CN203686843U - Portable solar aviation obstruction beacon - Google Patents
Portable solar aviation obstruction beacon Download PDFInfo
- Publication number
- CN203686843U CN203686843U CN201320787459.1U CN201320787459U CN203686843U CN 203686843 U CN203686843 U CN 203686843U CN 201320787459 U CN201320787459 U CN 201320787459U CN 203686843 U CN203686843 U CN 203686843U
- Authority
- CN
- China
- Prior art keywords
- solar
- battery
- aviation obstruction
- bracket
- obstruction beacon
- 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.)
- Expired - Lifetime
Links
- 238000013016 damping Methods 0.000 claims description 4
- 238000007789 sealing Methods 0.000 claims description 4
- 229920003229 poly(methyl methacrylate) Polymers 0.000 claims description 3
- 239000004926 polymethyl methacrylate Substances 0.000 claims description 3
- 238000007639 printing Methods 0.000 claims description 3
- 239000011241 protective layer Substances 0.000 claims description 3
- 238000005286 illumination Methods 0.000 abstract description 2
- 238000012423 maintenance Methods 0.000 description 6
- 230000009286 beneficial effect Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 230000005611 electricity Effects 0.000 description 3
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 2
- 230000006378 damage Effects 0.000 description 2
- 239000003292 glue Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008447 perception Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Images
Abstract
The utility model discloses a portable solar aviation obstruction beacon. The solar aviation obstruction beacon comprises a base, a solar bracket, a battery and a lamp cap, wherein the solar bracket is mounted on the base; the battery is mounted inside the solar bracket; the solar bracket is provided with a polygonal superface, and a foldable solar panel is mounted on each edge of the polygonal superface; the lamp cap is mounted in an opening formed in the center of the polygonal superface; an LED lamp panel is mounted inside the lamp cap, and is provided with a plurality of LED lamps; the battery is mounted at the lower part of the lamp cap inside the solar bracket through a battery mounting plate; the battery is electrically connected with a driving module in the lamp cap, and is used for supplying power to the LED lamps mounted in the LED lamp cap; simultaneously, the battery is further electrically connected with the solar panels; the solar panels are used for charging up the battery. By the adoption of the solar aviation obstruction beacon, the problems that the solar aviation obstruction beacon is large in size, small in illumination plane and inconvenient to maintain are solved.
Description
Technical field
The utility model relates to extraordinary technical field of lamps, particularly a kind of solar energy aviation obstruction beacon.
Background technology
Aviation obstruction beacon is a kind of signal lamp, its working method is glittering, and flashing rate is not less than 20 times per minute, not higher than 70 times per minute, and 360 ° of scopes of aviation obstruction beacon can obviously penetrate light, so that can its light signal sending of perception in space on this lamp.Aviation obstruction beacon is mainly used in high-altitude facility such as the outdoor service truck of squarer, crane, chimney, skyscraper, helicopter etc. need to be warned airborne vehicle and has equipment or the building of barrier.
Existing solar energy aviation obstruction beacon is as Fig. 1, shown in Fig. 2 and Fig. 3, mainly comprise mounting seat 1, annular LED Column being luminous 2, solar panel 4 and lampshade 3, wherein mounting seat 1 is provided with battery case 11, the outside of battery case 11 is provided with lid 12, multiple batteries 5 are housed in battery case 11, mounting seat 1 top can first be locked with annular Connection Block 13 use screws mutually, three boss 131 are set in the inner side of annular Connection Block 13, annular LED Column being luminous 2 is screwed on three boss 131 of annular Connection Block 13 inner sides, solar panel 4 is fixed on annular LED Column being luminous 2, lampshade 3 entangles on solar panel 4 and annular LED Column being luminous 2, the lower surface of lampshade 3 and annular Connection Block 13 fix by marine glue.In mounting seat 1, contain LED drive circuit and solar control circuit, LED drive circuit and solar control circuit can be arranged on same circuit board 6, LED drive circuit is electrically connected with annular LED Column being luminous 2, solar control circuit is electrically connected with the battery 5 in solar panel 4 and battery case 11 respectively, gauge tap 7 also can be housed in battery case 11, and then the battery 5 in battery case 11 is electrically connected with LED drive circuit by gauge tap 7.
Annular LED Column being luminous 2 can be made up of multiple LED lamp bars and upper and lower two gripper shoes, multiple LED lamp bars are by annular array, one end and upper backup pad plug, the other end and lower supporting plate plug, and make multiple LED lamp bars realize electrical connection by lower supporting plate, on each LED lamp bar, multiple LED illuminators are set, each LED illuminator is electrically connected with LED drive circuit in parallel.
, there is following shortcoming in the structure of existing solar energy aviation obstruction beacon above: 1, its lampshade marine glue is fixing by internal structure sealing, therefore light fixture is an entirety, needs destruction lampshade just can overhaul if interior wall construction damages, and causes maintenance inconvenience.2, solar panel is installed on solar energy obstruction light inside, cause the area of solar panel can not be very large, the electricity conversion of solar panel is generally not high at present in addition, it is longer that solar panel accumulators is full of the electricity time, if run into the weather that continuous solar radiation intensity is low, battery cannot obtain fast charging and supplement.If in order to improve the utilization rate of solar energy, just need to strengthen the area of solar panel, this has caused again solar energy aviation obstruction beacon volume to become large, carries inconvenience is installed.
Utility model content
(1) technical problem that will solve
In view of this, main purpose of the present utility model is to provide a kind of solar energy aviation obstruction beacon, large to solve solar energy aviation obstruction beacon volume, is subject to the problem that plane of illumination is little and maintenance maintenance is inconvenient.
(2) technical scheme
For achieving the above object, the utility model provides a kind of portable type solar energy aviation obstruction beacon, this solar energy aviation obstruction beacon comprises base 9, is installed on the solar bracket 2 on base 9 and is installed on battery 7 and the lamp holder 1 of solar bracket 2 inside, wherein, this solar bracket 2 has a polygon end face, along each limit of this polygon end face, a solar-powered collapsible cell panel 4 is all installed; This lamp holder 1 is installed in the perforate at this polygon end face center, and lamp holder 1 inside is provided with a LED lamp plate, and plurality of LEDs lamp is installed on LED lamp plate; This battery 7 is installed on the below of the inner lamp holder 1 of solar bracket 2 by battery installing plate 6, and battery 7 is electrically connected on the driver module in lamp holder 1, with thinking the LED lamp power supply of installing in LED lamp holder, battery 7 is also electrically connected on polylith solar panel 4 simultaneously, and solar panel 4 charges to battery 7.
In such scheme, the polygon end face of this solar bracket 2 is equilateral triangle, square, regular pentagon, regular hexagon, positive heptagon or octagon.
In such scheme, this solar panel 4 is first arranged on solar cell installing plate 5, be installed on many limits of solar bracket 2 polygon end faces by Damping hinge 3, in the time of work, solar panel 4 launches again, and when transportation or storage, solar panel 4 is folding.
In such scheme, the surface of this solar panel 4 has a high printing opacity PMMA protective layer.
In such scheme, between this lamp holder 1 and the polygon end face of solar bracket 2, use screw fastening, and between lamp holder 1 and polygon end face, water-proof sealing circle is installed.
In such scheme, the main body of this lamp holder 1 is obstruction light lamp body 16, obstruction light lamp body 16 tops are connected with PC outer cover 10 by screw, obstruction light lamp body 16 inside under PC outer cover 10 are provided with lens module 11, LED lamp plate 12, heat-conducting pad 13, heat sink 14 and driver module 15 from top to bottom successively, and this driver module 15 is from the cabling in the raised floor of obstruction light lamp body 16.
In such scheme, this battery 7 is installed on the solar bracket base plate 8 of the inner lamp holder of solar bracket 21 below by battery installing plate 6, then is arranged on the bottom of solar bracket 2 by solar bracket base plate 8.
In such scheme, the side of this solar bracket 2 is provided with switch 17 and dimmer switch 18, on this solar bracket base plate 8, air plug interface 19 is installed.
In such scheme, this solar bracket base plate 8 is affixed by screw with base 9.
In such scheme, this battery 7 is rechargeable battery.
(3) beneficial effect
Can find out from technique scheme, the utlity model has following beneficial effect:
1, the portable type solar energy aviation obstruction beacon that the utility model provides, is provided with polylith solar panel at its top, when conventionally transporting or storing, solar panel is folding, reduces the volume of solar energy aviation obstruction beacon, easy to carry and transport; In use solar panel is launched into level, has increased greatly and received the area of sunshine, and then can accelerate the charge rate of battery, even also can effectively charge to battery in the situation that weather conditions are not good.
2, the portable type solar energy aviation obstruction beacon that the utility model provides, obstruction light lamp holder and solar energy equipment are organically combined, and, with screw fastening, are detachable designs between the polygon end face of lamp holder and solar bracket, can change easily lamp holder, carry out maintenance support.
Accompanying drawing explanation
Fig. 1, Fig. 2 and Fig. 3 are the structural representations of existing solar energy aviation obstruction beacon.
Fig. 4 is the structural representation according to the portable type solar energy aviation obstruction beacon of the utility model embodiment.
Fig. 5 is the structural representation according to lamp holder in the portable type solar energy aviation obstruction beacon of the utility model embodiment.
Fig. 6 is the structural representation according to the portable type solar energy aviation obstruction beacon side of the utility model embodiment.
Fig. 7 is portable type solar energy aviation obstruction beacon according to the utility model embodiment schematic diagram after solar cell plate development.
The specific embodiment
For making the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with specific embodiment, and with reference to accompanying drawing, the utility model is further described.
The portable type solar energy aviation obstruction beacon that the utility model provides comprises base 9, is installed on the solar bracket 2 on base 9 and is installed on battery 7 and the lamp holder 1 of solar bracket 2 inside, wherein, this solar bracket 2 has a polygon end face, along each limit of this polygon end face, a solar-powered collapsible cell panel 4 is all installed; This lamp holder 1 is installed in the perforate at this polygon end face center, and lamp holder 1 inside is provided with a LED lamp plate, and plurality of LEDs lamp is installed on LED lamp plate; This battery 7 is installed on the below of the inner lamp holder 1 of solar bracket 2 by battery installing plate 6, and battery 7 is electrically connected on the driver module in lamp holder 1, with thinking the LED lamp power supply of installing in LED lamp holder, battery 7 is also electrically connected on polylith solar panel 4 simultaneously, and solar panel 4 charges to battery 7.
Wherein, the polygon end face of this solar bracket 2 is regular polygon, for example, can be equilateral triangle, square, regular pentagon, regular hexagon, positive heptagon or octagon etc.This solar panel 4 is first arranged on solar cell installing plate 5, be installed on again many limits of solar bracket 2 polygon end faces by Damping hinge 3, in the time of work, solar panel 4 is launched into level, increase greatly the area that receives sunshine, and then can accelerate the charge rate of battery, even also can effectively charge to battery in the situation that weather conditions are not good; When transportation or storage, solar panel 4 is folding, reduces the volume of solar energy aviation obstruction beacon, easy to carry and transport.In addition, the surface of this solar panel 4 also has a high printing opacity PMMA protective layer, protects, and increase the transmitance of sunshine in order to the surface to solar panel.
Between this lamp holder 1 and the polygon end face of solar bracket 2, use screw fastening, and between lamp holder 1 and polygon end face, water-proof sealing circle is installed.Between the polygon end face of lamp holder and solar bracket, with screw fastening, be detachable design, can change easily lamp holder, carry out maintenance support.
The main body of this lamp holder 1 is obstruction light lamp body 16, obstruction light lamp body 16 tops are connected with PC outer cover 10 by screw, obstruction light lamp body 16 inside under PC outer cover 10 are provided with lens module 11, LED lamp plate 12, heat-conducting pad 13, heat sink 14 and driver module 15 from top to bottom successively, and this driver module 15 is from the cabling in the raised floor of obstruction light lamp body 16.This battery 7 is installed on the solar bracket base plate 8 of the inner lamp holder of solar bracket 21 below by battery installing plate 6, then is arranged on the bottom of solar bracket 2 by solar bracket base plate 8.The side of this solar bracket 2 is provided with switch 17 and dimmer switch 18, on this solar bracket base plate 8, air plug interface 19 is installed.This solar bracket base plate 8 is affixed by screw with base 9, convenient installation.This battery 7 is rechargeable battery, for example lithium battery.
As shown in Figure 4, Fig. 4 is the structural representation according to the portable type solar energy aviation obstruction beacon of the utility model embodiment, in the present embodiment, the polygon end face of this solar bracket 2 is square, there are 4 limits, each limit is all provided with a solar-powered collapsible cell panel 4, and 4 solar panels are installed altogether.These 4 solar panels 4 are arranged on respectively on a solar cell installing plate 5, and solar cell installing plate 5 is installed on 4 limits of solar bracket 2 square end faces by Damping hinge 3.In the time of work, solar panel 4 is launched into level, as shown in Figure 7, has increased greatly and has received the area of sunshine, and then can accelerate the charge rate of battery, even also can effectively charge to battery in the situation that weather conditions are not good; When transportation or storage, solar panel 4 is folding, reduces the volume of solar energy aviation obstruction beacon, easy to carry and transport.
The structure of this lamp holder 1 as shown in Figure 5, it is installed in the perforate at this polygon end face center, the main body of this lamp holder 1 is obstruction light lamp body 16, obstruction light lamp body 16 tops are connected with PC outer cover 10 by screw, obstruction light lamp body 16 inside under PC outer cover 10 are provided with lens module 11, LED lamp plate 12, heat-conducting pad 13, heat sink 14 and driver module 15 from top to bottom successively, and this driver module 15 is from the cabling in the raised floor of obstruction light lamp body 16.
Below the inner lamp holder 1 of solar bracket 2, it is battery installing plate 6, battery 7 is rechargeable lithium battary, be installed on by this battery installing plate 6 on the solar bracket base plate 8 of the inner lamp holder of solar bracket 21 below, then be arranged on the bottom of solar bracket 2 by solar bracket base plate 8.Solar bracket 2 is installed on base 9 by solar bracket base plate 8.This solar bracket base plate 8 is affixed by screw with base 9, convenient installation.
As shown in Figure 6, the side of this solar bracket 2 is provided with switch 17 and dimmer switch 18, on this solar bracket base plate 8, air plug interface 19 is installed.Switch 17 is switches of controlling lamp holder power supply, and the work that can realize this obstruction light by switch 17 whether.Dimmer switch 18 connects driver module, and the mode of pressing by length can switching controls different circuit, and 4 lamps are a driving loop, by short by mode realize the LED drive current of the different brackets setting in control loop, realize the adjusting of the brightness to lamp.Air plug interface 19 can be realized the discrepancy of external power supply, and even battery does not have electricity, and provides light energy without good sunshine environment, can access externally fed equipment by air plug and power.
In the embodiment providing at the utility model, the polygon end face of this solar bracket 2 is square, has 4 limits, and each limit is all provided with a solar-powered collapsible cell panel 4, and 4 solar panels are installed altogether.In actual applications, the polygon end face of this solar bracket 2 can be also equilateral triangle, regular pentagon, regular hexagon, positive heptagon or octagon etc., correspondingly, 3 solar panels can be installed, 5 solar panels, 6 solar panels, 7 solar panels and 8 solar panels etc., it realizes principle, and to provide portable type solar energy aviation obstruction beacon with the utility model be consistent, all can be in the time conventionally transporting or store, solar panel is folding, reduce the volume of solar energy aviation obstruction beacon, easy to carry and transport, in use solar panel is launched into level, increase greatly the area that receives sunshine, and then can accelerate the charge rate of battery, even also can effectively charge to battery in the situation that weather conditions are not good, just repeat no more here.
In addition, in the embodiment providing at the utility model, obstruction light lamp holder and solar energy equipment are organically combined, between the polygon end face of lamp holder and solar bracket, use screw fastening, be detachable design, can change easily lamp holder, carry out maintenance support.
Above-described specific embodiment; the purpose of this utility model, technical scheme and beneficial effect are further described; institute is understood that; the foregoing is only specific embodiment of the utility model; be not limited to the utility model; all within spirit of the present utility model and principle, any modification of making, be equal to replacement, improvement etc., within all should being included in protection domain of the present utility model.
Claims (10)
1. a portable type solar energy aviation obstruction beacon, this solar energy aviation obstruction beacon comprises base (9), is installed on the solar bracket (2) on base (9) and is installed on solar bracket (2) inner battery (7) and lamp holder (1), it is characterized in that:
This solar bracket (2) has a polygon end face, along each limit of this polygon end face, a solar-powered collapsible cell panel (4) is all installed;
This lamp holder (1) is installed in the perforate at this polygon end face center, and lamp holder (1) inside is provided with a LED lamp plate, and plurality of LEDs lamp is installed on LED lamp plate;
This battery (7) is installed on the below of the inner lamp holder of solar bracket (2) (1) by battery installing plate (6), and battery (7) is electrically connected on the driver module in lamp holder (1), with thinking the LED lamp power supply of installing in LED lamp holder, battery (7) is also electrically connected on polylith solar panel (4) simultaneously, and solar panel (4) charges to battery (7).
2. portable type solar energy aviation obstruction beacon according to claim 1, is characterized in that, the polygon end face of this solar bracket (2) is equilateral triangle, square, regular pentagon, regular hexagon, positive heptagon or octagon.
3. portable type solar energy aviation obstruction beacon according to claim 1, it is characterized in that, this solar panel (4) is first arranged on solar cell installing plate (5), be installed on again many limits of solar bracket (2) polygon end face by Damping hinge (3), in the time of work, solar panel (4) launches, and when transportation or storage, solar panel (4) is folding.
4. according to the portable type solar energy aviation obstruction beacon described in claim 1 or 3, it is characterized in that, the surface of this solar panel (4) has a high printing opacity PMMA protective layer.
5. portable type solar energy aviation obstruction beacon according to claim 1, it is characterized in that, between the polygon end face of this lamp holder (1) and solar bracket (2), use screw fastening, and between lamp holder (1) and polygon end face, water-proof sealing circle is installed.
6. portable type solar energy aviation obstruction beacon according to claim 1, it is characterized in that, the main body of this lamp holder (1) is obstruction light lamp body (16), obstruction light lamp body (16) top is connected with PC outer cover (10) by screw, obstruction light lamp body (16) inside under PC outer cover (10) is provided with lens module (11), LED lamp plate (12), heat-conducting pad (13), heat sink (14) and driver module (15) from top to bottom successively, and this driver module (15) is from the cabling in the raised floor of obstruction light lamp body (16).
7. portable type solar energy aviation obstruction beacon according to claim 1, it is characterized in that, the solar bracket base plate (8) that this battery (7) is installed on the inner lamp holder of solar bracket (2) (1) below by battery installing plate (6) is upper, then is arranged on the bottom of solar bracket (2) by solar bracket base plate (8).
8. portable type solar energy aviation obstruction beacon according to claim 7, it is characterized in that, the side of this solar bracket (2) is provided with switch (17) and dimmer switch (18), on this solar bracket base plate (8), air plug interface (19) is installed.
9. portable type solar energy aviation obstruction beacon according to claim 7, is characterized in that, this solar bracket base plate (8) is affixed by screw with base (9).
10. portable type solar energy aviation obstruction beacon according to claim 1, is characterized in that, this battery (7) is rechargeable battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320787459.1U CN203686843U (en) | 2013-12-03 | 2013-12-03 | Portable solar aviation obstruction beacon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320787459.1U CN203686843U (en) | 2013-12-03 | 2013-12-03 | Portable solar aviation obstruction beacon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203686843U true CN203686843U (en) | 2014-07-02 |
Family
ID=51008734
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320787459.1U Expired - Lifetime CN203686843U (en) | 2013-12-03 | 2013-12-03 | Portable solar aviation obstruction beacon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203686843U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107830478A (en) * | 2017-09-27 | 2018-03-23 | 苏州城时实业有限公司 | Solar LED roadblock lamp manufacturing method |
-
2013
- 2013-12-03 CN CN201320787459.1U patent/CN203686843U/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107830478A (en) * | 2017-09-27 | 2018-03-23 | 苏州城时实业有限公司 | Solar LED roadblock lamp manufacturing method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102170250A (en) | Utility-type solar energy power supply apparatus | |
| JP2012227105A (en) | Illumination apparatus for street light | |
| CN203395795U (en) | LED (light-emitting diode) landscape lamp for new energy park | |
| CN203686843U (en) | Portable solar aviation obstruction beacon | |
| JP3168977U (en) | Street lighting fixtures | |
| CN202059348U (en) | Solar energy power supply apparatus with illuminating lamp | |
| CN202195406U (en) | Automatic adjusting solar light-emitting diode (LED) street lamp | |
| CN204164696U (en) | Portable solar LED searchlight | |
| CN204213799U (en) | Chapiter lamp | |
| CN204141281U (en) | A kind of movable type beacon | |
| CN203375323U (en) | Solar aviation obstruction beacon | |
| CN203771274U (en) | Landscape lamp | |
| CN202422635U (en) | Solar advertising light box | |
| CN104832864A (en) | Solar low-light-intensity aircraft obstruction beacon | |
| CN104108439A (en) | Illuminating device for golf cart | |
| CN202392669U (en) | Solar LED (Light-Emitting Diode) aircraft obstruction beacon | |
| CN204943276U (en) | A kind of street lamp with monitoring and radio function | |
| CN209744251U (en) | Ball bubble lamp with emergent function | |
| CN203868921U (en) | Navigation mark apparatus | |
| CN102635827A (en) | Desk lamp | |
| CN202532371U (en) | Solar remote control sensing night light | |
| CN207179504U (en) | A kind of solar LED landscape spotlight | |
| CN207999757U (en) | A kind of solar energy garden lamp | |
| CN212719273U (en) | LED lamp with solar cell panel | |
| CN215636902U (en) | Multifunctional road lighting device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140702 |
|
| CX01 | Expiry of patent term |