KR19980056934U - LED Arrangement Structure - Google Patents

LED Arrangement Structure Download PDF

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Publication number
KR19980056934U
KR19980056934U KR2019970001019U KR19970001019U KR19980056934U KR 19980056934 U KR19980056934 U KR 19980056934U KR 2019970001019 U KR2019970001019 U KR 2019970001019U KR 19970001019 U KR19970001019 U KR 19970001019U KR 19980056934 U KR19980056934 U KR 19980056934U
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South Korea
Prior art keywords
substrate
fixed
pedestal
rod
power
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KR2019970001019U
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Korean (ko)
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KR200158234Y1 (en
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황명근
김광호
박남식
정주신
심민보
이정재
김태수
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정태봉
주식회사 건화상사
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Priority to KR2019970001019U priority Critical patent/KR200158234Y1/en
Publication of KR19980056934U publication Critical patent/KR19980056934U/en
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Publication of KR200158234Y1 publication Critical patent/KR200158234Y1/en

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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
    • F21V19/00—Fastening of light sources or lamp holders
    • F21V19/001—Fastening of light sources or lamp holders the light sources being semiconductors devices, e.g. LEDs
    • F21V19/003—Fastening of light source holders, e.g. of circuit boards or substrates holding light sources
    • 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
    • F21K9/20—Light sources comprising attachment means
    • 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
    • F21W2107/00—Use or application of lighting devices on or in particular types of vehicles
    • F21W2107/30—Use or application of lighting devices on or in particular types of vehicles for aircraft
    • 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
    • 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
    • F21W2111/06—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00 for aircraft runways or the like
    • 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
    • F21Y2107/00—Light sources with three-dimensionally disposed light-generating elements
    • 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
    • F21Y2107/00—Light sources with three-dimensionally disposed light-generating elements
    • F21Y2107/40—Light sources with three-dimensionally disposed light-generating elements on the sides of polyhedrons, e.g. cubes or pyramids
    • 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]

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Optics & Photonics (AREA)
  • Non-Portable Lighting Devices Or Systems Thereof (AREA)
  • Arrangement Of Elements, Cooling, Sealing, Or The Like Of Lighting Devices (AREA)

Abstract

본 고안은 항공등 내부에 설치되는 조명체의 LED 배치구조 좀더 상세하게는 태양전지나 축전지를 전원(직류 12V)으로 하고 항공장애물을 표시하기 위한 항공등에 있어서 받침대에 소정의 베이스를 고정하고 이 베이스에 전원이 연결된 고정대를 2개 설치하여 여기에 상부 기판 및 하부 기판과 측면 기판에 의한 다각형의 구조로 조명체를 형성 고정하며 상기 상부 기판 및 측면 기판 표면에 조명용 LED를 각 기판의 회로에 따라 질서정연하게 배치한 후, 글로브를 덮으므로써 구성되는 항공등을 제공하고자 하는 것이다.The present invention is a LED arrangement structure of the illuminator installed inside the aircraft lighting More specifically, the solar cell or storage battery as a power supply (direct current 12V), in a aviation lamp for displaying aeronautical obstacles, a predetermined base is fixed to the base By installing two fixtures to which power is connected, lighting fixtures are fixed in a polygonal structure by upper and lower substrates and side substrates, and lighting LEDs are arranged on the upper and side substrate surfaces according to the circuit of each substrate. It is intended to provide an aviation lamp configured by covering the globe after arranging it.

외부와 고정되는 받침대(1)상에 원통상의 몸체(11)를 나사 고정하고 그 위에 다시 상기 원통상의 몸체(11)보다 넓게 하부 받침대(12)를 형성하며 여기에 글로브(2)가 내삽된 상부 받침대(13)를 나사 고정하고 글로브(2)의 중앙 상단에는 원통형의 통공(21)과 통공커버(22)를 형성한 항공등에 있어서 상기 글로브(2)내에는 상부 받침대(13)상에 고정 설치되어 전원을 각각 연결하는 막대형 지지구(31A, 31B)에 의하여 고정되는 고정판넬(32)상에 조명체(3)를 설치하는데 상기 조명체(3)는 일정간격을 두고 하부 기판(33) 및 이와 일정 간격을 둔 상부 기판(34)를 상기 막대형 지지구(31A, 31B)로 각각 고정한다. 상기 하부 기판(33) 상부 기판(34)은 필요에 따라 다각형의 형태로 형성하며 다각형의 각변에 인접하는 곳에 각각 삽입구(33A, 34A)를 형성한다. 상기 상부기판(34)은 각변의 삽입구(34A) 외측에 각변을 따라 일렬로 수개의 LED(34C)를 부착하며, 이면에는 회로기판에 의하여 전원이 막대형 지지구(31A, 31B) 각각 집중되도록 한다.The cylindrical body 11 is screwed on the pedestal 1 fixed to the outside, and the lower pedestal 12 is formed thereon wider than the cylindrical body 11, and the globe 2 is interpolated therein. The upper pedestal 13 and the upper end 13 in the glove 2 in an air lamp having a cylindrical through-hole 21 and a through-cover 22 formed at the center top of the glove 2. Fixtures 3 are installed on a fixed panel 32 fixed by rod supporters 31A and 31B that are fixedly installed to connect power sources, respectively. 33) and the upper substrate 34 spaced apart from each other by the rod-shaped supports 31A and 31B, respectively. The upper substrate 34 of the lower substrate 33 is formed in a polygonal shape as necessary, and the insertion openings 33A and 34A are formed at positions adjacent to each side of the polygon. The upper substrate 34 attaches a plurality of LEDs 34C in a line along each side outside the insertion hole 34A on each side, and on the back side thereof by a circuit board. The power is concentrated on the rod-shaped supports 31A and 31B, respectively.

또, 상기 하부기판(33) 및 상부기판(34)의 삽입구(33A, 34A)에 삽입되도록 중앙에 삽입돌기(35B, 35C)를 형성한 측면기판(35)의 외측 표면에는 일정한 간격으로 상하 좌우로 LED(35A)를 부착하고 이면에는 회로기판에 의해 전원이 좌우측면을 따라 집중되어 하부기판을 경유하여 막대형 지지구(31A, 31B)에 연결되도록 한다.In addition, the outer surface of the side substrate 35 having the insertion protrusions 35B and 35C formed at the center thereof so as to be inserted into the insertion holes 33A and 34A of the lower substrate 33 and the upper substrate 34 is arranged at regular intervals. LED (35A) is attached on the back side by circuit board. The power is concentrated along the left and right sides to be connected to the rod-shaped supports 31A and 31B via the lower substrate.

Description

항공등용 조명체의 LED 배치구조LED Arrangement Structure

제1도는 본 고안의 일부 절개 정면도1 is a front view of a partial incision of the present invention

제2도는 패널에 조명체가 설치되어 LED 배치구조를 나타내는 사시도.2 is a perspective view showing an LED arrangement structure in which an illuminator is installed on a panel.

제3A도는 LED가 배치된 상부 기판의 평면도,3A is a plan view of an upper substrate on which LEDs are disposed;

제3B도는 LED가 배치된 측면 기판의 정면도.3B is a front view of a side substrate on which LEDs are disposed.

제4도는 배치 구조를 달리한 일실시예의 상부 기판 평면도이다.4 is a plan view of an upper substrate of an embodiment having a different arrangement structure.

*도면의 주요 부분에 대한 부호의 설명** Description of the symbols for the main parts of the drawings *

1 : 받침대2 : 글로브1: base 2: glove

3 : 조명체31A, 31B : 막대형 지지구3: illuminator 31A, 31B: rod-shaped support

32 : 고정판넬33 : 하부기판32: fixed panel 33: lower substrate

34 : 상부기판35 : 측면기판34: upper substrate 35: side substrate

본 고안은 항공등 내부에 설치되는 조명체의 LED 배치구조 좀더 상세하게는 태양전지나 축전지를 전원(직류 12V)으로 하고 항공장애물을 표시하기 위한 항공등에 있어서 받침대에 소정의 베이스를 고정하고 이 베이스에 전원이 연결된 고정대를 2개 설치하여 여기에 상부 기판 및 하부 기판과 측면 기판에 의한 다각형의 구조로 조명체를 형성 고정하며 상기 상부기판 측면기판의 표면에 조명용 LED를 각 기판의 회로에 따라 질서정연하게 배치한 후, 글로브로 덮으므로서 구성되는 항공등을 제공하고자 하는 것이다.The present invention is a LED arrangement structure of the illuminator installed inside the aircraft lighting More specifically, the solar cell or storage battery as a power supply (direct current 12V), in a aviation lamp for displaying aeronautical obstacles fixed a predetermined base on the base and to this base By installing two fixtures to which power is connected, lighting fixtures are fixed in a polygonal structure by upper and lower substrates and side substrates, and lighting LEDs are arranged on the surface of the upper substrate side substrate according to the circuit of each substrate. It is intended to provide an aviation lamp that is configured by covering with a glove after being arranged.

종래 항공장애물 표시등을 보면, 받침대, 터미날박스, 하부받침대, 고정판, 내부커버, 전구, 케이스, 관통공 등을 가진 것에 있어서, 상기 내부커버의 상면에는 통기공을, 그 수직방향의 케이스에는 결합공을 각각 천공되고 그 하면 중앙에 연장관과 반경방향으로 복수개의 요흠을 직선 또는 곡선으로 형성한 상부캡과 그 상면 중앙에 또다른 연장판을 가진 하부캡을 마련하여 상기 상하캡을 베이스의 결합공 상하면에 밀착되게 서로 결합하여서 된 것으로 글로브 내부에는 전구용 소켓을 설치하여 주로 케이스내부 또는 내부커버 쪽으로 이물질과 빗물 등이 요입되지 못하면서 외부의 공기가 내부로 순환될 수 있게 함으로서 전구를 효과적으로 냉각시켜 필라멘트의 증발을 억제하여 수명을 연장시킬 수 있도록 함에 주안점을 둔 것이었다.In the conventional aviation obstacle indicator light, there is a pedestal, a terminal box, a bottom support, a fixing plate, an inner cover, a light bulb, a case, a through hole, etc., wherein the upper surface of the inner cover is provided with a ventilation hole, and a vertically coupled case with a coupling hole. And each of the upper and lower caps having a lower cap having another extension plate in the center and an upper cap formed in a straight or curved line with a plurality of concave grooves in the radial direction and an extension tube in the center thereof. The lamp socket is installed inside the glove so that the outside air can be circulated to the inside of the case or the inner cover without allowing the foreign matter and rainwater to flow into the inside, effectively cooling the bulb and evaporating the filament. The main focus was on restraining the proliferation and extending the lifespan.

그러나 이러한 것은 내부에 교류전원을 사용하는 전구를 사용하였기 때문에 전구의 발열로 내부가 과열되어 비록 대류현상에 의한 냉각을 한다하여도 필라멘트의 증발이 심해 수명이 단축되고 또 소정 조명도 이상을 유지하기 위하여는 많은 전기를 소모하였기 때문에 비경제적 이었다.However, since the bulb uses an AC power source inside, the inside of the bulb is overheated due to the heat generated by the bulb, and the filament evaporates even though it is cooled by convection, which shortens the lifespan and maintains the predetermined illumination level. It was uneconomical because it consumed a lot of electricity.

본 고안은 종래의 항공등에 있었던 교류전원에 의한 전구의 장기사용이라는 과제와 내부 전구가 과열로 수명이 단축된다는 문제점을 근본적으로 해결하기 위한 것으로, 조명시 발열이 되는 백열 등을 사용하지 않고 직류전원을 사용하여 발열이 거의 없는 LED를 조명등으로 사용토록하되 소정의 조명도를 유지할 수 있도록 LED를 기판에 규칙적으로 배열한 기판을 다각형의 형태로 배치한 조명체를 갖는 항공등을 제공하고자 하는 것으로 첨부도면에 의하여 설명하면 다음과 같다.The present invention is intended to fundamentally solve the problem of long-term use of the bulb by the AC power in the conventional aviation lamp and the problem that the internal bulb is shortened by overheating, and does not use an incandescent lamp that generates heat during lighting. To provide an aviation lamp having an illuminant in which polygons are arranged in a regular arrangement of LEDs on a substrate so that LEDs that generate little heat can be used as illumination lamps to maintain predetermined illumination levels. Explained as follows.

외부와 고정되는 받침대(1)상의 원통상의 몸체(11)를 나사 고정하고 그 위에 다시 상기 원통상의 몸체(11) 보다 넓게 하부 받침대(12)를 형성하며 여기에 글로브(2)가 내삽된 상부 받침대(13)를 나사 고정하고 글로브(2)의 중앙 상단에는 원통형의 통공(21)과 통공커버(22)를 형성한 항공등에 있어서 상기 글로브(2)내에는 상부 받침대(13)상에 고정 설치되어 전원을 각각 연결하는 막대형 지지구(31A, 31B)에 의하여 고정되는 고정판넬(32)상에 조명체(3)을 설치한다. 상기 조명체(3)은 일정간격을 두고 하부 기판(33) 및 이와 일정 간격을 둔 상부 기판(34)을 상기 막대형 지지구(31A, 31B)로 각각 고정하며 상기 하부 기판(33), 상부 기판(34)은 필요에 따라 다각형의 형태로 형성하며 다각형의 각변에 인접하는 곳에 각각 삽입구(33A, 34B)를 형성한다. 상기 상부기판(34)은 각변의 삽입구(34A) 외측에 각변을 따라 일렬로 수개의 LED(34B)를 부착하고 삽입구(34A) 내측으로 삼각형 또는 4각형등 일정 형태가 되도록 LED(34C)를 부착하며, 이면에는 회로기판에 의하여 전원이 막대형 지지구(31A, 31B)에 각각 집중되도록 한다.The cylindrical body 11 on the pedestal 1 fixed to the outside is screwed thereon, and the lower pedestal 12 is formed thereon wider than the cylindrical body 11 and the globe 2 is interpolated therein. The upper pedestal 13 is screwed and fixed on the upper pedestal 13 in the glove 2 in an air lamp having a cylindrical through hole 21 and a through cover 22 formed at the center upper end of the glove 2. The illuminator 3 is installed on a fixed panel 32 which is installed and fixed by the rod-shaped supports 31A and 31B for connecting the power sources, respectively. The illuminator 3 fixes the lower substrate 33 and the upper substrate 34 at regular intervals with the rod-shaped supports 31A and 31B, respectively. The board | substrate 34 is formed in the shape of a polygon as needed, and the insertion hole 33A, 34B is formed in the adjoining each side of a polygon, respectively. The upper substrate 34 attaches a plurality of LEDs 34B in a line along each side outside the insertion hole 34A on each side and attaches the LED 34C to a certain shape such as a triangle or a quadrilateral inside the insertion hole 34A. On the back side of the circuit board The power is concentrated on the rod-shaped supports 31A and 31B, respectively.

상기 하부기판(33) 및 상부기판(34)의 삽입구(33A, 34A)에 삽입되도록, 상단 하단부 중앙에 삽입돌기(35B, 35C)를 형성한 직4사각형의 측면기판(35)의 외측 표면에는 일정한 간격으로 상하 좌우로 LED(35A)를 부착하고 이면에는 회로기판에 의해 전원이 좌우측면을 따라 집중되어 하부기판을 경유하여 막대형 지지구(31A, 31B)에 연결되도록 한다.On the outer surface of the quadrangular side substrate 35 having the insertion projections 35B and 35C formed at the center of the upper lower end portion so as to be inserted into the insertion holes 33A and 34A of the lower substrate 33 and the upper substrate 34. Attach LED (35A) up, down, left and right at regular intervals, The power is concentrated along the left and right sides to be connected to the rod-shaped supports 31A and 31B via the lower substrate.

상기 상부기판(34) 및 하부기판(33)의 다각형 형태에 따라 각 변의 삽입구(33A, 34A)에 수개의 측면기판(35)을 사용하여 측벽을 둘러싸며 상부기판(34) 및 측면기판(35)의 LED를 위한 모든 전원은 회로기판에 의해 로 집중되어 막대형 지지구(11A, 11B)를 통하여 태양전지 또는 축전지 등의 직류전원에 연결된다.According to the polygonal shape of the upper substrate 34 and the lower substrate 33, several side substrates 35 are used at the insertion openings 33A and 34A of each side to surround the sidewalls of the upper substrate 34 and the side substrate 35. All power supply for LED is Concentrated by the rod-like support (11A, 11B) is connected to a DC power source such as a solar cell or a storage battery.

이와같이 구성된 본 고안의 항공등을 고층건물이나 크레인, 철탑, 송전탑 등에 받침대(11)를 나사 고정하여 설치하고 하부 받침대(12)상에 막대형 지지구(31A, 31B)를 2개 나사 고정하고 일정 간격을 두어 고정판넬(32)을 다시 나사 고정하며, 고정판넬(32)의 주변은 다시 하부 받침대(12)에 견고하게 고정한다. 고정판넬(32)에서 일정 간격을 두고 배면에 전극이 각각 집중되도록 회로기판이 설치된 다각형의 하부 기판(33)을 상기 막대형 지지구(31A, 31B)로 지지 고정하며 상기 하부 기판(33)의 각변에 연하여 설치된 삽입구(33A)에는 배면에 회로기판이 설치되어 극이 측면으로 연결되어 하부 기판(33)에 연결되고 표면에 LED(35A)가 일정하게 배열된 측면 기판(35)의 삽입돌기(35B)를 끼운다. 또, 상기 측면 기판(35)의 상부 삽입돌기(35C)는 배면에 회로기판에 의하여 극이 2개의 막대형 지지구(31A, 31B)에 연결되고 표면에는 각변을 따라 LED를 일렬(34B) 또는 일정한 형태(34C)로 형성한 상부 기판(34)의 삽입구(34A)내로 삽입한 후 상기 막대형 지지구(31A, 31B)로 고정하여 조명체를 조립한다. 글로브(2)의 하단이 내삽되어 있는 상부 받침대(13)를 하부 받침대(12)와 나사 고정하면 글로브가 조명체를 덮게되어 항공등이 완성되는 것이다.The aviation lamp of the present invention configured as described above is installed by screwing the pedestal 11 to a high-rise building, a crane, a steel tower or a transmission tower, and fixing two rod-shaped supports 31A and 31B on the lower pedestal 12 and The fixing panel 32 is screwed again at intervals, and the periphery of the fixing panel 32 is firmly fixed to the lower pedestal 12 again. In the fixed panel (32) at a certain interval on the back The lower substrate 33 having a polygonal circuit board installed thereon is supported by the rod-shaped support members 31A and 31B so that the electrodes are concentrated, and the insertion hole 33A which is connected to each side of the lower substrate 33 is disposed on the rear surface. Circuit board is installed The poles are connected laterally, connected to the lower substrate 33, and the insertion protrusion 35B of the side substrate 35 having the LED 35A constantly arranged on the surface is fitted. In addition, the upper insertion protrusion 35C of the side substrate 35 is formed on the back side by a circuit board. The pole is connected to the two rod-shaped supports 31A and 31B and the surface is inserted into the insertion hole 34A of the upper substrate 34 formed with a row 34B or a constant shape 34C along the sides. Fixing is assembled by the rod-shaped support (31A, 31B). When screwing the upper pedestal 13, the lower end of the glove 2 is inserted into the lower pedestal 12, the globe covers the illuminator to complete the flight lamp.

태양전지, 축전지 등의 직류전원으로부터 직류가 상기 막대형 지지구(31A, 31B)를 따라 각각 연결된 전선으로 인가되면 하부기판(33), 상부기판(34), 측면기판(35)의 배면에 형성된 기판회로에 의하여 모든 LED는 직렬로 연결되어에서로는 다음 LED의극으로 순차 연결되므로 모든 LED가 일시에 점등되게 된다.When direct current is applied to the wires connected along the rod-shaped supports 31A and 31B from direct current power sources such as solar cells and storage batteries, the lower substrate 33, the upper substrate 34 and the side substrate 35 are formed on the back surface. By the circuit board, all LEDs are connected in series in As the next LED Since the poles are connected sequentially, all the LEDs light up at a time.

이와같이 구성된 항공등은 수많은 LED가 동시에 점등되므로 소정의 조명도를 유지할 수 있고 통상은 적색 빛을 내는 LED를 사용하나 필요에 따라 색깔을 변형할 수 도 있다. 또, 점등되어 계속 ON상태로 하는 것이 보통이나 필요에 따라서는 일정시간 간격을 두고 점멸하게 하는 것도 가능하다.The air lamp configured as described above can maintain a predetermined degree of illumination because many LEDs are turned on at the same time, and usually uses red LEDs, but can also change the color as needed. In addition, it is normal to turn on and keep ON, but it is also possible to make it blink at regular intervals as needed.

이와같은 LED는 점등시에 매우 작은 열만을 발산하게 되는 것이나 이러한 미열도 글로브(2) 상부 중앙에 있는 통공(21)과 통공커버(22)의 공기구멍을 통하여 외부로 발산하게 되므로 내부의 열로 인한 LED의 손상 우려는 거의 없게 된다. 또, 상기 LED는 직류전원을 사용하고 그 소모량도 극히 적게되므로 태양전지 또는 축전지 등의 직류전원을 사용함으로써 장시간에 걸쳐 고장없이 항공등으로서의 기능을 수행할 수 있게 되는 것이다. 또, 조명체(3)를 구성하는 각 기판은 삽탈이 가능하므로 LED 고장시에는 해당 기판만을 분리하여 새로운 기판으로 교체하면 조명체(3) 전체를 교체하지 않아도 되는 편리함이 있다.The LED emits only a very small amount of heat when it is turned on, but such a small heat is emitted to the outside through the air hole of the through hole 21 and the through cover 22 in the upper center of the glove 2. There is little fear of damaging the LEDs. In addition, since the LED uses a DC power source and its consumption is extremely low, it is possible to perform a function as an aviation lamp without a failure for a long time by using a DC power source such as a solar cell or a storage battery. In addition, since each board constituting the lighting body 3 can be inserted and detached, in case of LED failure, there is a convenience in that it is not necessary to replace the entire lighting body 3 by removing only the corresponding board and replacing it with a new board.

Claims (2)

외부와 고정되는 받침대(1)상에 원통상의 몸체(11)를 나사 고정하고 그 위에 다시 상기 원통상의 몸체(11)보다 넓게 하부 받침대(12)를 형성하며 여기에 글로브(2)가 내삽된 상부 받침대(13)를 나사 고정하고 글로브(2)의 중앙 상단에는 원통형의 통공(21)과 통공커버(22)를 형성한 항공등에 있어서, 상기 글로브내에 상부 받침대(13)상에 고정되는 고정판넬(32)를 갖고 상기 고정판넬(32)에는 막대형 지지구(31A, 31B)를 설치하여 여기에 다각형의 하부기판(33) 및 상부기판(34)을 일정간격을 두고 설치하며 상기 기판 등의 각변에 천공된 삽입구(33A, 34A)에 삽입되는 삽입돌기(35B, 35C)를 갖는 직4각형의 측면기판(35)에 의하여 다각형의 조명체(3)를 형성하고 상기 상부기판(34)에는 삽입구(34A)의 외측에는 각변을 따라 일렬로 또 삽입구(34A) 내측에는 일정한 형태로 LED(34B, 34C)를 각각 부착하고 상기 측면기판(35) 외측에는 상하 좌우로 LED(35A)를 규칙적으로 배열하여서 된 것을 특징으로 하는 항공등용 조명체의 LED 배치구조.The cylindrical body 11 is screwed on the pedestal 1 fixed to the outside, and the lower pedestal 12 is formed thereon wider than the cylindrical body 11, and the globe 2 is interpolated therein. Fixed to the upper pedestal 13 in the glove in an aviation lamp having a screwed upper pedestal 13 and having a cylindrical through hole 21 and a through cover 22 formed at the center top of the glove 2. It has a panel 32 and the fixed panel 32 is provided with a rod-shaped support (31A, 31B) to install a polygonal lower substrate 33 and the upper substrate 34 at regular intervals, such as the substrate A polygonal illuminator 3 is formed by a rectangular quadrilateral side substrate 35 having insertion protrusions 35B and 35C inserted into insertion holes 33A and 34A bored at each side of the upper substrate 34. The LEDs 34B and 34C are arranged in a row along the sides of the insertion hole 34A and in a constant shape inside the insertion hole 34A. Attached to each of the side substrate 35, the LED arrangement structure of the illumination lamp for the aircraft, characterized in that the LED (35A) arranged regularly in the vertical direction. 제1항에 있어서, 상기 하부기판(33), 상부기판(34), 측면기판(35)의 내부에 회로기판을 설치하여 모든 전류가 막대형 지지구(31A, 31B)로 집중되어 각각 전극 역할을 할 수 있도록 함을 특징으로 하는 항공등용 조명체의 LED 배치구조.According to claim 1, wherein the lower substrate 33, the upper substrate 34, the side substrate 35 is installed inside the circuit board all the current is concentrated to the rod-shaped support (31A, 31B), respectively LED arrangement of the illuminating body for an aerial light, characterized in that it can act as an electrode.
KR2019970001019U 1997-01-25 1997-01-25 Led display structure of lighting device for air beacon KR200158234Y1 (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20010099240A (en) * 2001-09-14 2001-11-09 이훈기 Solar air light
KR20010106392A (en) * 2001-11-12 2001-11-29 이계선 Bulb-based LED lamp for the safety flying of aircraft
KR100317222B1 (en) * 1999-08-31 2001-12-22 정대열 a lamp of the aerial beacon
KR100502578B1 (en) * 2003-03-05 2005-07-20 유양산전 주식회사 Lamp For Aerial Navigation Lighting

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100707392B1 (en) * 2005-06-20 2007-04-13 에이피엘시스템(주) lamp cover for beacon-obstacle illuminator
KR100682072B1 (en) 2005-06-20 2007-02-15 에이피엘시스템(주) LED lamp for beacon-obstacle illuminator
KR100997092B1 (en) * 2008-03-07 2010-11-29 효성전기공업 주식회사 The ??? lamp use ??? element
KR101016942B1 (en) * 2008-03-12 2011-02-25 나정주 Lighting Device using LED
KR101026766B1 (en) * 2008-06-25 2011-04-11 (주) 아모엘이디 LED Lighting Apparatus And Method for Manufacturing The Same

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100317222B1 (en) * 1999-08-31 2001-12-22 정대열 a lamp of the aerial beacon
KR20010099240A (en) * 2001-09-14 2001-11-09 이훈기 Solar air light
KR20010106392A (en) * 2001-11-12 2001-11-29 이계선 Bulb-based LED lamp for the safety flying of aircraft
KR100502578B1 (en) * 2003-03-05 2005-07-20 유양산전 주식회사 Lamp For Aerial Navigation Lighting

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