KR101057037B1 - Aviation fault indicator for transmission cable with flashing signal - Google Patents

Aviation fault indicator for transmission cable with flashing signal Download PDF

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Publication number
KR101057037B1
KR101057037B1 KR1020090024777A KR20090024777A KR101057037B1 KR 101057037 B1 KR101057037 B1 KR 101057037B1 KR 1020090024777 A KR1020090024777 A KR 1020090024777A KR 20090024777 A KR20090024777 A KR 20090024777A KR 101057037 B1 KR101057037 B1 KR 101057037B1
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South Korea
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transmission cable
power transmission
aviation
failure indicator
flasher
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KR1020090024777A
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Korean (ko)
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KR20100106692A (en
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김주영
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김주영
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    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G1/00—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines
    • H02G1/02—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables
    • 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
    • F21V15/00—Protecting lighting devices from damage
    • F21V15/01—Housings, e.g. material or assembling of housing parts
    • 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
    • F21S9/037—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 and the lighting unit being located within or on the same housing
    • 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
    • F21V21/008—Suspending from a cable or suspension line
    • 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
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G7/00—Overhead installations of electric lines or cables
    • 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
    • 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]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
    • Y02B20/00—Energy efficient lighting technologies, e.g. halogen lamps or gas discharge lamps
    • Y02B20/30—Semiconductor lamps, e.g. solid state lamps [SSL] light emitting diodes [LED] or organic LED [OLED]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/50—Photovoltaic [PV] energy

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Locating Faults (AREA)
  • Non-Portable Lighting Devices Or Systems Thereof (AREA)
  • Suspension Of Electric Lines Or Cables (AREA)

Abstract

본 발명은 점멸신호기가 구비된 송전 케이블용 항공장애표시구에 관한 것으로서, 더욱 상세히 설명하면 송전탑 간에 연결된 송전 케이블의 중간에 설치하여 계절변화에 따라 송전 케이블이 늘어지거나, 팽팽해지는 변화에 따라 합선 및 방전되는 것을 방지하도록 평행하게 연결되는 다수개의 송전 케이블 간격을 유지하고, 주간에는 물론 악천후나 야간에도 헬리콥터와 같은 항공기가 운항중 송전 케이블에 걸리지 않도록 조종사에게 항공위험을 표시하게 점멸신호기가 부착되어 발광하는 것을 특징으로 한다.      The present invention relates to a aviation failure indicator for a transmission cable equipped with a flashing signal, and more specifically, installed in the middle of the transmission cable connected between the transmission tower, the transmission cable is stretched according to the seasonal change, the short circuit and the change in tension Maintains multiple transmission cable gaps connected in parallel to prevent discharge, and flashes with flashing signals to alert pilots of aviation hazards so that aircraft such as helicopters do not get caught in flight during daytime as well as in bad weather or at night Characterized in that.

송전탑, 점멸기, 항공장애표시구       Power transmission tower, flasher, aviation fault indicator

Description

점멸신호기가 구비된 송전 케이블용 항공장애표시구{Aviation obstacle indication device for power transmission cable to be equipped flickering a signal}   Aviation obstacle indication device for power transmission cable to be equipped flickering a signal}

본 발명은 항공장애표시구에 관한 것으로서, 더욱 상세히 설명하면 송전탑 간에 연결된 송전 케이블의 중간에 설치하여 계절변화에 따라 송전 케이블의 길이 변화에 따라 합선 및 방전되는 것을 방지하도록 다수개의 송전 케이블을 삽입 인출하여 서로 간격을 유지하고, 주간은 물론 악천후나 야간에도 헬리콥터와 같은 항공기가 운항중 송전 케이블에 걸리지 않도록 항공위험을 표시하는 점멸신호기가 부착되어 발광하는 것을 특징으로 한다.       The present invention relates to a aviation failure indicator, to be described in more detail installed in the middle of the transmission cable connected between the transmission tower inserted and pulled out a plurality of transmission cables to prevent the short-circuit and discharge according to the change in the length of the transmission cable according to the seasonal change By maintaining a distance from each other, and during the day as well as in bad weather or at night, the aircraft such as a helicopter is characterized in that the flashing signal indicating the aviation hazard is attached so as not to catch the transmission cable during operation.

일반적으로 송전탑은 발전소에서 만든 전력을 멀리 있는 공장이나 일반 가정 등으로 송전 케이블 통해 수송하는 과정을 송전이라 하며, 이때 사용하는 송전선로인 송전 케이블을 지지하기 위해 일정간격으로 설치하는 탑을 송전탑이라 한다.       In general, a transmission tower is a process of transporting electric power from a power plant to a distant factory or a general home through a transmission cable, and a tower that is installed at regular intervals to support a transmission cable, which is a transmission line used at this time, is called a transmission tower. .

이러한 송전탑은 오래전부터 존재해 왔던 것으로, 고압의 전압을 보내는데 사용되는 탑은 보통 강철로 만들어지고, 격자 브레이스(cross braces)에 의해 연결된 4개 이상의 레그를 가진다. Such transmission towers have existed for a long time, and towers used to transmit high voltages are usually made of steel and have four or more legs connected by cross braces.

상기 송전탑의 레그를 통해서는 다른 송전탑 간에 각각의 송전 케이블을 연결하고, 연결된 송전 케이블에는 수만에서 수십만 볼트의 고압이 흐르고 있기 때문에 여름철에는 높은 온도에 의해 길게 늘어나 흔들리며, 겨울철에는 차가운 온도에 의해 팽창된다.      Each transmission cable is connected between the other transmission towers through the legs of the transmission tower, and the connected transmission cable is tens of thousands to hundreds of thousands of volts of high voltage flowing in the summer, which is extended and shaken by high temperature in winter, and expands by cold temperature in winter. .

또한, 송전탑은 고압이 흐르기 때문에 인체에 유해한 전자파가 많이 발생하고, 감전의 위험을 항상 노출하고 있어 인적이 드문 곳에 주로 설치하는 데, 특히 산과 산 사이에 송전탑을 주로 설치하기 때문에 송전탑 사이에 연결된 송전 케이블에 헬리콥터가 운항중 걸리지않도록 조종사가 송전 케이블을 육안으로 용이하게 식별할 수 있게 어두운 색과 대비할 수 있는 밝은 색 계통의 항공위험 표시 기능을 갖는 구형상의 항공장애표시구를 송전 케이블 중간에 설치한다.       In addition, the transmission tower generates high frequency electromagnetic waves harmful to the human body due to the high pressure flow, and always exposes the risk of electric shock, so it is mainly installed in a rare place, especially because the transmission tower is installed between the mountains between the transmission towers A spherical aviation fault indicator is installed in the middle of the transmission cable with a light colored aviation hazard indication that allows the pilot to easily identify the transmission cable with the naked eye so that the cable does not get caught by the helicopter. .

또한, 상기 항공장애표시구는 고전압선로인 송전 케이블에 진동이 발생하면 멈추지 않고 계속 출렁거리기 때문에 송전탑 사이에 평행하게 지나가는 다수개의 송전 케이블이 서로 합선되지 않게 간격을 유지하는 애자기능도 함께 가지고 있다.       In addition, the aviation failure indicator has a insulator function that maintains a gap so that a plurality of transmission cables passing in parallel between transmission towers do not short circuit because they continue to move without stopping when vibration occurs in the transmission cable which is a high voltage line.

한편, 애자란 송전선이나 전기기기의 나선(裸線) 부분을 절연하고 동시에 기계적으로 유지 또는 지지하기 위하여 사용되는 자기(磁器)로 만든 것을 말한 것으로 종래에는 전기적으로 충분한 절연내력(絶緣耐力)이 필요로 하여 변질하지 않고 온도변화와 태양광 등의 환경에도 강한 기계력을 가지는 경질자기, 즉 점토, 석영, 장석(이하 세라믹이라고 칭하기로 한다)의 함량을 적당히 조절한 자기애자가 주로 사용되었다.      On the other hand, insulator is made of magnetic material used to insulate the spiral of transmission line or electric equipment and to maintain or support mechanically at the same time. Conventionally, sufficient electrical insulation strength is required. As a result, magnetic insulators with moderately controlled amounts of hard magnetics, that is, clays, quartz, and feldspar (hereinafter referred to as ceramics), which have a strong mechanical force even in environments such as temperature change and sunlight, are mainly used.

그러나 상기와 같이 송전탑 간에 각각의 레그에서 연결되는 송전 케이블의 중간에 설치되는 항공장애표시구는 주로 헬리콥터 등 항공기가 저공 비행을 할 때 조종사가 송전 케이블의 위치를 육안으로 식별할 수 있도록 하여 안전운항을 유도하나 야간이나 기상이 악조건일 때에는 조종사가 육안으로 식별하다는 것은 거의 불가능하여 안전사고의 위험성을 항상 가지고 있다.      However, as described above, the aviation failure indicators installed in the middle of the transmission cable connected to each leg between transmission towers mainly allow the pilot to visually identify the location of the transmission cable when the aircraft, such as a helicopter, fly low. Inducement, but at night or in bad weather conditions, it is almost impossible for the pilot to identify with the naked eye, so there is always a risk of a safety accident.

왜냐하면, 종래의 항공장애표시구는 주로 빨강색의 구형상을 갖는 절연체로 다수의 송전 케이블을 삽입 관통하여 간격을 유지할 수 있게 다수의 간격유지공이 형성된 구조로서, 송전케이블의 간격을 유지하는 기능은 아무런 문제가 없으나, 항공장애표시기능은 단순히 빨강색 안료를 혼합한 것으로서 야간이나 악천후에는 발광하지못하기 때문이다.      Because the conventional aviation failure indicator is a structure in which a plurality of gap retaining holes are formed to maintain a gap by inserting a plurality of transmission cables as an insulator mainly having a red spherical shape, there is no function to maintain the gap of transmission cables. There is no problem, but the aviation fault indication function is simply a mixture of red pigments, and it does not emit light at night or in bad weather.

따라서 상기와 같은 문제점을 해결하기 위한 수단으로 본 발명은 송전탑 사이에 설치된 항공장애표시구는 다수개의 송전 케이블을 삽입 인출하여 간격 유지는 물론 주간 및 야간이나 악천후에도 송전 케이블의 위치를 헬리콥터 조종사가 육안으로 식별할 수 있도록 자체 발광하는 점멸기를 부착하고, 송전탑의 송전케이블에 설치되는 장소의 특성상 한번 설치 후 유지보수를 할 수 없기 때문에 반영구적으로 점멸기에 안정적으로 전기를 공급할 수 있게 태양광 셀이 설치된 점멸신호기가 구비된 송전 케이블용 항공장애표시구를 제공한다.      Therefore, as a means for solving the above problems, the present invention is installed between the transmission tower, the aviation failure indicator is inserted and withdrawn a plurality of transmission cables to maintain the spacing as well as the location of the transmission cable during the day and night or bad weather helicopter pilot Blinker with self-illuminating flasher for identification, and solar cell is installed for stable supply of electricity to flasher semi-permanently because maintenance is not possible after installation once due to the nature of the place installed on the transmission cable of transmission tower. Provides a aviation failure indicator for the transmission cable is provided.

이상에서 설명한 것처럼 본 발명은 태양광셀에 의해 안정적으로 전원을 공급받기 때문에 주간 및 야간은 물론 기상조건이 악천후인 경우에 송전 케이블의 위치를 표시하기 위해 점멸기가 지속적으로 발광을 하기 때문에 항공기 조종사가 안전운항을 할 수 있도록 유도하는 효과가 있다.      As described above, since the present invention is stably supplied with solar cells, aircraft pilots are safe because the flasher continuously emits light to indicate the position of the transmission cable in bad weather as well as day and night. It is effective to induce navigation.

따라서 본 발명 항공장애표시구는 다수개의 송전 케이블이 합선되는 것을 방지하도록 간격을 유지하는 애자기능과 항공기의 안전운항을 유도하는 기능이 복합적으로 결합된 효과가 있다.      Therefore, the aviation failure indicator of the present invention has a combined effect of the insulator function to maintain the gap to prevent the short circuit of a plurality of power transmission cables and the function of inducing the safe operation of the aircraft.

이하 첨부된 도면에 의해 본 발명을 상세히 설명하면 다음과 같다.      Hereinafter, the present invention will be described in detail with reference to the accompanying drawings.

도 1은 본 발명 항공장애표시구를 도시해 보인 사시도 이고, 도 3은 본 발명 항공장애표시구를 도시해 보인 단면도이다.1 is a perspective view showing the present invention flight warning indicator, Figure 3 is a cross-sectional view showing the present invention flight warning indicator.

본 발명 항공장애표시구(1)는 송전탑(17) 사이를 연결하는 송전 케이블(12)의 간격을 유지하고, 송전 케이블(12)의 위치를 표시하도록 점멸 발광하는 구조로 이루어진다.      Aviation failure indicator 1 of the present invention is made of a structure that maintains the interval of the transmission cable 12 connecting between the power transmission tower 17, and blinks to emit light to indicate the position of the power transmission cable 12.

따라서 항공장애표시구(1)의 몸체(2)는 바람의 저항이 크지않도록 원통형상에 좌ㆍ우 양측이 밀폐된 구조를 갖는다.      Therefore, the body 2 of the aviation failure indicator 1 has a structure in which both the left and right sides are sealed on a cylindrical shape so that the wind resistance is not large.

한편, 상기 좌ㆍ우 양측은 몸체(2) 내부를 개폐할 수 있도록 볼트 또는 나선형을 따라 조임 체결할 수 있는 캡(15) 구조를 갖는 게 바람직하다.      On the other hand, the left and right sides preferably have a cap 15 structure that can be tightened fastening along the bolt or spiral to open and close the body (2).

또한, 몸체(2)의 좌우 양측에는 통공된 다수개의 간격유지공(8)이 형성되어 송전 케이블(12)이 삽입 관통되고, 송전 케이블(12)이 서로 합선되지않도록 간격을 유지하여 송전탑(17)에 연결된다.      In addition, the left and right sides of the body 2 are formed with a plurality of through-hole maintenance holes 8 are inserted through the power transmission cable 12 is inserted, the power transmission cable 12 by maintaining a gap so as not to short-circuit each other power transmission tower 17 )

상기 간격유지공(8)에는 송전 케이블(12)의 높은 전압에서 몸체(2) 및 기기를 보호할 수 있도록 길이방향으로 양측이 통공된 절연튜브(16)가 삽입된다.      Insulating tube (8) is inserted into the insulating tube 16 through both sides in the longitudinal direction so as to protect the body (2) and the device at a high voltage of the power transmission cable (12).

또한, 간격유지공(8)이 형성된 몸체의 좌ㆍ우 양측에는 태양광을 집광하여 직접 전력으로 변환하여 발전하는 태양광셀(7)을 부착한다.In addition, the left and right sides of the body on which the gap maintaining hole 8 is formed are attached with a solar cell 7 that collects sunlight and converts it directly into electric power.

상기 태양광셀(7)은 좌ㆍ우 양측 뿐만 아니라 몸체(2)의 외주면 둘레에 설치되는 점멸기(3)를 제외한 나머지 부분에도 태양광셀(7)을 부착하여 발전효율을 높일 수 있다.       The photovoltaic cell 7 may increase the power generation efficiency by attaching the photovoltaic cell 7 to not only the left and right sides but also the remaining parts except the flasher 3 installed around the outer circumferential surface of the body 2.

상기 태양광셀(7)은 다수개의 집진판으로 구성되어 몸체(2) 내부에 위치한 충전지(6)를 위치시켜 집진판에서 주간에 형성된 전기를 저장하다가 야간에 정전압회로를 통하여 점멸기(3) 내부의 램프(9)로 전압을 인가하여 램프(9)가 발광하도록 전기를 공급한다.      The photovoltaic cell 7 is composed of a plurality of dust collecting plates to position the rechargeable battery 6 located inside the body 2 to store the electricity formed during the day in the dust collecting plate and the lamp inside the flasher 3 through the constant voltage circuit at night ( A voltage is applied to 9 to supply electricity to the lamp 9 to emit light.

또한, 몸체(2)의 외주면 둘레에는 일정간격으로 부착되어 주간은 물론 야간 또는 악천후에 송전 케이블(12)의 위치를 표시하도록 발광하는 점멸기(3)가 부착된다.      In addition, around the outer circumferential surface of the body (2) is attached to the flasher (3) to emit light to indicate the position of the power transmission cable (12) during the day as well as night or bad weather is attached.

상기 점멸기(3)는 미리 설정된 프로그램에 의해 램프(9)를 자동으로 켰다 껐다 하면 점멸하여 발광하며, 램프(9)는 저전압을 사용하고 반영구적인 엘이디를 사용하는 게 바람직하다.      The flasher 3 flashes and emits light when the lamp 9 is automatically turned on and off by a preset program, and the lamp 9 preferably uses a low voltage and uses a semi-permanent LED.

또한, 상기 몸체(2) 내부에는 수납실(4)을 마련하여 태양광셀(7)에서 발생하 는 전기를 충전하는 충전지(6)를 설치하여 충전된 전기를 점멸기(3)로 공급하고, 상기 충전지(6)와 점멸기(3)를 제어하도록 리드선(14)에 의해 연결되어 전원공급 및 제어하는 제어부(5)가 설치된 구조이다.      In addition, the inside of the body (2) is provided with a charging chamber (6) for charging the electricity generated in the solar cell 7 by providing a storage chamber (4) to supply the charged electricity to the flasher (3), the rechargeable battery (6) and a control unit 5 connected by the lead wires 14 so as to control the flasher 3 to supply and control power.

도 2는 본 발명 항공장애표시구에 형광물질이 혼합된 것을 도시해 보인 사시도이다.      Figure 2 is a perspective view showing that the fluorescent material is mixed in the aviation failure indicator of the present invention.

본 발명 항공장애표시구(1)의 몸체(2)는 점멸기(3)가 발광할 때 램프(9)의 불빛에 의해 형광물질이 자극되어 점멸기(3)와 몸체(2) 전체가 발광하여 송전 케이블(12)의 위치를 더욱 확실하게 표현할 수 있도록 하는 것으로서, 몸체(2)를 제작할 때 형광물질(13)을 혼합하여 성형하거나 또는 외주면에 형광물질(13)을 도포할 수 있다.      In the present invention, the body 2 of the aviation failure indicator 1 has a fluorescent material stimulated by the light of the lamp 9 when the flasher 3 emits light so that the flasher 3 and the entire body 2 emit light to transmit power. In order to express the position of the cable 12 more reliably, when manufacturing the body 2, the fluorescent substance 13 may be mixed and molded, or the fluorescent substance 13 may be applied to the outer peripheral surface.

또한, 몸체(2)의 표면에는 형광물질(13)을 대신에 형광 테이프를 부착하여도 동일한 효과를 가질 수 있으나, 시간이 지날수록 형광 테이프의 접착력이 떨어져 몸체(2)에서 분리될 수 있어 형광물질(13)을 혼합하여 제작하는 게 바람직하다.      In addition, the surface of the body 2 may have the same effect by attaching a fluorescent tape instead of the fluorescent material 13, but as time passes, the adhesive force of the fluorescent tape may be separated from the body 2 and thus may be fluorescent. It is preferable to make the material 13 by mixing.

도 4는 본 발명 항공장애표시구에 설치된 점멸기를 확대 도시해 보인 측면도이다.       Figure 4 is an enlarged side view showing a flasher installed in the present invention flight indicator.

본 발명 점멸기(3)를 송전 케이블(12)에 설치한 상태에서 바람에 의해 흔들릴 때 점멸기(3)의 램프(9)가 흔들림에 의해 발생하는 진동에 따라 점멸하며 발광할 수 있도록 점멸기(3) 내부에는 진동을 감지하는 진동감지센서(10)와, 상기 진동감지센서(10)와 접점 및 단락되도록 점멸기(3)의 내벽에는 접점단자(11)가 부착된다.      When the present invention flasher 3 is installed on the power transmission cable 12 and shaken by wind, the lamp 9 of the flasher 3 flashes and emits light according to the vibration generated by the shaker. Vibration detecting sensor 10 for detecting vibrations therein, and a contact terminal 11 is attached to the inner wall of the flasher 3 so as to contact and short-circuit with the vibration detecting sensor 10.

또한, 상기 접점단자(11)는 상부에 위치한 램프(9)와 리드선(14)에 의해 연결되어 진동감지센서(10)가 진동을 감지하여 접점단자(11)와 접점 및 단락되어 발광한다.       In addition, the contact terminal 11 is connected by the lamp 9 and the lead wire 14 located on the upper side, the vibration sensor 10 detects the vibration and contacts and short-circuit with the contact terminal 11 to emit light.

도 5는 본 발명 항공장애표시구에 송전 케이블이 삽입된 상태를 도시해 보인 사시도이다.     5 is a perspective view illustrating a state in which a transmission cable is inserted into the aviation failure indicator of the present invention.

본 발명 항공장애표시구(1)의 간격유지공(8)으로 송전 케이블(12)이 삽입 및 인출된 상태에 서로 합선되지않도록 간격을 유지하고, 태양광셀(7)은 태양광을 집광하여 전력으로 변환한 전기를 충전지로 저장하여 주간은 물론 야간이나 악천후에 점멸기(3)에 전기를 공급하여 발광하도록 한다.      In the present invention, the interval maintaining hole 8 of the aviation failure indicator 1 maintains the gap so that the power transmission cable 12 is not shorted to each other in the inserted and drawn out state, and the solar cell 7 collects sunlight to power The electricity is converted into a rechargeable battery to be stored in the daytime, night or bad weather to supply electricity to the flasher (3) to emit light.

도 6은 본 발명 항공장애표시구를 송전탑 사이에 설치된 상태를 도시해 보인 사시도면으로, 발전소에서 만든 전력을 멀리 있는 공장이나 일반 가정 등으로 송전 케이블(12) 통해 수송하기 위해 산악 지대를 포함한 지역에 일정간격으로 송전탑(17)을 설치하고, 상기 송전탑(17) 사이에 위치하는 송전 케이블(12)에는 항공장애표시구(1)가 설치되어 기후변화에 따라 늘어지거나 팽창해지는 송전 케이블(12)이 서로 합선되지않도록 간격을 유지하며, 태양광셀(7)은 태양광을 직접 전력으로 변환하여 발전한 전기를 충전지(6)에 저장한 상태에서 야간이나 기상이 악천후일 때 점멸기(3)가 발광한다.      Figure 6 is a perspective view showing the state of the present invention the aviation failure indicator between the transmission tower, the area including a mountainous area for transporting the electric power made in the power plant through the power transmission cable 12 to a distant factory or home, etc. Transmission towers (17) are installed at regular intervals, and the transmission cable (12) located between the transmission towers (17) is provided with a aviation failure indicator (1) is a transmission cable 12 that stretches or expands in response to climate change. The interval is maintained so as not to short-circuit each other, the photovoltaic cell 7 emits light when the weather or the weather is bad weather in the state in which the solar cell 7 converts sunlight directly into electric power and stores electricity generated in the rechargeable battery 6. .

또한, 발광하는 점멸기(3)의 불빛에 의해 몸체(2)의 형광물질(13)도 발광하여 헬리콥터 등의 항공기 조종사가 송전 케이블(12)을 용이하게 식별할 할 수 있어 안전운항을 유도한다.       In addition, the fluorescent material 13 of the body 2 also emits light by the light of the flashing device 3 emitting light, so that an aircraft pilot such as a helicopter can easily identify the power transmission cable 12 to induce safe operation.

도 1은 본 발명 항공장애표시구를 도시해 보인 사시도.      1 is a perspective view showing the present invention flight indicator.

도 2는 본 발명 항공장애표시구에 형광물질이 혼합된 것을 도시해 보인 사시도.      Figure 2 is a perspective view showing that the fluorescent material is mixed in the present invention aviation failure indicator.

도 3은 본 발명 항공장애표시구를 도시해 보인 단면도.      Figure 3 is a cross-sectional view showing the present invention flight indicator.

도 4는 본 발명 항공장애표시구에 설치된 점멸기를 확대 도시해 보인 측면도.      Figure 4 is an enlarged side view showing a flasher installed in the present invention flight indicator.

도 5는 본 발명 항공장애표시구에 송전 케이블이 삽입된 상태를 도시해 보인 사시도.      Figure 5 is a perspective view showing a state in which a power transmission cable is inserted into the aviation failure indicator of the present invention.

도 6은 본 발명 항공장애표시구를 송전탑 사이에 설치된 상태를 도시해 보인 사시도.      Figure 6 is a perspective view showing a state in which the present invention is installed between the power failure tower aviation indicator.

< 도면의 주요 부분에 대한 부호의 설명 >      <Description of Symbols for Main Parts of Drawings>

1: 항공장애표시구 2: 몸체      1: Aviation failure indicator 2: Body

3: 점멸기 4: 수납실      3: flasher 4: storage

5: 제어부 6: 충전지      5: control unit 6: rechargeable battery

7: 태양광셀 8: 간격유지공      7: solar cell 8: gap holder

9: 램프 10: 진동감지센서      9: lamp 10: vibration sensor

11: 접점단자 12:송전 케이블      11: contact terminal 12: power transmission cable

13: 형광물질 14: 리드선      13: phosphor 14: lead wire

15: 캡 16: 절연튜브       15: Cap 16: Insulation tube

17: 송전탑      17: transmission tower

Claims (6)

좌ㆍ우 양측이 밀폐된 원통형상의 몸체(2)와;      A cylindrical body 2 in which left and right sides are sealed; 상기 몸체(2)의 좌우 양측에는 삽입 인출되어 송전탑(17)간에 연결되는 송전 케이블(12)의 간격을 유지하도록 통공된 다수개의 간격유지공(8)과;      A plurality of gap maintaining holes 8 inserted into and drawn out at left and right sides of the body 2 to maintain a gap of a power transmission cable 12 connected between power transmission towers 17; 상기 간격유지공(8)이 형성된 좌ㆍ우 양측 또는 몸체(2)의 외주면 둘레에는 태양광을 직접 전력으로 변환하여 발전하는 태양광셀(7)과:      Solar cells 7 for generating power by directly converting sunlight into electric power around the left and right sides or the outer circumferential surface of the body 2 on which the gap maintaining holes 8 are formed: 상기 몸체(2)의 외주면 둘레에는 일정간격으로 부착되어 송전 케이블(12)의 위치를 표시하도록 발광하는 점멸기(3)와;      A flasher (3) attached to the outer circumference of the body (2) at regular intervals to emit light to indicate the position of the power transmission cable (12); 상기 몸체(2) 내부에는 태양광셀(7)에서 발생하는 전기를 충전하는 충전지(6)와, 외부에서 발광하는 점멸기(3)를 리드선(14)에 의해 연결되어 전원공급 및 제어하는 제어부(5)가 설치된 수납실(4)로 구성되되,     Inside the body 2, a control unit 5 for supplying power and controlling the rechargeable battery 6 for charging electricity generated from the photovoltaic cell 7 and the flasher 3 emitting light from the outside are connected by a lead wire 14. ) Consists of a storage compartment (4) is installed, 상기 점멸기(3)는, 내부에 바람에 의해 발생하는 진동을 감지하도록 구비된 진동감지센서(10) 및 접점단자(11)가 일정 간격 이격되어 진동에 의해 상호 접점 및 단락되게 하여 램프가 발광하도록 한 것을 특징으로 점멸신호기가 구비된 송전 케이블용 항공장애표시구.The flasher (3), the vibration sensor 10 and the contact terminal 11 provided to detect the vibration generated by the wind therein is spaced at a predetermined interval to mutually contact and short circuit by the vibration so that the lamp emits light Aviation failure indicator for power transmission cable characterized by the flashing signal. 제 1항에 있어서, 상기 간격유지공(8) 내부를 절연할 수 있도록 좌ㆍ우 양측이 통공된 절연튜브(16)가 삽입된 것을 특징으로 하는 점멸신호기가 구비된 송전 케이블용 항공장애표시구.       The aviation failure indicator for a power transmission cable according to claim 1, wherein an insulating tube (16) through which both left and right sides are inserted is inserted to insulate the space maintaining hole (8). . 제 1항에 있어서, 상기 몸체(2)의 표면에는 형광물질(13)이 도포되거나 또는 혼합 성형된 것을 특징으로 하는 점멸신호기가 구비된 송전 케이블용 항공장애표시 구.       According to claim 1, wherein the surface of the body (2) fluorescent material (13) is applied or mixed molding characterized in that the aviation failure indicator sphere for a transmission cable with a flashing signal. 제 1항에 있어서, 상기 몸체(2)의 외주면 둘레에는 형광 테이프가 접착된 것을 특징으로 하는 점멸신호기가 구비된 송전 케이블용 항공장애표시구.       The aviation failure indicator for a power transmission cable according to claim 1, wherein a fluorescent tape is attached around the outer circumferential surface of the body (2). 삭제delete 제 1항에 있어서, 상기 태양광셀(7)이 부착된 좌ㆍ우 양측은 몸체(2) 내부를 개폐하도록 캡(15)으로 이루어진 것을 특징으로 점멸신호기가 구비된 송전 케이블용 항공장애표시구.       The aviation failure indicator for power transmission cable according to claim 1, wherein the left and right sides to which the photovoltaic cell (7) is attached are made of a cap (15) to open and close the inside of the body (2).
KR1020090024777A 2009-03-24 2009-03-24 Aviation fault indicator for transmission cable with flashing signal KR101057037B1 (en)

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KR102632512B1 (en) * 2016-09-23 2024-01-31 한국전력공사 Flight hindrance-showing ball apparatus
KR101921955B1 (en) 2018-09-07 2018-11-26 주식회사 무영씨엠건축사사무소 Monitoring system for overhead earth wire equiped aircraft warning sphere

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