DE20111539U1 - Fiber optic sensor for the detection of displacements - Google Patents
Fiber optic sensor for the detection of displacementsInfo
- 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
- Authority
- DE
- Germany
- Prior art keywords
- fiber optic
- optic sensor
- fiber
- fiber bundle
- detecting displacements
- 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.)
- Expired - Lifetime
Links
- 239000000835 fiber Substances 0.000 title claims description 21
- 238000006073 displacement reaction Methods 0.000 title claims description 15
- 238000001514 detection method Methods 0.000 title 1
- 238000011156 evaluation Methods 0.000 claims description 3
- 230000003287 optical effect Effects 0.000 claims description 3
- 239000013307 optical fiber Substances 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 claims description 2
- 238000011049 filling Methods 0.000 claims 2
- 238000000149 argon plasma sintering Methods 0.000 claims 1
- 238000011109 contamination Methods 0.000 claims 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B11/00—Measuring arrangements characterised by the use of optical techniques
- G01B11/16—Measuring arrangements characterised by the use of optical techniques for measuring the deformation in a solid, e.g. optical strain gauge
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Length Measuring Devices By Optical Means (AREA)
Description
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)
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 |
Applications Claiming Priority (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 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE20111539U1 true DE20111539U1 (en) | 2001-12-13 |
Family
ID=7959204
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE20111539U Expired - Lifetime DE20111539U1 (en) | 2001-07-13 | 2001-07-13 | Fiber optic sensor for the detection of displacements |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE20111539U1 (en) |
Cited By (5)
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 |
-
2001
- 2001-07-13 DE DE20111539U patent/DE20111539U1/en not_active Expired - Lifetime
Cited By (9)
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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Legal Events
Date | Code | Title | Description |
---|---|---|---|
R207 | Utility model specification |
Effective date: 20020124 |
|
R156 | Lapse of ip right after 3 years |
Effective date: 20050201 |