JPH05135608A - Flash control device for airplane warning light using solar battery electromotive force - Google Patents
Flash control device for airplane warning light using solar battery electromotive forceInfo
- Publication number
- JPH05135608A JPH05135608A JP27878091A JP27878091A JPH05135608A JP H05135608 A JPH05135608 A JP H05135608A JP 27878091 A JP27878091 A JP 27878091A JP 27878091 A JP27878091 A JP 27878091A JP H05135608 A JPH05135608 A JP H05135608A
- Authority
- JP
- Japan
- Prior art keywords
- electromotive force
- warning light
- solar battery
- control device
- solar cell
- Prior art date
- Legal status (The legal status 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 status listed.)
- Pending
Links
Landscapes
- Non-Portable Lighting Devices Or Systems Thereof (AREA)
Abstract
Description
【０００１】[0001]
【産業上の利用分野】本発明は航空障害灯の点滅制御装
置、さらに詳しくいえば無線通信中継用鉄塔に設置され
る航空障害灯設備の点滅制御装置に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a blinking control device for an aviation obstruction light, and more particularly to a blinking control device for an aviation obstruction light equipment installed in a radio communication relay tower.
【０００２】[0002]
【従来の技術】無線通信中継用鉄塔は航空機にとって障
害になることから、その存在を示すために航空障害灯が
設置されている。図２は従来の航空障害灯の点滅制御装
置の一例を示す回路図である。航空障害灯３が制御用リ
レー４の接点５を介して蓄電池２に接続されており、ま
た、通信機等の負荷８が直接蓄電池２に接続されてい
る。制御用リレー４は照光感知器７およびその駆動系で
駆動される接点９を介して蓄電池２に接続されている。
蓄電池２は太陽電池１によって充電される。照光感知器
（Photo cell）７は環境の照度を抵抗値に変換してお
り、設定抵抗値になったとき、接点９を閉じて制御用リ
レー４を駆動し、その接点５を閉じ航空障害灯３を夜間
点灯する。昼間は接点９が閉じ、航空障害灯３を消灯す
る。2. Description of the Related Art Since a radio communication relay tower is an obstacle to an aircraft, an aviation obstacle light is installed to indicate its existence. FIG. 2 is a circuit diagram showing an example of a conventional blinking control device for an aviation obstruction light. The aviation obstruction light 3 is connected to the storage battery 2 via the contact 5 of the control relay 4, and the load 8 such as a communication device is directly connected to the storage battery 2. The control relay 4 is connected to the storage battery 2 via an illumination sensor 7 and a contact 9 driven by its drive system.
The storage battery 2 is charged by the solar cell 1. An illumination sensor (Photo cell) 7 converts the illuminance of the environment into a resistance value, and when the set resistance value is reached, the contact 9 is closed to drive the control relay 4, and the contact 5 is closed to close the aviation obstruction light. Turn on 3 at night. During the daytime, the contact 9 is closed and the aviation obstruction light 3 is turned off.
【０００３】[0003]
【発明が解決しようとする課題】従来の航空障害灯の点
滅制御装置はこのように照光感知器７によって明暗を検
知して航空障害灯を点滅制御している。上記照光感知器
７は直流電源で駆動するものであり、一般に海外では入
手が困難で、高価なものである。そのため、航空障害灯
の制御系に占める価格の割合が大きいという問題があっ
た。本発明の目的は上記問題を解決するもので、太陽電
池の起電力を直接航空障害灯点滅制御用リレーの駆動に
用いることにより、従来装置に比較し価格を低減化し信
頼性の向上を図った航空障害灯の点滅制御装置を提供す
ることにある。As described above, the conventional blinking control device for an aviation obstruction light controls the blinking control of the aviation obstruction light by detecting the light and darkness by the illumination sensor 7. The illumination sensor 7 is driven by a DC power source, and is generally difficult to obtain overseas and expensive. Therefore, there is a problem that the price of the aviation obstruction light control system is large. The object of the present invention is to solve the above problems, by directly using the electromotive force of the solar cell to drive the aviation obstruction light flashing control relay, the price is reduced and the reliability is improved as compared with the conventional device. An object is to provide a blinking control device for an aviation obstruction light.
【０００４】[0004]
【課題を解決するための手段】前記目的を達成するため
に本発明による太陽電池起電力を利用した航空障害灯の
点滅制御装置は太陽電池と、前記太陽電池の起電力で起
動させられる制御用リレーと、前記太陽電池で充電され
る蓄電池と、前記制御用リレーの接点を介して前記蓄電
池に接続された航空障害灯とを含み、前記太陽電池の起
電力によって前記航空障害灯の点滅制御を行うように構
成されている。In order to achieve the above object, a blinking control device for an aviation obstruction light using a solar cell electromotive force according to the present invention is a solar cell and a control device which is activated by the electromotive force of the solar cell. A relay, a storage battery charged by the solar cell, and an aviation obstruction light connected to the storage battery via a contact of the control relay, and blinking control of the aviation obstruction light by the electromotive force of the solar cell. Is configured to do.
【０００５】[0005]
【実施例】以下、図面を参照して本発明をさらに詳しく
説明する。図１は本発明による太陽電池起電力を利用し
た航空障害灯の点滅制御装置の実施例を示す回路図であ
る。蓄電池２には制御用リレー４の接点５を介して航空
障害灯３が、さらに直接通信機等の負荷８が接続されて
いる。太陽電池１と制御用リレー４は並列に接続されダ
イオード６を介して蓄電池２に接続されている。昼間太
陽電池１の起電力が大きいときはダイオード６を介して
蓄電池２が充電される。制御用リレー４も太陽電池の起
電力により駆動され、接点５はオフ状態に保持される。
そのため、昼間は航空障害等３は消灯しており、通信機
等の負荷８にのみ蓄電池２の電力が供給される。夜間に
なると太陽電池１の起電力が小さくなるので、蓄電池２
の充電が停止するとともに制御用リレー４も起動されな
い。そのため接点５はオン状態になり航空障害灯３に昼
間蓄積された蓄電池の電力が供給され航空障害灯３は点
灯する。DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will be described in more detail below with reference to the drawings. FIG. 1 is a circuit diagram showing an embodiment of a blinking control device for an aviation obstruction light using a solar cell electromotive force according to the present invention. The aviation obstruction light 3 is further connected to the storage battery 2 via the contact 5 of the control relay 4, and the load 8 such as a communication device is directly connected to the storage battery 2. The solar cell 1 and the control relay 4 are connected in parallel and are connected to the storage battery 2 via the diode 6. When the electromotive force of the solar cell 1 in the daytime is large, the storage battery 2 is charged via the diode 6. The control relay 4 is also driven by the electromotive force of the solar cell, and the contact 5 is held in the off state.
Therefore, during the daytime, the aviation obstacle 3 is turned off, and the power of the storage battery 2 is supplied only to the load 8 such as a communication device. Since the electromotive force of the solar cell 1 decreases at night, the storage battery 2
And the control relay 4 is not activated. Therefore, the contact 5 is turned on, the electric power of the storage battery accumulated in the daytime is supplied to the aviation obstruction light 3, and the aviation obstruction light 3 is turned on.
【０００６】[0006]
【発明の効果】以上，説明したように本発明による航空
障害灯の点滅制御装置は太陽電池の起電力を利用して制
御用リレーを駆動制御し航空障害灯と蓄電池の間に挿入
された接点を開閉制御するようにして従来使用していた
照光感知器およびその駆動系を省略したものである。し
たがって、航空障害灯制御盤のコストを低減化でき、信
頼性の向上させることができる。また、調達する部品入
手期間の短縮にも寄与するという効果がある。As described above, the flicker control device for an aviation obstruction light according to the present invention uses the electromotive force of the solar cell to drive and control the control relay, and the contact inserted between the aviation obstruction light and the storage battery. The illumination sensor and its drive system, which have been used in the past, are controlled by opening and closing. Therefore, the cost of the aviation obstruction light control panel can be reduced, and the reliability can be improved. It also has the effect of contributing to the shortening of the procurement period of parts to be procured.
【図１】本発明による太陽電池起電力を利用した航空障
害灯の点滅制御装置の実施例を示す回路図である。FIG. 1 is a circuit diagram showing an embodiment of a blinking control device for an aviation obstruction light using a solar cell electromotive force according to the present invention.
【図２】従来の航空障害灯の点滅制御装置の一例を示す
回路図である。FIG. 2 is a circuit diagram showing an example of a conventional blink control device for an aviation obstruction light.
１…太陽電池 ２…蓄電池 ３…航空障害灯 ４…制御用リレー ５…接点 ６…ダイオード ７…照明感知器／駆動系 ８…通信機等の負荷 DESCRIPTION OF SYMBOLS 1 ... Solar cell 2 ... Storage battery 3 ... Aviation obstruction light 4 ... Control relay 5 ... Contact point 6 ... Diode 7 ... Lighting sensor / driving system 8 ... Load of communication equipment etc.
Claims (1)
動させられる制御用リレーと、前記太陽電池で充電され
る蓄電池と、前記制御用リレーの接点を介して前記蓄電
池に接続された航空障害灯とを含み、前記太陽電池の起
電力によって前記航空障害灯の点滅制御を行うことを特
徴とする太陽電池起電力を利用した航空障害灯の点滅制
御装置。1. A solar cell, a control relay activated by an electromotive force of the solar cell, a storage battery charged by the solar cell, and an aircraft connected to the storage battery via a contact of the control relay. A blinking control device for an aviation obstruction light using solar cell electromotive force, comprising: an obstruction light; and controlling the blinking of the aviation obstruction light by the electromotive force of the solar cell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP27878091A JPH05135608A (en) | 1991-09-30 | 1991-09-30 | Flash control device for airplane warning light using solar battery electromotive force |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP27878091A JPH05135608A (en) | 1991-09-30 | 1991-09-30 | Flash control device for airplane warning light using solar battery electromotive force |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH05135608A true JPH05135608A (en) | 1993-06-01 |
Family
ID=17602078
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP27878091A Pending JPH05135608A (en) | 1991-09-30 | 1991-09-30 | Flash control device for airplane warning light using solar battery electromotive force |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH05135608A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100719641B1 (en) * | 2000-01-31 | 2007-05-17 | 이데미쓰 고산 가부시키가이샤 | Organic electroluminescence display unit and production method therefor |
-
1991
- 1991-09-30 JP JP27878091A patent/JPH05135608A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100719641B1 (en) * | 2000-01-31 | 2007-05-17 | 이데미쓰 고산 가부시키가이샤 | Organic electroluminescence display unit and production method therefor |
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