CN205482968U - Integrated fiber gyroscope of crystal - Google Patents

Integrated fiber gyroscope of crystal Download PDF

Info

Publication number
CN205482968U
CN205482968U CN201620254777.5U CN201620254777U CN205482968U CN 205482968 U CN205482968 U CN 205482968U CN 201620254777 U CN201620254777 U CN 201620254777U CN 205482968 U CN205482968 U CN 205482968U
Authority
CN
China
Prior art keywords
optical fiber
port
tunable laser
detector
tail optical
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 - Fee Related
Application number
CN201620254777.5U
Other languages
Chinese (zh)
Inventor
朱奎宝
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.)
Fuzhou Sun Sensing Technology Co ltd
Original Assignee
Shenzhen Taiyangxun Sensing Technology Co ltd
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 Shenzhen Taiyangxun Sensing Technology Co ltd filed Critical Shenzhen Taiyangxun Sensing Technology Co ltd
Priority to CN201620254777.5U priority Critical patent/CN205482968U/en
Application granted granted Critical
Publication of CN205482968U publication Critical patent/CN205482968U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Gyroscopes (AREA)

Abstract

The utility model provides an integrated fiber gyroscope of crystal, integrated fiber gyroscope of crystal includes tunable laser, polarization beam split five terminal mouthpart spare, optic fibre ring, postpones ring, bi -polar tail optical fiber detector and detection circuitry, tunable laser, optic fibre ring, postpone ring sum bi -polar tail optical fiber detector with polarization beam split five terminal mouthpart spare is connected, detection circuitry with bi -polar tail optical fiber detector is connected. The utility model discloses integrated fiber gyroscope of crystal is through setting up tunable laser, polarization beam split five terminal mouthpart spare, optic fibre ring, postponing ring, bi -polar tail optical fiber detector and detection circuitry to with tunable laser, optic fibre ring, postpone ring sum bi -polar tail optical fiber detector and be connected with polarization beam split five terminal mouthpart spare, can simplify the structure of light path, improvement fiber optic gyroscope's reliability and stability reduce fiber optic gyroscope's volume, greatly reduced fiber optic gyroscope's cost.

Description

A kind of crystal integrated optical fiber gyroscope instrument
Technical field
This utility model relates to inertial sensor manufacturing technology field, particularly relates to a kind of crystal integrated optical fiber top Spiral shell instrument.
Background technology
Fibre optic gyroscope is with optical fibers coil as sensing element, fibre optic gyroscope and traditional mechanical gyro Instrument is compared, and advantage is all solid state, does not has rotary part and friction means, and the life-span is long, and dynamic range is big, wink Shi Qidong, simple in construction, size is little, lightweight.Compared with lasergyro, fibre optic gyroscope does not close Lock problem, goes out light path without Precision Machining on quartz wedge, and technique is simple, low cost.But existing light Fiber gyroscope optics is discrete components and parts, the tail optical fiber mutual welding of needs of device, the fusing point of increase, Bring interference for light path, increase the noise of light path, reduce the reliability of light path, inside existing fiber gyro Device be special optics, especially integrated optical modulator, structure is complicated, and production difficulty is big, Cost is the highest, adds manufacture difficulty and the cost of optical fibre gyro.
Utility model content
The technical problems to be solved in the utility model is to provide a kind of crystal integrated optical fiber gyroscope instrument, it is possible to simplify The structure of light path, improves the reliability of optical fibre gyro.
For solving above-mentioned technical problem, embodiment of the present utility model provides a kind of crystal integrated optical fiber gyroscope instrument, Described crystal integrated optical fiber gyroscope instrument include tunable laser, polarization spectro five port devices, fiber optic loop, Ring retard, both-end tail optical fiber detector and testing circuit, described tunable laser, fiber optic loop, ring retard and Both-end tail optical fiber detector is connected with described polarization spectro five port devices, described testing circuit and described both-end tail Fine detector connects.
Preferably, described tunable laser is connected with the first port of described polarization spectro five port devices, The two ends of described fiber optic loop are connected with the second port and the 3rd port of described polarization spectro five port devices, institute State the two ends of ring retard respectively with the 4th port of polarization spectro five port devices and both-end tail optical fiber detector even Connecing, described both-end tail optical fiber detector is respectively with the fifth port of polarization spectro five port devices and testing circuit even Connect.
Preferably, described tunable laser is connected with tunable laser driver.
Preferably, described both-end tail optical fiber detector is photoelectricity both-end tail optical fiber detector.
Preferably, it is provided with beam splitter and splicer in described polarization spectro five port devices.
Having the beneficial effect that of technique scheme of the present utility model:
In such scheme, by arrange tunable laser, polarization spectro five port devices, fiber optic loop, Ring retard, both-end tail optical fiber detector and testing circuit, and by tunable laser, fiber optic loop, ring retard and Both-end tail optical fiber detector is connected with polarization spectro five port devices, it is possible to simplify the loaded down with trivial details journey that gyroscope is installed Degree, improves device integration, it is ensured that the reliability and stability of optical fibre gyro, is substantially reduced optical fibre gyro Cost.
Accompanying drawing explanation
Fig. 1 is the crystal integrated optical fiber gyroscope instrument structure connection diagram of this utility model embodiment;
Fig. 2 is the crystal integrated optical fiber gyroscope instrument signal pulse schematic diagram of this utility model embodiment.
[main element symbol description]
Tunable laser 1;
Polarization spectro five port devices 2;
Fiber optic loop 3;
Ring retard 4;
Both-end tail optical fiber detector 5;
Testing circuit 6;
Tunable laser driver 7.
Detailed description of the invention
For making the technical problems to be solved in the utility model, technical scheme and advantage clearer, below will knot Conjunction drawings and the specific embodiments are described in detail.
As it is shown in figure 1, a kind of crystal integrated optical fiber gyroscope instrument that embodiment of the present utility model provides, described Crystal integrated optical fiber gyroscope instrument include tunable laser 1, polarization spectro five port devices 2, fiber optic loop 3, Ring retard 4, both-end tail optical fiber detector 5 and testing circuit 6, described tunable laser 1, fiber optic loop 3, Ring retard 4 and both-end tail optical fiber detector 5 are connected with described polarization spectro five port devices 2, described detection electricity Road 6 is connected with described both-end tail optical fiber detector 5.
Preferably, described tunable laser 1 connects with the first port of described polarization spectro five port devices 2 Connect, the two ends of described fiber optic loop 3 and the second port of described polarization spectro five port devices 2 and the 3rd port Connect, the two ends of described ring retard 4 respectively with the 4th port and the both-end tail of polarization spectro five port devices 2 Fine detector 5 connects, described both-end tail optical fiber detector 5 respectively with the 5th of polarization spectro five port devices 2 Port and testing circuit 6 connect.
Preferably, described tunable laser 1 is connected with tunable laser driver 7.
Preferably, described both-end tail optical fiber detector 5 is photoelectricity both-end tail optical fiber detector.
Preferably, it is provided with beam splitter and splicer in described polarization spectro five port devices 2.
In use, driving, temperature control current and tuning square wave letter that tunable laser driver provides are utilized Number, tunable laser sends polarized optical pulse pulse, and the width of pulse is true by the amplitude tuning signal square wave Fixed, for 1/2nd of fiber optic loop transition time τ.Polarized optical pulse is divided into two bundle polarizations through five ports The polarized optical pulse that state is mutually orthogonal, light CW the most clockwise and light CCW counterclockwise.CW and CCW light It is coupled into fiber optic loop, propagates in opposite directions through fiber optic loop, be coupled into polarization spectro five port devices respectively, As in figure 2 it is shown, after closing light and light splitting, form the light pulse that two bundles are orthogonal, be coupled into both-end respectively Tail optical fiber detector and ring retard, light, through transition time τ/2 that time delay is fiber optic loop of ring retard, enters Entering the other end of both-end tail optical fiber detector, two-beam pulse arrives the time interval of both-end tail optical fiber detector and is τ/2, two light pulses, after both-end tail optical fiber detector opto-electronic conversion, successively enter testing circuit number Wordization is sampled.The crystal integrated optical fiber gyroscope instrument of this utility model embodiment, by arrange tunable laser, Polarization spectro five port devices, fiber optic loop, ring retard, both-end tail optical fiber detector and testing circuit, and can Tuned laser, fiber optic loop, ring retard and both-end tail optical fiber detector are connected with polarization spectro five port devices, The structure of light path can be simplified, improve the reliability and stability of optical fibre gyro, reduce the volume of optical fibre gyro, It is substantially reduced the cost of optical fibre gyro.The above is preferred implementation of the present utility model, it is noted that For those skilled in the art, in the premise without departing from principle described in the utility model Under, it is also possible to making some improvements and modifications, these improvements and modifications also should be regarded as protection of the present utility model Scope.

Claims (5)

1. a crystal integrated optical fiber gyroscope instrument, it is characterised in that described crystal integrated optical fiber gyroscope instrument includes Tunable laser, polarization spectro five port devices, fiber optic loop, ring retard, both-end tail optical fiber detector and inspection Slowdown monitoring circuit, described tunable laser, fiber optic loop, ring retard and both-end tail optical fiber detector divide with described polarization Light five port devices connects, and described testing circuit is connected with described both-end tail optical fiber detector.
Crystal integrated optical fiber gyroscope instrument the most according to claim 1, it is characterised in that described tunable Laser instrument is connected with the first port of described polarization spectro five port devices, and the two ends of described fiber optic loop are with described Second port of polarization spectro five port devices and the 3rd port connect, the two ends of described ring retard respectively with partially 4th port of light splitting five port devices of shaking and both-end tail optical fiber detector connect, and described both-end tail optical fiber detector divides It is not connected with fifth port and the testing circuit of polarization spectro five port devices.
Crystal integrated optical fiber gyroscope instrument the most according to claim 1, it is characterised in that described tunable Laser instrument is connected with tunable laser driver.
Crystal integrated optical fiber gyroscope instrument the most according to claim 1, it is characterised in that described both-end tail Fine detector is photoelectricity both-end tail optical fiber detector.
Crystal integrated optical fiber gyroscope instrument the most according to claim 1, it is characterised in that described polarization divides It is provided with beam splitter and splicer in light five port devices.
CN201620254777.5U 2016-03-31 2016-03-31 Integrated fiber gyroscope of crystal Expired - Fee Related CN205482968U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620254777.5U CN205482968U (en) 2016-03-31 2016-03-31 Integrated fiber gyroscope of crystal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620254777.5U CN205482968U (en) 2016-03-31 2016-03-31 Integrated fiber gyroscope of crystal

Publications (1)

Publication Number Publication Date
CN205482968U true CN205482968U (en) 2016-08-17

Family

ID=56648930

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620254777.5U Expired - Fee Related CN205482968U (en) 2016-03-31 2016-03-31 Integrated fiber gyroscope of crystal

Country Status (1)

Country Link
CN (1) CN205482968U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110455270A (en) * 2019-08-07 2019-11-15 湖南航天机电设备与特种材料研究所 A kind of singly polarization wide-spectrum optical fiber light source and optical fibre gyro

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110455270A (en) * 2019-08-07 2019-11-15 湖南航天机电设备与特种材料研究所 A kind of singly polarization wide-spectrum optical fiber light source and optical fibre gyro

Similar Documents

Publication Publication Date Title
CN104075704B (en) A kind of digital closed-loop optic fiber gyroscope instrument with dual interferometer system
CN103697880B (en) A kind of optical fibre gyro of low random walk coefficient
CN101532838B (en) Triaxial integration resonant mode optical fiber gyro for optical path multiplexing
CN101694386B (en) High-sensitivity optical fiber gyroscope
CN103076155B (en) Optical fiber Verdet constant measurement system on basis of double optical paths
US20160116288A1 (en) Angular velocity detection method adopting bi-directional full reciprocal coupling optoelectronic oscillator
CN101482412B (en) Closed-loop optic fiber gyroscope light path structure with low polarization error
CN103411597B (en) A kind of interfere type closed-loop fiber optic gyroscope instrument based on circulation multi-turn effect
CN109883412A (en) A kind of double path optical fiber gyroscopes
CN112066975B (en) Gyroscope and accelerometer integrated system based on double resonant cavities and preparation method thereof
CN108195367B (en) Optical fiber gyroscope with double sensitivity
CN101566475A (en) Biaxial optical gyroscope
CN205482968U (en) Integrated fiber gyroscope of crystal
US20120013912A1 (en) All-fiber interferometric fiber optic gyroscope having a minimum reciprocal configuration
CN102207387A (en) Triaxial integration all-optical fiber inertia sensing device
CN1228609C (en) Beat frequency detection method for travelling-wave annular resonance cavity of non-mechanical gyro
CN101922935A (en) Interference type all-optic fiber gyroscope with minimum reciprocal structure
CN102226699B (en) All-fiber inertial sensing device
CN203405499U (en) A reflective all-fiber optical current transformer
CN203615937U (en) Optical demodulating device for four-frequency differential laser gyro
CN105157693B (en) A kind of ring resonator and its resonance type optical fiber gyro
CN110440786B (en) Single-light-source biaxial optical fiber gyroscope and biaxial electric signal demodulation method thereof
CN107607106A (en) A kind of tunable optical fiber gyroscope
CN208333488U (en) A kind of open-loop optical fiber gyro
JP7216951B2 (en) Interferometric fiber optic gyro and sensing coil mechanism

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CP03 Change of name, title or address
CP03 Change of name, title or address

Address after: 350001 North of 1st Floor of Block B, No. 8, Tangxia Road, Jianxin Town, Cangshan District, Fuzhou City, Fujian Province

Patentee after: Fuzhou sun Sensing Technology Co.,Ltd.

Address before: 100022 Shuangjing Fuli Gemini in Chaoyang District, Beijing

Patentee before: SHENZHEN TAIYANGXUN SENSING TECHNOLOGY Co.,Ltd.

CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160817