DE1807247A1 - Light guide arrangement for measuring rotational speeds - Google Patents
Light guide arrangement for measuring rotational speedsInfo
- Publication number
- DE1807247A1 DE1807247A1 DE19681807247 DE1807247A DE1807247A1 DE 1807247 A1 DE1807247 A1 DE 1807247A1 DE 19681807247 DE19681807247 DE 19681807247 DE 1807247 A DE1807247 A DE 1807247A DE 1807247 A1 DE1807247 A1 DE 1807247A1
- Authority
- DE
- Germany
- Prior art keywords
- coil
- light guide
- guide arrangement
- rotational speeds
- measuring rotational
- 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
- 239000000835 fiber Substances 0.000 claims description 6
- 230000001427 coherent effect Effects 0.000 claims description 4
- 230000035945 sensitivity Effects 0.000 claims description 3
- 230000000694 effects Effects 0.000 claims description 2
- 239000003365 glass fiber Substances 0.000 description 6
- 238000005259 measurement Methods 0.000 description 6
- 239000011152 fibreglass Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 230000006735 deficit Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000010363 phase shift Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01J—MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
- G01J9/00—Measuring optical phase difference; Determining degree of coherence; Measuring optical wavelength
- G01J9/02—Measuring optical phase difference; Determining degree of coherence; Measuring optical wavelength by interferometric methods
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/58—Turn-sensitive devices without moving masses
- G01C19/64—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
- G01C19/72—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams with counter-rotating light beams in a passive ring, e.g. fibre laser gyrometers
- G01C19/721—Details
- G01C19/722—Details of the mechanical construction
Description
IUI (III IlIUI (III Il
m 3o 008 """" m 3 o 008 """" 18072471807247
Kre/SohöKre / Sohö
Bie Erfindung bezieht sich auf eine Lichtleitanordnung zur Messung von Drehgeschwindigkeiten unter Verwendung des Sagnao-Effektes, wobei die Empfindlichkeit eines Sagnac-Interferometers zur Messung eines mit und eines entgegen der Rotation umlaufenden Lichtstrahles herangezogen wird.The invention relates to a light guide arrangement for measuring Rotational speeds using the Sagnao effect, with the Sensitivity of a Sagnac interferometer is used to measure one with and one against the rotation circulating light beam.
Es sind schon Anordnungen vorgeschlagen worden, bei denen die Empfindlichkeit eines Sagnac-Interferometers erhöht wird durch Messung der In- ' terferenz eines mehrfach umlaufenden Lichtstrahls mittels einer Luoite-Röhre, wobei der Lichtstrahl jeweils in einer transparenten Glasspulβ oder gemäß einer weiteren Anordnung mittels einer kohärenten Lichtquelle in einer Spule aus Glasfasern mit und in einer Spule entgegen der Rotation des Messkörpers zum Mehrfachumlauf gebracht wird. Die Vorteile dieser Anordnungen sind unbestreitbar. Für die Erfordernisse genaue ster Messungen jedoch zeigte es sich, daß vor allem thermische Unterschiede in den einzelnen Spulen Messfehler hervorrufen. ™Arrangements have already been proposed in which the sensitivity of a Sagnac interferometer is increased by measuring the in- ' interference of a multiple circulating light beam by means of a Luoite tube, the light beam in each case in a transparent glass pulse or according to a further arrangement by means of a coherent light source in a coil made of glass fibers with and in a coil the rotation of the measuring body is brought to multiple revolutions. The advantages of these arrangements are undeniable. For the requirements of the most precise measurements, however, it was found that primarily thermal differences in the individual coils cause measurement errors. ™
Ber Erfindung liegt die Aufgabe zugrunde eine Anordnung zu schaffen, bei der auftretende Fehler durch thermische, akustische oder chemische Unterschiede an den einzelnen Glasfasern eliminiert werden und dadurch Messfehler vermieden werden können*The object of the invention is to create an arrangement the errors that occur due to thermal, acoustic or chemical differences in the individual glass fibers can be eliminated and thereby Measurement errors can be avoided *
Bie Erfindung löst die Aufgabe, indem am Ausgang einer kohärenten Lichtquelle «in· ein«ig· Glasfaserspul· angeordnet ist und zwisohen Lichtquelle und Spul· ein Strahlteiler so gelegt ist, daß in J*d·· Ende derThe invention solves the problem by arranging a coherent light source in a single fiberglass spool and placing a beam splitter between the light source and the spool in such a way that the end of the
009822/1127 ' 2 "009822/1127 ' 2 "
ENTVICKLUNGSRING SÜD GMBH - 2 - 5.11.1968ENTVICKLUNGSRING SÜD GMBH - 2 - November 5, 1968
MÜNCHENMUNICH
EM 30 008
Kre/SchöEM 30 008
Kre / Schö
Spule ein Strahl' einfällt.Coil a beam 'is incident.
Durch diese Maßnahmen werden Unterschiedlichkeiten, vor allem in der Erwärmung der einzelnen Glasfasern wie sie bisher durch die Anordnung von zwei Spulen aufgetreten sind, eliminiert, denn der mit der Rotation laufende Strahl und derjenige entgegen der Rotation treffen innerhalb einer einzigen Spule immer auf die gleichen unterschiedlichen Verhältnisse, das heißt, sie haben beide dieselben Bedingungen und sind beide mit denselben Veränderungen behaftet (Phasenverschiebung), wenn sie wieder aus den Enden der Spule austreten. Hierdurch wird die Meßgenauigkeit der Anordnung ganz wesentlich erhöht.Through these measures, differences, especially in the Heating of the individual glass fibers as they were previously due to the arrangement of two coils have occurred, because the beam moving with the rotation and the one against the rotation meet within a single coil always has the same different ratios, that is, they both have the same conditions and are both afflicted with the same changes (phase shift) when they emerge again from the ends of the coil. This increases the measurement accuracy the arrangement increased significantly.
In weiterer Ausbildung der Anordnung wird vorgeschlagen, daß die Stirnfläche der Enden der Glasfaserspule unter einem bestimmten Winkel zur Faserachse angeschliffen sind. Diese Maßnahme verhindert, daß das von der Glasfaserstirnfläche reflektierte Licht in das Interferometer gelangt und dadurch das Meßergebnis ganz beträchtlich verfälscht. Bei einem geeigneten Anschliffwinkel der Glasfaserenden kann sogar nahezu völlige Reflexionslosigkeit erzielt werden.In a further development of the arrangement it is proposed that the end face the ends of the fiberglass spool are ground at a certain angle to the fiber axis. This measure prevents the The light reflected from the glass fiber end face enters the interferometer and thereby significantly falsifies the measurement result. at With a suitable bevel angle of the glass fiber ends, it is even possible to achieve almost complete absence of reflection.
Die Erfindung ist nachfolgend in einem Ausführungsbeispiel beschrieben und gezeichnet. Es zeigernThe invention is described below in an exemplary embodiment and drawn. Show it
Figur 1 eine Schemaskizze der erflndungsgeraäßen Anordnung Figur 2 die Einzelheit A gemäß Fig. 1 in vergrößertem Maßetab.FIG. 1 is a schematic diagram of the arrangement according to the invention FIG. 2 shows the detail A according to FIG. 1 on an enlarged scale.
009822/1127 "3"009822/1127 " 3 "
BAD ORIGINALBATH ORIGINAL
ENTWICKLÜNGSRING SÜD GMBH - 3 - 5.11.1968ENTWICKLÜNGSRING SÜD GMBH - 3 - November 5, 1968
MÜNCHENMUNICH
EM 50 008
Kre/SchöEM 50 008
Kre / Schö
Auf einer Plattform 10, die sich mit der Winkelgeschwindigkeit^? in Pfeilriohtung dreht, ist eine kohärente Lichtquelle 20 - beispielsweise eine Laseranordnung - gelagert. Vor dieser befindet sich ein Strahlteiler 21 an den die beiden Enden 31» 32 einer Glasfaserspule 30 in jeweilB entsprechendem Winkel herangeführt sind, so daß der eine Teil des Lichtstrahles 22 durch den Strahlteiler 21 direkt in das S lenende 31 einfällt und der andere Teil des Lichtstrahles 22 abgelenkt % wird und in das andere Spulenende 32 zum gegenläufigen Mehrfaohumlavf einfällt. TJm nun die Reflexe, die beim Auftreffen des Lichtstrahles 22 auf die Stirnflächen der Glasfaserenden 31* 32 entstehen, vom Interferometer abzulenken, sind die Enden 31» 32 unter einem bestimmten Winkel zur Faserachse angeschliffen. Es ist bei entsprechender Präzision möglich, den Anschliffwinkel so zu wählen, daß die Stirnflächen praktisch reflexionslos sind. Im allgemeinen sind die Reflexe wesentlich lichtstärker als das durch die ganze Spula umlaufende Licht. Letzteres jedoch kann ohne Beeinträchtigung - im Hinblick auf Inten- « sität, Geschwindigkeit etc. - in derselben Ebene bzw. Linie gegeneinander verlaufen, so daß für den gegen und den mit der Rotation gehenden Umlauf eines Richtstrahles eine einzige Lichtleitspule auereicht. Dadurch aber ist es möglich, nahezu alle Fehlerquellen auszuschalten, da jeder der gegeneinanderlaufenden Strahlen die gleichen Veränderungen erfährt, welche beispielsweise auf thermische, chemische, akustische oder auch mechanische Einflüsse zurückzuführen sind. Die Messgenauigkeit der Anlage wird durch die erfindungsgemäße Maßnahme ganz wesentlich gesteigert und die bieher noch vorhandenen Fehlerquellen nahezu vollständig beseitigt.On a platform 10, which moves with the angular velocity ^? rotates in arrow direction, a coherent light source 20 - for example a laser arrangement - is mounted. In front of this is a beam splitter 21 to which the two ends 31 »32 of a fiber optic coil 30 are brought in at a corresponding angle, so that one part of the light beam 22 falls through the beam splitter 21 directly into the end 31 and the other part of the light beam 22 % is deflected and falls into the other end of the coil 32 to the counter-rotating Mehrfaohumlavf. In order to deflect from the interferometer the reflections that arise when the light beam 22 hits the end faces of the glass fiber ends 31 * 32, the ends 31 »32 are ground at a certain angle to the fiber axis. With the appropriate precision, it is possible to choose the bevel angle so that the end faces are practically non-reflective. In general, the reflections are much more intense than the light circulating through the entire coil. The latter, however, can run against one another in the same plane or line without impairment - with regard to intensity, speed, etc. - so that a single fiber optic coil is sufficient for the counter and the rotation of a directional beam. In this way, however, it is possible to eliminate almost all sources of error, since each of the beams running in opposite directions experiences the same changes, which can be attributed, for example, to thermal, chemical, acoustic or also mechanical influences. The measure according to the invention increases the measurement accuracy of the system quite considerably and the sources of error that were still present before are almost completely eliminated.
009822/1127 UDOHQlNM. 009822/1127 UDOHQlNM.
Claims (2)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19681807247 DE1807247B2 (en) | 1968-11-06 | 1968-11-06 | ARRANGEMENT FOR MEASURING ROTATION SPEEDS |
GB1258172D GB1258172A (en) | 1968-11-06 | 1969-10-24 | |
FR6938179A FR2022712A1 (en) | 1968-11-06 | 1969-11-06 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19681807247 DE1807247B2 (en) | 1968-11-06 | 1968-11-06 | ARRANGEMENT FOR MEASURING ROTATION SPEEDS |
Publications (2)
Publication Number | Publication Date |
---|---|
DE1807247A1 true DE1807247A1 (en) | 1970-05-27 |
DE1807247B2 DE1807247B2 (en) | 1971-09-16 |
Family
ID=5712499
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19681807247 Pending DE1807247B2 (en) | 1968-11-06 | 1968-11-06 | ARRANGEMENT FOR MEASURING ROTATION SPEEDS |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1807247B2 (en) |
FR (1) | FR2022712A1 (en) |
GB (1) | GB1258172A (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2122920A1 (en) * | 1970-06-01 | 1971-12-16 | Gievers J | Rotation sensitive polarization converter |
US4013365A (en) * | 1974-08-29 | 1977-03-22 | The University Of Utah | Laser gyroscope |
US4120588A (en) * | 1976-07-12 | 1978-10-17 | Erik Chaum | Multiple path configuration for a laser interferometer |
US4120587A (en) * | 1975-11-24 | 1978-10-17 | University Of Utah Research Institute | Double optical fiber waveguide ring laser gyroscope |
US4138196A (en) * | 1977-07-06 | 1979-02-06 | The United States Of America As Represented By The Secretary Of The Army | Fiber interferometer rotary motion sensor |
FR2446481A1 (en) * | 1979-01-15 | 1980-08-08 | Max Planck Gesellschaft | METHOD AND DEVICE FOR MEASURING ROTATION RATES BY THE SAGNAC EFFECT |
US4299490A (en) * | 1978-12-07 | 1981-11-10 | Mcdonnell Douglas Corporation | Phase nulling optical gyro |
US4461574A (en) * | 1979-12-18 | 1984-07-24 | The United States Of America As Represented By The Secretary Of The Air Force | Environmentally independent fiber optic rotation sensor |
US4735506A (en) * | 1985-04-01 | 1988-04-05 | Litton Systems, Inc. | Phase nulling optical gyroscope |
US4842358A (en) * | 1987-02-20 | 1989-06-27 | Litton Systems, Inc. | Apparatus and method for optical signal source stabilization |
US4915503A (en) * | 1987-09-01 | 1990-04-10 | Litton Systems, Inc. | Fiber optic gyroscope with improved bias stability and repeatability and method |
US4997282A (en) * | 1986-09-19 | 1991-03-05 | Litton Systems, Inc. | Dual fiber optic gyroscope |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4208128A (en) * | 1978-08-23 | 1980-06-17 | Rockwell International Corporation | Interferometer gyro using heterodyne phase detection without severe light source coherence requirements |
CA1136744A (en) * | 1978-08-23 | 1982-11-30 | Rockwell International Corporation | Interferometer gyro using heterodyne phase detection |
DE2906870A1 (en) * | 1979-02-22 | 1980-09-04 | Max Planck Gesellschaft | Rotation and revolution rate measurement - using sagnac effect and circularly polarised light faraday phase shift control |
FR2461956A1 (en) * | 1979-07-24 | 1981-02-06 | Thomson Csf | INTERFEROMETRIC DEVICE FOR MEASURING ELECTRICAL CURRENT WITH OPTICAL FIBER |
DE3332718C2 (en) * | 1983-09-10 | 1994-12-22 | Sel Alcatel Ag | Device for measuring the speed of rotation |
-
1968
- 1968-11-06 DE DE19681807247 patent/DE1807247B2/en active Pending
-
1969
- 1969-10-24 GB GB1258172D patent/GB1258172A/en not_active Expired
- 1969-11-06 FR FR6938179A patent/FR2022712A1/fr not_active Withdrawn
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2122920A1 (en) * | 1970-06-01 | 1971-12-16 | Gievers J | Rotation sensitive polarization converter |
US4013365A (en) * | 1974-08-29 | 1977-03-22 | The University Of Utah | Laser gyroscope |
US4120587A (en) * | 1975-11-24 | 1978-10-17 | University Of Utah Research Institute | Double optical fiber waveguide ring laser gyroscope |
US4120588A (en) * | 1976-07-12 | 1978-10-17 | Erik Chaum | Multiple path configuration for a laser interferometer |
US4138196A (en) * | 1977-07-06 | 1979-02-06 | The United States Of America As Represented By The Secretary Of The Army | Fiber interferometer rotary motion sensor |
US4299490A (en) * | 1978-12-07 | 1981-11-10 | Mcdonnell Douglas Corporation | Phase nulling optical gyro |
FR2446481A1 (en) * | 1979-01-15 | 1980-08-08 | Max Planck Gesellschaft | METHOD AND DEVICE FOR MEASURING ROTATION RATES BY THE SAGNAC EFFECT |
US4461574A (en) * | 1979-12-18 | 1984-07-24 | The United States Of America As Represented By The Secretary Of The Air Force | Environmentally independent fiber optic rotation sensor |
US4735506A (en) * | 1985-04-01 | 1988-04-05 | Litton Systems, Inc. | Phase nulling optical gyroscope |
US4997282A (en) * | 1986-09-19 | 1991-03-05 | Litton Systems, Inc. | Dual fiber optic gyroscope |
US4842358A (en) * | 1987-02-20 | 1989-06-27 | Litton Systems, Inc. | Apparatus and method for optical signal source stabilization |
US4915503A (en) * | 1987-09-01 | 1990-04-10 | Litton Systems, Inc. | Fiber optic gyroscope with improved bias stability and repeatability and method |
Also Published As
Publication number | Publication date |
---|---|
GB1258172A (en) | 1971-12-22 |
FR2022712A1 (en) | 1970-08-07 |
DE1807247B2 (en) | 1971-09-16 |
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