CN103697879A - Fiber-optic gyroscope light path - Google Patents

Fiber-optic gyroscope light path Download PDF

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Publication number
CN103697879A
CN103697879A CN201310715026.XA CN201310715026A CN103697879A CN 103697879 A CN103697879 A CN 103697879A CN 201310715026 A CN201310715026 A CN 201310715026A CN 103697879 A CN103697879 A CN 103697879A
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CN
China
Prior art keywords
fiber
light path
optical fibre
fibre gyro
coupled
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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.)
Pending
Application number
CN201310715026.XA
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Chinese (zh)
Inventor
耿一璠
马西保
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Hebei Hanguang Heavy Industry Ltd
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Hebei Hanguang Heavy Industry Ltd
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Application filed by Hebei Hanguang Heavy Industry Ltd filed Critical Hebei Hanguang Heavy Industry Ltd
Priority to CN201310715026.XA priority Critical patent/CN103697879A/en
Publication of CN103697879A publication Critical patent/CN103697879A/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/58Turn-sensitive devices without moving masses
    • G01C19/64Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
    • G01C19/72Gyrometers 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
    • G01C19/725Gyrometers 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 using nxn optical couplers, e.g. 3x3 couplers
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/58Turn-sensitive devices without moving masses
    • G01C19/64Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
    • G01C19/72Gyrometers 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
    • G01C19/728Assemblies for measuring along different axes, e.g. triads

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  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Optics & Photonics (AREA)
  • Electromagnetism (AREA)
  • Power Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Gyroscopes (AREA)

Abstract

The invention relates to a fiber-optic gyroscope light path. The fiber-optic gyroscope light path is characterized in that a superfluorescence light source is coupled into a 1*3 optical fiber coupler after passing through an isolator, output superfluorescence is divided into three paths, each path of the output superfluorescence is coupled into first, second and third detectors and first, second and third Y waveguides by virtue of first, second and third 2*2 optical fiber couplers, and the two optical fiber emergent end surfaces of the first, second and third Y waveguides are coupled with two tail fibers of first, second and third optical fiber rings. The fiber-optic gyroscope light path provided by the invention has the advantages that the stability is good, the precision is high, and a fiber-optic gyroscope inertial navigation system has a miniaturization property.

Description

A kind of optical fibre gyro light path
Technical field
The light path that the present invention relates to a kind of optical fibre gyro, is applied to three axis optical fibre gyro.
Background technology
Development along with optical fibre gyro inertial navigation system, optical fibre gyro is widely used, but three single axis fiber gyros that three directions are mutually orthogonal in inertial navigation system, have been used, make like this cost of inertial navigation system higher, size is larger, and in each optical fibre gyro, super-fluorescence light source exists inevitable difference and makes the precision of each optical fibre gyro different, and then has limited the overall precision of optical fibre gyro inertial navigation system.
Summary of the invention
In order to overcome the shortcoming of prior art, the invention provides a kind of optical fibre gyro light path, its good stability, precision is high, can make the miniaturization of optical fibre gyro inertial navigation system.
The present invention solves the technical scheme that its technical matters takes: super-fluorescence light source is coupled into 1 * 3 fiber coupler by isolator, the superfluorescence of output is divided into three tunnels, each road is coupled with first, second, third detector and first, second, third Y waveguide respectively through 2 * 2 first, second, third fiber couplers, two optical fiber outgoing end faces of first, second, third Y waveguide and first, second, third fiber optic loop two pigtail couplings.
The invention enables three mutually orthogonal fiber optic loop to share a super-fluorescence light source, and after super-fluorescence light source, add an isolator, to improve stability and the precision of optical fibre gyro, thereby make the miniaturization of optical fibre gyro inertial navigation system.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the present invention is further described.
Fig. 1 is index path of the present invention.
Embodiment
As shown in Figure 1, super-fluorescence light source 1 is coupled into 1 * 3 fiber coupler 2 by isolator 14, the superfluorescence of output is divided into three tunnels, each road is coupled with first, second, third detector 3,12,13 and first, second, third Y waveguide 5,9,10 respectively through 2 * 2 first, second, third fiber couplers 4,11,15, two optical fiber outgoing end faces of first, second, third Y waveguide 5,9,10 and 6,7,8 liang of pigtail couplings of first, second, third fiber optic loop.
The light emitting tail fiber of described isolator 14 should with 1 * 3 fiber coupler 2 coupled fiber pattern match.
First, second, third 2 * 2 described fiber coupler 4,11,15 residue fiber end faces are cut oblique 45 °, in case swash, penetrate.
First, second, third 2 * 2 described fiber coupler 4,11,15 should enter fine pattern match with first, second, third Y waveguide 5,9,10.
First, second, third described Y waveguide 5,9,10 tail optical fibers should with fiber optic loop first, second, third 6,7,8 tail optical fiber pattern match.

Claims (5)

1. an optical fibre gyro light path, it is characterized in that: super-fluorescence light source (1) is coupled into 1 * 3 fiber coupler (2) by isolator (14), the superfluorescence of output is divided into three tunnels, each road is coupled with first, second, third detector (3,12,13) and first, second, third Y waveguide (5,9,10) respectively through 2 * 2 first, second, third fiber couplers (4,11,15), two optical fiber outgoing end faces of first, second, third Y waveguide (5,9,10) and first, second, third fiber optic loop (6,7,8), two pigtail couplings.
2. optical fibre gyro light path according to claim 1, is characterized in that: the light emitting tail fiber of described isolator (14) should with 1 * 3 fiber coupler (2) coupled fiber pattern match.
3. optical fibre gyro light path according to claim 1, is characterized in that: first, second, third 2 * 2 described fiber coupler (4,11,15) residue fiber end face is cut oblique 45 °.
4. optical fibre gyro light path according to claim 1, is characterized in that: first, second, third 2 * 2 described fiber coupler (4,11,15) should enter fine pattern match with first, second, third Y waveguide (5,9,1) 0.
5. optical fibre gyro light path according to claim 1, is characterized in that: first, second, third described Y waveguide (5,9,10) tail optical fiber should with fiber optic loop first, second, third (6,7,8) tail optical fiber pattern match.
CN201310715026.XA 2013-12-20 2013-12-20 Fiber-optic gyroscope light path Pending CN103697879A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310715026.XA CN103697879A (en) 2013-12-20 2013-12-20 Fiber-optic gyroscope light path

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310715026.XA CN103697879A (en) 2013-12-20 2013-12-20 Fiber-optic gyroscope light path

Publications (1)

Publication Number Publication Date
CN103697879A true CN103697879A (en) 2014-04-02

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106596075A (en) * 2016-12-29 2017-04-26 北京航天时代光电科技有限公司 Interferometer assembling quality detection system
CN110579204A (en) * 2019-08-20 2019-12-17 北京航空航天大学 Optical fiber coupler array for triaxial integrated optical fiber gyroscope
CN112781579A (en) * 2021-01-29 2021-05-11 湖北三江航天红峰控制有限公司 Six-axis integrated optical fiber gyroscope light path structure
CN113804178A (en) * 2021-08-20 2021-12-17 北京航天时代光电科技有限公司 High-precision and miniaturized triaxial integrated optical fiber gyroscope based on double erbium source redundancy design

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102207387A (en) * 2011-04-12 2011-10-05 浙江大学 Triaxial integration all-optical fiber inertia sensing device

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102207387A (en) * 2011-04-12 2011-10-05 浙江大学 Triaxial integration all-optical fiber inertia sensing device

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
吴军伟等: "微小型三轴光纤陀螺技术", 《红外与激光工程》 *
翁炬等: "向高精度发展的干涉型光纤陀螺仪技术", 《中国惯性技术学报》 *

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106596075A (en) * 2016-12-29 2017-04-26 北京航天时代光电科技有限公司 Interferometer assembling quality detection system
CN110579204A (en) * 2019-08-20 2019-12-17 北京航空航天大学 Optical fiber coupler array for triaxial integrated optical fiber gyroscope
CN112781579A (en) * 2021-01-29 2021-05-11 湖北三江航天红峰控制有限公司 Six-axis integrated optical fiber gyroscope light path structure
CN112781579B (en) * 2021-01-29 2022-03-08 湖北三江航天红峰控制有限公司 Six-axis integrated optical fiber gyroscope light path structure
CN113804178A (en) * 2021-08-20 2021-12-17 北京航天时代光电科技有限公司 High-precision and miniaturized triaxial integrated optical fiber gyroscope based on double erbium source redundancy design
CN113804178B (en) * 2021-08-20 2023-02-24 北京航天时代光电科技有限公司 High-precision miniaturized triaxial integrated optical fiber gyroscope based on double erbium source redundancy design

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Application publication date: 20140402