CN102829421A - Solar aviation obstruction lamp - Google Patents
Solar aviation obstruction lamp Download PDFInfo
- Publication number
- CN102829421A CN102829421A CN 201110173418 CN201110173418A CN102829421A CN 102829421 A CN102829421 A CN 102829421A CN 201110173418 CN201110173418 CN 201110173418 CN 201110173418 A CN201110173418 A CN 201110173418A CN 102829421 A CN102829421 A CN 102829421A
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- China
- Prior art keywords
- power supply
- solar
- aviation obstruction
- support
- lamp body
- 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.)
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- Non-Portable Lighting Devices Or Systems Thereof (AREA)
Abstract
The invention discloses a solar aviation obstruction lamp which comprises a base, a support bar, a support base, a power supply and a lamp body, wherein the power supply is a storage battery, the support base is detachably connected with a cover body, and the power supply and the lamp body are fully positioned in the cover body; the support base is fixedly connected with a solar cell panel through a support, and one side of the support is fixedly connected with a cambered protective cap which can cover the solar cell panel; and the protective cap is of a telescopic structure, the solar cell panel, the power supply and the lamp body are connected through wires so as to form a closed loop circuit. According to the invention, solar energy is utilized to supply power to the lamp body, the trouble of installing electric wires is reduced, the energy source utilization is saved, the solar aviation obstruction lamp is provided with the cover body, and rainwater is prevented from permeating into the power supply and further causing breakage; and the solar aviation obstruction lamp is provided with the protective cap which can cover the solar cell panel on rain days, the solar cell panel is prevented from showering through rainwater and further being damaged, the protective cap is retractable, and the protective cap can be used along with the weather variation.
Description
Technical field
The present invention relates to a kind of aviation obstruction beacon, relate in particular to a kind of solar energy aviation obstruction beacon.
Background technology
Present aviation obstruction beacon adopted all is that the electric energy supplied with through electric wire is luminous, when mounted, just electric wire must be installed, and also can cause the loss of electric weight halfway, caused the waste of the energy; The life-span of aviation obstruction beacon is 1000 hours, and on rainy day, rainwater can penetrate into power supply, causes the aviation obstruction beacon can't operate as normal, thereby has potential safety hazard, and people are often keeped in repair it, and is very inconvenient.
Summary of the invention
To the problem that above-mentioned prior art exists, the object of the invention is to provide a kind of solar powered aviation obstruction beacon that adopts.
Technical scheme of the present invention is: a kind of solar energy aviation obstruction beacon; Comprise base, support bar, supporting seat, power supply and lamp body, said power supply is a battery, and a cover body removably connects on the said supporting seat; And power supply and lamp body are positioned at this cover body fully; Also be fixedly connected with a solar panel through support on the said supporting seat, the side fixed connection one of said support can cover the guard shield of the arc of solar panel, and this guard shield is a telescopic structure; Said solar panel, power supply and lamp body are connected through lead, and form the closed-loop path.
As preferably: saidly be detachably connected as clamping.
The invention has the beneficial effects as follows: the present invention is supplied power to lamp body by solar energy, has both reduced the trouble that electric wire is installed, the use of having saved the energy again; Have cover body, avoid rain penetration to advance power supply, cause damage; Have guard shield, can cover solar panel on rainy day, the back of avoiding being soaked with rain is damaged; Guard shield is scalable, can use with the variation of weather.
Description of drawings
Fig. 1 is a structural representation of the present invention.
Among the figure: 1, supporting seat; 2, support bar; 3, power supply; 4, lamp body; 5, cover body; 6, support; 7, solar panel; 8, guard shield.
The specific embodiment
Be described further for the present invention below in conjunction with accompanying drawing.
Embodiment: referring to Fig. 1; The present invention includes base, support bar 2, supporting seat 1, power supply 3 and lamp body 4, said power supply 3 is a battery, clamping one cover body 5 on the said supporting seat 1; And power supply 3 is positioned at this cover body 5 fully with lamp body 4; Also be fixedly connected with a solar panel 7 through support 6 on the said supporting seat 1, the side fixed connection one of said support 6 can cover the guard shield 8 of the arc of solar panel 7, and this guard shield 8 is a telescopic structure; Said solar panel 7, power supply 3 and lamp body 4 are connected through lead, and form the closed-loop path.
The present invention gives lamp body 4 power supplies by solar energy, has both reduced the trouble that electric wire is installed, the use of having saved the energy again; Have cover body 5, avoid rain penetration to advance power supply 3, cause damage; Have guard shield 8, can cover solar panel 7 on rainy day, the back of avoiding being soaked with rain is damaged; Guard shield 8 is scalable, can use with the variation of weather.
Claims (2)
1. solar energy aviation obstruction beacon; Comprise base, support bar, supporting seat, power supply and lamp body, it is characterized in that: said power supply is a battery, and a cover body removably connects on the said supporting seat; And power supply and lamp body are positioned at this cover body fully; Also be fixedly connected with a solar panel through support on the said supporting seat, the side fixed connection one of said support can cover the guard shield of the arc of solar panel, and this guard shield is a telescopic structure; Said solar panel, power supply and lamp body are connected through lead, and form the closed-loop path.
2. according to the described solar energy aviation obstruction beacon of claim 1, it is characterized in that: saidly be detachably connected as clamping.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110173418 CN102829421A (en) | 2011-06-14 | 2011-06-14 | Solar aviation obstruction lamp |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110173418 CN102829421A (en) | 2011-06-14 | 2011-06-14 | Solar aviation obstruction lamp |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102829421A true CN102829421A (en) | 2012-12-19 |
Family
ID=47332650
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201110173418 Pending CN102829421A (en) | 2011-06-14 | 2011-06-14 | Solar aviation obstruction lamp |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102829421A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106595087A (en) * | 2015-10-15 | 2017-04-26 | 天津七禾创意科技有限公司 | Photo-electro-mechanical integrated solar water heater |
| CN110594679A (en) * | 2019-09-18 | 2019-12-20 | 陆玉琴 | Aviation obstruction beacon |
-
2011
- 2011-06-14 CN CN 201110173418 patent/CN102829421A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106595087A (en) * | 2015-10-15 | 2017-04-26 | 天津七禾创意科技有限公司 | Photo-electro-mechanical integrated solar water heater |
| CN110594679A (en) * | 2019-09-18 | 2019-12-20 | 陆玉琴 | Aviation obstruction beacon |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| DD01 | Delivery of document by public notice |
Addressee: Yang Rui Document name: Notification that Application Deemed to be Withdrawn |
|
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20121219 |