FR2497003A1 - Passive tethered radar reflector - uses inflated aerofoil coated with metallic surface to reflect electromagnetic rays and has blade structure for wind stability - Google Patents

Passive tethered radar reflector - uses inflated aerofoil coated with metallic surface to reflect electromagnetic rays and has blade structure for wind stability Download PDF

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Publication number
FR2497003A1
FR2497003A1 FR8027407A FR8027407A FR2497003A1 FR 2497003 A1 FR2497003 A1 FR 2497003A1 FR 8027407 A FR8027407 A FR 8027407A FR 8027407 A FR8027407 A FR 8027407A FR 2497003 A1 FR2497003 A1 FR 2497003A1
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FR
France
Prior art keywords
envelope
aerofoil
tethered
passive
radar reflector
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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.)
Withdrawn
Application number
FR8027407A
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French (fr)
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Individual
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Individual
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Publication date
Application filed by Individual filed Critical Individual
Priority to FR8027407A priority Critical patent/FR2497003A1/en
Publication of FR2497003A1 publication Critical patent/FR2497003A1/en
Withdrawn legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/08Means for collapsing antennas or parts thereof
    • H01Q1/081Inflatable antennas
    • H01Q1/082Balloon antennas

Abstract

The passive radar reflector includes a container housing a cylinder of compressed gas. This is connected via a valve and pressure controlling assembly to an inflatable envelope. The envelope is folded within the container, but may be released under the pressure of the gas from the cylinder. A line restraining the unfolded envelope is attached to a drum. The envelope is made of flexible material coated with a metallic layer, and when inflated forms an aerofoil structure. When tethered by the line at an appropriate angle, the aerofoil is held up by the wind. The aerofoil is released automatically when it is fully inflated, using the differential pressure effect inside the aerofoil envelope. The arrangement can be used in light dinghies for transmission of distress signals.

Description

La présente invention concerne les dispositifs du type "ré- flecteur radar", permettant de provoquer l'écho d'un faisceau d'ondes électromagnétiques. The present invention relates to devices of the "radar reflector" type, making it possible to cause the echo of a beam of electromagnetic waves.

L'efficacité des réflecteurs classiques dépend des possibilités qu'ont leurs utilisateurs de les installer suffisamment haut pour entrer dans le champ du radar La nécessité de supporter ces réflecteurs par des moyens rigides, limite la hauteur possible de leur installation. De tels dispositifs deviennent totalement inefficaces en cas de démâtage ou de chavirage d'une embarcation, et ne sont pas adaptés aux équipements de survie classiques tels que les canots pneumatiques ou les gilets de sauvetage. On connait d'autres moyens destinés au repérage, comme les émetteurs radio, consommateurs d'énergie, ou les fusées éclairantes, dont l'effet est limité dans le temps. The efficiency of conventional reflectors depends on the possibilities of their users to install them high enough to enter the radar field. The need to support these reflectors by rigid means, limits the possible height of their installation. Such devices become totally ineffective in the event of dismasting or capsizing of a boat, and are not suitable for conventional survival equipment such as inflatable boats or life jackets. Other means are known for tracking, such as radio transmitters, energy consumers, or flares, whose effect is limited in time.

Le réflecteur selon l'invention permet d'éviter ces inconvénients, et d'étendre l'usage de la recherche par détection ra dar Il est en effet conçu pour que sa visualisation optique ou radar se fasse à une altitude suffisamment importante pour échapper au masquage -du relief. D'autre part, son conditionnement en volume réduit et sa simplicité de mise en oeuvre en font un accessoire peu genant pour l'utilisateur. The reflector according to the invention makes it possible to avoid these drawbacks, and to extend the use of research by ra dar detection. It is in fact designed so that its optical or radar visualization is done at an altitude sufficiently high to escape masking. -relief. On the other hand, its packaging in reduced volume and its simplicity of implementation make it an inconvenient accessory for the user.

te réflecteur est une structure gonflable, réalisée en matière souple métallisée, maintenue en altitude par aérostation, reliée à l'utilisateur par un filin solidaire d'un ensemble de conditionnement et de remplissage. The reflector is an inflatable structure, made of metallized flexible material, maintained at altitude by ballooning, connected to the user by a rope secured to a packaging and filling assembly.

Selon une première variante, le moyen de mise en oeuvre est. According to a first variant, the means of implementation is.

manuel, donc nécessitant l'intervention de l'utilisateur.manual, therefore requiring user intervention.

Selon une deuxième variante, le moyen de mise en oeuvre est associé à un déclencheur adapté à l'usage du porteur et au milieu dans lequel il évolue. According to a second variant, the means of implementation is associated with a trigger adapted to the use of the wearer and to the environment in which he operates.

Le dessin annexé 1/4 représente l'ensemble de l'équipement hors utilisation, quand le moyen de mise en oeuvre est manuel
Le dessin annexé 2/4 représente le raccord éjectable G.
The attached drawing 1/4 represents all the equipment not in use, when the means of implementation is manual
The attached drawing 2/4 shows the ejection connector G.

Le dessin annexé 3/4 représente l'enveloppe gonflable 4 en service, et l'action des tuyères dont elle est pourvue. The attached drawing 3/4 shows the inflatable casing 4 in service, and the action of the nozzles with which it is provided.

Le dessin annexé 4/4 représente le réflecteur en service, équipant un canot de survie. The attached drawing 4/4 shows the reflector in service, fitted to a lifeboat.

Tel qu'il est représenté sur le dessin l/4, l'ensemble de l'équipement comprend une enveloppe de conditionnement 1 et son moyen de fixation à l'utilisateur, une cartouche de gaz comprimé 2, un robinet 3 commandant le remplissage de l'enveloppe 4, par l'intermédiaire d"un détendeur 5 et d'un ensemble de raccords éjectables 6. Le filin T assurant la liaison entre l'enveloppe 4 et llutilisateur, est enroulé sur la bobine 8.  As shown in drawing l / 4, the entire equipment includes a packaging envelope 1 and its means of attachment to the user, a compressed gas cartridge 2, a tap 3 controlling the filling of the casing 4, by means of a regulator 5 and a set of ejectable fittings 6. The rope T ensuring the connection between the casing 4 and the user, is wound on the reel 8.

Tel qu'il est représenté sur le dessin 2/4, le raccord éiec- table 6 fonctionne par différence de pression. La pression exercée sur le piston 10 par le gaz non détendu, en passant par l'orifice i, provoque le serrage de la pince t2. Celle-ci assure le positionnement du raccord de remplissage de 11 enveloppe 4 sur l'arrivée de gaz détendu 9. Le gaz détendu- exerce une pression opposée à la précédente en passant par l'orifice BI En fin de remplissage, la pression du gaz, préalablement dosé en quantité, décruait en k, et équilibre la pression appliquée en B. Le ressort tt provoque alors le recul du piston tO, commandant ainsi l'ouverture de la pince 12 qui libère le raccord de remplissage de l'enveloppe 4. Dès lors, ce11e-ci prend de l'altitude jusqu'à dévidage complet du filin X.  As shown in drawing 2/4, the electrical connection 6 operates by pressure difference. The pressure exerted on the piston 10 by the non-expanded gas, passing through the orifice i, causes the clamp t2 to be tightened. This ensures the positioning of the filling connector of 11 casing 4 on the expanded gas inlet 9. The expanded gas- exerts a pressure opposite to the previous one passing through the orifice BI At the end of filling, the gas pressure , previously dosed in quantity, decreased in k, and balances the pressure applied at B. The spring tt then causes the piston tO to recede, thus controlling the opening of the clamp 12 which releases the filling connection from the casing 4. From then on, this one gains altitude until the wire X is completely unwound.

Telle qu'elle est représentée sur le dessin 3/4, l'enveloppe 4 comporte un système de tuyères permettant de provoquer une réaction tendant à limiter l'inclinaison du réflecteur sous l'effet du vent
Tel qu'il est représenté sur le dessin 4/4, le réflecteuren service présente une surface réfléchissante importante, à une altitude suffisante pour être visualisé par un radar équipant un avion ou un navire.
As shown in the drawing 3/4, the casing 4 includes a nozzle system making it possible to cause a reaction tending to limit the inclination of the reflector under the effect of the wind
As shown in drawing 4/4, the reflector in service has a large reflecting surface, at an altitude sufficient to be viewed by a radar fitted to an airplane or a ship.

Le dispositif objet de l'invention peut être utilisé dans tous les cas où les conditions climatiques, la nuit, l'étendue importante d'une zone de recherches, rendent celles-ci longues et difficiles. Citons en particulier les océans, les déserts, les zones enneigées, les régions au relief accidenté ou à végétation dense. C'est un équipement annexe particulièrement adapté aux canots pneumatiques, gilets de sauvetage, embarcations légères. The device which is the subject of the invention can be used in all cases where the climatic conditions, at night, the large extent of a research area, make them long and difficult. Let us cite in particular the oceans, deserts, snow-covered areas, regions with uneven relief or dense vegetation. It is additional equipment particularly suitable for inflatable boats, life jackets, light boats.

Son utilisation peut concerner aussi les aéronefs contraints à un atterrissage forcé, les véhicules terrestres immobilisés ou égarés, de même que tous les objets dont la recherche présente un intérêt particulier. Its use can also relate to aircraft forced to a forced landing, land vehicles immobilized or lost, as well as all objects whose research is of particular interest.

Claims (4)

REVENDICATIONS 1. Réflecteur radar passif associé à un ensemble de conditionnement et de remplissage, caractérisé par le fait que l'enveloppe réfléchissante (4) est une structure gonflable, captive, maintenue en altitude par aérostation. 1. Passive radar reflector associated with a conditioning and filling assembly, characterized in that the reflecting envelope (4) is an inflatable, captive structure, maintained in altitude by aerostation. 2. Réflecteur selon la revendication t, caractérisé en ce que l'enveloppe (4) est réalisée en matière souple métallisée. 2. Reflector according to claim t, characterized in that the envelope (4) is made of metallized flexible material. 3. Réflecteur selon la revendication 1, caractérisé en ce que l'enveloppe (4) est dotée d'un système de tuyères assurant son maintien en altitude sous l'effet du vent. 3. Reflector according to claim 1, characterized in that the casing (4) is provided with a nozzle system ensuring its maintenance in altitude under the effect of the wind. 4. Réflecteur selon la revendication t, caractérisé en ce que le largage de l'enveloppe (4) se fait automatiquement dès que son remplissage est terminé, au moyen d'un dispositif anne ze (6) utilisant l'effet de pression différentielle.  4. Reflector according to claim t, characterized in that the release of the envelope (4) is done automatically as soon as its filling is completed, by means of an anne ze device (6) using the differential pressure effect.
FR8027407A 1980-12-22 1980-12-22 Passive tethered radar reflector - uses inflated aerofoil coated with metallic surface to reflect electromagnetic rays and has blade structure for wind stability Withdrawn FR2497003A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8027407A FR2497003A1 (en) 1980-12-22 1980-12-22 Passive tethered radar reflector - uses inflated aerofoil coated with metallic surface to reflect electromagnetic rays and has blade structure for wind stability

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8027407A FR2497003A1 (en) 1980-12-22 1980-12-22 Passive tethered radar reflector - uses inflated aerofoil coated with metallic surface to reflect electromagnetic rays and has blade structure for wind stability

Publications (1)

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FR2497003A1 true FR2497003A1 (en) 1982-06-25

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FR8027407A Withdrawn FR2497003A1 (en) 1980-12-22 1980-12-22 Passive tethered radar reflector - uses inflated aerofoil coated with metallic surface to reflect electromagnetic rays and has blade structure for wind stability

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2637809A1 (en) * 1988-10-19 1990-04-20 Gautier Richard Device for locating persons in distress using an automatically inflating captive air balloon
US20150191231A1 (en) * 2012-09-24 2015-07-09 Korea Institute Of Ocean Scienec & Technology Radar reflector operating device for indicating emergency position
CN109018246A (en) * 2018-09-11 2018-12-18 广东宏穗晶科技服务有限公司 A kind of water life-saving robot
CN110658519A (en) * 2019-09-18 2020-01-07 武汉大学 Wind turbine generator blade state monitoring method based on external radiation source radar

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2778332A (en) * 1954-03-15 1957-01-22 Reed Tollefsen Means for locating crashed airplanes
US3279419A (en) * 1965-05-03 1966-10-18 Michael A Demarco Signal balloon device
US3395877A (en) * 1966-09-26 1968-08-06 Schjeldahl Co G T Aerodynamic site marker balloon
US3727229A (en) * 1971-07-29 1973-04-10 R Parthum Balloon signalling apparatus
US4120259A (en) * 1977-02-23 1978-10-17 The Raymond Lee Organization, Inc. Visual and radar emergency detection balloon
FR2469934A1 (en) * 1979-11-19 1981-05-29 Menguy Daniel Ship wreck marking balloon - comprises helium filled bottle connected by hose to balloon reflecting radar waves

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2778332A (en) * 1954-03-15 1957-01-22 Reed Tollefsen Means for locating crashed airplanes
US3279419A (en) * 1965-05-03 1966-10-18 Michael A Demarco Signal balloon device
US3395877A (en) * 1966-09-26 1968-08-06 Schjeldahl Co G T Aerodynamic site marker balloon
US3727229A (en) * 1971-07-29 1973-04-10 R Parthum Balloon signalling apparatus
US4120259A (en) * 1977-02-23 1978-10-17 The Raymond Lee Organization, Inc. Visual and radar emergency detection balloon
FR2469934A1 (en) * 1979-11-19 1981-05-29 Menguy Daniel Ship wreck marking balloon - comprises helium filled bottle connected by hose to balloon reflecting radar waves

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2637809A1 (en) * 1988-10-19 1990-04-20 Gautier Richard Device for locating persons in distress using an automatically inflating captive air balloon
US20150191231A1 (en) * 2012-09-24 2015-07-09 Korea Institute Of Ocean Scienec & Technology Radar reflector operating device for indicating emergency position
US9273937B2 (en) * 2012-09-24 2016-03-01 Korea Institute Of Ocean Science & Technology Radar reflector operating device for indicating emergency position
CN109018246A (en) * 2018-09-11 2018-12-18 广东宏穗晶科技服务有限公司 A kind of water life-saving robot
CN110658519A (en) * 2019-09-18 2020-01-07 武汉大学 Wind turbine generator blade state monitoring method based on external radiation source radar
CN110658519B (en) * 2019-09-18 2021-09-03 武汉大学 Wind turbine generator blade state monitoring method based on external radiation source radar

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