CN203375326U - Solar power low-light-intensity duplex aviation obstruction beacon - Google Patents

Solar power low-light-intensity duplex aviation obstruction beacon Download PDF

Info

Publication number
CN203375326U
CN203375326U CN201320478327.0U CN201320478327U CN203375326U CN 203375326 U CN203375326 U CN 203375326U CN 201320478327 U CN201320478327 U CN 201320478327U CN 203375326 U CN203375326 U CN 203375326U
Authority
CN
China
Prior art keywords
aviation obstruction
obstruction beacon
light intensity
solar energy
duplex
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201320478327.0U
Other languages
Chinese (zh)
Inventor
肖飞
谭爱军
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SHANGHAI NANHUA ELECTRONICS CO Ltd
Original Assignee
SHANGHAI NANHUA ELECTRONICS CO Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SHANGHAI NANHUA ELECTRONICS CO Ltd filed Critical SHANGHAI NANHUA ELECTRONICS CO Ltd
Priority to CN201320478327.0U priority Critical patent/CN203375326U/en
Application granted granted Critical
Publication of CN203375326U publication Critical patent/CN203375326U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The utility model relates to a solar power low-light-intensity duplex aviation obstruction beacon. The solar power low-light-intensity duplex aviation obstruction beacon comprises a machine box, a beacon hood, a base, a box cover, a solar panel, a solar panel support, a non-spherical optical lens, an LED lamp plate, an angle adjusting support, a nickel-metal hydride battery and a circuit board. The nickel-metal hydride battery and the circuit board are arranged in the machine box, the non-spherical optical lens and the LED lamp plate are fixed on the base through tapping screws and a control circuit and an LED constant-current drive circuit are integrated on the circuit board. An LED on the lamp plate is located at the focus of the non-spherical optical lens. The solar panel is fixed on the machine box through the solar panel support. The circuit board in the machine box is connected with a double-LED lamp. The solar power light-intensity duplex aviation obstruction beacon is free of light pollution, long in service life, low in energy consumption, high in light emitting efficiency, good in uniformity, small in size, light in weight, easy to install, reliable and stable.

Description

Solar energy hangs down light intensity duplex aviation obstruction beacon
[technical field]
The utility model relates to aeronautical beacon tool technical field, specifically, is the low light intensity duplex aviation obstruction beacon of a kind of solar energy.
[background technology]
The solar energy aviation obstruction beacon is generally used for the place that in high building, chimney, steel tower, airport, vehicle or other moving obstacles etc. serve as warning to aircraft.
At present, traditional aviation obstruction beacon does not almost have optical system or only has simple optical system, and the light loss is large, and light utilization efficiency is low, and at upper and lower, light can be seen in unnecessary ground, has caused light pollution; The tradition aviation obstruction beacon is generally used incandescent lamp, Halogen lamp LED and xenon lamp, and these light sources exist luminous efficiency low, and energy consumption is high, life-span is short, and lamp body volume, weight are all bigger than normal, because aviation obstruction beacon is arranged on high place, the installation and maintenance somewhat expensive, and the installation and maintenance process is extremely dangerous and difficult; And LED(Light Emitting Diode) light source body is low-voltage power supply, and energy consumption is low, and luminous efficiency is high, although some country has adopted the LED light source body to do aviation obstruction beacon, its uniformity of luminance is poor, is still a technical barrier; Traditional aviation obstruction beacon is generally used external power supply, and the installation and maintenance expense is high, and wastes energy, and uses solar powered mode just can save the problems such as lead-in wire, makes installation and maintenance simpler.
Chinese patent application CN:201220673170.2 discloses a kind of aero-obstruction lantern with low light intensity.Chinese patent application CN:CN201110173418.9 discloses a kind of solar energy aviation obstruction beacon.But about a kind of, good uniformity high without light pollution, life-span length, solar energy, luminous efficiency, volume weight little Yi installs and the reliable and stable low light intensity duplex aviation obstruction beacon of solar energy yet there are no report.
[summary of the invention]
The purpose of this utility model is, provide a kind of without light pollution, the life-span is long, energy consumption is low, luminous efficiency is high, good uniformity, volume weight are little, easily install and the reliable and stable low light intensity duplex aviation obstruction beacon of solar energy.
For achieving the above object, the technical scheme that the utility model is taked is:
A kind of solar energy hangs down light intensity duplex aviation obstruction beacon, comprise cabinet, lampshade, base, case lid, solar panel, solar-cell panel support, the aspherics lens, the LED lamp plate, angle-adjusting bracket, Ni-MH battery, wiring board, Ni-MH battery and wiring board are arranged in described cabinet, described LED lamp plate is provided with LED, described aspherics lens and LED lamp plate are fixed on base by self-tapping screw, integrated control circuit and LED constant-current drive circuit on described wiring board, LED on described lamp plate is positioned on the focus of aspherics lens, described solar panel is fixed on cabinet by solar-cell panel support, wiring board in described cabinet is connected with two LED lamps.
Described case lid is provided with stopper.
Be provided with screwed hole in the middle of described case lid.
Described stopper carries the screw thread with the case lid coupling.
Described stopper and case lid are fixed by screwed.
Described cabinet bottom is provided with the G3/4 screw thread.
Described cabinet and case lid are by foam sealing strip sealing of silica gel.
Described cabinet is threaded by 6 anticreeps with case lid.
Described base by thread is fixed on cabinet.
Described lampshade is provided with the spiral buckle.
The utility model advantage is:
1, the utility model is provided with non-spherical lens, these lens are according to Design of Aspherical Lenses, and when LED is placed on this lens focus, the light sent by LED light source is offset after lens reflection, form certain lighting angle, thereby meet remote irradiation demand.
2, adopt solar energy as power supply mode, environmental protection, easily installation and maintenance, and, without circumscripted power line, not limited by place.
3, LED adopts the constant current-supplying mode, has guaranteed the service life of LED.
4, light source is single-primary-color LED, and energy consumption is low, luminous efficiency is high.
5, mounting means adopts the G3/4 gas thread, is easy to install and use.
6, active and standby lamp automatically switches, and reduces the installation and maintenance operation, increases service life.
7, stopper can be used for preventing that rainwater from entering lamp body inside, has solved the risk of product water inlet, and minimizing brings maintenance because of the switch corrosion and ageing
[accompanying drawing explanation]
Accompanying drawing 1 is contour structures schematic diagram of the present utility model.
Accompanying drawing 2 is exploded perspective view of the present utility model.
Accompanying drawing 3 is case lid of the present utility model and stopper schematic diagram.
Accompanying drawing 4 is aspherics lens schematic diagram of the present utility model.
Accompanying drawing 5 is cabinet schematic diagram of the present utility model.
Accompanying drawing 6 is principle of luminosity schematic diagram of the present utility model.
The Reference numeral and the part that in accompanying drawing, relate to are as follows:
Cabinet 10 lampshades 20
Base 30 case lids 40
Stopper 50 solar panels 60
Solar-cell panel support 70 self-tapping screws 80
Aspherics lens 90 LED lamp plates 100
Angle-adjusting bracket 110 bolts 120
Ni-MH battery 130 wiring boards 140
Anti-drop screw 150 LED160
[specific embodiment]
Below in conjunction with embodiment and with reference to accompanying drawing, the utility model is further described.
As shown in Figure 1, the empty obstruction light of the low light intensity duplex of described solar energy is provided with cabinet 10, lampshade 20, base 30, case lid 40, stopper 50, solar panel 60, solar-cell panel support 70, described lampshade 20 is connected and fixed with the mode of base 30 by rotating buckle, with cabinet 10, by the G3/4 gas thread, (per inch tooth number is 14 to base 30, pitch 1.814mm, large footpath 26.441mm, path 24.117mm) connect, solar panel 60 is fixed on cabinet 10 by solar-cell panel support 70, case lid 40 is fixed by screwed with stopper 50, silica gel foaming sealing strip is housed on case lid 40.
As shown in Figure 2, Fig. 2 is the exploded perspective view of the low light intensity duplex aviation obstruction beacon of the utility model solar energy.The empty obstruction light of the low light intensity duplex of described solar energy boat is provided with cabinet 10, lampshade 20, base 30, case lid 40, stopper 50, solar panel 60, solar-cell panel support 70, self-tapping screw 80, aspherics lens 90, LED lamp plate 100, angle-adjusting bracket 110, bolt 120, Ni-MH battery 130, wiring board 140, anti-drop screw 150, described lampshade 20 is connected and fixed with the mode of base 30 by rotating buckle, aspherics lens 90 and LED lamp plate 100 are fixed on base 30 by 3 self-tapping screws 80, base 30 is connected by the G3/4 gas thread with cabinet 10, solar panel 60 is fixed on cabinet 10 by solar-cell panel support 70 use bolts 120, adjust angle by angle-adjusting bracket 110, be provided with Ni-MH battery 130 and wiring board 140 in cabinet 10, solar panel 60 is converted into electric energy by the solar energy collected, Ni-MH battery 130 is for storing these electric energy, case lid 40 is fixed by screwed with stopper 50, silica gel foaming sealing strip is housed on case lid 40, by 6 anticreep spiral shells, 150 are connected with cabinet 10, the silica gel sealing bar can effectively prevent the casing water inlet, prevent the internal circuit damage of making moist, strengthen the practicality of the utility model at rainy weather.
As shown in Figure 3; figure tri-is the low light intensity duplex aviation obstruction beacon case lid of the utility model solar energy and stopper schematic diagram; be provided with screwed hole in the middle of described case lid 40; carry the screw thread with case lid 40 couplings on stopper 50; open stopper and can stir power switch (not marking in figure); play the effect of protection switch, extend the service life of whole lamp.
As shown in Figure 4, figure tetra-is the low light intensity duplex aviation obstruction beacon aspherics lens schematic diagrames of the utility model solar energy, described aspherics lens 90 are fixing together with LED lamp plate 100, and the LED on LED lamp plate 100 is positioned on the focus of aspherics lens 90.
As shown in Figure 5, figure five is the low light intensity duplex aviation obstruction beacon cabinet schematic diagrames of the utility model solar energy, and the gas thread that described cabinet bottom is provided with G3/4 is connected with on-the-spot support, effective fixed lamp body, simple installation.
As shown in Figure 6, figure six is principle of luminosity figure of the utility model solar energy aero-obstruction lantern with low light intensity, described LED160 is fixed on LED lamp plate 100, LED160 is positioned on the focus of aspherics lens 90, the ordinary ray that LED160 sends, through unirefringence and a total reflection of aspherics lens 90, is polymerized to the light belt of 360 ° of approximately parallel levels, can eliminate light pollution, improve luminous efficiency, and the light good uniformity.
The above is only preferred embodiment of the present utility model; it should be pointed out that for those skilled in the art, under the prerequisite that does not break away from the utility model principle; can also make some improvement and supplement, these improvement and supplement and also should be considered as protection domain of the present utility model.

Claims (10)

1. a solar energy hangs down light intensity duplex aviation obstruction beacon, comprise cabinet, lampshade, base, case lid, solar panel, solar-cell panel support, the aspherics lens, the LED lamp plate, angle-adjusting bracket, Ni-MH battery, wiring board, Ni-MH battery and wiring board are arranged in described cabinet, described LED lamp plate is provided with LED, described aspherics lens and LED lamp plate are fixed on base by self-tapping screw, integrated control circuit and LED constant-current drive circuit on described wiring board, LED on described lamp plate is positioned on the focus of aspherics lens, described solar panel is fixed on cabinet by solar-cell panel support, it is characterized in that, wiring board in described cabinet is connected with two LED lamps.
2. the low light intensity duplex aviation obstruction beacon of solar energy according to claim 1, is characterized in that, described case lid is provided with stopper.
3. the low light intensity duplex aviation obstruction beacon of solar energy according to claim 1 and 2, is characterized in that, is provided with screwed hole in the middle of described case lid.
4. the low light intensity duplex aviation obstruction beacon of solar energy according to claim 1, is characterized in that, described stopper carries the screw thread with the case lid coupling.
5. according to claim 1 or the low light intensity duplex aviation obstruction beacon of 2 or 4 described solar energy, it is characterized in that, described stopper and case lid are fixed by screwed.
6. the low light intensity duplex aviation obstruction beacon of solar energy according to claim 1, is characterized in that, described cabinet bottom is provided with the G3/4 screw thread.
7. the low light intensity duplex aviation obstruction beacon of solar energy according to claim 1, is characterized in that, described cabinet and case lid seal by the silica gel sealing strip that foams.
8. the low light intensity duplex aviation obstruction beacon of solar energy according to claim 1, is characterized in that, described cabinet is threaded by 6 anticreeps with case lid.
9. the low light intensity duplex aviation obstruction beacon of solar energy according to claim 1, is characterized in that, described base by thread is fixed on cabinet.
10. the low light intensity duplex aviation obstruction beacon of solar energy according to claim 1, is characterized in that, described lampshade is provided with the spiral buckle.
CN201320478327.0U 2013-08-07 2013-08-07 Solar power low-light-intensity duplex aviation obstruction beacon Active CN203375326U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320478327.0U CN203375326U (en) 2013-08-07 2013-08-07 Solar power low-light-intensity duplex aviation obstruction beacon

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320478327.0U CN203375326U (en) 2013-08-07 2013-08-07 Solar power low-light-intensity duplex aviation obstruction beacon

Publications (1)

Publication Number Publication Date
CN203375326U true CN203375326U (en) 2014-01-01

Family

ID=49837853

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201320478327.0U Active CN203375326U (en) 2013-08-07 2013-08-07 Solar power low-light-intensity duplex aviation obstruction beacon

Country Status (1)

Country Link
CN (1) CN203375326U (en)

Similar Documents

Publication Publication Date Title
CN203240470U (en) Novel street lamp
CN201916840U (en) Solar-energy LED garden lamp
CN205299357U (en) Solar garden lamp
CN204943297U (en) A kind of floor projection automation street lamp
CN206398610U (en) A kind of LED street lamp
CN205909068U (en) LED (Light emitting diode) tri -proof lamp
CN203375326U (en) Solar power low-light-intensity duplex aviation obstruction beacon
CN103225758A (en) Emergency LED lamp for airfield runway
CN203963787U (en) A kind of novel energy-saving road lamp
CN209495254U (en) A kind of energy-saving and environment-friendly luminous energy wisdom street lamp
CN203848128U (en) Novel LED ceiling lamp
CN203980110U (en) Solar street light
CN203375323U (en) Solar aviation obstruction beacon
CN203023966U (en) Novel intelligent LED (Light Emitting Diode) wall wash lamp
CN207702168U (en) A kind of explosion-proof searchlight
CN206347466U (en) A kind of high radiating novel LED projection lamp
CN202056727U (en) Led solar energy lawn lamp
CN205208422U (en) Novel novel LED street lamp of solar energy power supply
CN202660401U (en) Low-light intensity aviation obstruction beacon
CN203686843U (en) Portable solar aviation obstruction beacon
CN203571459U (en) Big-power LED anti-explosion emergency light
CN203810261U (en) Flashing obstacle lamp
CN108980746A (en) A kind of intelligent solar LED street lamp
CN202972781U (en) Mine tunnel lamp
CN203703737U (en) LED (Light Emitting Diode) module street lamp with lower air hole

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant