CN112161247A - Solar aviation obstruction beacon - Google Patents
Solar aviation obstruction beacon Download PDFInfo
- Publication number
- CN112161247A CN112161247A CN202011230014.4A CN202011230014A CN112161247A CN 112161247 A CN112161247 A CN 112161247A CN 202011230014 A CN202011230014 A CN 202011230014A CN 112161247 A CN112161247 A CN 112161247A
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- CN
- China
- Prior art keywords
- solar
- energy storage
- storage box
- aviation obstruction
- light
- 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.)
- Pending
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21S—NON-PORTABLE LIGHTING DEVICES; SYSTEMS THEREOF; VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLE EXTERIORS
- F21S9/00—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply
- F21S9/02—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply the power supply being a battery or accumulator
- F21S9/03—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply the power supply being a battery or accumulator rechargeable by exposure to light
- F21S9/035—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply the power supply being a battery or accumulator rechargeable by exposure to light the solar unit being integrated within the support for the lighting unit, e.g. within or on a pole
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V21/00—Supporting, suspending, or attaching arrangements for lighting devices; Hand grips
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V23/00—Arrangement of electric circuit elements in or on lighting devices
- F21V23/003—Arrangement of electric circuit elements in or on lighting devices the elements being electronics drivers or controllers for operating the light source, e.g. for a LED array
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V23/00—Arrangement of electric circuit elements in or on lighting devices
- F21V23/02—Arrangement of electric circuit elements in or on lighting devices the elements being transformers, impedances or power supply units, e.g. a transformer with a rectifier
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V23/00—Arrangement of electric circuit elements in or on lighting devices
- F21V23/04—Arrangement of electric circuit elements in or on lighting devices the elements being switches
- F21V23/0442—Arrangement of electric circuit elements in or on lighting devices the elements being switches activated by means of a sensor, e.g. motion or photodetectors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V23/00—Arrangement of electric circuit elements in or on lighting devices
- F21V23/04—Arrangement of electric circuit elements in or on lighting devices the elements being switches
- F21V23/0442—Arrangement of electric circuit elements in or on lighting devices the elements being switches activated by means of a sensor, e.g. motion or photodetectors
- F21V23/0464—Arrangement of electric circuit elements in or on lighting devices the elements being switches activated by means of a sensor, e.g. motion or photodetectors the sensor sensing the level of ambient illumination, e.g. dawn or dusk sensors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V25/00—Safety devices structurally associated with lighting devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V3/00—Globes; Bowls; Cover glasses
- F21V3/04—Globes; Bowls; Cover glasses characterised by materials, surface treatments or coatings
- F21V3/06—Globes; Bowls; Cover glasses characterised by materials, surface treatments or coatings characterised by the material
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21W—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
- F21W2111/00—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00
- F21W2111/04—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00 for waterways
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO THE FORM OR THE KIND OF THE LIGHT SOURCES OR OF THE COLOUR OF THE LIGHT EMITTED
- F21Y2115/00—Light-generating elements of semiconductor light sources
- F21Y2115/10—Light-emitting diodes [LED]
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Power Engineering (AREA)
- Arrangement Of Elements, Cooling, Sealing, Or The Like Of Lighting Devices (AREA)
Abstract
The invention provides a solar aviation obstruction light which comprises a light body, a solar charging panel and an energy storage box, wherein a storage battery and a circuit board electrically connected with the storage battery are arranged in the energy storage box, and the light body and the solar charging panel are arranged on the outer wall of the energy storage box and are electrically connected with the circuit board. According to the invention, the solar charging panel electrically connected with the storage battery is arranged on the outer wall of the energy storage box, the solar charging panel absorbs solar energy and converts the solar energy into electric energy to be stored in the storage battery, so that the aviation obstruction light can still perform marking work when an external power supply is powered off or damaged, the occurrence probability of aviation accidents is reduced, and the safety and the use limitation of the aviation obstruction light are improved.
Description
[ technical field ] A method for producing a semiconductor device
The invention relates to a barrier lamp, in particular to a solar aviation barrier lamp.
[ background of the invention ]
The Aviation Obstruction light (also called as navigation light equipment) is a special lamp for marking obstacles, and has the advantages of energy conservation, environmental protection, safety, simple and convenient installation, automatic control, green lighting, low power consumption, long service life, no radiation, high stability and the like. The aviation obstruction light marks the potential aviation danger obstruction such as a square tower, a building, a lighting beacon of a large open stadium, a high-voltage power transmission tower and the like through a normally bright or flickering red light.
The existing aviation obstruction light needs to be connected with an external power supply, so that the obstruction cannot be identified under the condition that the external power supply is powered off or damaged, the probability of occurrence of an aviation accident is greatly improved, and the safety and the use limitation of the aviation obstruction light are low.
Therefore, there is a need for an improved structure of the above-mentioned aviation obstruction light.
[ summary of the invention ]
The technical problem to be solved by the invention is as follows: the utility model provides a solar energy aviation obstruction beacon, the lower problem of security and the use limitation of aviation obstruction beacon among the solution prior art.
In order to solve the technical problems, the invention adopts the technical scheme that:
the embodiment of the invention provides a solar aviation obstruction light, which comprises: the solar energy charging device comprises a lamp body, a solar charging panel and an energy storage box, wherein a storage battery and a circuit board electrically connected with the storage battery are arranged in the energy storage box, and the lamp body and the solar charging panel are both arranged on the outer wall of the energy storage box and are both electrically connected with the circuit board.
In some embodiments, the solar aviation obstruction light further comprises: the support, the support sets up on the energy storage box, lamp body and solar charging panel all set up on the support.
In some embodiments, the stent comprises: plane portion reaches and follows plane portion is to keeping away from the rake of plane portion direction slope, the energy storage box is located plane portion one side, the lamp body is located plane portion is kept away from energy storage box one side, solar charging panel locates the rake.
In some embodiments, the solar aviation obstruction light further comprises: the base is arranged on the energy storage box and is far away from one side of the lamp body.
In some embodiments, a control module is integrated on the circuit board, and the outer wall of the energy storage box is provided with at least one sensor electrically connected with the control module.
In some implementations, the type of sensor includes at least one of a temperature sensor, a humidity sensor, a concentration sensor, and a light sensitive sensor.
In some embodiments, the lamp body includes: the lamp shade and locate in the lamp shade and with the light source that the circuit board electricity is connected.
In some embodiments, the light source is an LED light source.
In some embodiments, the material of the lamp cover is a transparent material, and the material of the energy storage box is an aluminum alloy.
In some embodiments, the solar aviation obstruction light further comprises: the lightning rod sets up the lamp shade is kept away from energy storage box one side, and the part stretches into the lamp shade, the lightning rod stretches into lamp shade partial ground connection.
From the above description, compared with the prior art, the invention has the following beneficial effects:
set up the solar charging panel of being connected with the battery electricity at energy storage box outer wall, solar charging panel absorbs solar energy to convert solar energy into the electric energy and save in the battery, make when external power outage or damage, the aviation obstruction light still can carry out sign work, reduces the emergence probability of aviation accident, promotes the security and the use limitation of aviation obstruction light.
[ description of the drawings ]
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below. It is to be understood that the drawings in the following description are of some, but not all, embodiments of the invention. For a person skilled in the art, other figures can also be obtained from the provided figures without inventive effort.
FIG. 1 is a schematic structural diagram of a solar aviation obstruction light provided by an embodiment of the invention;
fig. 2 is another schematic structural diagram of a solar aviation obstruction light provided by the embodiment of the invention.
[ detailed description ] embodiments
For purposes of promoting a clear understanding of the objects, aspects and advantages of the invention, reference will now be made in detail to the present embodiments of the invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements throughout. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention. In addition, the technical features involved in the embodiments of the present invention described below may be combined with each other as long as they do not conflict with each other.
Referring to fig. 1, fig. 1 is a schematic structural diagram of a solar aviation obstruction light according to an embodiment of the present invention.
As shown in fig. 1, an embodiment of the invention provides a solar aviation obstruction light, which includes a light body 1, a solar charging panel 2 and an energy storage box 3, wherein a storage battery (not shown) and a circuit board (not shown) electrically connected to the storage battery are disposed in the energy storage box 3, and the light body 1 and the solar charging panel 2 are both disposed on an outer wall of the energy storage box 3 and are both electrically connected to the circuit board.
In practical application, solar energy is absorbed by solar charging panel 2 to convert solar energy into electric energy and store in the battery, and when the external power supply that aviation obstruction light is connected cuts off the power supply or damages, lamp body 1 can utilize the electric energy of storage in the battery to carry out sign work. It can be understood that when the lamp body 1 performs the marking operation, the lamp body can emit a normally bright red light, or a flashing red light, or lights with other colors, which is not limited in the embodiment of the present invention.
As an example, the solar charging panel 2 may be a high-efficiency silicon solar panel, the storage battery may be a high-efficiency low-temperature maintenance-free storage battery, and a power supply system composed of the high-efficiency silicon solar panel and the high-efficiency low-temperature maintenance-free storage battery can ensure that the solar aviation obstruction light normally works for at least 20 days in continuous rainy days.
Referring to fig. 2, fig. 2 is another schematic structural diagram of a solar aviation obstruction light according to an embodiment of the present invention.
As a feasible implementation manner, the solar aviation obstruction light may further include a bracket 4, the bracket 4 needs to be disposed on the energy storage box 3, and the lamp body 1 and the solar charging panel 2 are both disposed on the bracket 4, so as to ensure connection stability between the lamp body 1, the solar charging panel 2 and the energy storage box 3. Specifically, as shown in fig. 2, the bracket may include a planar portion 41 and an inclined portion 42 inclined along the planar portion 41 in a direction away from the planar portion 41, in this case, the energy storage tank 3 is disposed on one side of the planar portion 41, the lamp body 1 is disposed on one side of the planar portion 41 away from the energy storage tank 3, and the solar charging panel 3 is disposed on the inclined portion 42. It is understood that, in other embodiments, the structural composition of the bracket 4 is not limited to the above form, and may be other structural compositions having the same or similar functions, which is not limited by the embodiment of the present invention.
Further, in order to ensure the overall stability of the lamp body 1, the solar charging panel 2, the energy storage box 3 and the support 4, the solar aviation obstruction light can further comprise a base 5, and the base 5 needs to be arranged on one side of the energy storage box 3 away from the lamp body 1. It can be understood that, when the solar aviation obstruction light is located on the installation surface, the side of the base 5 away from the energy storage box 3 contacts the installation surface, and the end of the inclined portion 42 of the bracket 4 close to the installation surface may contact the installation surface or may be spaced from the installation surface, which is not limited in the embodiment of the present invention.
Furthermore, as shown in fig. 2, in order to implement the automatic control function of the solar aviation obstruction light, the solar aviation obstruction light may further include a sensor 6 disposed on an outer wall of the energy storage box 3, and a control module integrated on the circuit board and electrically connected to the sensor 6, wherein when the sensor 6 detects that an external environment changes, the control module controls the light body 1 to perform an identification operation according to a detection result of the sensor 6. As an example, when the external environment is fog, the sensor 6 may be a concentration sensor, and controls the identification of the lamp body 1 to work by detecting whether the concentration of the external environment reaches a preset threshold; when the external environment is at night, the sensor 6 can be a photosensitive sensor, and controls the identification work of the lamp body 1 by detecting whether the brightness of the external environment is lower than a preset threshold value; when external environment is rainy weather, the sensor 6 can be the combination of humidity transducer and temperature sensor, and whether humidity and temperature through detecting external environment reach the predetermined threshold value, the sign work of control lamp body 1. It is understood that the type and number of the sensors 6 are determined according to a specific application scenario, and the embodiment of the present invention is not limited thereto.
As another possible implementation, the lamp body 1 in the solar aviation obstruction light is composed of a lamp shade 11 and a light source arranged in the lamp shade 11, and in this case, the light source needs to be electrically connected with a circuit board. The light source in the lamp housing 11 may be an LED light source, or other types of light sources, which is not limited in the embodiment of the present invention.
It can be understood that, in order to ensure that the light source in the lamp shade 11 can play the role of identification, the material of the lamp shade 11 needs to adopt a transparent material, and in order to ensure the sealing and waterproof effect of the energy storage box 3, the material of the energy storage box 3 can adopt an aluminum alloy and apply a watertight structure.
In addition, as shown in fig. 2, in order to avoid damaging the aviation obstruction light by lightning in rainy weather, the solar aviation obstruction light may further include a lightning rod 7 disposed on one side of the lampshade 11 far away from the energy storage box 3, the lightning rod 7 partially extends into the lampshade 11, and the lightning rod 7 partially extends into the lampshade 11 and is grounded. In practical application, the thunder and lightning can be led into the ground through the lightning rod 7, and then the phenomenon that the aviation obstruction light is damaged by the thunder and lightning is avoided.
It should be noted that, in the summary of the present invention, each embodiment is described in a progressive manner, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments may be referred to each other.
It is further noted that, in the present disclosure, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present disclosure. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined in this disclosure may be applied to other embodiments without departing from the spirit or scope of the disclosure. Thus, the present disclosure is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (10)
1. A solar aviation obstruction light, comprising: the solar energy charging device comprises a lamp body, a solar charging panel and an energy storage box, wherein a storage battery and a circuit board electrically connected with the storage battery are arranged in the energy storage box, and the lamp body and the solar charging panel are both arranged on the outer wall of the energy storage box and are both electrically connected with the circuit board.
2. The solar aviation obstruction light of claim 1, further comprising: the support, the support sets up on the energy storage box, lamp body and solar charging panel all set up on the support.
3. The solar aviation obstruction light of claim 2, wherein the bracket comprises: plane portion reaches and follows plane portion is to keeping away from the rake of plane portion direction slope, the energy storage box is located plane portion one side, the lamp body is located plane portion is kept away from energy storage box one side, solar charging panel locates the rake.
4. The solar aviation obstruction light of claim 3, further comprising: the base is arranged on the energy storage box and is far away from one side of the lamp body.
5. The solar aviation obstruction light of claim 1, wherein a control module is integrated on the circuit board, and the outer wall of the energy storage box is provided with at least one sensor electrically connected with the control module.
6. The solar aviation obstruction light of claim 5, wherein the type of sensor comprises at least one of a temperature sensor, a humidity sensor, a concentration sensor, and a light sensitive sensor.
7. The solar aviation obstruction light of claim 1, wherein the light body comprises: the lamp shade and locate in the lamp shade and with the light source that the circuit board electricity is connected.
8. The solar aviation obstruction light of claim 7, wherein the light source is an LED light source.
9. The solar aviation obstruction light of claim 8, wherein the material of the light shade is a transparent material, and the material of the energy storage tank is an aluminum alloy.
10. The solar aviation obstruction light of claim 7, further comprising: the lightning rod sets up the lamp shade is kept away from energy storage box one side, and the part stretches into the lamp shade, the lightning rod stretches into lamp shade partial ground connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011230014.4A CN112161247A (en) | 2020-11-06 | 2020-11-06 | Solar aviation obstruction beacon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011230014.4A CN112161247A (en) | 2020-11-06 | 2020-11-06 | Solar aviation obstruction beacon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112161247A true CN112161247A (en) | 2021-01-01 |
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ID=73865632
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011230014.4A Pending CN112161247A (en) | 2020-11-06 | 2020-11-06 | Solar aviation obstruction beacon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112161247A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115628420A (en) * | 2022-09-07 | 2023-01-20 | 广州市新航科技有限公司 | Dual supply aviation obstruction beacon |
-
2020
- 2020-11-06 CN CN202011230014.4A patent/CN112161247A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115628420A (en) * | 2022-09-07 | 2023-01-20 | 广州市新航科技有限公司 | Dual supply aviation obstruction beacon |
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