KR20170005659A - The aerial flashing light equipment using electromagnetic inductive method - Google Patents
The aerial flashing light equipment using electromagnetic inductive method Download PDFInfo
- Publication number
- KR20170005659A KR20170005659A KR1020150096023A KR20150096023A KR20170005659A KR 20170005659 A KR20170005659 A KR 20170005659A KR 1020150096023 A KR1020150096023 A KR 1020150096023A KR 20150096023 A KR20150096023 A KR 20150096023A KR 20170005659 A KR20170005659 A KR 20170005659A
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- KR
- South Korea
- Prior art keywords
- magnetic induction
- transmission line
- air
- obstacle
- voltage transmission
- Prior art date
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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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21K—NON-ELECTRIC LIGHT SOURCES USING LUMINESCENCE; LIGHT SOURCES USING ELECTROCHEMILUMINESCENCE; LIGHT SOURCES USING CHARGES OF COMBUSTIBLE MATERIAL; LIGHT SOURCES USING SEMICONDUCTOR DEVICES AS LIGHT-GENERATING ELEMENTS; LIGHT SOURCES NOT OTHERWISE PROVIDED FOR
- F21K9/00—Light sources using semiconductor devices as light-generating elements, e.g. using light-emitting diodes [LED] or lasers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21S—NON-PORTABLE LIGHTING DEVICES; SYSTEMS THEREOF; VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLE EXTERIORS
- F21S2/00—Systems of lighting devices, not provided for in main groups F21S4/00 - F21S10/00 or F21S19/00, e.g. of modular construction
- F21S2/005—Systems of lighting devices, not provided for in main groups F21S4/00 - F21S10/00 or F21S19/00, e.g. of modular construction of modular construction
-
- 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
- F21V17/00—Fastening of component parts of lighting devices, e.g. shades, globes, refractors, reflectors, filters, screens, grids or protective cages
- F21V17/10—Fastening of component parts of lighting devices, e.g. shades, globes, refractors, reflectors, filters, screens, grids or protective cages characterised by specific fastening means or way of fastening
-
- 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
-
- 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
- F21V3/049—Patterns or structured surfaces for diffusing light, e.g. frosted surfaces
-
- 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
- F21V33/00—Structural combinations of lighting devices with other articles, not otherwise provided for
- F21V33/0064—Health, life-saving or fire-fighting equipment
- F21V33/0076—Safety or security signalisation, e.g. smoke or burglar alarms, earthquake detectors; Self-defence devices
-
- H05B37/0281—
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Computer Security & Cryptography (AREA)
- Environmental & Geological Engineering (AREA)
- Physics & Mathematics (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Optics & Photonics (AREA)
- Non-Portable Lighting Devices Or Systems Thereof (AREA)
Abstract
Description
[0001] The present invention relates to an airbag indicator using a magnetic induction system, and more particularly, to an airbag indicator using a magnetic induction method for providing an identification of a transmission line of an airplane pilot in a day or night by installing the airbag indicator on a ground wire for protecting a high- The present invention relates to an airbag indicator lamp using an airbag.
Generally, the ground wire for protecting the high-voltage transmission line or the communication line or the transmission line from lightning is connected to each other by a transmission tower or the like. However, a helicopter such as a helicopter or an airplane, It is very difficult.
Therefore, the aircraft obstacle display device is suspended on the processing branch line between the transmission towers, so that the pilot will notice the emergence of the transmission line.
On the other hand, the conventional air traffic obstacle display device is colored with a predetermined color and is used as a daytime identification means, including a light emission means, as a nighttime identification means.
Since the conventional airborne obstacle display device is suspended in a high angle, it is strongly influenced by the wind and swings vertically and horizontally, so that it is formed into a streamline or spherical shape in order to reduce it to some extent.
1, which is a perspective view of an airborne obstacle display device according to the related art, a conventional airborne obstacle display device includes
A flange fastening member 156 and a
Meanwhile, in order to improve the efficiency of visual identification, conventionally, the airborne obstacle display area is generally colored with orange or the like so as to reflect sunlight well.
In addition, a method of using the luminous material as a night identification means of the
However, in the method of applying the phosphorescent material to the
In addition, a method of using a battery and a light emitting element is inconvenient to replace a battery, and maintenance and maintenance thereof are expensive.
Accordingly, a method using a solar cell and a light emitting element is currently used as the most useful means, which is variously disclosed in the registered patent No. 10-0400260.
Meanwhile, in the above patent, the solar cell is placed in an upper part of the upper hemisphere to generate electricity by locating the solar cell, the light emitting element is positioned inside the display sphere, and the electricity generated by the solar cell is emitted. Lt; RTI ID = 0.0 > optical < / RTI >
However, the above-described method has a problem in that it is difficult to protect the optical fiber from the external environment, and there are problems such as difficulty in manufacturing and increase in manufacturing cost.
Further, since the solar cell is located only at the upper end of the display, it is not effectively exposed to the sunlight, so that it is difficult to smoothly supply power to the light emitting device.
The present invention has been made to solve the above-mentioned problems, and it is an object of the present invention to provide a high-voltage transmission line which can induce a magnetic field of a high voltage transmission line without using a battery or a solar module, The purpose is to provide airborne fault indicators using induction method.
Another object of the present invention is to provide an aviation obstacle indicator using a magnetic induction system capable of mixing an aviation disturbance indicator and a street light depending on the selection of an illuminant.
In addition, a timer or an illuminance sensor for preventing the illuminator from lighting during the day is provided to prevent abuse of the luminous body, and dimples are formed on the surface of the airborne obstacle, Another object of the present invention is to provide an air fault indicator using a magnetic induction method.
In the meantime, the objects of the present invention are not limited to the above-mentioned objects, and other objects not mentioned can be clearly understood by those skilled in the art from the following description.
The present invention provides a high-voltage transmission line for generating a magnetic field, a ground line for protecting the transmission line from a lightning stroke, and an air disturbance indicator installed on the ground line, An aviation obstacle provided with an illuminant inside so as to be visually distinguished; A connecting joint for fixing the air obstacle to the ground line; And a magnetic induction unit provided at a lower portion of the connection joint for generating and storing electric power by inducing a magnetic field generated in the high voltage transmission line, wherein the air obstacle is detached from the magnetic induction unit, Lt; / RTI >
Preferably, the light emitting unit may comprise a xenon lamp or an LED lamp.
Preferably, the air obstacle may be provided with a timer or an illuminance sensor for adjusting the lighting time of the illuminator, and a surface of the air obstacle may be provided with a plurality of dimples for reducing the air resistance applied to the air obstacle, .
The present invention has the following excellent effects.
First, it induces the magnetic field of the high-voltage transmission line without the need of the battery or the photovoltaic module and uses it as the power of the luminous body, so that it can be used semi-permanently and maintenance cost is low.
In addition, according to the selection of the light emitting body, it is possible to use the air disturbance indicator and the streetlight in combination, and a timer or an illuminance sensor for preventing the light emitting body from being turned on during the day can be provided to prevent abuse of the light emitting body.
In addition, dimples are formed on the surface of the air obstacle so as to prevent the air obstacle indicator from fluctuating due to the air resistance.
1 is a perspective view of an airborne obstacle indicator according to the prior art.
2 is a perspective view of an airborne fault indicator using a magnetic induction method according to the present invention.
FIG. 3 is an exploded perspective view of an air disturbance indicator using a magnetic induction method according to the present invention. FIG.
Fig. 4 is a vertical sectional view of the air-obstacle indicator using the magnetic induction method shown in Fig.
FIG. 5 is a state of use of the aerial failure indicator using the magnetic induction method shown in FIG.
The term used in the present invention is a general term that is widely used at present. However, in some cases, there is a term selected arbitrarily by the applicant. In this case, the term used in the present invention It is necessary to understand the meaning.
Hereinafter, the technical structure of the present invention will be described in detail with reference to preferred embodiments shown in the accompanying drawings.
FIG. 2 is an exploded perspective view of an aviation obstacle indicator using a magnetic induction method according to the present invention, FIG. 4 is an exploded perspective view of an aviation obstacle indicator using the magnetic induction method according to the present invention, FIG. 5 is a use state of the air disturbance indicator using the magnetic induction system shown in FIG. 1. FIG.
2 to 5, the
In this case, the
The surface of the
Meanwhile, the
Accordingly, in order to solve the above-mentioned problem, the
Meanwhile, the
At this time, the
Meanwhile, the
At this time, the xenon lamp is used in the case where the
However, in the embodiment of the present invention, corrosion resistance and durability due to rainwater or the like may be enhanced. In particular, the
Meanwhile, the
As shown in FIGS. 2 and 3, the
As a result, the
Meanwhile, the
Generally, the high-
At this time, since a high-voltage AC power flows through the
The present invention generates and stores electric power for lighting the
Meanwhile, the
In this case, various methods can be used for the attachment / detachment of the
The
Meanwhile, the
In this regard, the
Therefore, the continuous lighting of the
In order to solve the above-mentioned problem, in one embodiment of the present invention, the timer is provided so that the
Also, in order to achieve the same purpose as the timer, the illuminance sensor may be provided to sense the amount of light of main and night sun and light the
As a result, the air-obstacle indicator using the self-induction method according to an embodiment of the present invention induces the magnetic field of the high-voltage transmission line without using a battery or a solar module through the technical constructions described above, It can be used semi-permanently and its maintenance cost is low.
In addition, according to the selection of the light emitting body, it is possible to use a combination of the air disturbance indicator light and the street light, and a timer or an illuminance sensor for preventing the light emitting body from being turned on during the day can be provided to prevent abuse of the light emitting body, So that it is possible to prevent the fluctuation of the air disturbance indicator according to the air resistance.
While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, it is clearly understood that the same is by way of illustration and example only and is not to be taken by way of limitation in the present invention. Various changes and modifications may be made by those skilled in the art.
200: Aviation trouble indicator using magnetic induction method
210: Aviation obstacle
211: dimple
212:
213: Bolt
220: connection joint
221: Clamp
222: hole
223: tightening pin
230: magnetic induction portion
231: Nuts
310: High voltage transmission line
320: Machined branch line
Claims (4)
An aviation obstacle provided with an illuminant inside so as to visually identify whether the high-voltage transmission line is installed;
A connecting joint for fixing the air obstacle to the ground line; And
And a magnetic induction unit provided at a lower portion of the connection joint for generating and storing electric power by inducing a magnetic field generated from the high voltage transmission line,
Wherein the air obstacle is detached from the magnetic induction portion, and the light emitting body is illuminated with electric power induced through the magnetic induction portion.
Wherein the light emitting unit comprises a xenon lamp or an LED lamp.
Wherein the air obstacle is provided with a timer or an illuminance sensor for controlling the lighting time of the illuminant.
And a plurality of dimples for reducing the air resistance applied to the air obstacle is formed on the surface of the air obstacle.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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KR1020150096023A KR20170005659A (en) | 2015-07-06 | 2015-07-06 | The aerial flashing light equipment using electromagnetic inductive method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150096023A KR20170005659A (en) | 2015-07-06 | 2015-07-06 | The aerial flashing light equipment using electromagnetic inductive method |
Publications (1)
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KR20170005659A true KR20170005659A (en) | 2017-01-16 |
Family
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KR1020150096023A KR20170005659A (en) | 2015-07-06 | 2015-07-06 | The aerial flashing light equipment using electromagnetic inductive method |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101886191B1 (en) | 2017-08-16 | 2018-08-08 | 한국전력공사 | Light emitting apparatus installed power line and light emitting system in power line |
KR102053124B1 (en) | 2019-08-14 | 2019-12-11 | (주)신아엔지니어링 | High-voltage electrical safety signs |
KR102115408B1 (en) * | 2019-11-11 | 2020-05-27 | (주)신우기업 | Light assembly for rafter |
KR20200118547A (en) | 2019-04-08 | 2020-10-16 | 주식회사 신성일렉스 | Aviation obstacle lights for suspended power line |
KR102195398B1 (en) * | 2020-09-29 | 2020-12-28 | 조복연 | Aviation obstable indicator with vibration prevention |
-
2015
- 2015-07-06 KR KR1020150096023A patent/KR20170005659A/en not_active Application Discontinuation
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101886191B1 (en) | 2017-08-16 | 2018-08-08 | 한국전력공사 | Light emitting apparatus installed power line and light emitting system in power line |
KR20200118547A (en) | 2019-04-08 | 2020-10-16 | 주식회사 신성일렉스 | Aviation obstacle lights for suspended power line |
KR102053124B1 (en) | 2019-08-14 | 2019-12-11 | (주)신아엔지니어링 | High-voltage electrical safety signs |
KR102115408B1 (en) * | 2019-11-11 | 2020-05-27 | (주)신우기업 | Light assembly for rafter |
KR102195398B1 (en) * | 2020-09-29 | 2020-12-28 | 조복연 | Aviation obstable indicator with vibration prevention |
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