KR910005747Y1 - Panel fixed apparatus - Google Patents
Panel fixed apparatus Download PDFInfo
- Publication number
- KR910005747Y1 KR910005747Y1 KR2019890001133U KR890001133U KR910005747Y1 KR 910005747 Y1 KR910005747 Y1 KR 910005747Y1 KR 2019890001133 U KR2019890001133 U KR 2019890001133U KR 890001133 U KR890001133 U KR 890001133U KR 910005747 Y1 KR910005747 Y1 KR 910005747Y1
- Authority
- KR
- South Korea
- Prior art keywords
- panel
- light receiving
- receiving panel
- angle
- light
- Prior art date
Links
- 238000009434 installation Methods 0.000 description 8
- 238000000034 method Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000001464 adherent effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S20/00—Supporting structures for PV modules
- H02S20/30—Supporting structures being movable or adjustable, e.g. for angle adjustment
-
- 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
-
- 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
Abstract
내용 없음.No content.
Description
제 1 도는 이 고안의 일부분해 사시도.1 is a perspective view partly of this invention.
제 2 도는 측면구성도2 is a side view
제 3 도는 제 2 도의 A-A'선 단면으로서 포스트 플랜지의 상세도.3 is a detail view of the post flange as a cross-sectional view taken along line AA 'of FIG.
제 4 도는 평면 구성도.4 is a plan view.
제 5 도는 설치 예시도.5 is an installation example.
* 도면의 주요부분에 대한 부호의 설명* Explanation of symbols for main parts of the drawings
1 : 수광패널 2 : 전지판1: light receiving panel 2: panel
3 : 포스트 4 : 경사각 조절기구3: post 4: tilt angle adjustment mechanism
5 : 브라케트 6 : 방위각 조절기구5: bracket 6: azimuth adjustment mechanism
41 : 취부밴드 42 : 힌지부41: mounting band 42: hinge portion
43 : 취부시트 44 : 볼트43: mounting sheet 44: bolt
45 : 조절간 46 : 볼트공45: adjustment period 46: bolt hole
61 : 관상부재 62 : 축부61: tubular member 62: shaft portion
63 : 볼트 64,64' : 플랜지63: bolt 64,64 ': flange
65 : 장공 66 : 볼트공65: long hole 66: bolt hole
이 고안은 항공장애 표시등 전원공급용 태양전지판의 수광패널장치에 관한 것으로 특히 제약된 설치 환경하에서 최적의 수광각도 및 방향을 유지시킬 수 있게 되어 있는 것이다.The present invention relates to a light receiving panel device of a solar panel for power supply of a fault indicator light, which is capable of maintaining an optimal light receiving angle and direction, particularly in a restricted installation environment.
항공장애표시등은 항공기의 충돌을 피하기 위하여 항로상의 장애물에 설치되는 것으로서 주로 하천을 가로지르는 고압선의 철탑이나 송전선로 또는 돌기된 지형 장애물에 설치되고 있는 것이다.Aviation obstacle indicators are installed on obstacles in the air route to avoid collisions of aircraft. They are usually installed on high-voltage pylons, transmission lines or raised terrain obstacles across rivers.
이와 같은 항공장애 표시등은 비행물체로부터 쉽게 식별 될수 있도록 야간에 점등하게 되며, 점등용 전원을 외부로부터 공급하거나 본원 고안자가 등록받은 실용신안공고 87-1036호에 기재한 바와 같이 태양전지판을 설치하여 얻고 있는 것이다.Such a aviation failure indicator lights up at night so that it can be easily identified from the flying object, and is supplied by supplying lighting power from the outside or by installing a solar panel as described in Utility Model Publication No. 87-1036 registered by the inventor of the present invention. It is.
그러므로 항공장애 표시등에 수반되는 태양전지의 수광판은 철탑 구조물 또는 돌출지형이나 돌출 건축물등과 같이 위험하고 현저한 제약이 가해지는 환경하에서 설치되므로 태양전지판의 최적 수광각도 및 방향을 유지하기가 곤란해지는 것이다.Therefore, it is difficult to maintain the optimal light receiving angle and direction of the solar panel because the solar light receiving plate accompanying the aviation obstacle indicator is installed under dangerous and constrained environment such as steel tower structure or protruding topography or protruding structure. will be.
이 고안은 상기와 같은 항공장애 표시등 전원 공급용 태양 전지판의 수광패널 고정장치를 제공함에 있어서, 수광판의 설치 방향이나 설치 각도를 임의로 조절할 수 있게 함으로써 언제든지 최적의 수광각도 및 방향으로 설치할 수 있고 또한 설치 작업을 안전하게 수행할 수 있게 되어 있는 것이다.The present invention provides a light receiving panel fixing device of a solar panel for supplying a power failure indicator light as described above, and can be installed at an optimal light receiving angle and direction at any time by allowing the installation direction or installation angle of the light receiving plate to be arbitrarily adjusted. It is also designed to safely perform installation work.
이 고안을 첨부 도면에 따라서 상세히 설명하면 다음과 같다.This invention is described in detail with reference to the accompanying drawings as follows.
수광패널(1)은 태양전지판(2)을 부착한 패널로서 포스트(3)상에 경사각 조절기구(4)로서 취부되어 있으며, 상기 포스트(3)는 브라케트(5)상에 방위각 조절기구(6)로서 취부되어 있다.The light receiving panel 1 is a panel to which the solar panel 2 is attached, and is mounted on the post 3 as an inclination angle adjusting mechanism 4, and the post 3 is mounted on the bracket 5. It is attached as 6).
상기 경사각 조절기구(4)는 포스트(3) 상부의 취부밴드(41)와 상기 취부밴드(41)와 수광패널(1) 사이의 힌지부(42)와 패널양측에 힌지접속되고 동시에 포스트(3)측의 취부시트(43)에 볼트(44)로 고정되는 조절간(45)으로 구성되어 있으며, 상기 조절간(45)상의 볼트공(46)은 수광패널(1)을 조절각(θ)내에서 동작시킬 수 있게 분포되어 있다. 상기 방위각 조절기구(6)는 브라케트(5)의 관상부재(61)상에 끼워지는 축부(62)와 상기 포스트(3)측 및 광상부재(61)상에 부착되어 대응되며 또한 볼트(63)로써 고정되는 플랜지(64)(64')쌍으로 되어 있으며, 상기 플랜지(64)와 (64')에 장공(65)과 볼트공(66)을 각각 대응시킴으로써 포스트의 방위각회동이 가능하게 되어 있는 것이고, 상기의 장공은 제3도의 (a)(b)에서와 같이 일정한 방위 조절각(θ)을 허용할 수 있게 배려되어 있는 것이다.The inclination angle adjusting mechanism 4 is hinged to both sides of the panel and the hinge portion 42 between the mounting band 41 and the mounting band 41 and the light receiving panel 1 on the post 3 and at the same time the post 3 It consists of a control rod 45 is fixed to the mounting sheet 43 of the side) with a bolt 44, the bolt hole 46 on the control interval 45 is the light receiving panel 1 to adjust the angle (θ) It is distributed so that it can operate inside. The azimuth adjustment mechanism 6 is attached to the shaft portion 62 fitted on the tubular member 61 of the bracket 5 and on the post 3 side and the depositing member 61, and also corresponds to the bolt 63. And a pair of flanges 64 and 64 'fixed to each other. The long holes 65 and the bolt holes 66 correspond to the flanges 64 and 64', respectively, so that the azimuth rotation of the post is possible. The above-mentioned long hole is considered to allow a constant azimuth angle? As in (a) and (b) of FIG.
이 고안의 작용 효과를 설명하면 다음과 같다.The effect of this invention is explained as follows.
설치방법을 설명하면, 먼저 브라케트(5)를 피착 구조물에 고정한 후, 포스트(3)의 축부(62)를 관상부재(61)에 꽂아 놓고 포스트(3)를 조절각(θ)내에서 소망하는 방향으로 회전시켜 방위각을 선택하며 또한 볼트(63)를 조여 플랜지(64)와 플랜지(64')를 부착시킴으로써 수광패널(1)의 방위각의 조절을 행하는 것이고, 조절간(46)을 조절각(θ)내에서 동작시켜 힌지부(42)를 동축으로 수광패널(1)의 기울기를 선택한 후 볼트(44)로 조절간(4)을 취부시트(43)에 고정시킴으로써 방위각의 조절을 행하는 것이다.To explain the installation method, first, the bracket 5 is fixed to the adherend structure, the shaft 62 of the post 3 is inserted into the tubular member 61, and the post 3 is desired within the adjustment angle θ. Direction to select the azimuth angle and tighten the bolt 63 to attach the flange 64 and the flange 64 'to adjust the azimuth angle of the light-receiving panel 1, and the adjustment angle 46 is adjusted. The azimuth angle is adjusted by operating within (θ) and selecting the inclination of the light receiving panel 1 coaxially with the hinge portion 42, and then fixing the adjustment section 4 to the mounting sheet 43 with the bolt 44. .
상기의 방위각의 조절 과정은 피착부재에 미리 고정시킨 브라케트(5)의 관상부재(61)에 포스트(3)의 축부(62)를 꽂은 다음 각도의 조절을 행하게 되어 철탑에서와 같은 위험한 환경하에서 안전하게 작업을 행할수 있는 것이고, 상기의 경사각 조절과정 역시 고정된 포스트(3)상에서 수광패널(1)의 기울기를 조절하게 되어 안전하게 작업을 행할 수가 있는 것이다.In the azimuth adjustment process, the shaft portion 62 of the post 3 is inserted into the tubular member 61 of the bracket 5 fixed in advance to the adherent member, and then the angle is adjusted to perform the angle adjustment under a dangerous environment such as in a pylon. The work can be safely performed, and the inclination angle adjustment process can also be performed safely by adjusting the inclination of the light receiving panel 1 on the fixed post (3).
상기와 같이 이 고안은 수광패널의 경사각과 방위각을 임의로 조절할 수 있어 제약된 항공장애 표시등의 설치 환경하에서 조절할 수 있어 제약된 항공장애 표시등의 설치 환경하에서 최적 수광각도 및 방향을 유지시킬수가 있는 것이며, 방위각과 경사각의조절을 안전하에 행할 수 있는 항공장애 표시등 전원공급용 태양전지판의 수광패널 장치를 제공하는 효과가 있다.As described above, the present invention can arbitrarily adjust the inclination angle and the azimuth angle of the light receiving panel so that it can be adjusted under the installation environment of the restricted aviation fault indicator light, so that the optimal light reception angle and direction can be maintained under the installation environment of the restricted aviation fault indicator light. In addition, there is an effect of providing a light-receiving panel device of a solar panel for power supply of a aviation obstacle indicator that can safely control azimuth and inclination angles.
Claims (3)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR2019890001133U KR910005747Y1 (en) | 1989-02-01 | 1989-02-01 | Panel fixed apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR2019890001133U KR910005747Y1 (en) | 1989-02-01 | 1989-02-01 | Panel fixed apparatus |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| KR900015924U KR900015924U (en) | 1990-09-03 |
| KR910005747Y1 true KR910005747Y1 (en) | 1991-08-02 |
Family
ID=19283527
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| KR2019890001133U KR910005747Y1 (en) | 1989-02-01 | 1989-02-01 | Panel fixed apparatus |
Country Status (1)
| Country | Link |
|---|---|
| KR (1) | KR910005747Y1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102107468B1 (en) * | 2019-11-06 | 2020-05-07 | 주식회사 프로텍타코리아 | Aircraft warning light power line |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101988738B1 (en) | 2017-10-30 | 2019-06-12 | 주식회사 포스코 | Solar panel unit and solar panel structere |
-
1989
- 1989-02-01 KR KR2019890001133U patent/KR910005747Y1/en not_active IP Right Cessation
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102107468B1 (en) * | 2019-11-06 | 2020-05-07 | 주식회사 프로텍타코리아 | Aircraft warning light power line |
Also Published As
| Publication number | Publication date |
|---|---|
| KR900015924U (en) | 1990-09-03 |
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