KR900005699Y1 - Obstruction light - Google Patents

Obstruction light Download PDF

Info

Publication number
KR900005699Y1
KR900005699Y1 KR2019870003078U KR870003078U KR900005699Y1 KR 900005699 Y1 KR900005699 Y1 KR 900005699Y1 KR 2019870003078 U KR2019870003078 U KR 2019870003078U KR 870003078 U KR870003078 U KR 870003078U KR 900005699 Y1 KR900005699 Y1 KR 900005699Y1
Authority
KR
South Korea
Prior art keywords
lens
light
aviation
lower body
present
Prior art date
Application number
KR2019870003078U
Other languages
Korean (ko)
Other versions
KR880018218U (en
Inventor
손영웅
Original Assignee
주식회사 성광조명
손영웅
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.)
Filing date
Publication date
Application filed by 주식회사 성광조명, 손영웅 filed Critical 주식회사 성광조명
Priority to KR2019870003078U priority Critical patent/KR900005699Y1/en
Publication of KR880018218U publication Critical patent/KR880018218U/en
Application granted granted Critical
Publication of KR900005699Y1 publication Critical patent/KR900005699Y1/en

Links

Classifications

    • 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
    • F21V5/00—Refractors for light sources
    • F21V5/04—Refractors for light sources of lens shape
    • 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
    • F21V29/00—Protecting lighting devices from thermal damage; Cooling or heating arrangements specially adapted for lighting devices or systems
    • F21V29/50—Cooling arrangements
    • F21V29/70—Cooling arrangements characterised by passive heat-dissipating elements, e.g. heat-sinks
    • F21V29/83—Cooling arrangements characterised by passive heat-dissipating elements, e.g. heat-sinks the elements having apertures, ducts or channels, e.g. heat radiation holes
    • 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
    • F21V5/00—Refractors for light sources
    • F21V5/02—Refractors for light sources of prismatic shape
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Arrangement Of Elements, Cooling, Sealing, Or The Like Of Lighting Devices (AREA)
  • Non-Portable Lighting Devices Or Systems Thereof (AREA)

Abstract

내용 없음.No content.

Description

항공 장해등Aviation obstacle

제1도는 본 고안의 일부절개 사시도.1 is a partially cutaway perspective view of the present invention.

제2도는 제1도의 종단면도이다.2 is a longitudinal cross-sectional view of FIG.

* 도면의 주요부분에 대한 부호의 설명* Explanation of symbols for main parts of the drawings

1 : 하부몸체 2 : 상부몸체1: lower body 2: upper body

3-5 : 렌즈 6-8 : 렌즈지지링3-5: Lens 6-8: Lens Support Ring

9 : 링지지봉 10 : 지지봉9: ring support rod 10: support rod

11 : 덮개 12 : 통기공11: cover 12: vent

13 : 체결구 14, 14' : 소켓13 fastener 14, 14 'socket

15, 15' : 전구 16, 16' : 필터15, 15 ': bulb 16, 16': filter

17 : 나비너트 18, 18' : 소켓지지체17: Butterfly nut 18, 18 ': Socket support

본 고안은 항공법에서 요구하는 고광도의 항공장애등에 관한것으로, 특히 등기구의 방열효과와 빛의 방사효과를 증진시키도록 개량한 항공장애등에 관한것이다.The present invention relates to the high brightness aviation obstacles required by the aviation law, and more particularly to the aviation obstacles improved to enhance the heat radiation effect and the radiation effect of light.

항공장애등은 비행기의 야간비행시 안건을 도모하기 위하여 비행장이나 60m이상의 고층건물에 설치하도록법으로써 규정해 놓고있는데. 고광도의 항공장애등과 저광도의 항공장애등으로 구분하여 설치하도록 하고있다.Aviation obstacles, etc., are required by law to be installed in aerodromes or high-rise buildings over 60m to promote the agenda during night flight. Installation is divided into high brightness aviation lights and low light aviation lights.

이중 고광도의 항공장애등은 최대광도가 2,000칸델라(Candela)이상인 것으로 분당명멸횟수가 20 내지 60회정도이여 수평면하 15도상방의 모든 방향에서 항공장애등 위치를 식별할 수 있는 것이어야 한다.The high aviation obstacle lights should have a maximum brightness of more than 2,000 Candelas, with 20 to 60 flashes per minute, and should be able to identify the location of the aviation lights in all directions 15 degrees above the horizontal plane.

그런데 상기한 규정에 의해 설치되는 종괘의 항공장애등은 램프에서 발상된 빛이 렌즈를 통과한 후에는 거의 수평면으로 반사되어 15도 상방에서의 식별이 곤란하고, 램프에서 고광도의 빛을 장시간 방사함으로인해 발생되는 열이 제대로 방열되지 못해서 렌즈의 파열을 초래함은 물론 방수 밋 램프의 수명에 악영향을 끼치게 되는 결점이 있었다.However, the aviation obstacle lamp installed according to the above provisions is difficult to be distinguished from the 15 degree upward because the light generated from the lamp passes through the lens and is almost reflected on the horizontal plane. There was a drawback that the heat generated could not be properly dissipated, causing the lens to rupture and adversely affect the life of the waterproof met lamp.

따라서 본 고안은 상기한 결점을 해소하기 위하여 등기구의 밑면에 체결구를 돌출시킴과 더불어 통기공을 형성시키고 등기구의 상부에 배기통로를 형성시켜 대기에 의한 램프의 방열효과를 증진시키고, 램프주의의 렌즈를 외부로 프리즘처리하되 각 프리즘의 빛의 방사 방향을 상향에서 하향으로 각도를 달리하여 방사하게 하므로써 수평면 15도 상방에서도 양호하게 관측되도륵 원 항공장애등을 제공하고자 하는 것으로, 이를 첨부도면에 의거하여 상세히 설명하면 다음과 갈다.Therefore, the present invention protrudes the fasteners on the bottom of the luminaire to solve the above-mentioned drawbacks, and forms a vent hole and an exhaust passage on the upper part of the luminaire to enhance the heat dissipation effect of the lamp by the atmosphere. By prisming the lens to the outside, the radiation direction of each prism is radiated at different angles from upwards to downwards to provide a circular aviation obstacle that is well observed even at 15 degrees above the horizontal plane. If you explain in detail as follows.

제1도는 본고안의 일부절개사시도를 나타내고, 제2도 본고안의 종단면도를 나타내는 것으로, 하부몸체(1)와 상부몸체(2)사이에 하부렌즈즈(3)와 중간렌즈(4) 및 상부렌즈(5)가 차례로 설치되되 각렌즈(3)(4)(5)사이에는 렌즈지지령(6-8)이 설치되어있고, 하부몸체(1)와 렌즈 지지링(6) 및 렌즈지지링(7)과 랜즈지지링(8)사이에는 링지지봉(9)이 실치되어 있으며, 상부몸체(2)의 위에는 지지봉(10)을 매개하여 덮개(11)가 설치된 구조로 되어있다.1 shows a partial cutaway perspective view of the present invention, and FIG. 2 shows a longitudinal cross-sectional view of the present invention, wherein the lower lenses 3, the intermediate lens 4, and the upper lens are disposed between the lower body 1 and the upper body 2; (5) are installed one by one, the lens support (6-8) is installed between each lens (3) (4) (5), the lower body (1) and the lens support ring (6) and the lens support ring ( A ring support rod 9 is mounted between 7) and the lens support ring 8, and the cover 11 is installed on the upper body 2 via the support rod 10.

또한 하부몸체(1)의 밑면에는 앙카형의 통기공(12)이 형성되어 있고, 등기구를 체결시키기 위한 체결구(13)가 하부몸체(1)의 밑면보다 약간 돌출되게 형성되어 있으며, 이와같은 등기구의 내부에는 소켓(14)(14')과 전구(15)(15') 및 필터(16)(16')가 설치되어 있다In addition, the bottom of the lower body (1) is formed with an anchor vent hole 12, the fastener 13 for fastening the luminaire is formed to protrude slightly than the bottom of the lower body (1), such Inside the luminaire, sockets 14 and 14 ', bulbs 15 and 15' and filters 16 and 16 'are provided.

또 각렌즈(3-5)는 외부가 볼록렌즈 또는 프리즘역할을 하도륵 요철이 형성되어 있고, 내부는 평면형으로 되어있는데, 프리즘 역할을 하는 요철구조에 의해서 전구(15)(15')로부터 발생된 빛이 상부와 하부 및 수평방향에 고르게 방사되게 된다.In addition, the angular lens (3-5) is formed with concave and convexities on the outside to act as a convex lens or prism, and the inside of the angular lens (3-5) has a flat shape. The light is radiated evenly in the upper, lower and horizontal directions.

따라서 전구(15)(15')를 중심으로 수평면하 15도 상방에서도 항공장애등의 위치를 용이하게 인식할수 있게된다.Therefore, the position of the aviation obstacle light can be easily recognized even at a level 15 degrees below the horizontal plane around the bulbs 15 and 15 '.

본 고안의 항공장애등은 고광도용이기 때문에 전구(15)(15')는 통상 500W정도의 것을 사용하여 광도 2,000칸델라 이상의 빛을 발하게 되므로써 전구(15)(15')로부터 상당한 열이 발생되게 되는데, 전구(15)(15')에 의해서 더워진 공기는 방사되는 빛의 색깔을 규정하는 필터(16)(16')내부를 통해 상승되어서 상부몸체(2)와 덮개(11)사이에 지지링(10)에 의해 형성된 공간을 통하여 밖으로 빠져나가고 외부의 차가운 공기가 하부몸체(1)의 통기공(12)을 통하여 등기구 내부로 유입된다.Since the aviation obstacle lamp of the present invention is for high brightness, the light bulbs 15 and 15 'typically emit light of more than 2,000 candelas using a light of about 500W, so that considerable heat is generated from the light bulbs 15 and 15'. The air warmed by the bulbs 15, 15 'is raised through the interior of the filter 16, 16' which defines the color of the emitted light so that a support ring between the upper body 2 and the cover 11 Out through the space formed by 10) and the outside cold air is introduced into the luminaire through the vent hole 12 of the lower body (1).

따라서 공기의 대류현상으로 인하여 등기구의 방열을 효과적으로 도모할 수 있게되는 것이다.Therefore, it is possible to effectively heat radiation of the luminaire due to the air convection phenomenon.

한편 본 고안에서는 전구(15)(15')의 교체작업을 쉽게 하기위하여 렌즈지지링(6)(7)을 분리할수 있도록 설치하고 나비너트(17)로써 고정시킬수 있게 하였다.On the other hand, in the present invention, in order to easily replace the bulb 15, 15 'of the lens support ring (6) (7) is installed so that it can be fixed with a butterfly nut (17).

이 렌즈지지링(6)(7)의 내부에는 황색이나 적색등의 필터(16)(16')를 고정시키도록 되어있다.Inside the lens support rings 6 and 7, the filters 16 and 16 'such as yellow or red are fixed.

또한 소켓의 누수에 의한 절연을 위하여 하부몸체(1) 및 상부몸체(2)에다 소켓지지체(18)(18')를 설치하였다.In addition, the socket supports 18 and 18 'were installed in the lower body 1 and the upper body 2 for insulation by leakage of the socket.

하부몸체(1)밑면에 형성된 체결구(13)는 평평한 고정면에 본 고안의 항공장애등을 고정시키더라도 통기공(12)으로 외부의 찬공기가 유입되도톡 하부몸체(1)밑으로 약 10㎝정도 돌출시켰다.Fasteners 13 formed on the bottom of the lower body (1) is about 10 below the lower body (1) so that outside cold air flows into the vent hole (12) even if fixing the aviation obstacle of the present invention on a flat fixed surface It protruded about cm.

따라서 대류공기의 소통이 자유롭게 될뿐만 아니라 방수효과도 볼 수 있게되는 것이다.Therefore, not only the communication of convection air is free, but also the waterproofing effect can be seen.

상기한 바와같이 본 고안은 하부몸체와 상부몸체의 통기공을 통하여 공기를 대류시킬 수 있게되므로써 방열효과를 높일 수 있을뿐만 아니라 렌즈외부에 빛의 방사방향을 다르게 프리즘역할을 하는 돌기를 형성시키므로써 수평면상방 15도에서도 항공장해등의 식별을 용이하게 할수 있는 효과가 있다.As described above, the present invention can increase the heat dissipation effect by allowing air to be convection through the air vents of the lower body and the upper body, and by forming protrusions that act as prisms differently in the radial direction of light outside the lens. Even at 15 degrees above the horizontal plane, there is an effect that can facilitate identification of aeronautical obstacles.

Claims (1)

상, 중, 하부렌즈(3)(4)(5)를 가진 것에 있어서, 통기공(12)을 가진 하부몸체(1)와 덮개(11)를 가진 상부몸체(2)에 각각의 전구(15)(15')를 설치토록 구성하여서 된 항공장해등.In the upper, middle and lower lenses 3, 4 and 5, each bulb 15 is provided in the lower body 1 having the ventilation holes 12 and the upper body 2 having the cover 11; Air obstacles, etc., made up of 15 ').
KR2019870003078U 1987-03-11 1987-03-11 Obstruction light KR900005699Y1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR2019870003078U KR900005699Y1 (en) 1987-03-11 1987-03-11 Obstruction light

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR2019870003078U KR900005699Y1 (en) 1987-03-11 1987-03-11 Obstruction light

Publications (2)

Publication Number Publication Date
KR880018218U KR880018218U (en) 1988-10-28
KR900005699Y1 true KR900005699Y1 (en) 1990-06-28

Family

ID=19260465

Family Applications (1)

Application Number Title Priority Date Filing Date
KR2019870003078U KR900005699Y1 (en) 1987-03-11 1987-03-11 Obstruction light

Country Status (1)

Country Link
KR (1) KR900005699Y1 (en)

Also Published As

Publication number Publication date
KR880018218U (en) 1988-10-28

Similar Documents

Publication Publication Date Title
US20160053982A1 (en) Outdoor lighting fixture
KR20220114440A (en) Infrared LED aircraft warning lights
US2699515A (en) Lamp construction
KR900005699Y1 (en) Obstruction light
US2481054A (en) Light projector
KR101123284B1 (en) Led high intensity whole-side floodlights having a light diffusing lens
CN211551387U (en) Outdoor street lamp holder of intelligent adjustable light elemi
CA3038496C (en) Luminaire with adapter collar
KR101269080B1 (en) Led exposed approach light including a heat sink plate
KR200158233Y1 (en) Ventilation structure of glove for air beacon
CN205480554U (en) LED advances nearly permanent fiber lamp
KR200377596Y1 (en) Ceiling light
US3189736A (en) Lighting fixture
CN220728189U (en) Four-primary-color laser lamp
KR940001318Y1 (en) Alarm lamp
CN217978644U (en) Multi-color high-heat-dissipation landscape lamp
JP6279928B2 (en) Aviation Obstruction Light
CN216744041U (en) LED shot-light of lamp cup combination formula
CN211232640U (en) High heat dissipation LED industrial and mining lamp
CN211372130U (en) Ceiling lamp with adjustable irradiation range
JPH046086Y2 (en)
CN209101204U (en) A kind of automotive LED headlamp
US2304208A (en) Luminaire for blackout lighting
KR101347061B1 (en) Diffusion cover for street light
CN207350231U (en) A kind of motorcycle headlamp air-penetrable waterproof structure

Legal Events

Date Code Title Description
A201 Request for examination
E902 Notification of reason for refusal
E701 Decision to grant or registration of patent right
REGI Registration of establishment
LAPS Lapse due to unpaid annual fee