CN205026562U - Solar energy aviation obstruction beacon - Google Patents
Solar energy aviation obstruction beacon Download PDFInfo
- Publication number
- CN205026562U CN205026562U CN201520620483.5U CN201520620483U CN205026562U CN 205026562 U CN205026562 U CN 205026562U CN 201520620483 U CN201520620483 U CN 201520620483U CN 205026562 U CN205026562 U CN 205026562U
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- CN
- China
- Prior art keywords
- battery
- solar panels
- lamp body
- aviation obstruction
- lamp
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- 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 - Fee Related
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- Non-Portable Lighting Devices Or Systems Thereof (AREA)
Abstract
The utility model provides a solar energy aviation obstruction beacon, including lamp stand, lamp body, lamp shade, battery box, solar panel and battery, lamp body and battery box are all located on the lamp stand, the lamp body outside is located to the lamp shade, the battery box is located by the lamp shade, the battery is located in the battery box, the battery passes through the wire and connects the lamp body, solar panel connects the battery, the battery box upper end is equipped with the fixed plate, solar panel is equipped with two, two solar panel's upper end contacts each other, its lower extreme symmetry is fixed in the both sides of fixed plate, two solar panel are for the equal inclination beta of fixed plate, 30 <= beta <= 75, and form the isosceles triangle structure with the fixed plate. The utility model has the advantages of with positive effect be: the utility model discloses a solar energy is supplied power for the lamp body, has both reduced the trouble of installation electric wire, the use of having saved the energy again, and convenient and practical, maneuverability is strong.
Description
Technical field
The utility model belongs to aviation obstruction beacon field, especially relates to a kind of solar energy aviation obstruction beacon.
Background technology
Aviation obstruction beacon is the extraordinary light fixture of mark barrier.In order to distinguish to some extent with general purpose illuminating lamp, aviation obstruction beacon is not normal light yellow but glittering, and aero-obstruction lantern with low light intensity is Chang Liang, and middle light intensity navigation obstacle lamp and high light intensity navigation obstacle lamp are for glisten, flashing rate is not less than 20 times per minute, not higher than 70 times per minute.The effect of aviation obstruction beacon is exactly the profile demonstrating structures, makes height and the profile of aircraft operators energy disturbance in judgement thing, plays warning function.The electric energy that what current aviation obstruction beacon adopted is all is supplied by electric wire is luminous, when mounted, and just must installing wire, and the loss of electricity also can be caused halfway, cause the waste of the energy.
Summary of the invention
Problem to be solved in the utility model is to provide a kind of solar energy aviation obstruction beacon, can solve the problem.
For solving the problems of the technologies described above, the technical solution adopted in the utility model is: a kind of solar energy aviation obstruction beacon, comprise lamp socket, lamp body, lampshade, battery case, solar panels and battery, described lamp body and battery case are all located on lamp socket, lamp body outside is located at by lampshade, battery case is located at by lampshade, battery is located in battery case, battery connects lamp body by wire, solar panels connect battery, battery case upper end is provided with fixed head, solar panels are provided with two, the upper end of two solar panels contacts with each other, its lower end is symmetrically fixed on the both sides of fixed head, two solar panels are relative to the equal inclination angle beta of fixed head, 30 °≤β≤75 °, and form isosceles triangular structure with fixed head.
Further, cutting and the mutual grafting of slot of coupling is passed through in the upper end of two described solar panels.
Further, be detachably provided with cushion block between described fixed head and solar panels, cushion block is cuboid, and two arris that its upper surface is relative and solar panels contact with each other.
Further, the arris place described cushion block contacted with solar panels is provided with rubber bound edge.
The advantage that the utility model has and good effect are: the utility model adopts solar energy to power to lamp body, has both decreased the trouble of installing wire, has in turn saved the use of the energy, convenient and practical, workable.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the structural representation of described cushion block;
In figure: 1-lampshade; 2-lamp body; 3-solar panels; 4-cushion block; 5-lamp socket; 6-fixed head; 7-battery case; 8-rubber bound edge; 9-cutting.
Detailed description of the invention
Below in conjunction with accompanying drawing, specific embodiment of the utility model is elaborated.
As shown in Fig. 1 ~ 2, a kind of solar energy aviation obstruction beacon, comprise lamp socket 8, lamp body 2, lampshade 1, battery case 7, solar panels 3 and battery, described lamp body 2 and battery case 7 are all located on lamp socket 8, it is outside that lamp body 2 is located at by lampshade 1, it is other that lampshade 1 is located at by battery case 7, battery is located in battery case 7, battery connects lamp body 2 by wire, solar panels 3 connect battery, battery case 7 upper end is provided with fixed head 6, solar panels 3 are provided with two, the upper end of two solar panels 3 contacts with each other, its lower end is symmetrically fixed on fixed head 6 both sides, two solar panels 3 are relative to the equal inclination angle beta of fixed head 6, it is 45 °, and form isosceles triangular structure with fixed head 6.
Cutting 9 and the mutual grafting of slot of coupling are passed through in the upper end of two solar panels 3.Make triangular structure more firm, prevent solar panels from lodging.
Detachably be provided with cushion block 4 between fixed head 6 and solar panels 3, cushion block 4 is cuboid, and two arris that its upper surface is relative and solar panels 3 contact with each other.The arris place that cushion block 4 contacts with solar panels 3 is provided with rubber bound edge 8.
During use, two opposing settings of solar panels 3, fully can absorb the sunlight of all directions, make the higher of the conversion ratio of solar energy.Adopt cushion block 4 to be arranged on bottom two solar panels 3, can play a supporting role to solar panels 3, make triangular structure more firm.
Above an embodiment of the present utility model has been described in detail, but described content being only preferred embodiment of the present utility model, can not being considered to for limiting practical range of the present utility model.All equalizations done according to the utility model application range change and improve, and all should still belong within patent covering scope of the present utility model.
Claims (4)
1. a solar energy aviation obstruction beacon, it is characterized in that: comprise lamp socket (8), lamp body (2), lampshade (1), battery case (7), solar panels (3) and battery, described lamp body (2) and battery case (7) are all located on lamp socket (8), it is outside that lamp body (2) is located at by lampshade (1), it is other that lampshade (1) is located at by battery case (7), battery is located in battery case (7), battery connects lamp body (2) by wire, solar panels (3) connect battery, battery case (7) upper end is provided with fixed head (6), solar panels (3) are provided with two, the upper end of two solar panels (3) contacts with each other, its lower end is symmetrically fixed on fixed head (6) both sides, two solar panels (3) are relative to the equal inclination angle beta of fixed head (6), 30 °≤β≤75 °, and form isosceles triangular structure with fixed head (6).
2. solar energy aviation obstruction beacon according to claim 1, is characterized in that: cutting (9) and the mutual grafting of slot of coupling are passed through in the upper end of two described solar panels (3).
3. solar energy aviation obstruction beacon according to claim 1 and 2, it is characterized in that: between described fixed head (6) and solar panels (3), be detachably provided with cushion block (4), cushion block (4) is cuboid, and two arris that its upper surface is relative and solar panels (3) contact with each other.
4. solar energy aviation obstruction beacon according to claim 3, is characterized in that: the upper arris place contacted with solar panels (3) of described cushion block (4) is provided with rubber bound edge (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520620483.5U CN205026562U (en) | 2015-08-17 | 2015-08-17 | Solar energy aviation obstruction beacon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520620483.5U CN205026562U (en) | 2015-08-17 | 2015-08-17 | Solar energy aviation obstruction beacon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205026562U true CN205026562U (en) | 2016-02-10 |
Family
ID=55259089
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520620483.5U Expired - Fee Related CN205026562U (en) | 2015-08-17 | 2015-08-17 | Solar energy aviation obstruction beacon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205026562U (en) |
-
2015
- 2015-08-17 CN CN201520620483.5U patent/CN205026562U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160210 Termination date: 20160817 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |