DE20111539U1 - Fiber optic sensor for the detection of displacements - Google Patents

Fiber optic sensor for the detection of displacements

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Publication number
DE20111539U1
DE20111539U1 DE20111539U DE20111539U DE20111539U1 DE 20111539 U1 DE20111539 U1 DE 20111539U1 DE 20111539 U DE20111539 U DE 20111539U DE 20111539 U DE20111539 U DE 20111539U DE 20111539 U1 DE20111539 U1 DE 20111539U1
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fiber optic
optic sensor
fiber
fiber bundle
detecting displacements
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DE20111539U
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German (de)
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00Measuring arrangements characterised by the use of optical techniques
    • G01B11/16Measuring arrangements characterised by the use of optical techniques for measuring the deformation in a solid, e.g. optical strain gauge

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Length Measuring Devices By Optical Means (AREA)

Description

Faseroptischer Sensor zur Erfassung von VerschiebungenFiber optic sensor for detecting displacements

Mit bekannten technischen Lösungen werden Bauelementdeformationen beispielsweise an Rotorblättern von Windkraftanlagen mit Dehnmeßstreifen, wenn elektrische Einrichtungen nicht zulässig sind, mit faseroptischen Bragg-Gittern erfasst und ausgewertet. Eine andere Variante wertet die infolge Verformung entstehenden Intensitätsänderungen eines fokusierten Lichtstrahles auf den einzelnen Orten einer matrixförmigen optischen Empfängerfläche aus.With known technical solutions, component deformations, for example on rotor blades of wind turbines with strain gauges, are recorded and evaluated with fiber-optic Bragg gratings when electrical devices are not permitted. Another variant evaluates the intensity changes of a focused light beam resulting from deformation at the individual locations of a matrix-shaped optical receiver surface.

Die dargestellte Erfindung stellt eine Lösung dar, die wiederum die Forderungen nach ausschließlich optischer Meßtechnik im Flügelblattbereich erfüllt, dabei aber durch Ausnutzung geometrischer Verschiebungen zweier Lichtwellenleiter-Faserbündel zueinander auswertbare Intensitätsunterschiede in den einzelnen Fasern erzeugt.The invention presented represents a solution which again meets the requirements for exclusively optical measuring technology in the blade area, but generates evaluable intensity differences in the individual fibers by utilizing geometric displacements of two optical fiber bundles relative to each other.

Figur 1 verdeutlicht beispielhaft das Wirkprinzip des Sensors.Figure 1 provides an example of how the sensor works.

Licht einer Lichtquelle (1) wird als Strahlengang (2) nahezu gleichmäßiger Intensität über ein kabeiförmiges Bündel von Lichtwellenleiterfasern (3) zum Ort der zu erfassenden Verschiebung geführt und tritt dort an einem geschliffenen Endes (4) des Bündels über die einzelnen Faserquerschnitte aus. Ein definierter Spalt (5), der den Strahlengang optisch nicht wesentlich verändert aber eine Verschiebung des Endes (4) gegenüber dem Ende (6) über geeignete Führungen (8) und eine Drehachse (9) ermöglicht, koppelt das Ende (4) mit dem Ende (6), welches das Licht mit einer während der Spaltpassage möglicherweise veränderten Intensitätsverteilung im Strahlengang (2) wiederum über ein Faserbündel (3) einer Auswerteeinheit (7) zuführt.Light from a light source (1) is guided as a beam path (2) of almost uniform intensity via a cable-shaped bundle of optical fibers (3) to the location of the displacement to be detected and exits there at a ground end (4) of the bundle via the individual fiber cross-sections. A defined gap (5), which does not optically change the beam path significantly but enables a displacement of the end (4) relative to the end (6) via suitable guides (8) and a rotation axis (9), couples the end (4) to the end (6), which in turn feeds the light with an intensity distribution in the beam path (2) that may have changed during the passage through the gap via a fiber bundle (3) to an evaluation unit (7).

Je nach Stellung der beiden Enden (4) und (6) zueinander liegen die Querschnitte (10;l 1) der einzelnen Fasern entweder deckungsgleich übereinander, wie im oberen Bild dargestellt oder weisen eine Verschiebung zueinander auf, wie unten gezeigt. Die beiden Enden (4) und (6) sind jeweils fest mit unterschiedlichen Stellen des zu detektierenden Bauelementes verbunden, so dass eine Deformation des Bauelementes direkt proportional eine Verschiebung der Enden (4) und (6) zueinander ergibt.Depending on the position of the two ends (4) and (6) relative to each other, the cross-sections (10;l 1) of the individual fibers either lie congruently on top of each other, as shown in the upper image, or are offset relative to each other, as shown below. The two ends (4) and (6) are each firmly connected to different points on the component to be detected, so that a deformation of the component results in a displacement of the ends (4) and (6) relative to each other in direct proportion.

Im Falle von Deckungsgleichheit erfolgt die Lichtübertragung mit nahezu ungeminderter Intensität, im Falle von Verschiebungen wird die Intensität proportional der sich einstellenden kleineren Überlappungsfläche (12) absinken. Der Vergleich der Intensitäten mehrerer verschobener Überlappungsflächen (12) erlaubt nach Auswertung eine Aussage über die Art und Größe der Verschiebung der Enden (4) und (6) gegeneinander.In the case of congruence, the light transmission occurs with almost no reduction in intensity; in the case of displacements, the intensity will decrease in proportion to the resulting smaller overlap area (12). The comparison of the intensities of several displaced overlap areas (12) allows, after evaluation, a statement to be made about the type and size of the displacement of the ends (4) and (6) relative to each other.

Durch geeignete Dimensionierung der Führungen (8), der Drehachse (9) und der Befestigung der Enden (4) und (6) am zu detektierenden Bauelement, beispielsweise einem Rotorblatt einer Windkraftanlage, kann das Verhältnis zwischen Intensitätsänderung im Strahlengang und Verschiebungsgröße optimiert werden.By appropriate dimensioning of the guides (8), the axis of rotation (9) and the fastening of the ends (4) and (6) to the component to be detected, for example a rotor blade of a wind turbine, the relationship between the change in intensity in the beam path and the displacement size can be optimized.

Claims (6)

1. Faseroptischer Sensor zur Erfassung von Verschiebungen, gekennzeichnet dadurch, dass: ein Lichtwellenleiter-Faserbündel planflächig unterbrochen ist und die beiden Enden des Bündels jeweils mit einer Seite des deformierten und zu detektierenden Bauelementes fest verbunden sind. 1. Fiber optic sensor for detecting displacements, characterized in that: an optical waveguide fiber bundle is interrupted in a plane surface and the two ends of the bundle are each firmly connected to one side of the deformed component to be detected. 2. Faseroptischer Sensor zur Erfassung von Verschiebungen, gekennzeichnet dadurch, dass: die Faserbündelenden so angeordnet sind, dass die Lichtübertragung im nicht deformierten Zustand in allen Fasern nahezu ungedämpfferfolgt, bei Verdrehung oder Verschiebung der Faserbündelenden in der Schnittebene gegeneinander aber auswertbare Intensitätsunterschiede in den einzelnen Lichtwellenleiterfasern auftreten, da sich die Faserquerschnitte nicht mehr optimal gegenüberstehen. 2. Fiber optic sensor for detecting displacements, characterized in that: the fiber bundle ends are arranged in such a way that the light transmission in the non-deformed state is almost undamped in all fibers, but when the fiber bundle ends are twisted or shifted in the cutting plane against each other, evaluable intensity differences occur in the individual optical fibers because the fiber cross-sections are no longer optimally aligned. 3. Faseroptischer Sensor zur Erfassung von Verschiebungen, gekennzeichnet dadurch, dass: der Spalt zwischen den Faserbündelenden durch geeignete Füllung so gestaltet ist, dass weder eine Streuung des Lichtes noch eine zusätzliche Dämpfung auftreten. 3. Fiber optic sensor for detecting displacements, characterized in that: the gap between the fiber bundle ends is designed by suitable filling so that neither scattering of the light nor additional attenuation occurs. 4. Faseroptischer Sensor zur Erfassung von Verschiebungen, gekennzeichnet dadurch, dass: der Spalt zwischen den Faserbündelenden durch geeignete Füllung eine Relativbewegung der beiden Schliffflächen gegeneinander in der Spaltebene zulässt und dabei eine Verschmutzung und Lichtstreuung ausgeschlossen wird. 4. Fiber optic sensor for detecting displacements, characterized in that: the gap between the fiber bundle ends allows a relative movement of the two ground surfaces against each other in the gap plane by means of a suitable filling and contamination and light scattering are excluded. 5. Faseroptischer Sensor zur Erfassung von Verschiebungen, gekennzeichnet dadurch, dass: die Führung oder der Drehpunkt zur Fixierung der beiden Faserbündelenden so ausgearbeitet ist, dass zwischen der Deformation des zu detektierenden Bauelementes und den sich einstellenden Intensitätsunterschieden in den einzelnen Fasern eindeutige Zusammenhänge bestehen und die Intensitätsunterschiede zur Auswertung hinreichend groß sind. 5. Fiber optic sensor for detecting displacements, characterized in that: the guide or the pivot point for fixing the two fiber bundle ends is designed in such a way that there are clear relationships between the deformation of the component to be detected and the resulting intensity differences in the individual fibers and the intensity differences are sufficiently large for evaluation. 6. Faseroptischer Sensor zur Erfassung von Verschiebungen, gekennzeichnet dadurch, dass: die Anschlagpunkte des Sensors am zu detektierenden Bauelement so gestaltet und dimensioniert sind, dass Eigenverformungen des Sensors und Rückstellkräfte auf das Bauelement minimiert und die vorhandenen Deformationen durch geeignete Längenverhältnisse hinreichend vergrößert werden. 6. Fiber optic sensor for detecting displacements, characterized in that: the stop points of the sensor on the component to be detected are designed and dimensioned in such a way that inherent deformations of the sensor and restoring forces on the component are minimized and the existing deformations are sufficiently increased by suitable length ratios.
DE20111539U 2001-07-13 2001-07-13 Fiber optic sensor for the detection of displacements Expired - Lifetime DE20111539U1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE20111539U DE20111539U1 (en) 2001-07-13 2001-07-13 Fiber optic sensor for the detection of displacements

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10238991A1 (en) * 2002-08-20 2004-03-11 Günther GmbH Fiber optic sensor for measuring component deformation, has a monomode light source connected to a transmission optical fiber with the light detected by receiving fibers in a sensor head and measured using photo-diodes
DE102006002708A1 (en) * 2006-01-19 2007-07-26 Siemens Ag Rotor of a wind turbine
DE102006059439A1 (en) * 2006-12-15 2008-06-19 Prüftechnik Dieter Busch AG Method and device for dynamically measuring the axial deformation of a rotating hollow shaft
WO2009007295A1 (en) * 2007-07-06 2009-01-15 Technische Universität Carolo-Wilhelmina Zu Braunschweig Measuring device for determining relative displacements
US7780328B2 (en) 2006-07-14 2010-08-24 Bae Systems Plc Heat distribution in a distributed lighting apparatus

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10238991A1 (en) * 2002-08-20 2004-03-11 Günther GmbH Fiber optic sensor for measuring component deformation, has a monomode light source connected to a transmission optical fiber with the light detected by receiving fibers in a sensor head and measured using photo-diodes
DE10238991B4 (en) * 2002-08-20 2004-08-19 Günther GmbH Fiber optic sensor
DE102006002708A1 (en) * 2006-01-19 2007-07-26 Siemens Ag Rotor of a wind turbine
DE102006002708B4 (en) * 2006-01-19 2007-12-06 Siemens Ag Rotor of a wind turbine
US7780328B2 (en) 2006-07-14 2010-08-24 Bae Systems Plc Heat distribution in a distributed lighting apparatus
DE102006059439A1 (en) * 2006-12-15 2008-06-19 Prüftechnik Dieter Busch AG Method and device for dynamically measuring the axial deformation of a rotating hollow shaft
US7634948B2 (en) 2006-12-15 2009-12-22 Prueftechnik Dieter Busch Ag Process and device for dynamic measurement of the axial deformation of a rotating hollow shaft
DE102006059439B4 (en) * 2006-12-15 2018-01-25 Prüftechnik Dieter Busch AG Method and device for dynamically measuring the axial deformation of a rotating hollow shaft
WO2009007295A1 (en) * 2007-07-06 2009-01-15 Technische Universität Carolo-Wilhelmina Zu Braunschweig Measuring device for determining relative displacements

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