EP0472815A2 - Guidance wire - Google Patents

Guidance wire Download PDF

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Publication number
EP0472815A2
EP0472815A2 EP19910107294 EP91107294A EP0472815A2 EP 0472815 A2 EP0472815 A2 EP 0472815A2 EP 19910107294 EP19910107294 EP 19910107294 EP 91107294 A EP91107294 A EP 91107294A EP 0472815 A2 EP0472815 A2 EP 0472815A2
Authority
EP
European Patent Office
Prior art keywords
steering cable
fluorescent
cable
guidance wire
fiber
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.)
Granted
Application number
EP19910107294
Other languages
German (de)
French (fr)
Other versions
EP0472815B1 (en
EP0472815A3 (en
Inventor
Bernd Schunk
Reinfried Stollewerk
Gerhard Dr. Hubricht
Jörg Dr. Peters
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Industrie AG
Original Assignee
Rheinmetall Industrie AG
Rheinmetall GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Rheinmetall Industrie AG, Rheinmetall GmbH filed Critical Rheinmetall Industrie AG
Publication of EP0472815A2 publication Critical patent/EP0472815A2/en
Publication of EP0472815A3 publication Critical patent/EP0472815A3/en
Application granted granted Critical
Publication of EP0472815B1 publication Critical patent/EP0472815B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/30Command link guidance systems
    • F41G7/32Command link guidance systems for wire-guided missiles

Definitions

  • the invention relates to a steering cable for guided missiles.
  • the invention is therefore based on the object of developing a steering cable for remotely steerable missiles which can be found and disposed of in a simple manner after the missile has been fired.
  • the invention is therefore based on the idea of applying a surface layer to the steering cable which, when irradiated, for. B. fluorescent with UV light.
  • the resulting increase in contrast to the surroundings makes the steering cable easily visible. This enables manual or automatic disposal.
  • Fig. 1, 1 is a missile, e.g. B. a rocket is shown, which was started by a starter 2 and which is connected to a command transmitter 3 via a steering cable, preferably an optical fiber.
  • a steering cable preferably an optical fiber.
  • the structure of a light guide according to the invention is shown in FIG. 20 ⁇ m) and a hard coating of z. B. 250 microns, also made of acrylate.
  • the hard coating was doped with a fluorescent dye.
  • the corresponding dye particles are designated 440.
  • BBQ benzimidazo-benzisochonolin-7-one
  • the fluorescent dye is especially the case with benzene derivatives.
  • BBQ benzimidazo-benzisochonolin-7-one
  • the corresponding emission band is approximately between 530 and 680 nm. It is precisely in this area that natural vegetation has a minimum reflection (cf. curve 7 in FIG. 5), so that there is a relatively high contrast between the luminescent glass fiber and the surroundings.
  • Curve 6 in Fig. 4 shows the absorption spectrum of BBQ. It can be seen that for the production of luminescence, irradiation of UV light (280 to 400 nm) leads to luminescence.
  • the collector can wear glasses with filters that let light through in the range of 500 to 550 nm.
  • FIG. 3 shows a further exemplary embodiment of a light guide 40 'according to the invention, in which a lacquer layer with a fluorescent dye 46 is additionally carried out on the hard surface layer 45 known per se.
  • the layer thickness of layer 46 can be, for example, 2 ⁇ m.

Abstract

It is the object of the invention to develop a guidance wire (4, 40, 40') for guided missiles (1), which can be easily located and disposed of after the missile (1) has been shot. <??>This object is achieved when the surface layer (44, 46) of the guidance wire (4) contains a material which fluoresces upon illumination by light of a prescribed waveband. It is preferable to use a dye whose emission spectrum is approximately between 530 and 690 nm. <IMAGE>

Description

Die Erfindung betrifft ein Lenkkabel für ferngelenkte Flugkörper.The invention relates to a steering cable for guided missiles.

Zur Fernlenkung von Flugkörpern dienen sowohl elektrische Kabel als auch Lichtwellenleiter. In neuerer Zeit ist man allerdings vor allem bestrebt, aufgrund der großen Bandbreite zur Signalübertragung Lichtwellenleiter zu verwenden.Both electrical cables and optical fibers are used for the remote control of missiles. In recent times, however, efforts have been made above all to use optical fibers because of the large bandwidth for signal transmission.

Besonders nachteilig ist bei der Verwendung von Lenkkabeln, daß das Kabel nach dem Verschießen des Flugkörpers im Gelände verbleibt. Aus Gründen der Umweltverträglichkeit (Gefahr für Tiere durch Wildfraß oder Verfangen in dem Draht bzw. der Glasfaser) wird es in Zukunft erforderlich sein, das Lenkkabel zu entfernen. Bisher ist dies mit vertretbarem Aufwand nicht möglich, da z. B. die Glasfasser praktisch nicht zu erkennen ist. Ein Wiederaufwickeln ist aufgrund der geringen Zugfestigkeit der Faser ebenfalls nicht oder nur stückweise möglich.It is particularly disadvantageous when using steering cables that the cable remains in the field after the missile has been fired. In the future, it will be necessary to remove the steering cable for reasons of environmental compatibility (danger to animals due to game feeding or entanglement in the wire or glass fiber). So far, this has not been possible with reasonable effort, since e.g. B. the glass barrel is practically invisible. Due to the low tensile strength of the fiber, rewinding is also not possible or only possible in parts.

Der Erfindung liegt daher die Aufgabe zugrunde, ein Lenkkabel für fernlenkbare Flugkörper zu entwickeln, welches nach dem Verschießen des Flugkörpers auf einfache Weise aufgefunden und entsorgt werden kann.The invention is therefore based on the object of developing a steering cable for remotely steerable missiles which can be found and disposed of in a simple manner after the missile has been fired.

Erfindungsgemäß wird diese Aufgabe durch die Merkmale des kennzeichnenden Teiles des Anspruchs 1 gelöst.According to the invention, this object is achieved by the features of the characterizing part of claim 1.

Besonders vorteilhafte Ausgestaltungen der Erfindung ergeben sich aus den Unteransprüchen.Particularly advantageous embodiments of the invention result from the subclaims.

Der Erfindung liegt also der Gedanke zugrunde, auf das Lenkkabel eine Oberflächenschicht aufzubringen, die bei Bestrahlung, z. B. mit UV-Licht, fluoresziert. Das Lenkkabel wird durch die daraus resultierende Konstrasterhöhung gegenüber der Umgebung leicht sichtbar. Dadurch wird eine manuelle oder automatische Entsorgung ermöglicht.The invention is therefore based on the idea of applying a surface layer to the steering cable which, when irradiated, for. B. fluorescent with UV light. The resulting increase in contrast to the surroundings makes the steering cable easily visible. This enables manual or automatic disposal.

Weitere Vorteile und Einzelheiten der Erfindung werden im folgenden anhand von Ausführungsbeispielen und mit Hilfe von Figuren näher erläutert.Further advantages and details of the invention are explained in more detail below on the basis of exemplary embodiments and with the aid of figures.

Es zeigen:

Fig. 1
schematisch einen Flugkörper, der über ein Lenkkabel mit einem Kommandogeber verbunden ist;
Fig. 2 und Fig. 3
zwei Ausführungsbeispiele eines erfindungsgemäßen Lenkkabels;
Fig. 4 und Fig. 5
zwei Diagramme zur Erläuterung der Erfindung.
Show it:
Fig. 1
schematically a missile, which is connected via a steering cable to a command transmitter;
2 and 3
two embodiments of a steering cable according to the invention;
4 and 5
two diagrams for explaining the invention.

In Fig. 1 ist mit 1 ein Flugkörper, z. B. eine Rakete, dargestellt, die von einer Startvorrichtung 2 gestartet wurde und die mit einem Kommandogeber 3 über ein Lenkkabel, vorzugsweise einem Lichtwellenleiter, verbunden ist.In Fig. 1, 1 is a missile, e.g. B. a rocket is shown, which was started by a starter 2 and which is connected to a command transmitter 3 via a steering cable, preferably an optical fiber.

Den Aufbau eines erfindungsgemäßen Lichtleiters zeigt Fig. 2. Wie bekannte Lichtwellenleiter besteht er aus einem Kern 41, der beispielsweise 9 µm dick ist, einem den Kern 1 umgebenden Glasmantel 42 von beispielsweise 125 µm Dicke sowie einer weichen Umhüllung aus Acrylat (z. B. 20 µm) und einer harten Umhüllung von z. B. 250 µm, ebenfalls aus Acrylat. Erfindungsgemäß wurde die harte Umhüllung mit einem Fluoreszensfarbstoff dotiert. Die entsprechenden Farbstoffpartikel sind mit 440 bezeichnet.The structure of a light guide according to the invention is shown in FIG. 20 µm) and a hard coating of z. B. 250 microns, also made of acrylate. According to the invention, the hard coating was doped with a fluorescent dye. The corresponding dye particles are designated 440.

Als fluoreszierender Farbstoff können beispielsweise organische Stoffe verwendet werden, die fluoreszierende Erscheinungen aufweisen. Dieses ist vor allem bei Benzolderivaten der Fall. Besonders geeignet für den vorliegenden Fall ist BBQ (Benzimidazo-benzisochonolin-7-on), weil die entsprechende Emissionsbande etwa zwischen 530 und 680 nm liegt. Gerade in diesem Bereich besitzt aber die natürliche Vegetation ein Reflexionsminimum (vgl. Kurve 7 in Fig. 5), so daß sich ein relativ hoher Kontrast zwischen der lumineszierenden Glasfaser und der Umgebung ergibt.For example, organic substances which have fluorescent phenomena can be used as the fluorescent dye. This is especially the case with benzene derivatives. BBQ (benzimidazo-benzisochonolin-7-one) is particularly suitable for the present case because the corresponding emission band is approximately between 530 and 680 nm. It is precisely in this area that natural vegetation has a minimum reflection (cf. curve 7 in FIG. 5), so that there is a relatively high contrast between the luminescent glass fiber and the surroundings.

Kurve 6 in Fig. 4 zeigt das Absorptionsspektrum von BBQ. Ihr läßt sich entnehmen, daß zur Erzeugung von Lumineszens eine Bestrahlung von UV-Licht (280 bis 400 nm) zu einer Lumineszens führt.Curve 6 in Fig. 4 shows the absorption spectrum of BBQ. It can be seen that for the production of luminescence, irradiation of UV light (280 to 400 nm) leads to luminescence.

Zur manuellen Entsorgung wird das Gelände im Bereich, wo der Lichtwellenleiter vermutet wird, mit UV-Lampen beleuchtet bzw. abgescant. Die aufleuchtenden Bruchstücke der Faser werden anschließend von Hand aufgesammelt. Zur höheren Effektivität kann der Sammler eine Brille mit Filtern tragen, die Licht im Bereich von 500 bis 550 nm durchlassen.For manual disposal, the area in the area where the optical fiber is suspected is illuminated or scanned with UV lamps. The illuminated fragments of the fiber are then picked up by hand. For greater effectiveness, the collector can wear glasses with filters that let light through in the range of 500 to 550 nm.

Denkbar ist auch eine automatische Entsorgung mit Kleinfahrzeugen, die mit einer Filterkamera (530 bis 560 nm) ausgerüstet sind und ein Bildverarbeitungssystem, UV-Scheinwerfer und einen Saugrüssel zum Aufsaugen der Glasfaser aufweisen. Mit Hilfe der Wellenlängen begrenzten Fluoreszensstrahlung der Faser kann ein spezieller Bildverarbeitungsalgorithmus die Position der Faser im Gelände bestimmen. Die Bildverarbeitung berechnet die Position der Glasfaser und steuert den Saugrüssel. Die Bildverarbeitung wird unterstützt durch die Kamera, deren Filter bevorzugt den Wellenlängenbereich der Fluoreszenzstrahlung durchläßt.Automatic disposal is also conceivable with small vehicles that are equipped with a filter camera (530 to 560 nm) and have an image processing system, UV headlights and a suction nozzle for sucking up the glass fiber. With the help of the wavelength-limited fluorescence radiation of the fiber, a special image processing algorithm can determine the position of the fiber in the field. Image processing calculates the position of the fiber and controls the proboscis. The image processing is supported by the camera, the filter of which preferably passes the wavelength range of the fluorescent radiation.

In Fig. 3 ist ein weiteres Ausführungsbeispiel eines erfindungsgemäßen Lichtleiters 40' wiedergegeben, bei dem zusätzlich auf der an sich bekannten harten Oberflächenschicht 45 eine Lackschicht mit einem fluoreszierenden Farbstoff 46 erfolgt. Die Schichtdicke der Schicht 46 kann beispielsweise 2 µm betragen.FIG. 3 shows a further exemplary embodiment of a light guide 40 'according to the invention, in which a lacquer layer with a fluorescent dye 46 is additionally carried out on the hard surface layer 45 known per se. The layer thickness of layer 46 can be, for example, 2 μm.

BezugszeichenlisteReference symbol list

11
Flugkörper / LenkraketeMissile / guided missile
22nd
StartvorrichtungStarting device
33rd
KommandogeberCommander
44th
Lenkkabel, LichtwellenleiterSteering cable, fiber optic cable
55
fluoresz. Spektrumfluorescent. spectrum
66
Absorptionsspektrum von BBQAbsorption spectrum of BBQ
77
Reflexionsspektrum der natürlichen VegetationReflection spectrum of natural vegetation
40, 40'40, 40 '
Lichtwellenleiteroptical fiber
4141
Kerncore
4242
GlasmantelGlass jacket
4343
AcrylatschichtAcrylic layer
4444
Oberflächenschicht mit fluoresz. FarbstoffSurface layer with fluorescent. dye
4545
harte Schichthard layer
4646
Oberflächenschicht aus fluoresz. FarbstoffFluorescent surface layer. dye
440440
fluoresz. Farbstoff-Partikelfluorescent. Dye particles

Claims (4)

Lenkkabel (4, 40, 40') für fernlenkbare Flugkörper (1), dadurch gekennzeichnet, daß die Oberflächenschicht (44, 46) des Lenkkabels (4) ein Material enthält, welches bei Beleuchtung mit Licht eines vorgegebenen Wellenlängenbereiches fluoresziert.Guiding cable (4, 40, 40 ') for remotely steerable missiles (1), characterized in that the surface layer (44, 46) of the guiding cable (4) contains a material which fluoresces when illuminated with light of a predetermined wavelength range. Lenkkabel, dadurch gekennzeichnet, daß als fluoreszierendes Material (440, 46) ein fluoreszierender Farbstoff verwendet wird, dessen Emissionsspektrum etwa zwischen 530 und 690 nm liegt.Steering cable, characterized in that a fluorescent dye is used as the fluorescent material (440, 46), the emission spectrum of which is approximately between 530 and 690 nm. Lenkkabel nach Anspruch 2, dadurch gekennzeichnet, daß als fluoreszierendes Material (440, 46) BBQ verwendet wird.Steering cable according to claim 2, characterized in that BBQ is used as the fluorescent material (440, 46). Lenkkabel nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, daß es sich bei dem Lenkkabel (4, 40, 40') um einen Lichtwellenleiter handelt.Steering cable according to one of claims 1 to 3, characterized in that the steering cable (4, 40, 40 ') is an optical waveguide.
EP91107294A 1990-08-29 1991-05-06 Guidance wire Expired - Lifetime EP0472815B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4027295 1990-08-29
DE4027295A DE4027295A1 (en) 1990-08-29 1990-08-29 STEERING CABLE

Publications (3)

Publication Number Publication Date
EP0472815A2 true EP0472815A2 (en) 1992-03-04
EP0472815A3 EP0472815A3 (en) 1992-06-10
EP0472815B1 EP0472815B1 (en) 1995-02-22

Family

ID=6413143

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EP91107294A Expired - Lifetime EP0472815B1 (en) 1990-08-29 1991-05-06 Guidance wire

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US (1) US5111524A (en)
EP (1) EP0472815B1 (en)
JP (1) JPH04234716A (en)
DE (2) DE4027295A1 (en)
IL (1) IL99116A0 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5696863A (en) * 1982-08-06 1997-12-09 Kleinerman; Marcos Y. Distributed fiber optic temperature sensors and systems
US5317667A (en) * 1992-11-23 1994-05-31 Ford Motor Company Electrophoretic switch for a light pipe
JPH1010378A (en) * 1996-06-25 1998-01-16 Toshiba Corp Coated optical fiber, optical fiber coil and production of coated optical fiber
US6602601B2 (en) 2000-12-22 2003-08-05 Corning Incorporated Optical fiber coating compositions

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4770370A (en) * 1987-03-31 1988-09-13 The Boeing Company Optical fiber guided tube-launched projectile system
GB2209617A (en) * 1987-09-09 1989-05-17 Abu Nijaila Valerie Ann Emergency signal device

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4626068A (en) * 1982-07-29 1986-12-02 The United States Of America As Represented By The Secretary Of The Air Force Photoactive coating for hardening optical fibers
US4884860A (en) * 1986-02-05 1989-12-05 Brown David C Linear lens and method for concentrating radiant energy and multiplying phosphor luminance output intensity
US4934712A (en) * 1986-03-26 1990-06-19 Byrd Thomas R Weighted objects with tether and means for twisting tether to raise and lower objects
US4950049A (en) * 1989-02-28 1990-08-21 At&T Bell Laboratories Stable package of elongated optical fiber strand material
US5005930A (en) * 1990-02-23 1991-04-09 Hughes Aircraft Company Multi-directional payout fiber optic canister

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4770370A (en) * 1987-03-31 1988-09-13 The Boeing Company Optical fiber guided tube-launched projectile system
GB2209617A (en) * 1987-09-09 1989-05-17 Abu Nijaila Valerie Ann Emergency signal device

Also Published As

Publication number Publication date
IL99116A0 (en) 1992-07-15
JPH04234716A (en) 1992-08-24
EP0472815B1 (en) 1995-02-22
EP0472815A3 (en) 1992-06-10
DE4027295A1 (en) 1992-03-05
DE59104669D1 (en) 1995-03-30
US5111524A (en) 1992-05-05

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