CN104832864B - A kind of solar energy aero-obstruction lantern with low light intensity - Google Patents
A kind of solar energy aero-obstruction lantern with low light intensity Download PDFInfo
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- CN104832864B CN104832864B CN201510153840.6A CN201510153840A CN104832864B CN 104832864 B CN104832864 B CN 104832864B CN 201510153840 A CN201510153840 A CN 201510153840A CN 104832864 B CN104832864 B CN 104832864B
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- column
- solar panels
- circuit plate
- battery
- mcu microprocessor
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- 238000000034 method Methods 0.000 claims description 11
- 201000009310 astigmatism Diseases 0.000 claims description 7
- 230000005611 electricity Effects 0.000 claims description 7
- 238000007789 sealing Methods 0.000 claims description 6
- 238000012545 processing Methods 0.000 claims description 4
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 238000009826 distribution Methods 0.000 claims description 3
- 238000001125 extrusion Methods 0.000 claims description 3
- 238000007689 inspection Methods 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
- 238000005265 energy consumption Methods 0.000 description 4
- 238000009434 installation Methods 0.000 description 4
- 238000004146 energy storage Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000005530 etching Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- 206010054949 Metaplasia Diseases 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 229910052736 halogen Inorganic materials 0.000 description 1
- 150000002367 halogens Chemical class 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000015689 metaplastic ossification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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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 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21S—NON-PORTABLE LIGHTING DEVICES; SYSTEMS THEREOF; VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLE EXTERIORS
- F21S9/00—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply
- F21S9/02—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply the power supply being a battery or accumulator
- F21S9/03—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply the power supply being a battery or accumulator rechargeable by exposure to light
- F21S9/037—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply the power supply being a battery or accumulator rechargeable by exposure to light the solar unit and the lighting unit being located within or on the same housing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V23/00—Arrangement of electric circuit elements in or on lighting devices
- F21V23/003—Arrangement of electric circuit elements in or on lighting devices the elements being electronics drivers or controllers for operating the light source, e.g. for a LED array
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V5/00—Refractors for light sources
- F21V5/04—Refractors for light sources of lens shape
- F21V5/045—Refractors for light sources of lens shape the lens having discontinuous faces, e.g. Fresnel lenses
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21W—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
- F21W2111/00—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00
- F21W2111/06—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00 for aircraft runways or the like
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Non-Portable Lighting Devices Or Systems Thereof (AREA)
- Arrangement Of Elements, Cooling, Sealing, Or The Like Of Lighting Devices (AREA)
Abstract
The invention discloses a kind of solar energy aero-obstruction lantern with low light intensity, including Transparent lamp shade, lamp body and lamp holder, Fresnel Lenses is distributed on Transparent lamp shade, Transparent lamp shade top surface is provided with a main solar panels；Lamp body is located in Transparent lamp shade, lamp body includes column, illuminator and mounting platform, LED drive circuit plate is provided at the top of column, column bottom is provided with charging control circuit plate and battery management circuit plate, and column side is equipped with illuminator, and illuminator is located at the focal point of Fresnel Lenses, column is connect with plane on mounting platform, and mounting platform side is equipped with from solar panels；Lamp body is fixed on lamp holder, and two groups of battery packs are provided in lamp holder；Aviation obstruction beacon further includes MCU microprocessor, and MCU microprocessor connects and control main solar panels, from solar panels, charging control circuit plate and battery management circuit plate, and battery pack, LED drive circuit plate and illuminator.Solar energy aero-obstruction lantern with low light intensity light source utilization rate of the invention is high, long service life.
Description
Technical field
The present invention relates to aeronautical beacon technical field more particularly to a kind of solar energy aero-obstruction lantern with low light intensity.
Background technique
Aero-obstruction lantern with low light intensity is usually mounted to high building, chimney, steel tower, vehicle or other moving obstacles etc. in airport
The place to serve as warning to aircraft.
Traditional aviation obstruction beacon is almost without the optical system or only simple optical system for being directed to LED light source, light ease
It dissipates greatly, light utilization efficiency is low, and can see light on the unnecessary ground of upper and lower, causes light pollution；Traditional aviation obstruction beacon
Incandescent lamp and Metal halogen lamp are generally used, that there are luminous efficiencies is low for these light sources, and energy consumption is high, and the service life is short, lamp body volume, weight
Disadvantage bigger than normal.LED light source body is as fourth generation of new light source, and using low-voltage power supply, low energy consumption, and luminous efficiency is high, display,
The every field such as backlight, general lighting and urban landscape lamp are widely applied, but LED aviation obstruction beacon used at present
It is bad that there are still uniformities, the low problem of light source utilization rate.
In addition, used by traditional aviation obstruction beacon being shone by electric wire supply of electrical energy, installation procedure is not only increased,
Also bring the loss of electricity and the waste of the energy.Solar energy is a kind of Novel clean renewable energy.Use to solar energy,
Sunlight usually is received by solar panels, converts electric energy for the luminous energy of sunlight.Traditional solar energy aviation obstruction beacon
Used is external solar panels, and solar panels are directly exposed to air, and after prolonged use, can bring ash
The bulk deposition of dirt and different degrees of corrosion, influence the service life of solar panels；In addition, traditional solar energy flying obstacle
Lamp is much higher than the charge mode of cell voltage using solar panels output voltage, is able to satisfy in the morning or not rainy days and fills
Electricity requires.
Summary of the invention
In order to solve the problems in the prior art, high, service life that the object of the present invention is to provide a kind of light source utilization rates
Solar energy aero-obstruction lantern with low light intensity long, performance is stable.
The technical solution adopted by the present invention: a kind of solar energy aero-obstruction lantern with low light intensity, including Transparent lamp shade, lamp body and lamp
Seat, the lamp body are arranged on lamp holder, and the Transparent lamp shade covers lamp body, and is detachably mounted on lamp holder, special
Sign is, Fresnel Lenses is distributed on the Transparent lamp shade, and the Transparent lamp shade inside top surface is provided with a main sun
It can plate；The lamp body includes column, illuminator and mounting platform, is provided with LED drive circuit plate, institute at the top of the column
The column bottom stated is provided with charging control circuit plate and battery management circuit plate, and the column side is equipped with illuminator,
The illuminator is located at the focal point of the Fresnel Lenses, and plane connects on the column and mounting platform, described
Mounting platform is trapezoid platform, and the trapezoid platform side is equipped with from solar panels；The lamp body passes through mounting platform
It is fixed on lamp holder, two groups of battery packs is provided in the lamp holder；The aviation obstruction beacon further includes MCU microprocessor,
The MCU microprocessor connects and controls the main solar panels, from solar panels, charging control circuit plate, cell tube
Circuit board, battery pack, LED drive circuit plate and illuminator are managed, guarantees the normal operation of aviation obstruction beacon.
Preferably, the Fresnel Lenses is in rotationally symmetrical distribution on Transparent lamp shade.
Preferably, the illuminator is LED light.
Wherein, the column is polyhedron column, and the polyhedron column forms for Extrusion Process of Aluminum Alloy Profile, and described is more
Face body column is hexahedron column, octahedra column, decahedron column, dodecahedron column or ten hexahedron columns.
Wherein, the solar panels that the main solar panels of Transparent lamp shade inside top surface setting are 5V/1.8W.
Wherein, the column is fixed on mounting platform using 4 screws.
Wherein, the LED drive circuit plate is the drive circuit board of current constant control and PID closed-loop control.
Wherein, the Transparent lamp shade and lamp holder junction are provided with capillary groove and water-proof sealing strip.
Wherein, the lamp holder lower end is provided with bottom plate, is provided with water-proof sealing strip between the lamp holder and bottom plate.
Wherein, the charging control circuit plate is invariable power charging control circuit plate.
Wherein, the Transparent lamp shade and pedestal have anti-dropout wirerope.
Wherein, astigmatism nicking is additionally provided in the Transparent lamp shade.
Wherein, the LED light is 3528,5050,5630,5730 or CP7P type patch.
Wherein, the solar energy aero-obstruction lantern with low light intensity further includes warning note unit.
Compared with prior art, the present invention realize the utility model has the advantages that solar energy aero-obstruction lantern with low light intensity of the invention will
LED light is set in the focus of Fresnel Lenses, and it is flat that the light that LED light issues is polymerized to an approximation after Fresnel Lenses reflects
Row light belt, eliminates light pollution, improves luminous efficiency；Solar energy aero-obstruction lantern with low light intensity of the invention is by five solar energy
Plate is mounted in Transparent lamp shade, on the one hand advantageously accounts for the dust-proof problem of solar energy and solar panels are directly exposed to air band
The etching problem come, the astigmatism nicking that another aspect Transparent lamp shade inside is arranged is optically focused lines, is conducive to external irradiation
Light reaches bigger energy on solar panels；What solar energy aero-obstruction lantern with low light intensity of the invention was arranged on column
LED light is LED patch, low in energy consumption, small in size, is easily installed and safeguards；Solar energy aero-obstruction lantern with low light intensity of the invention is adopted
With invariable power charge mode, the charge mode bring disadvantage that traditional solar panels are much higher than cell voltage with output voltage is avoided
End, it is ensured that solar panels are in the morning and rainy days may be battery charging, improve the utilization rate of solar energy；This hair
Bright solar energy aero-obstruction lantern with low light intensity uses double cell mode, and one group of battery is in operating mode, and another group of battery is in
Charge mode avoids battery because only using part electric energy for a long time and causing to store up by the handover management of MCU microprocessor
The harm that energy function reduces；Solar energy aero-obstruction lantern with low light intensity of the invention drives Fresnel Lenses, LED light, column, LED
Dynamic circuit board, charging control circuit plate and battery management circuit plate are effectively bonded together, it is ensured that production installation accuracy, drop
The low complexity of technique；Solar energy aero-obstruction lantern with low light intensity of the invention controls solar panels using MCU microprocessor,
Battery pack and the triangular charge and discharge process of LED light, the job stability that the charge efficiency and LED for improving solar energy use.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, present invention be described in more detail:
Fig. 1 is the structural schematic diagram of aviation obstruction beacon of the invention；
Fig. 2 is the sectional view in the direction aviation obstruction beacon A-A of the invention；
Fig. 3 is the cross-sectional view of aviation obstruction beacon column of the invention；
Fig. 4 is the operation schematic diagram of the MCU microprocessor of aviation obstruction beacon of the invention；
Fig. 5 is the MCU microprocessor of aviation obstruction beacon of the invention and the annexation figure of solar panels；
Fig. 6 is the MCU microprocessor of aviation obstruction beacon of the invention and the annexation figure of battery pack.
Specific embodiment
Such as Fig. 1, shown in 2,3, a kind of solar energy aero-obstruction lantern with low light intensity, including Transparent lamp shade 1, lamp body and lamp holder 2, institute
The lamp body stated is arranged on lamp holder 2, and the Transparent lamp shade 1 covers lamp body, and is detachably mounted on lamp holder 2, feature
It is, Fresnel Lenses 3 is distributed on the Transparent lamp shade 1, and 1 inside top surface of Transparent lamp shade is provided with a main sun
It can plate 4；The lamp body includes column 6, illuminator 11 and mounting platform 5, and LED driving electricity is provided at the top of the column 6
Road plate 7,6 bottom of column are provided with charging control circuit plate 14 and battery management circuit plate 12,6 side of column
Illuminator 11 is installed, the illuminator 11 is located at the focal point of the Fresnel Lenses 3, and the column 6 and installation are flat
Plane connects on platform 5, and the mounting platform 5 is trapezoid platform, and 5 side of trapezoid platform is equipped with from solar panels
15；The lamp body is fixed on lamp holder 2 by mounting platform 5, and two groups of battery packs 8 are provided in the lamp holder 2；Described
Aviation obstruction beacon further includes MCU microprocessor 9, and the MCU microprocessor 9 connects and control the main solar panels 4, from
Solar panels 15, charging control circuit plate 14, battery management circuit plate 12, battery pack 8, LED drive circuit plate 7 and illuminator
11, guarantee the normal operation of aviation obstruction beacon.
The Fresnel Lenses 3 is in rotationally symmetrical distribution on Transparent lamp shade 1.
The illuminator 11 is LED light.
The column 6 is polyhedron column, and the polyhedron column 6 is that Extrusion Process of Aluminum Alloy Profile stretches, described
Polyhedron column 6 is hexahedron column, octahedra column, decahedron column, dodecahedron column or ten hexahedron columns.
The column 6 is fixed on mounting platform 5 using 4 screws.
The LED drive circuit plate 7 is the drive circuit board of current constant control and PID closed-loop control.
The Transparent lamp shade 1 and 2 junction of lamp holder is provided with capillary groove and water-proof sealing strip.
2 lower end of lamp holder is provided with bottom plate 10, is provided with waterproof sealing between the lamp holder 2 and bottom plate 10
Item.
The charging control circuit plate 14 is invariable power charging control circuit plate.
As shown in figures 1 and 2, Fresnel Lenses 3 is distributed with outside Transparent lamp shade 1, LED light 11 is located at the focus of Fresnel Lenses 3
Place, the light that LED light 11 issues are polymerized to a less parallel light belt after the refraction of Fresnel Lenses 3, eliminate light pollution, improves
Luminous efficiency；It is provided with astigmatism nicking 13 in Transparent lamp shade 1, has the effect of optically focused, is conducive to the light of external irradiation,
The energy for reaching bigger is acted on solar panels by astigmatism nicking 13, improves the utilization rate of sunlight.Polyhedron
LED drive circuit plate 7 is provided at the top of column 6,6 bottom of column is provided with charging control circuit plate 14 and battery management circuit plate
12,6 side of column is equipped with LED light 11, and the circuit board of about 6 two end faces of polyhedron column is welded with LED light 11 respectively, protects
The consistency of lamp body is demonstrate,proved.LED light 11, polyhedron column 6, charging control circuit plate 14, battery management circuit plate 12, LED drive
The wick that dynamic circuit board 7 forms is located in Transparent lamp shade 1, and is fixed on lamp holder 2 by mounting platform 5, ensure that LED light 11
Reliable location simplifies the mounting process of aviation obstruction beacon in the focus of Fresnel Lenses 3, is advantageously implemented scale metaplasia
It produces.
As shown in figure 4, MCU microprocessor 9 and main solar panels 4, from solar panels 15, battery pack 8 and LED drive circuit
Plate 7 connect, main solar panels 4 and from solar panels 15 receive sunlight, convert electric energy for the luminous energy of sunlight, and transmit letter
Number give MCU microprocessor 9, MCU microprocessor 9 control main solar panels 4 and from solar panels 15 use boost charge mode pair
Battery pack 8 charges, and battery pack 8 issues voltage feedback signal to MCU microprocessor 9, and MCU microprocessor 9 is according to feedback letter
Number automatic switchover management is carried out, one group of battery pack is placed in charge mode, another group of battery pack is placed in operating mode, is in work
Electric energy needed for the battery pack of mode provides LED light 11.MCU microprocessor 9 is also connected with flash pattern unit, warning note list
Member, communication unit and GPS guarantee that solar energy aero-obstruction lantern with low light intensity of the invention is in normal operating conditions.
Such as the connection schematic diagram that Fig. 5 is aviation obstruction beacon MCU microprocessor and solar panels of the invention, the sun
Can plate include be arranged in Transparent lamp shade inside top surface main solar panels 4 and four groups of mounting platform side from solar panels 15,
The main solar panels 4 are 5V/1.8W, also can provide electric energy in rainy days or early morning for MCU microprocessor 9, ensure that
MCU microprocessor 9 controls the normal work that five groups of solar panels charge.Five groups of solar panels convert received luminous energy to
Electric energy, and voltage signal is passed into MCU microprocessor 9 respectively, to charging control circuit plate 14 after the processing of MCU microprocessor 9
Voltage up control signal is issued, charging control circuit plate 14 after signal processing, charges to battery pack 8, to realize yin
Rainy day or early morning solar panels also can be carried out the effect of charging.
Such as the connection schematic diagram that Fig. 6 is aviation obstruction beacon MCU microprocessor and battery pack of the invention.In master (from) sun
During energy plate is to battery pack charging, the charge circuit of battery pack 1 is rechargeable battery set in an ON state, battery pack 2
Charge circuit is in an off state, and is working battery group, and main (from) solar panels are anti-to the sending of MCU microprocessor 9 charging current
Feedback signal, MCU microprocessor 9 carry out signal processing, when detecting that charging current reaches maximum charging current, MCU micro process
Device 9 issues instruction, so that the charge circuit of battery pack 1 disconnects, becomes working battery group, the charge circuit of battery pack 2 is connected, become
At rechargeable battery set；Working battery group during providing electric energy for LED light 11, send out to MCU microprocessor 9 by working battery group
Voltage feedback signal out, when detecting that operating voltage reaches minimum voltage, MCU microprocessor 9 issues signal instruction, controls work
Become rechargeable battery set as battery pack, rechargeable battery set becomes working battery group.Repeatedly, in master (from) solar panels to electricity
During pond group charges, remain that one group of battery pack is in charge mode, another group of battery pack is in operating mode, avoids
The harm that battery pack causes energy storage function to decline because of part electric energy is only used for a long time.
The MCU microprocessor 9 that the present invention uses, control solar panels fill battery pack 8 using boost charge mode
Electricity, it is ensured that can also charge to battery pack 8 when rainy days or early morning, improve the utilization rate of solar energy.The present invention passes through
MCU microprocessor 9 automatically switch management, so that two groups of battery packs 8 is respectively at charge mode and operating mode, avoid battery because
The harm for causing energy-storage function to reduce to only use part electric energy for a long time.
LED light is set in the focus of Fresnel Lenses by solar energy aero-obstruction lantern with low light intensity of the invention, LED light hair
Light out is polymerized to a less parallel light belt after Fresnel Lenses reflects, and eliminates light pollution, improves luminous efficiency；This
Five solar panels are mounted in Transparent lamp shade by the solar energy aero-obstruction lantern with low light intensity of invention, are on the one hand advantageously accounted for too
The dust-proof problem of sun energy and solar panels are directly exposed to air bring etching problem, setting on the inside of another aspect Transparent lamp shade
Astigmatism nicking be optically focused lines, the light for being conducive to external irradiation reaches bigger energy on solar panels；The present invention
The LED light that is arranged on column of solar energy aero-obstruction lantern with low light intensity be LED patch, it is low in energy consumption, it is small in size, be easily installed with
Maintenance；Solar energy aero-obstruction lantern with low light intensity of the invention uses invariable power charge mode, avoids traditional solar panels with defeated
The drawbacks of voltage is brought much higher than the charge mode of cell voltage out, it is ensured that solar panels are in the morning and rainy days can also
Think that battery charges, improves the utilization rate of solar energy；Solar energy aero-obstruction lantern with low light intensity of the invention uses double cell mould
Formula, one group of battery are in operating mode, and another group of battery is in charge mode and is avoided by the handover management of MCU microprocessor
The harm that battery causes energy-storage function to reduce because of part electric energy is only used for a long time；The low light intensity boat of solar energy of the invention
Empty obstruction light is by Fresnel Lenses, LED light, column, LED drive circuit plate, charging control circuit plate and battery management circuit plate
It is effectively bonded together, it is ensured that production installation accuracy reduces the complexity of technique；The low light intensity of solar energy of the invention
Aviation obstruction beacon controls solar panels, battery pack and the triangular charge and discharge process of LED light using MCU microprocessor, improves
The job stability that the charge efficiency and LED of solar energy use.
The above specific embodiments are only exemplary, is to preferably make skilled artisans appreciate that originally
Patent, be not to be construed as include to this patent range limitation；As long as appointing made by the spirit according to disclosed in this patent
How with change or modification, the range that this patent includes is each fallen within.
Claims (7)
1. a kind of solar energy aero-obstruction lantern with low light intensity, including Transparent lamp shade (1), lamp body and lamp holder (2), the lamp body setting
On lamp holder (2), the Transparent lamp shade (1) covers lamp body, and is detachably mounted on lamp holder (2), which is characterized in that
It is distributed with Fresnel Lenses (3) on the Transparent lamp shade (1), the Transparent lamp shade (1) inside top surface is provided with one
Main solar panels (4)；
The lamp body includes column (6), illuminator (11) and mounting platform (5), is provided with LED at the top of the column (6)
Drive circuit board (7), the column (6) bottom are provided with charging control circuit plate (14) and battery management circuit plate (12),
Described column (6) side is equipped with illuminator (11), and the illuminator (11) is located at the focus of the Fresnel Lenses (3)
Place, the column (6) are connect with plane on mounting platform (5), and the mounting platform (5) is trapezoid platform, the ladder
Shape platform (5) side is equipped with from solar panels (15)；
The lamp body is fixed on lamp holder (2) by mounting platform (5), is provided with two groups of battery packs in the lamp holder (2)
(8)；
The aviation obstruction beacon further includes MCU microprocessor (9), and the MCU microprocessor (9) is connected and controlled described
Main solar panels (4), from solar panels (15), charging control circuit plate (14), battery management circuit plate (12), battery pack (8),
LED drive circuit plate (7) and illuminator (11), guarantee the normal operation of aviation obstruction beacon；
It is additionally provided with astigmatism nicking (13) in the Transparent lamp shade (1), the astigmatism nicking (13) is optically focused lines；
The Fresnel Lenses (3) is in rotationally symmetrical distribution on Transparent lamp shade (1)；
The charging control circuit plate is invariable power charging control circuit plate；
The aviation obstruction beacon further includes MCU microprocessor, the MCU microprocessor connect and control main solar panels, from
Solar panels, charging control circuit plate, battery management circuit plate, two groups of battery packs, LED drive circuit plate and illuminator；Master is too
It is positive plate and sunlight to be received from solar panels, electric energy is converted by the luminous energy of sunlight, and deliver a signal to MCU micro process
Device, MCU microprocessor are controlled main solar panels and are charged from solar panels using boost charge mode to battery pack, battery
Group issues voltage feedback signal to MCU microprocessor, and MCU microprocessor carries out automatic switchover management based on the feedback signal, by one
Group battery pack is placed in charge mode, and another group of battery pack is placed in operating mode, and the battery pack in operating mode provides illuminator
Required electric energy；Main solar panels and/or from solar panels to battery pack charge during, the charge circuit of battery pack 1
It in an ON state, is rechargeable battery set, the charge circuit of battery pack 2 is in an off state, and is working battery group, main solar energy
Plate and from solar panels to MCU microprocessor issue charging current feedback signal, MCU microprocessor carry out signal processing, work as inspection
When measuring charging current and reaching maximum charging current, MCU microprocessor issues instruction, so that the charge circuit of battery pack disconnects,
Become working battery group, the charge circuit of battery pack 2 is connected, and rechargeable battery set is become；Working battery group is providing electricity for LED light
During energy, working battery group issues voltage feedback signal to MCU microprocessor, when detecting that operating voltage reaches minimum electricity
When pressure, MCU microprocessor issues signal instruction, and control working battery group becomes rechargeable battery set, and rechargeable battery set becomes work
Battery pack.
2. a kind of solar energy aero-obstruction lantern with low light intensity as described in claim 1, which is characterized in that the illuminator (11)
For LED light.
3. a kind of solar energy aero-obstruction lantern with low light intensity as described in claim 1, which is characterized in that the column (6) is
Polyhedron column, the polyhedron column (6) form for Extrusion Process of Aluminum Alloy Profile, and the polyhedron column (6) is vertical for hexahedron
Column, octahedra column, decahedron column, dodecahedron column or ten hexahedron columns.
4. a kind of solar energy aero-obstruction lantern with low light intensity as described in claim 1, which is characterized in that the Transparent lamp shade
(1) solar panels that the main solar panels (4) of inside top surface setting are 5V/1.8W.
5. a kind of solar energy aero-obstruction lantern with low light intensity as described in claim 1, which is characterized in that the column (6) is adopted
It is fixed on mounting platform (5) with 4 screws.
6. a kind of solar energy aero-obstruction lantern with low light intensity as described in claim 1, which is characterized in that the Transparent lamp shade
(1) and lamp holder (2) junction is provided with capillary groove and water-proof sealing strip.
7. a kind of solar energy aero-obstruction lantern with low light intensity as described in claim 1, which is characterized in that under the lamp holder (2)
End is provided with bottom plate (10), is provided with water-proof sealing strip between the lamp holder (2) and bottom plate (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510153840.6A CN104832864B (en) | 2015-04-02 | 2015-04-02 | A kind of solar energy aero-obstruction lantern with low light intensity |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510153840.6A CN104832864B (en) | 2015-04-02 | 2015-04-02 | A kind of solar energy aero-obstruction lantern with low light intensity |
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| Publication Number | Publication Date |
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| CN104832864A CN104832864A (en) | 2015-08-12 |
| CN104832864B true CN104832864B (en) | 2019-08-09 |
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| CN201510153840.6A Expired - Fee Related CN104832864B (en) | 2015-04-02 | 2015-04-02 | A kind of solar energy aero-obstruction lantern with low light intensity |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN107830478A (en) * | 2017-09-27 | 2018-03-23 | 苏州城时实业有限公司 | Solar LED roadblock lamp manufacturing method |
| CN110307510A (en) * | 2019-06-21 | 2019-10-08 | 深圳星标科技股份有限公司 | Solar energy aviation obstruction beacon |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2004319198A (en) * | 2003-04-15 | 2004-11-11 | Kansai Electric Power Co Inc:The | Airplane warning light |
| CN202629889U (en) * | 2012-05-30 | 2012-12-26 | 上海复弗机电有限公司 | Solar energy aviation obstruction light |
| CN202660401U (en) * | 2012-06-27 | 2013-01-09 | 上海南华机电有限公司 | Low-light intensity aviation obstruction beacon |
| CN203286394U (en) * | 2013-05-29 | 2013-11-13 | 无锡安邦电气有限公司 | High-power light-emitting diode (LED) aircraft obstruction light |
| JP2014182961A (en) * | 2013-03-19 | 2014-09-29 | Toshiba Lighting & Technology Corp | Airplane warning light |
| CN104329627A (en) * | 2014-10-30 | 2015-02-04 | 遵义火炎焱光电科技有限公司 | Solar LED (Light-Emitting Diode) point source lamp |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101728846B (en) * | 2008-10-30 | 2012-07-04 | 纬创资通股份有限公司 | Charging system and charging method |
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Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2004319198A (en) * | 2003-04-15 | 2004-11-11 | Kansai Electric Power Co Inc:The | Airplane warning light |
| CN202629889U (en) * | 2012-05-30 | 2012-12-26 | 上海复弗机电有限公司 | Solar energy aviation obstruction light |
| CN202660401U (en) * | 2012-06-27 | 2013-01-09 | 上海南华机电有限公司 | Low-light intensity aviation obstruction beacon |
| JP2014182961A (en) * | 2013-03-19 | 2014-09-29 | Toshiba Lighting & Technology Corp | Airplane warning light |
| CN203286394U (en) * | 2013-05-29 | 2013-11-13 | 无锡安邦电气有限公司 | High-power light-emitting diode (LED) aircraft obstruction light |
| CN104329627A (en) * | 2014-10-30 | 2015-02-04 | 遵义火炎焱光电科技有限公司 | Solar LED (Light-Emitting Diode) point source lamp |
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| CN104832864A (en) | 2015-08-12 |
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