JPH03262100A - Synchronizing light emitting system for airplane warning light - Google Patents
Synchronizing light emitting system for airplane warning lightInfo
- Publication number
- JPH03262100A JPH03262100A JP6178490A JP6178490A JPH03262100A JP H03262100 A JPH03262100 A JP H03262100A JP 6178490 A JP6178490 A JP 6178490A JP 6178490 A JP6178490 A JP 6178490A JP H03262100 A JPH03262100 A JP H03262100A
- Authority
- JP
- Japan
- Prior art keywords
- lamp
- airplane
- light
- flashing
- aircraft
- 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
- 230000004397 blinking Effects 0.000 claims description 9
- 230000001360 synchronised effect Effects 0.000 claims description 8
- 238000001514 detection method Methods 0.000 claims description 7
- 238000010586 diagram Methods 0.000 description 3
- 238000007493 shaping process Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 230000008054 signal transmission Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
Abstract
Description
【発明の詳細な説明】
（産業上の利用分野）
本発明は複数の地点に設置されている高光度航空障害灯
の同期発光システムに関するものである。DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a synchronized lighting system for high-intensity aviation obstacle lights installed at multiple locations.
（従来の技術及び解決しようとする課題）従来、離れた
２地点に設置されている航空障害灯の点滅を同期させる
ためには、上記２地間に同期信号を伝送するシステムが
必要であり、この伝送システムとしては有線又は無線が
用いられている。(Prior Art and Problems to be Solved) Conventionally, in order to synchronize the flashing of aircraft obstacle lights installed at two distant locations, a system is required to transmit a synchronization signal between the two locations. A wired or wireless transmission system is used for this transmission system.
しかし、有線で同期信号を伝送する場合には、条件によ
っては線路を敷設できない場所があり、又距離が離れて
いる場合にはコスト高になるという問題点があった。又
無線を用いた場合にもコスト高になるという問題点があ
った。However, when transmitting the synchronization signal by wire, there are some places where it is impossible to lay a line depending on the conditions, and there are problems in that the cost is high when the distance is far. There is also a problem in that the cost is high even when wireless is used.
（課題を解決するための手段）
本発明は上述の問題点を解消した航空障害灯同期発光シ
ステムを提供するもので、その特徴は、複数の地点に航
空障害灯が設置された地域において、一つの地点の航空
障害灯にホトダイオードを具えた発光検出部を設置し、
上記発光検出部にて他地点の航空灯ランプの点滅を検出
し、この点滅に自地点の航空灯ランプの点滅を同期させ
ることにある。(Means for Solving the Problems) The present invention provides a synchronized lighting system for aircraft obstacle lights that solves the above-mentioned problems. A light emission detection unit equipped with a photodiode is installed on the aircraft obstacle lights at two locations.
The purpose of the present invention is to detect the blinking of an aircraft light lamp at another location using the light emission detection section, and to synchronize the blinking of an aircraft light lamp at the own location with this blinking.
（作用）
上述した本発明の航空障害灯同期発光システムにおいて
は、離れた地点に設置されている航空障害灯の航空灯ラ
ンプの点滅（通常１．５秒毎）している発光状況を発光
検出部で検出し、この吠況を自地点の航空障害灯に入力
し、この信号で航空灯ランプを発光させることが出来、
従来のような同期信号の伝送システムを設置することが
なく、安価に同期を得ることが出来るシステムである。(Function) In the above-mentioned aviation obstacle light synchronous lighting system of the present invention, light emission is detected in the blinking (usually every 1.5 seconds) light emission situation of the aviation light lamp of the aviation obstacle light installed at a distant point. This signal is detected by the aircraft, and this signal is input to the aircraft obstruction light at the aircraft's own location.
This is a system that can obtain synchronization at low cost without installing a synchronization signal transmission system like in the past.
（実施例）
第１図は本発明の航空障害灯同期発光システムの具体例
の説明図である。(Example) FIG. 1 is an explanatory diagram of a specific example of the aircraft obstacle light synchronous light emission system of the present invention.
図面において、（１）（１″）は離れた２地点に設置さ
れている航空障害灯の航空灯ランプ、（２）（２′）は
それぞれの航空発光制御盤、（３）は一つの地点の航空
障害灯に設置されている発光検出部である。In the drawing, (1) (1'') are the aviation light lamps of the aviation obstruction lights installed at two separate locations, (2) (2') are the respective aviation lighting control panels, and (3) is one location. This is a light emission detection unit installed in aircraft obstacle lights.
上記発光検出部（３）は集光レンズ（３３）、ホトダイ
オード（３２）、アンプ（３３）、整形回路（３４）及
びこれらを収納した筐体（３５）により構成されている
。離れた地点の航空灯ランプ（ｌ′）の点滅している発
光を集光レンズ（３１）で集光し、この集光した光信号
をホトダイオード（３２）で電気信号に変換し、これを
アンプ（３３）で増幅し、得られた信号を整形回路（３
４）でパルス化する。このパルス化された信号は第２図
に示す航空ランプ発光制御盤（２）の信号処理部（２１
）に送られ、さらに制御回路（２２）にて自地点の航空
灯ランプ（１）の発光タイミングを修正し、両者の航空
ランプ（１）（＋’ ）の発光を同期させる。The light emission detection section (3) is composed of a condensing lens (33), a photodiode (32), an amplifier (33), a shaping circuit (34), and a housing (35) housing these. A condensing lens (31) condenses the blinking light emitted from an aviation light lamp (l') at a distant point, and the condensed optical signal is converted into an electrical signal by a photodiode (32), which is then sent to an amplifier. (33) and the resulting signal is amplified by the shaping circuit (33).
4) Pulse. This pulsed signal is transmitted to the signal processing section (21) of the aircraft lamp emission control panel (2) shown in Figure 2.
), and further, the control circuit (22) corrects the light emission timing of the aircraft light lamp (1) at the own location, and synchronizes the light emission of both aircraft lamps (1) (+').
（発明の効果）
°ｈ
１以上説明したように、本発明の航空障害灯同期発光シ
ステムによれば、離れた地点に設置されている航空障害
灯の航空灯ランプの点滅を一つの地点に設置した発光検
出部にて検出し、これにより自地点の航空灯ランプの点
滅を同期させるので、２地点間に同期信号の伝送システ
ムを設置する必要がなく、簡易でかつ安価に離れた地点
間の航空ランプ点滅の同期を得ることができる。(Effect of the invention) °h As explained above, according to the aviation obstacle light synchronous lighting system of the present invention, the blinking of the aviation obstacle lights installed at distant locations can be set at one location. Since the flashing of the aircraft light lamp at the own point is synchronized, there is no need to install a synchronization signal transmission system between two points, making it easy and inexpensive to connect distant points. It is possible to obtain synchronization of aviation lamp flashing.
第１図は本発明の航空障害灯同期発光システムの具体例
の説明図、第２図は航空灯ランプ発光制御盤の回路図で
ある。
１．１″・・・航空灯ランプ、２．２’・・・航空灯ラ
ンプ発光制御盤、２】・・・信号処理部、２２・・・航
空灯ランプ制御回路、３・・・発光検出部、３１・・・
集光レンズ、３２・・・ホトダイオード、３３・・・ア
ンプ、３４・・・整形回路、３５・・・収納筐体。FIG. 1 is an explanatory diagram of a specific example of the aircraft obstacle light synchronous light emission system of the present invention, and FIG. 2 is a circuit diagram of the aircraft light lamp emission control panel. 1.1''...Aviation light lamp, 2.2'...Aviation light lamp emission control panel, 2]...Signal processing section, 22...Aviation light lamp control circuit, 3...Emission detection Part, 31...
Condensing lens, 32... Photodiode, 33... Amplifier, 34... Shaping circuit, 35... Storage casing.
Claims (1)
て、一つの地点の航空障害灯にホトダイオードを具えた
発光検出部を設置し、上記発光検出部にて他地点の航空
灯ランプの点滅を検出し、この点滅に自地点の航空灯ラ
ンプの点滅を同期させることを特徴とする航空障害灯同
期発光システム。(1) In areas where aviation obstruction lights are installed at multiple points, a light emission detection unit equipped with a photodiode is installed in the aviation obstruction light at one point, and the light emission detection unit blinks the aviation light lamps at other points. An aircraft obstruction light synchronous lighting system characterized by detecting the blinking of the aircraft light and synchronizing the blinking of the aircraft light lamp at the own point with this blinking.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6178490A JPH03262100A (en) | 1990-03-13 | 1990-03-13 | Synchronizing light emitting system for airplane warning light |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6178490A JPH03262100A (en) | 1990-03-13 | 1990-03-13 | Synchronizing light emitting system for airplane warning light |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH03262100A true JPH03262100A (en) | 1991-11-21 |
Family
ID=13181062
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6178490A Pending JPH03262100A (en) | 1990-03-13 | 1990-03-13 | Synchronizing light emitting system for airplane warning light |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH03262100A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH08253198A (en) * | 1995-03-17 | 1996-10-01 | Minikamu Res:Kk | Light emitting marker lamp and light emitting marker lamp device |
| JPH11193774A (en) * | 1997-12-27 | 1999-07-21 | Koito Ind Ltd | Aerogenerator and aerial obstruction lamp used in the same |
| JP2003533789A (en) * | 2000-05-09 | 2003-11-11 | アロイス・ヴォベン | Wind warning light device for wind power equipment |
-
1990
- 1990-03-13 JP JP6178490A patent/JPH03262100A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH08253198A (en) * | 1995-03-17 | 1996-10-01 | Minikamu Res:Kk | Light emitting marker lamp and light emitting marker lamp device |
| JPH11193774A (en) * | 1997-12-27 | 1999-07-21 | Koito Ind Ltd | Aerogenerator and aerial obstruction lamp used in the same |
| JP2003533789A (en) * | 2000-05-09 | 2003-11-11 | アロイス・ヴォベン | Wind warning light device for wind power equipment |
| US7355522B2 (en) | 2000-05-09 | 2008-04-08 | Aloys Wobben | Aircraft beacon device on wind power installations |
| AU2006201917B2 (en) * | 2000-05-09 | 2009-06-04 | Aloys Wobben | Aircraft beacon device on wind power installations |
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