JPH04289306A - Method for guiding view line in fog - Google Patents
Method for guiding view line in fogInfo
- Publication number
- JPH04289306A JPH04289306A JP3054892A JP5489291A JPH04289306A JP H04289306 A JPH04289306 A JP H04289306A JP 3054892 A JP3054892 A JP 3054892A JP 5489291 A JP5489291 A JP 5489291A JP H04289306 A JPH04289306 A JP H04289306A
- Authority
- JP
- Japan
- Prior art keywords
- fog
- laser beam
- line
- laser
- irradiation device
- 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
- 238000000034 method Methods 0.000 title claims description 24
- 239000002245 particle Substances 0.000 claims abstract description 9
- 230000003287 optical effect Effects 0.000 abstract description 10
- 239000012530 fluid Substances 0.000 abstract description 5
- 230000001678 irradiating effect Effects 0.000 abstract 1
- 239000003897 fog Substances 0.000 description 49
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 14
- 229910002092 carbon dioxide Inorganic materials 0.000 description 7
- 239000001569 carbon dioxide Substances 0.000 description 6
- 239000003595 mist Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 3
- 239000003665 fog water Substances 0.000 description 2
- 230000002238 attenuated effect Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 230000008685 targeting Effects 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Traffic Control Systems (AREA)
- Radar Systems Or Details Thereof (AREA)
- Road Signs Or Road Markings (AREA)
Abstract
Description
【0001】0001
【産業上の利用分野】本発明は、道路、港湾、飛行場に
おける安全通行を確保するために、霧による視線障害を
解消する技術に関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a technology for eliminating visual obstruction caused by fog in order to ensure safe passage on roads, ports, and airports.
【0002】0002
【従来の技術】道路、港湾、飛行場等における霧による
視線障害を抜本的に解決する方法の一つは、霧を人工的
に消散させることで、従来数多くの原理に基いて研究が
続けられている。その中で確実、安全かつ経済的に実用
化可能な方法は、対象地域の気温を上昇させて霧を蒸発
させる方法である。例えば特願平01−073168号
公報に開示された霧の除去方法は、霧を消散させる必要
のある地域に温風管を配置し、該温風管から温風を噴射
して対象地域の気温を上昇させ、霧を消散させる方法で
ある。[Prior Art] One way to fundamentally solve the visibility obstruction caused by fog on roads, ports, airports, etc. is to artificially dissipate the fog. There is. Among these, a reliable, safe and economically practical method is to raise the temperature of the target area and evaporate the fog. For example, in the fog removal method disclosed in Japanese Patent Application No. 01-073168, hot air pipes are placed in areas where fog needs to be dissipated, and warm air is injected from the hot air pipes to reduce the temperature of the target area. This is a method to raise the fog and dissipate the fog.
【0003】また霧対策にレーザーを利用する方法もあ
る。例えば、Mullany et al. (AS
tudy of Fog Clearing Usin
g a CO2 Laser,J.Aircraft,
Vol 8 108−113,1971)は、水が炭
酸ガスレーザをよく吸収することから、原理的に炭酸ガ
スレーザは消霧に利用できることを示している。[0003] There is also a method of using a laser as a countermeasure against fog. For example, Mullany et al. (A.S.
study of Fog Clearing Usin
g a CO2 Laser, J. Aircraft,
Vol. 8, 108-113, 1971) shows that since water absorbs carbon dioxide gas well, carbon dioxide laser can in principle be used for fogging.
【0004】0004
【発明が解決しようとする課題】ところで温風を噴射し
て消霧する方法は、道路のように消霧対象区域(道路幅
×高さ)が小さい場合は有効であるが、飛行場全域とい
った消霧対象区域が広い場合は、風により消霧対象区域
が吹き流されるという問題がある。すなわち霧を消散さ
せるべき範囲は上空ほど滑走路から風下側へずれてしま
うわけである。これを防止するために、例えばより風上
側から噴射すれば、消霧範囲が不必要に広くなり経済的
に不都合となる。[Problem to be solved by the invention] By the way, the method of dissipating fog by blowing warm air is effective when the area to be dissipated (road width x height) is small, such as a road, but it is If the fogging target area is wide, there is a problem that the fogging target area is blown away by the wind. In other words, the area in which fog should be dissipated shifts further downwind from the runway the higher up in the sky. In order to prevent this, for example, if spraying is performed from the windward side, the area of fogging will become unnecessarily wide, which will be economically disadvantageous.
【0005】またレーザを使用する方法は、原理的には
霧を加熱し蒸発させる方法である。この場合まずレーザ
のエネルギ効率が問題となる。炭酸ガスレーザの場合、
電気からレーザ光への変換効率は20%に過ぎず、消霧
に利用するには経済的に難点がある。さらにレーザによ
る消霧においては、霧粒の空間密度が小さいことが問題
である。すなわち霧粒の大きさとその平均的な間隔は、
それぞれ10μmと2〜3mmであり、この程度ではレ
ーザ光の光束と霧粒が衝突する頻度が小さいので、消霧
の効率は低くなる。それに強力な炭酸ガスレーザを照射
するので、安全性にも問題がある。[0005] The method using a laser is, in principle, a method of heating and vaporizing fog. In this case, the first issue is the energy efficiency of the laser. In the case of carbon dioxide laser,
The conversion efficiency from electricity to laser light is only 20%, making it economically difficult to use it for fogging. Furthermore, a problem with laser fogging is that the spatial density of fog particles is small. In other words, the size of the mist droplets and their average spacing are
They are 10 μm and 2 to 3 mm, respectively, and at these levels, the frequency of collision between the laser beam and the fog particles is low, so the efficiency of fog elimination is low. It also involves safety issues since it uses a powerful carbon dioxide laser to irradiate it.
【0006】本発明は上記従来装置の問題点を解消する
ためになされたもので、操縦者の視線を誘導することに
より、濃霧の中でも車両や航空機あるいは船舶の運航を
可能にする視線誘導方法を提供しようとするものである
。なお温風噴射による消霧方法と併用することにより、
該消霧方法における風による影響を除去することが可能
である。The present invention has been made to solve the problems of the conventional devices described above, and provides a line-of-sight guidance method that enables the operation of a vehicle, aircraft, or ship even in dense fog by guiding the operator's line of sight. This is what we are trying to provide. In addition, by using it in conjunction with the fogging method using hot air jet,
It is possible to eliminate the influence of wind in the fogging method.
【0007】[0007]
【課題を解決するための手段】上記目的を達成するため
、本発明は道路、飛行場あるいは港湾の要部にレーザ光
照射装置を配置し、霧発生時レーザ光を照射し得るよう
に構成した。[Means for Solving the Problems] In order to achieve the above object, the present invention is configured such that a laser beam irradiation device is arranged at a main part of a road, an airport, or a port, and can irradiate the laser beam when fog occurs.
【0008】[0008]
【作用】霧の中で照射されたレーザ光(例えばHe 、
Ne レーザ)は、霧粒により反射散乱され、その光軸
は赤色に発光し可視化される。前述したように霧粒の空
間密度は小さいので、レーザ光は大きく減衰することな
く霧の中を直進する。炭酸ガスレーザによる消霧ではデ
ィメリットとなった霧の性質が、この方法の場合はメリ
ットとなる。車や航空機の操縦者はこの可視化された光
軸を見ながら車や航空機を操縦すればよく、濃霧中でも
操縦可能となる。[Operation] Laser light irradiated in fog (e.g. He,
Ne laser) is reflected and scattered by fog particles, and its optical axis emits red light and is visualized. As mentioned above, since the spatial density of fog particles is small, the laser light travels straight through the fog without being significantly attenuated. The nature of the fog, which is a disadvantage when using a carbon dioxide laser, is an advantage when using this method. The operator of a car or aircraft can operate the vehicle or aircraft while looking at this visualized optical axis, making it possible to operate the vehicle or aircraft even in dense fog.
【0009】なお飛行場を対象とした場合は、本発明に
よる視線誘導と併せ、温風噴射による消霧方法を使用す
ることが必要である。風の影響で消霧域が吹き流されて
いる上空では、可視化された光軸により正規の進入経路
を知るとともに、高度を低下させて接地点近くになれば
、温風噴射により消霧された滑走路を視認できることと
なる。一般に計器誘導の設備を備えた飛行場では、操縦
士が計器に頼ることなく操縦しなければならないのは、
対地高度60m、または30mから接地点までである。
したがってレーザ光による視線誘導は、短距離で十分で
ある。ただし視線誘導で進入経路を知ることができても
、滑走路を視認できなければ着陸できないので、着陸機
の誘導においては、消霧方法を併用することは絶対条件
である。[0009] When targeting an airport, it is necessary to use a misting method using hot air injection in addition to the line-of-sight guidance according to the present invention. In the upper atmosphere, where the fog dissipation area is blown away by the influence of the wind, the normal approach route is determined by the visualized optical axis, and when the altitude is lowered and the fog is near the grounding point, the fog is dissipated by the hot air jet. The runway will be visible. Generally, at airfields equipped with instrument guidance equipment, pilots must operate without relying on instruments.
The height above the ground is 60m or 30m to the grounding point. Therefore, short distance guidance by laser light is sufficient. However, even if the approach route can be determined through line-of-sight guidance, it will not be possible to land if the runway cannot be seen, so it is an absolute prerequisite to use fog removal methods in conjunction with the guidance of landing aircraft.
【0010】0010
【実施例】図1は本発明の実験装置の断面図で、図中1
は風洞、2は霧発生装置、3は2流体ノズル、4は送気
管、5はハニカム壁、6はレーザ光照射装置、7はフォ
トセルである。図にみるように、実験装置は長さ6m、
断面2m×2mの風洞1の一端に霧発生装置2を付設し
てなるものである。霧発生装置2内には2流体ノズル3
と送気管4が配設されており、2流体ノズル3により発
生した霧は、送気管4より送られる一定流量の圧縮空気
により、ハニカム壁5を介し整流され一定速度で風洞1
内へ送給される。[Example] Figure 1 is a sectional view of the experimental apparatus of the present invention.
2 is a wind tunnel, 2 is a fog generator, 3 is a two-fluid nozzle, 4 is an air pipe, 5 is a honeycomb wall, 6 is a laser beam irradiation device, and 7 is a photocell. As shown in the figure, the experimental equipment is 6 m long.
A fog generator 2 is attached to one end of a wind tunnel 1 having a cross section of 2 m x 2 m. There is a two-fluid nozzle 3 in the fog generator 2.
The mist generated by the two-fluid nozzle 3 is rectified through a honeycomb wall 5 by a constant flow of compressed air sent from the air pipe 4, and is sent to the wind tunnel 1 at a constant speed.
sent inside.
【0011】この実験装置により、霧粒の半径は5〜2
0μm、霧水量は0.05〜1.5g/m3 の範囲で
実験を行い以下の結果を得た。この条件範囲は霧粒が小
さく霧水量が少ない放射霧、滑昇霧などから、逆に霧粒
が大きく霧水量が多い海霧にいたるまでの自然状態のあ
らゆる種類の霧を再現可能である。[0011] With this experimental device, the radius of the mist droplets is 5 to 2.
Experiments were conducted with a mist of 0 μm and a mist amount in the range of 0.05 to 1.5 g/m 3 and the following results were obtained. This range of conditions makes it possible to reproduce all types of fog in natural conditions, from radiation fog and gliding fog, which have small fog particles and a small amount of fog water, to sea fog, which has large fog particles and a large amount of fog water.
【0012】風洞1の一端に波長780nmの半導体レ
ーザ6を設置して照射したところ、霧の中に赤色の直線
が可視化された。この直線の明るさは、霧の中で操縦者
が進行方向を知るのに十分なものである。さらにレーザ
光の強さを調べるため、風洞1の風下側にフォトセル7
を配置した。霧の有無によるフォトセル7の出力を比較
した結果、距離6mではレーザ光の減衰は10%以下で
あった。すなわち長距離に亘ってレーザ光による視線誘
導は可能である。When a semiconductor laser 6 with a wavelength of 780 nm was installed at one end of the wind tunnel 1 and irradiated, a red straight line was visualized in the fog. The brightness of this straight line is sufficient for the pilot to know the direction of travel in fog. Furthermore, in order to investigate the intensity of the laser beam, a photocell 7 was placed on the leeward side of the wind tunnel 1.
was placed. As a result of comparing the output of the photocell 7 with and without fog, the attenuation of the laser light was 10% or less at a distance of 6 m. In other words, it is possible to guide the line of sight using laser light over a long distance.
【0013】ついで風洞1内にポリゴンミラーを配置し
、これにレーザ光を照射したところ赤色の光幕ができた
。このことから直線だけでなく光幕による視線誘導も可
能であることが判る。[0013] Next, a polygon mirror was placed in the wind tunnel 1, and when a laser beam was irradiated onto it, a red light screen was created. This shows that it is possible to guide the line of sight not only by straight lines but also by light curtains.
【0014】このレーザ光を、例えば道路の両側の路肩
に沿って照射すれば、レーザ光の光軸は可視化され濃霧
中でも車の運転者は道路の輪郭が見える。したがって運
転者はその可視化された光軸に沿って運転すれば濃霧中
でも運転できることとなる。同様に飛行場の滑走路の着
陸接地点付近の進入経路、誘導路及び駐機場などの航空
機の進行方向に沿ってレーザ照射装置を配設すれば、濃
霧中着陸する航空機を可視化された光軸に沿って視線誘
導することが可能となり、また船舶の接岸岸壁に沿って
レーザ光照射装置を配設すれば、霧中で船舶を視線誘導
することができることとなる。なお操縦者は可視化され
た光軸により進行方向を知るのであるから、炭酸ガスレ
ーザによる消霧と異なり危険性は少ない。[0014] If this laser light is irradiated, for example, along the shoulders on both sides of the road, the optical axis of the laser light will be made visible and the driver of the car will be able to see the outline of the road even in dense fog. Therefore, the driver can drive even in dense fog by driving along the visualized optical axis. Similarly, if a laser irradiation device is placed along the approach path, taxiway, and apron near the landing point of an airfield runway, along the direction of aircraft movement, aircraft landing in dense fog can be directed to a visible optical axis. If a laser beam irradiation device is installed along the berth of a ship, it becomes possible to guide the line of sight of a ship in fog. Since the operator knows the direction of travel from the visualized optical axis, there is less danger than fogging using a carbon dioxide laser.
【0015】また上記実施例は、道路、飛行場あるいは
港湾における使用例であるが、本発明に係る視線誘導方
法は、道路、飛行場、港湾に限らず広く利用できるもの
である。Furthermore, although the above embodiments are examples of use on roads, airports, and ports, the line-of-sight guidance method according to the present invention can be widely used not only on roads, airports, and ports.
【0016】[0016]
【発明の効果】本発明は、霧中にレーザ光を照射し、レ
ーザ光を霧粒に当てて反射散乱させることによりレーザ
光光軸を可視化し、車や航空機の操縦者の視線誘導を可
能としたので、濃霧中でも車の運転や航空機の着陸誘導
を可能ならしめ、霧による交通障害を防止するという優
れた効果を挙げることとなった。[Effects of the Invention] The present invention irradiates a laser beam into fog, and by reflecting and scattering the laser beam on the fog particles, the optical axis of the laser beam is visualized, making it possible to guide the line of sight of the operator of a car or aircraft. As a result, it has become possible to drive cars and guide aircraft to land even in dense fog, and has the excellent effect of preventing traffic obstructions caused by fog.
【0017】また温風噴射による消霧方法と併用するこ
とにより、風による消霧効果への影響を除去できるので
、消霧コストを低減させることとなる。[0017] Furthermore, by using the method in combination with a fogging method using warm air jetting, the influence of wind on the fogging effect can be eliminated, so that the cost of fogging can be reduced.
【図1】本発明の実験装置の断面図である。FIG. 1 is a sectional view of an experimental apparatus of the present invention.
1………風洞 2………霧発生装置、 3………2流体ノズル、 4………送気管、 5………ハニカム壁、 6………レーザ光照射装置、 7………フォトセル。 1……Wind tunnel 2... Fog generator, 3...2 fluid nozzle, 4...Air pipe, 5……honeycomb wall, 6... Laser light irradiation device, 7...Photocell.
Claims (4)
ーザ光照射装置を配置し、霧発生時レーザ光を照射して
霧粒により反射散乱せしめ、レーザ光軸を可視化するこ
とにより、車、航空機及び船舶の視線誘導を可能ならし
めたことを特徴とする霧中における視線誘導方法。Claim 1: A laser beam irradiation device is installed at the main part of a road, airport, or port, and when fog occurs, the laser beam is irradiated and reflected and scattered by the fog particles, and the laser beam axis is visualized. and a line-of-sight guidance method in fog, characterized by making it possible to guide the line-of-sight of a ship.
進行方向に沿ってレーザ光照射装置を配設し、車や航空
機を誘導するようにしたことを特徴とする請求項1に記
載の霧中における視線誘導方法。2. The method according to claim 1, wherein a laser beam irradiation device is arranged along the traveling direction of a car or aircraft on a road or an airport to guide the car or aircraft. Eye guidance method.
し、船舶を誘導するようにしたことを特徴とする請求項
1に記載の霧中における視線誘導方法。3. The line-of-sight guidance method in fog according to claim 1, wherein a laser beam irradiation device is arranged along the route to guide the ship.
に霧を消散させる方法とを組合わせて視線誘導を行うこ
とを特徴とする霧中における視線誘導方法。4. A line-of-sight guidance method in fog, characterized in that line-of-sight guidance is performed by combining a line-of-sight guidance method using laser light and a method of artificially dissipating fog.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3054892A JPH04289306A (en) | 1991-03-19 | 1991-03-19 | Method for guiding view line in fog |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3054892A JPH04289306A (en) | 1991-03-19 | 1991-03-19 | Method for guiding view line in fog |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH04289306A true JPH04289306A (en) | 1992-10-14 |
Family
ID=12983250
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP3054892A Pending JPH04289306A (en) | 1991-03-19 | 1991-03-19 | Method for guiding view line in fog |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH04289306A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0710744A1 (en) * | 1994-09-23 | 1996-05-08 | ADVENT S.r.l. | A traffic aid apparatus to be used under conditions of low visibility |
JP2015135028A (en) * | 2014-01-20 | 2015-07-27 | 三菱電機株式会社 | Shading screen device |
-
1991
- 1991-03-19 JP JP3054892A patent/JPH04289306A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0710744A1 (en) * | 1994-09-23 | 1996-05-08 | ADVENT S.r.l. | A traffic aid apparatus to be used under conditions of low visibility |
JP2015135028A (en) * | 2014-01-20 | 2015-07-27 | 三菱電機株式会社 | Shading screen device |
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