CN205026560U - Height -adjustable's solar energy aviation obstruction beacon - Google Patents
Height -adjustable's solar energy aviation obstruction beacon Download PDFInfo
- Publication number
- CN205026560U CN205026560U CN201520619085.1U CN201520619085U CN205026560U CN 205026560 U CN205026560 U CN 205026560U CN 201520619085 U CN201520619085 U CN 201520619085U CN 205026560 U CN205026560 U CN 205026560U
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- China
- Prior art keywords
- battery
- height
- adjustable
- lamp body
- base
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- Expired - Fee Related
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- 238000005516 engineering process Methods 0.000 claims description 5
- 241000168254 Siro Species 0.000 claims description 3
- 238000009987 spinning Methods 0.000 claims description 3
- 230000007306 turnover Effects 0.000 claims description 3
- 238000009434 installation Methods 0.000 abstract 1
- 230000008092 positive effect Effects 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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- Non-Portable Lighting Devices Or Systems Thereof (AREA)
Abstract
The utility model provides a height -adjustable's solar energy aviation obstruction beacon, including lamp body, pull formula lamp stand, base, cell support and solar cell panel, on pull formula lamp stand and cell support all were fixed in the base, pull formula lamp stand included two the same pull units that vertical stack set up, connected through the pivot between solar cell panel and the cell support, and solar cell panel passes through the wire and connects the battery, and in the base was located to the battery, the battery passed through the wire and connects the lamp body. 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, the height -adjustable of lamp body, height that can according to actual need adjustment lamp body, solar cell panel is equipped with rain -proof lid, can play rain -proof function, and maneuverability is strong.
Description
Technical field
The utility model belongs to aviation obstruction beacon field, especially relates to a kind of adjustable for height 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.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, just must installing wire, also can cause the loss of electricity halfway, cause the waste of the energy.And in actual use, the height of aviation obstruction beacon is nonadjustable often.
Summary of the invention
Problem to be solved in the utility model is to provide a kind of adjustable for height 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 adjustable for height solar energy aviation obstruction beacon, comprise lamp body, drawing and pulling type lamp socket, base, battery carrier and solar panel, described drawing and pulling type lamp socket and battery carrier are all fixed on base, the pull-out unit that drawing and pulling type lamp socket two of comprising that vertically superposition arranges are identical, connected by rotating shaft between solar panel and battery carrier, solar panel connects battery by wire, battery is located in base, and battery connects lamp body by wire.
Further, the wire between described solar panel and battery is successively through in rotating shaft, battery carrier and base.
Further, one end of described solar panel is provided with turnover rain-proof cover.
Further, described pull-out unit comprises fixed head, sleeve and loop bar, and loop bar can be connected to sleeve by pull, compact siro spinning technology between sleeve and loop bar, and loop bar upper end is located at by fixed head.
The advantage that the utility model has and good effect are: the utility model adopts solar energy to power to lamp body, both the trouble of installing wire had been decreased, in turn save the use of the energy, convenient and practical, the height adjustable of lamp body, can adjust the height of lamp body according to actual needs, solar panel is provided with rain-proof cover, can rainproof function be played, workable.
Accompanying drawing explanation
Fig. 1 is the structural representation of described lamp body when being in extreme higher position;
Fig. 2 is the structural representation of described lamp body when being in extreme lower position;
Fig. 3 is the structural representation of described lamp body when mediating;
In figure: 1-lamp body; 2-fixed head; 3-loop bar; 4-sleeve; 5-base; 6-battery; 7-rain-proof cover; 8-solar panel; 9-rotating shaft; 10-battery carrier.
Detailed description of the invention
Below in conjunction with accompanying drawing, specific embodiment of the utility model is elaborated.
As shown in Figures 1 to 3, a kind of adjustable for height solar energy aviation obstruction beacon, comprise lamp body 1, drawing and pulling type lamp socket, base 5, battery carrier 10 and solar panel 8, described drawing and pulling type lamp socket and battery carrier 10 are all fixed on base 5, the pull-out unit that drawing and pulling type lamp socket two of comprising that vertically superposition arranges are identical, connected by rotating shaft 9 between solar panel 8 and battery carrier 10, solar panel 8 connects battery 6 by wire, battery 6 is located in base 5, and battery 6 connects lamp body 1 by wire.
Wire between solar panel 8 and battery 6 is successively through in rotating shaft 9, battery carrier 10 and base 5.
One end of solar panel 8 is provided with turnover rain-proof cover 7.
Pull-out unit comprises fixed head 2, sleeve 4 and loop bar 3, and loop bar 3 can be connected to sleeve 4 by pull, compact siro spinning technology between sleeve 4 and loop bar 3, and loop bar 3 upper end is located at by fixed head 2.
During use, when the loop bar 3 of two pull-out units all pulls out sleeve 4, lamp body 1 is in extreme higher position; When the loop bar 3 of one of them pull-out unit pulls out sleeve 4, when the loop bar 3 of another pull-out unit does not pull out sleeve 4, lamp body 1 mediates; When the loop bar 3 of two pull-out units does not all pull out sleeve 4, lamp body 1 is in extreme lower position.When raining, rain-proof cover 7 can be anchored on solar panel 8.
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. an adjustable for height solar energy aviation obstruction beacon, it is characterized in that: comprise lamp body (1), drawing and pulling type lamp socket, base (5), battery carrier (10) and solar panel (8), described drawing and pulling type lamp socket and battery carrier (10) are all fixed on base (5), the pull-out unit that drawing and pulling type lamp socket two of comprising that vertically superposition arranges are identical, connected by rotating shaft (9) between solar panel (8) and battery carrier (10), solar panel (8) connects battery (6) by wire, battery (6) is located in base (5), battery (6) connects lamp body (1) by wire.
2. adjustable for height solar energy aviation obstruction beacon according to claim 1, is characterized in that: the wire between described solar panel (8) and battery (6) is successively through in rotating shaft (9), battery carrier (10) and base (5).
3. adjustable for height solar energy aviation obstruction beacon according to claim 2, is characterized in that: one end of described solar panel (8) is provided with turnover rain-proof cover (7).
4. the adjustable for height solar energy aviation obstruction beacon according to any one of claims 1 to 3, it is characterized in that: described pull-out unit comprises fixed head (2), sleeve (4) and loop bar (3), loop bar (3) can be connected to sleeve (4) by pull, compact siro spinning technology between sleeve (4) and loop bar (3), loop bar (3) upper end is located at by fixed head (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520619085.1U CN205026560U (en) | 2015-08-17 | 2015-08-17 | Height -adjustable's solar energy aviation obstruction beacon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520619085.1U CN205026560U (en) | 2015-08-17 | 2015-08-17 | Height -adjustable's solar energy aviation obstruction beacon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205026560U true CN205026560U (en) | 2016-02-10 |
Family
ID=55259087
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520619085.1U Expired - Fee Related CN205026560U (en) | 2015-08-17 | 2015-08-17 | Height -adjustable's solar energy aviation obstruction beacon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205026560U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108105706A (en) * | 2017-12-30 | 2018-06-01 | 英利能源(中国)有限公司 | Solar energy aviation obstruction beacon |
-
2015
- 2015-08-17 CN CN201520619085.1U patent/CN205026560U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108105706A (en) * | 2017-12-30 | 2018-06-01 | 英利能源(中国)有限公司 | Solar energy aviation obstruction beacon |
| CN108105706B (en) * | 2017-12-30 | 2024-04-05 | 英利能源(中国)有限公司 | Solar aviation obstruction light |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160210 Termination date: 20160817 |