connected with heater strip.The utility model heats solar panel and lampshade to control heater strip, to achieve the effect that snow removing, solves the problems, such as that solar energy aviation obstruction beacon can not work normally in the case of accumulated snow automatically by detecting temperature and light information outside lamp body.
Description
Technical field
The utility model belongs to aviation obstruction beacon technical field more particularly to a kind of solar energy aviation obstruction beacon.
Background technology
According to national standard, the skyscraper at 45 meters above ground level of top or more needs that aviation obstruction beacon is arranged, with aobvious
The profile of building is shown, to be served as a warning to the operator of aircraft.With the continuous development of technology, occur
Solar energy aviation obstruction beacon provides a kind of new technical solution for the powering mode of aviation obstruction beacon.Aviation obstruction beacon utilizes
Solar panel converts solar energy into electrical energy, to power for the lamp body of obstruction light.
However, the solar panel of traditional solar energy aviation obstruction beacon and the lampshade of obstruction light are usually all directly sudden and violent
In air, in the case of occurring accumulated snow in winter solar panel will be unable to work normally dew, while obstruction light is sent out
Light causes solar energy aviation obstruction beacon can not work normally since the covering of accumulated snow can not also blaze abroad, thus can not be right
The operator of aircraft serves as a warning.
Utility model content
In view of this, the utility model embodiment provides solar energy aviation obstruction beacon, to solve the sun in the prior art
The problem of energy aviation obstruction beacon can not work normally in the case of accumulated snow.
The utility model embodiment provides a kind of solar energy aviation obstruction beacon, including：Lamp body base, lamp body, solar energy
Solar panel and control device, the lamp body are arranged in the top of the lamp body base, and the lamp body base is arranged in control device
Top, the solar panel is arranged in the side of the control device；
It is characterized in that, further including photoinduction sensor, temperature sense sensor and heater strip, the photoinduction sensor
It is arranged on lamp body base with temperature sense sensor, the heater strip setting is in lamp body and on solar panel；Institute
The input terminal for stating control device is connect with the photoinduction sensor and the temperature sense sensor, the control device it is defeated
Outlet is connected with the heater strip, the light information and the acquisition of temperature sense sensor for receiving the acquisition of photoinduction sensor
Temperature information sends out corresponding control instruction according to the light information of reception and temperature information and is transferred to the heater strip.
Optionally, the control device includes：Micro-control unit and accumulator；The input terminal of the micro-control unit and institute
It states photoinduction sensor with temperature sense sensor to be connected, the output end of the micro-control unit is connected with the heater strip；Institute
The input terminal for stating accumulator is connected with the solar panel, the output end of the accumulator respectively with the lamp body, light sensation
Inductive sensing device, temperature sense sensor, heater strip are connected with micro-control unit.
Optionally, the lamp body includes：Lampshade and light emitting diode, the lampshade is located on the lamp body base, described
Light emitting diode is located in the cavity that the lampshade and the lamp body base are formed, and the heater strip is arranged in the lamp body base
Above and in the cavity.
Optionally, the junction of the lampshade and lamp body base is provided with waterproof grommet.
Optionally, the solar panel includes：Multiple solar battery sheets and setting are above solar battery sheet
Tempered glass, the solar battery sheet is horizontal alignment arrangement, between the adjacent edge of the solar battery sheet there are
Gap, the heater strip are arranged in tempered glass corresponding with the interstitial site of solar battery sheet.
Optionally, the heater strip is the low temperature silk of carbon fiber line.
Optionally, the output end of the control device is also connected with the light emitting diode, and the light emitting diode is used for
Receive the control instruction that the control device is sent out.
Optionally, the solar energy aviation obstruction beacon further includes range sensor, and the range sensor is arranged in lamp body
On pedestal, the output end of the range sensor is connected with the control device.
Optionally, the solar energy aviation obstruction beacon further includes micro alarm, and the micro alarm is arranged in lamp body
On pedestal, the input terminal of the micro alarm is connected with the control device.
Optionally, the solar energy aviation obstruction beacon further includes micro alarm, and the micro alarm is arranged in lamp body
On pedestal, the input terminal of the micro alarm is connected with the control device.
Existing advantageous effect is the utility model embodiment compared with prior art：By in solar energy aviation obstruction beacon
Lamp body base part setting photoinduction sensor detect whether aviation obstruction beacon glistens, while by hindering in solar energy aviation
Hinder the lamp body base part of lamp that temperature sense sensor is set to detect the temperature around lamp body, by being set below lamp body base
The temperature information that the light information and temperature sense sensor for setting control device to receive the acquisition of photoinduction sensor acquire, and root
Corresponding control instruction is sent out according to the light information and temperature information of reception, is arranged in lamp body and adding on solar panel
Heated filament is heated according to the instruction of reception to eliminate the accumulated snow on lampshade and solar panel, to solve in the prior art too
The problem of positive energy aviation obstruction beacon can not work normally in the case of accumulated snow.
Description of the drawings
It, below will be to embodiment or the prior art in order to illustrate more clearly of the technical scheme in the embodiment of the utility model
Attached drawing needed in description is briefly described, it should be apparent that, the accompanying drawings in the following description is only that this practicality is new
Some embodiments of type for those of ordinary skill in the art without having to pay creative labor, can be with
Obtain other attached drawings according to these attached drawings.
Fig. 1 is the dimensional structure diagram for the solar energy aviation obstruction beacon that the utility model embodiment provides；
Fig. 2 is the structure chart for the control device that the utility model embodiment provides；
Fig. 3 is a kind of structure chart for the lamp body base that the utility model embodiment provides；
Fig. 4 is the structural schematic diagram of heater strip in the lamp body of the utility model embodiment offer；
Fig. 5 is the structural exploded view for the solar panel that the utility model embodiment provides；
Fig. 6 is the vertical view for the solar panel that the utility model embodiment provides.
Specific implementation mode
In being described below, for illustration and not for limitation, it is proposed that such as tool of particular system structure, technology etc
Body details, to understand thoroughly the utility model embodiment.However, it will be clear to one skilled in the art that there is no these
The utility model can also be realized in the other embodiments of detail.In other situations, omit to well-known system,
The detailed description of apparatus, circuit and method, in case unnecessary details interferes the description of the utility model.
In order to illustrate technical solution described in the utility model, illustrated below by specific embodiment.
Referring to Fig. 1, a kind of dimensional structure diagram of solar energy aviation obstruction beacon is provided, details are as follows：
Solar energy aviation obstruction beacon includes lamp body base 101, lamp body 102, solar panel 103 and control device 104,
Lamp body 102 is arranged in the top of lamp body base 101, and lamp body base 101 is arranged in the top of control device 104, solar cell
Plate 103 is arranged in the side of control device 104, and solar panel is 45 degree to 60 with the angle on control device vertical direction
The section of degree so that solar panel 103 can preferably collect solar energy, and is converted into electric energy.
Wherein, solar energy aviation obstruction beacon further includes photoinduction sensor 105, temperature sense sensor 106 and heater strip,
Photoinduction sensor 105 and temperature sense sensor 106 are arranged on lamp body base 101, heater strip setting in lamp body 102 with
And on solar panel 103；The input terminal of control device 104 connects with photoinduction sensor 105 and temperature sense sensor 106
It connects, the output end of control device 104 is connected with heater strip, light information and temperature for receiving the acquisition of photoinduction sensor 105
The temperature information that inductive pick-up 106 acquires is spent, corresponding control instruction is sent out according to the light information of reception and temperature information
And it is transferred to heater strip.
In addition, plant bottom case 107 is additionally provided in the lower section of control device 104, so that control device 104 and ground
There are a certain distance so that control device 104 is not contacted with ground, is reduced control device 104 by the corrosion on ground, is extended dress
The service life set.
Utility model people has found in the process of implementing the utility model, the feelings of solar energy aviation obstruction beacon accumulated snow in winter
It can make under condition outside the lampshade of aviation obstruction beacon and there is accumulated snow the outside of solar panel, and blocking due to accumulated snow,
Solar panel will be unable to work normally, or even battery hot spot effect occurs, damage solar panel；Aviation obstruction beacon is sent out simultaneously
Light will also be blocked by accumulated snow, to can not be played a warning role to the operator of aircraft.
The utility model passes through photoinduction by the way that photoinduction sensor and temperature sense sensor are arranged on lamp body base
Sensor and temperature sense sensor detect the light information and ambient temperature information outside lamp body, and are arranged control device receipts
Collect light information and ambient temperature information, and the information of reception is handled, when control device is not received by light information,
Simultaneously when the temperature information of reception is less than preset value, control device sends out control instruction to heating wire so that heating wire starts
Heating, to eliminate the accumulated snow outside the accumulated snow and solar panel outside lamp body.
Optionally, referring to Fig. 2, show that the composition figure of control device 104, control device 104 include micro-control unit
1041 and accumulator 1042；The input terminal of micro-control unit 1041 and 106 phase of photoinduction sensor 105 and temperature sense sensor
Even, the output end of micro-control unit 1041 is connected with heater strip；The input terminal of accumulator 1042 and 103 phase of solar panel
Even, the output end of accumulator 1042 respectively with the lamp body 102, photoinduction sensor 105, temperature sense sensor 106, heating
Silk is connected with micro-control unit 1041.
Wherein, control device 104 includes 1,042 two parts of micro-control unit 1041 and accumulator, micro-control unit 1041
The information acquired for receiving photoinduction sensor 105 and temperature sense sensor 106, and the information of reception is identified and
Judge, judges whether current state is in the state of snow cover.
The course of work of photoinduction sensor 105 and temperature sense sensor 106 is as follows：Photoinduction sensor 105 is being examined
When measuring optical signal, electric signal can be converted optical signals to and be transferred in control device 104 micro-control unit 1041；Temperature
Infrared temperature sensor may be used in inductive pick-up 106, and infrared temperature sensor can incude the temperature of surrounding, when object
When temperature is higher than absolute zero, infra-red radiation is will produce, and infra-red radiation caused by object is related with the temperature of object,
Temperature is higher, and infra-red radiation is stronger, and infrared temperature sensor will produce corresponding electricity after receiving these infrared radiation signals
Signal, and the micro-control unit 1041 being transferred in device 104 processed, micro-control unit 1041 judge further according to the electric signal of reception
Ambient condition.
Referring to Fig. 3, show that photoinduction sensor and temperature sense sensor in a kind of facilities of lamp body base, are
The accuracy for ensuring the light information and temperature information of photoinduction sensor and the detection of temperature sense sensor, here in lamp body
Two photoinduction sensors and temperature sense sensor are respectively provided on pedestal.Wherein, photoinduction sensor 1051 and 1052
It is separately positioned in the horizontal direction of lamp holder, temperature sense sensor 1061 and 1062 is separately positioned on the vertical direction of lamp holder
On.It is readily comprehensible, it is only here a kind of embodiment for the setting of the quantity of sensor and position, rather than limit it
It is fixed.
Illustratively, the micro-control unit 1041 of control device 104 judges current environment shape according to the electric signal of reception
The process of state is：The signal of dull thread is sent out when micro-control unit 1041 continuously receives photoinduction sensor 1051 and 1052,
Temperature sense sensor 1061 and 1062 is received simultaneously when sending out the signal less than 0 degree Celsius, then judges that current environment is
It is covered with the state of accumulated snow, and sends out the signal of heating to heater strip；When micro-control unit 1041 continuously receives light sensation inductive sensing
One in device 1051 and 1052 sends out the signal of dull thread, at the same receive in temperature sense sensor 1061 and 1062 one
When a signal for sending out 30 degrees centigrades, then judge that current environment rests on for organism near obstruction light, and sends out corresponding
Signal；When micro-control unit 1041 continuously receives a letter for sending out dull thread in photoinduction sensor 1051 and 1052
Number, while when receiving one in temperature sense sensor 1061 or 1062 signal sent out less than 0 degree Celsius, then judging to work as
Preceding environment is snowy state, and acquiescence snow can melt automatically, without sending the signal of heating to heater strip.
In addition, the effect of the accumulator 1042 in control device 104 is to store the electricity that solar panel 103 generates
Can, and shine for lamp body and provide electric energy in the luminous of night.Wherein, the output end of accumulator also with photoinduction sensor, temperature
Inductive pick-up, heater strip and in order to control unit be connected, for providing electric energy for its normal work.
Optionally, referring to Fig. 4, lamp body includes：Lampshade 401 and light emitting diode, lampshade are located on lamp body base, and luminous two
Pole pipe is located in the cavity that the lampshade and the lamp body base are formed, and heater strip 402 is arranged on lamp body base and is located at chamber
In body.Heater strip is connected by conducting wire 403 with control device again.
In order to enable heater strip can quickly eliminate the accumulated snow outside lampshade, herein by heater strip with continuous U-typed shape
State is evenly distributed on close to the side of lampshade, increases the calorific value of heater strip by the way that heating wire is arranged to U-typed shape.It is logical
Cross the side that heater strip is positioned close to lampshade so that preferentially conduction comes the heat that heater strip generates to close to the side of lampshade
The accumulated snow on lampshade is eliminated, for example, heater strip, close to lampshade inner wall, the maximum distance between heater strip and lampshade is less than threshold value,
Such as the threshold value can be 1/10th of the diameter at the lampshade cylinder.
Readily comprehensible, the setting herein for heater strip shape and position is only a kind of embodiment, rather than to it
It limits.The present embodiment is used as light source, LED light and traditional xenon using light emitting diode (Light Emitting Diode, LED)
Gas lamp pipe is compared, and has the advantages that service life is long, low in energy consumption.
Optionally, the junction of lampshade and lamp body base is provided with waterproof grommet.By in lampshade and Shade base
Junction is arranged waterproof grommet and is flowed into lampshade come rainwater when avoiding sleety weather, and prevents in accumulated snow by adding
Heated filament adds thermogenetic rainwater to be flowed into lamp body on lampshade, causes the damage of circuit in lamp body, to extend aviation obstruction beacon
Service life.
Optionally, solar panel includes：Multiple solar battery sheets and the steel being arranged above solar battery sheet
Change glass, the solar battery sheet is arranged for horizontal alignment, and there are gap, institutes between the adjacent edge of the solar battery sheet
Heater strip is stated to be arranged in tempered glass corresponding with the interstitial site of solar battery sheet.
Referring to Fig. 5, the structural exploded view of solar panel is shown, wherein solar panel includes front tempering
Glass 501 and back side tempered glass 505, EVA encapsulated layers 502 and 504 and solar battery sheet 503.Front tempered glass 501
It is directly contacted with sunlight, sunlight penetrates front tempered glass 501 and EVA encapsulated layers 502, on solar battery sheet 503
Convert light energy into electric energy.Wherein, heater strip is printed in front tempered glass 501, and close to the outer surface of glass, therefore is added
Temperature will preferentially be transmitted to the outer surface of accumulated snow when hot.For example, when the thickness of front tempered glass is 4 to 6 millimeters, then add
Heated filament can be positioned close to 1 millimeter to 1.5 millimeters of glass outer surface.
Referring to Fig. 6, the vertical view of solar panel is shown.Wherein 601 indicate to be printed in the tempered glass of front
Heater strip, 602 indicate solar battery sheet.Illustratively, the arrangement of the solar battery sheet of 3 rows 5 row is given here
Mode, solar battery sheet forms the spread pattern of 3 rows 5 row by way of serial or parallel connection, in every two row or every two
It all can there are certain gaps between the solar battery sheet of row.Here we using in tempered glass between cell piece between
Heater strip is arranged in gap corresponding position, to avoid heater strip from influencing the power generation of solar battery sheet.It is shown in the figure one
Kind utilizes the case where gap setting heater strip between two row cell pieces, can additionally utilize the gap between two row cell pieces
Heater strip is set, does not do specific restriction here.
Optionally, heater strip is the low temperature silk of carbon fiber line.The low temperature silk of carbon fiber line is a kind of heating wire of threadiness,
It is a kind of new material with electricity, mechanics and thermal property, has the characteristics that stability, long lifespan and thermal conversion rate are high.
Due to the effect of carbon molecules, heating wire surface is enabled to be brought rapidly up.
Herein, because the minimum softening temperature of EVA is 70 DEG C in EVA encapsulated layers, the heating temperature range of heater strip can be with
0 DEG C -70 DEG C are set as, to ensure heater strip during heating, internal surface temperature does not exceed 70 DEG C.It is tested by experiment
Card, when heater strip temperature reaches 70 DEG C, temperature sense Sensor monitoring reaches 55 DEG C to external temperature, continuous heating 1-4
Minute can reach the purpose of snow removing, the 6-10 minutes purposes that can reach deicing of continuous heating.
Optionally, the output end of control device is also connected with the light emitting diode, and the light emitting diode is for receiving
The control instruction that the control device is sent out.
The solar energy aviation obstruction beacon that the utility model embodiment provides, which also has, has monitored whether that organism falls in lamp body
On the sensor of pedestal.Illustratively, when micro-control unit 1041 continuously receives one in photoinduction sensor 1051 and 1052
It is a to send out the signal of dull thread, while receiving one in temperature sense sensor 1061 and 1062 and sending out 30 degrees centigrades
Signal when, then judge that current environment rests on for organism near obstruction light, micro-control unit 1041, which is sent out, at this time drives life
The signal of object is to light emitting diode so that and LED flash certain period of time is to drive organism, in case organism exists
Excrement is left on lamp body base, ensures that photoinduction sensor and temperature sense sensor can be with the temperature of normal acquisition lamp body attachment
Information and light information.Certainly, such situation assumes that the obstruction light is in non-24 hours operating modes, when obstruction light is in
When 24 hours operating modes, obstruction light, which will be in, persistently flickers state, and also there will be no organisms to rest near obstruction light
.
Optionally, solar energy aviation obstruction beacon further includes range sensor, and the range sensor is arranged in lamp body base
On, the output end of the range sensor is connected with the control device.
It is additionally provided with range sensor in the aviation obstruction beacon that the utility model embodiment provides, and by the Distance-sensing
Device is also disposed on lamp body base, and the object around moved is detected at a distance from obstruction light by range sensor, and will inspection
The signal of survey is sent to control device, and the micro-control unit in control device is sent out for analyzing received signal
Corresponding instruction.
Optionally, solar energy aviation obstruction beacon further includes micro alarm, and the micro alarm is arranged in lamp body base
On, the input terminal of the micro alarm is connected with the control device.
When the signal that the micro-control unit in control device analyzes the range sensor of reception is less than preset value, then
Control signal is sent out to micro alarm so that alarm sends out sound-light alarm information, to remind the operator of aircraft so that
The function of the solar energy aviation obstruction beacon is more comprehensive, can not melt in the external accumulated snow of aviation obstruction beacon and aviation is caused to hinder
When hindering lamp that can not work temporarily, the operator of aircraft is reminded.
Optionally, referring to Fig. 1, lamp body top, which is provided with to take shelter from the thunder, fills 108.One can be played by the way that lightning arrester 108 is arranged
Fixed lightning protection effect, reduces the risk that aviation obstruction beacon is damaged by thunder and lightning.
Above-mentioned solar energy aviation obstruction beacon, by the way that photoinduction sensor and temperature sense sensor are arranged on lamp body base
Setting, the light information and ambient temperature information outside lamp body are detected by photoinduction sensor and temperature sense sensor,
And control device is set and collects light information and ambient temperature information, and the information of reception is handled, when control device does not have
Light information is received, while when the temperature information of reception is less than preset value, control device sends out control instruction to electric heating
Silk so that heating wire is begun to warm up, to eliminate the accumulated snow outside the accumulated snow and solar panel outside lamp body, and meanwhile it is described
Obstruction light sends out the sound and the functions such as waterproof, lightning-arrest of alarm when detecting object close to obstruction light, to extend barrier
Hinder the service life of lamp.
It is apparent to those skilled in the art that for convenience of description and succinctly, only with above-mentioned each work(
Can module division progress for example, in practical application, can be as needed and by above-mentioned function distribution by different functions
Unit, module are completed, i.e., the internal structure of described device are divided into different functional units or module, to complete above description
All or part of function.Can be that each unit physically exists alone in embodiment, it can also two or more lists
Member is integrated in a unit, and the form that hardware had both may be used in above-mentioned integrated unit is realized, software function can also be used
The form of unit is realized.In addition, the specific name of each functional unit, module is also only to facilitate mutually differentiation, is not used to
Limit the protection domain of the application.The specific work process of module in above-described embodiment can refer to pair in previous embodiment
Process is answered, details are not described herein.
Those of ordinary skill in the art may realize that moulds described in conjunction with the examples disclosed in the embodiments of the present disclosure
Block can be realized with the combination of electronic hardware or computer software and electronic hardware.These functions actually with hardware still
Software mode executes, and depends on the specific application and design constraint of technical solution.Professional technician can be to each
It is specific to apply to use different methods to achieve the described function, but this realization is it is not considered that exceed the utility model
Range.
In embodiment provided by the utility model, it should be understood that disclosed device, it can be by others side
Formula is realized.For example, the apparatus embodiments described above are merely exemplary, for example, the division of the module, only one
Kind of division of logic function, formula that in actual implementation, there may be another division manner, such as multiple units or component can combine or
It is desirably integrated into another system, or some features can be ignored or not executed.Another point, it is shown or discussed it is mutual it
Between coupling or direct-coupling or communication connection can be by some interfaces, the INDIRECT COUPLING or communication of device or unit connect
It connects, can be electrical, machinery or other forms.
The unit illustrated as separating component may or may not be physically separated, aobvious as unit
The component shown may or may not be physical unit, you can be located at a place, or may be distributed over multiple
In network element.Some or all of unit therein can be selected according to the actual needs to realize the mesh of this embodiment scheme
's.
In addition, can be that each unit physically exists alone in each embodiment of utility model, it can also be two or two
During a above unit is integrated in one unit.The form that hardware had both may be used in above-mentioned integrated unit is realized, can also be used
The form of SFU software functional unit is realized.
Embodiment described above is only to illustrate the technical solution of utility model, rather than its limitations；Although with reference to aforementioned
The utility model is described in detail in embodiment, it will be understood by those of ordinary skill in the art that：It still can be right
Technical solution recorded in foregoing embodiments is modified or equivalent replacement of some of the technical features；And this
A little modification or replacements, various embodiments of the utility model technical solution that it does not separate the essence of the corresponding technical solution spirit and
Range should be included within the scope of protection of this utility model.
Claims (10)
1. a kind of solar energy aviation obstruction beacon, including：Lamp body base, lamp body, solar panel and control device, the lamp body
It is arranged in the top of the lamp body base, the lamp body base is arranged in the top of control device, and the solar panel is set
It sets in the side of the control device；
It is characterized in that, further include photoinduction sensor, temperature sense sensor and heater strip, the photoinduction sensor and temperature
It spends inductive pick-up to be arranged on lamp body base, the heater strip setting is in lamp body and on solar panel；
The input terminal of the control device is connect with the photoinduction sensor and the temperature sense sensor, the control dress
The output end set is connected with the heater strip, and the control device is used to receive the light information and temperature of photoinduction sensor acquisition
The temperature information for spending inductive pick-up acquisition, sends out corresponding control instruction according to the light information of reception and temperature information and passes
It is defeated by the heater strip.
2. solar energy aviation obstruction beacon as described in claim 1, which is characterized in that the control device includes：Microcontroller list
Member and accumulator；The input terminal of the micro-control unit is connected with the photoinduction sensor and temperature sense sensor, described
The output end of micro-control unit is connected with the heater strip；The input terminal of the accumulator is connected with the solar panel,
The output end of the accumulator respectively with the lamp body, photoinduction sensor, temperature sense sensor, heater strip and microcontroller list
Member is connected.
3. solar energy aviation obstruction beacon as described in claim 1, which is characterized in that the lamp body includes：Lampshade and luminous two
Pole pipe, the lampshade are located on the lamp body base, and the light emitting diode is located at the lampshade and the lamp body base is formed
Cavity in, the heater strip is arranged on the lamp body base and in the cavity.
4. solar energy aviation obstruction beacon as claimed in claim 3, which is characterized in that the junction of the lampshade and lamp body base
It is provided with waterproof grommet.
5. solar energy aviation obstruction beacon as described in claim 1, which is characterized in that the solar panel includes：It is multiple
Solar battery sheet and the tempered glass being arranged above solar battery sheet, the solar battery sheet are arranged for horizontal alignment
Cloth, there are gaps, the heater strip to be arranged in the gap with solar battery sheet between the adjacent edge of the solar battery sheet
In the corresponding tempered glass in position.
6. solar energy aviation obstruction beacon as described in claim 1, which is characterized in that the heater strip is the low temperature of carbon fiber line
Silk.
7. solar energy aviation obstruction beacon as claimed in claim 3, which is characterized in that the output end of the control device also with institute
It states light emitting diode to be connected, the light emitting diode is for receiving the control instruction that the control device is sent out.
8. solar energy aviation obstruction beacon as described in claim 1, which is characterized in that the solar energy aviation obstruction beacon further includes
Range sensor, the range sensor are arranged on lamp body base, and the output end of the range sensor is filled with the control
It sets connected.
9. solar energy aviation obstruction beacon as described in claim 1, which is characterized in that the solar energy aviation obstruction beacon further includes
Micro alarm, the micro alarm are arranged on lamp body base, and the input terminal of the micro alarm is filled with the control
It sets connected.
10. such as claim 1-9 any one of them solar energy aviation obstruction beacons, which is characterized in that setting above the lamp body
There is lightning arrester.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201721920589.2U CN207729452U (en) | 2017-12-30 | 2017-12-30 | Solar energy aviation obstruction beacon |
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| CN201721920589.2U CN207729452U (en) | 2017-12-30 | 2017-12-30 | Solar energy aviation obstruction beacon |
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| CN207729452U true CN207729452U (en) | 2018-08-14 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108105706A (en) * | 2017-12-30 | 2018-06-01 | 英利能源（中国）有限公司 | Solar energy aviation obstruction beacon |
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2017
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108105706A (en) * | 2017-12-30 | 2018-06-01 | 英利能源（中国）有限公司 | Solar energy aviation obstruction beacon |
| CN108105706B (en) * | 2017-12-30 | 2024-04-05 | 英利能源（中国）有限公司 | Solar aviation obstruction light |
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