KR20170005659A - The aerial flashing light equipment using electromagnetic inductive method - Google Patents

The aerial flashing light equipment using electromagnetic inductive method Download PDF

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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
Application number
KR1020150096023A
Other languages
Korean (ko)
Inventor
허영민
범철원
김남훈
Original Assignee
조선대학교산학협력단
허영민
범철원
Priority date (The priority date 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 date listed.)
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Application filed by 조선대학교산학협력단, 허영민, 범철원 filed Critical 조선대학교산학협력단
Priority to KR1020150096023A priority Critical patent/KR20170005659A/en
Publication of KR20170005659A publication Critical patent/KR20170005659A/en

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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

The present invention relates to an aircraft warning light using magnetic induction. The aircraft warning light is installed at an overhead ground wire for protecting a high-voltage transmission line, which generates a magnetic field, from a stroke of lightning so as to ensure an aircraft pilot to recognize the transmission line by day and night. The aircraft warning light includes: an aircraft warning sphere provided therein with a light-emitting body to visually recognize whether a high-voltage transmission line is installed; a connection joint for fixing the aircraft warning sphere to an overhead ground wire; 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 aircraft warning sphere is detachably attached to the magnetic induction unit, and the light-emitting body is turned on by the electric power generated by the magnetic induction through the magnetic induction unit.

Description

[0001] The present invention relates to an aerial flashing light equipment using an electromagnetic induction method,

[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 flanges 152 and 154, a rim 164, And includes a top hemisphere 100a and a bottom hemisphere 100b each including a nozzle 140, a rim fastener member 162, and a passageway 170, respectively.

A flange fastening member 156 and a rim fastening member 162 for reinforcing the coupling strength of the upper hemispherical 100a and the lower hemisphere 100b are also included.

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 conventional display device 100 includes a method of applying a phosphorescent material to the surface of the display device 100, a method of using a battery and a light emitting element, a method of using a solar cell and a light emitting element Is commonly used.

However, in the method of applying the phosphorescent material to the display 100, the light is gradually weakened as time elapses after sunset, and the night identification means can not fulfill its role.

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 air disturbance indicator 200 using the magnetic induction method according to an embodiment of the present invention includes a high-voltage transmission line 310 for generating a magnetic field, a high-voltage transmission line 310 for generating a magnetic field, And an aviation obstacle indicator installed on the ground line 320. The aviation obstacle indicator is installed on the ground line 320 for protecting the ground line 320. The high- (210).

In this case, the aviation obstacle 210 may have various shapes, but the aviation obstacle 210 according to an embodiment of the present invention may detect whether the aviation obstacle 210 exists in all directions, In such a way that it can be recognized by the naked eye of the user.

The surface of the obstacle 210 may be painted with various colors, but it is preferably painted with a red color including orange so as to secure the visibility distance during the daytime.

Meanwhile, the air obstacle 210 is generally suspended at a high altitude, and thus, there is a problem that the air obstacle severely swings upward, downward, leftward and rightward due to strong winds.

Accordingly, in order to solve the above-mentioned problem, the air disturbance indicator 200 using the magnetic induction method according to an embodiment of the present invention includes a plurality of dimples (dimple) ) 211 are formed.

Meanwhile, the air disturbance indicator 200 using the magnetic induction method according to the embodiment of the present invention is provided with a light emitter 212 inside the air obstacle 210.

At this time, the light emitting body 212 is a means for lighting light at night, and the light emitting body 212 is lighted so that the pilot or pilot can easily identify the air obstacle 210 at night.

Meanwhile, the light emitting unit 212 may use various light emitting means. In an embodiment of the present invention, a xenon lamp or an LED lamp is used.

At this time, the xenon lamp is used in the case where the air obstacle 210 is installed in an unusual area, and in a region where the air conditioner is applied, the lamp 212 serves as a street light illuminating the applied area An LED lamp may be used instead of the xenon lamp.

However, in the embodiment of the present invention, corrosion resistance and durability due to rainwater or the like may be enhanced. In particular, the air obstacle 210 may include a light emitting body 210 212 are made of reinforced plastic of translucent material so that light of the inside of the air obstruction 210 can be transmitted to the outside.

Meanwhile, the aerial failure indicator 200 using the magnetic induction method according to an embodiment of the present invention includes a connection joint 220 for fixing the air obstacle 210 to the ground line 320.

As shown in FIGS. 2 and 3, the connection joint 220 includes a U-shaped clamp 221, which is open at the top and surrounds the outer peripheral surface of the ground wire 320, And a tightening pin 223 inserted into the hole 222 formed in the upper portion of the clamp 221 in a state of wrapping the ground wire 320 to tighten the upper opening portion of the clamp 221.

As a result, the air obstacle 210 seats the ground wire 320 through the upper opening portion of the clamp 221 and then passes the upper opening portion of the clamp 221 through the tightening pin 223 And tightly fixes the airbag 210 on the ground line 320 by tightening.

Meanwhile, the aerial failure indicator 200 using the magnetic induction method according to an embodiment of the present invention is provided at the lower portion of the connection joint 220 and induces a magnetic field generated in the high voltage transmission line 310 to generate electric power And a magnetic induction unit 230 for generating and storing.

Generally, the high-voltage transmission line 310 transmits a high-voltage alternating-current power to a line provided for sending power generated by a power plant to a certain area.

At this time, since a high-voltage AC power flows through the transmission line 310, a strong magnetic field is generated around the transmission line 310.

The present invention generates and stores electric power for lighting the light emitting body 212 by inducing a magnetic field generated in the transmission line 310 through the magnetic induction unit 230.

Meanwhile, the air obstacle 210 is detached from the magnetic induction unit 230 provided below the connection joint 220.

In this case, various methods can be used for the attachment / detachment of the air obstruction 210 and the magnetic induction unit 230. However, in an embodiment of the present invention, as shown in FIGS. 3 and 4, And a nut 231 integrally formed with the magnetic induction unit 230 at a lower portion of the magnetic induction unit 230. The air induction hole 210 is formed in the magnetic induction unit 230, (Not shown).

The bolt 213 and the nut 231 are electrically connected to each other through the bolt 213 and the bolt 213. The bolt 213 is electrically connected to the light emitting body 212 so that electric power generated through the self- And transmits the light to the light emitting body 212 through the bolt 231 and the bolt 213 to light the light emitting body 212.

Meanwhile, the air disturbance indicator 200 using the self-induction method according to an embodiment of the present invention may include a timer or illuminance control unit for controlling the lighting time of the illuminant 212 on the outside or inside of the air obstruction 210, A sensor (not shown) is provided.

In this regard, the light emitter 212 is turned on to allow the pilot or the pilot to visually check the presence or absence of the transmission line on the flight route at night, as described above.

Therefore, the continuous lighting of the light emitting body 212 during the day has a problem of shortening the lifetime due to power consumption and abuse of the illuminated light emitting body.

In order to solve the above-mentioned problem, in one embodiment of the present invention, the timer is provided so that the light emitting body 212 can be turned on only from 1800 to 0600 the next day.

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 illuminant 212 only at night.

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)

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 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.
The method according to claim 1,
Wherein the light emitting unit comprises a xenon lamp or an LED lamp.
3. The method according to claim 1 or 2,
Wherein the air obstacle is provided with a timer or an illuminance sensor for controlling the lighting time of the illuminant.
3. The method according to claim 1 or 2,
And a plurality of dimples for reducing the air resistance applied to the air obstacle is formed on the surface of the air obstacle.
KR1020150096023A 2015-07-06 2015-07-06 The aerial flashing light equipment using electromagnetic inductive method KR20170005659A (en)

Priority Applications (1)

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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

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KR20170005659A true KR20170005659A (en) 2017-01-16

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Cited By (5)

* Cited by examiner, † Cited by third party
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

Cited By (5)

* Cited by examiner, † Cited by third party
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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