CN105910597A - Combined type fiber loop framework for fiber-optic gyroscope - Google Patents

Combined type fiber loop framework for fiber-optic gyroscope Download PDF

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Publication number
CN105910597A
CN105910597A CN201610458249.6A CN201610458249A CN105910597A CN 105910597 A CN105910597 A CN 105910597A CN 201610458249 A CN201610458249 A CN 201610458249A CN 105910597 A CN105910597 A CN 105910597A
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CN
China
Prior art keywords
fiber
face
optical fiber
optical
ring skeleton
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
Application number
CN201610458249.6A
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Chinese (zh)
Inventor
杨鹏
何虹锋
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Shaanxi Baocheng Aviation Instrument Co Ltd
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Shaanxi Baocheng Aviation Instrument 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.)
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Publication date
Application filed by Shaanxi Baocheng Aviation Instrument Co Ltd filed Critical Shaanxi Baocheng Aviation Instrument Co Ltd
Priority to CN201610458249.6A priority Critical patent/CN105910597A/en
Publication of CN105910597A publication Critical patent/CN105910597A/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
    • G01C19/721Details
    • G01C19/722Details of the mechanical construction

Abstract

The invention provides a combined type fiber loop framework for a fiber-optic gyroscope. The combined type fiber loop framework is provided with an internal fiber loop framework body, an external fiber loop framework body and a mounting plate. The internal fiber loop framework body and the external fiber framework body are both of I-shaped loop structures, and the lower end face of the internal fiber loop framework body is fixed to the mounting plate. An optical fiber winding loop face I and an optical fiber winding loop face II are both provided with optical fibers wound in a quadrupolar symmetry mode, and gluing discs at the two optical fiber outlet ends of the optical fiber on each of the optical fiber winding loop face I and the optical fiber winding loop face II are mounted on the optical fiber winding loop face I and the optical fiber winding loop face. The internal fiber loop framework body is embedded into a center hole of the external fiber loop framework body, and the lower end of the external fiber loop framework body is fixed to the mounting plate. The high-precision fiber loop winding length is distributed to the internal fiber loop framework body and the external fiber loop framework body, the number of winding turns is reduced, the winding difficulty for staff is lowered, and the yield is increased; meanwhile, quadrupolar symmetry optical fiber winding is adopted, so that the influence of the temperature gradient effect on the performance of the fiber-optic gyroscope is effectively reduced, the vibration performance of the fiber-optic gyroscope is improved, the structure is simple, and operation is easy.

Description

A kind of modular fiber optic ring skeleton for optical fibre gyro
Technical field
The invention belongs to fiber-optics gyroscope field, be specifically related to a kind of combination type light for optical fibre gyro Fine ring skeleton.
Background technology
Optical fibre gyro is a kind of novel inertia device, and it is with the Sagnac effect of light as theoretical basis, and light Fine ring is to cause two to restraint Sagnac phase contrast between light wave in opposite directions for sensitizing input angular velocity in optical fibre gyro Parts, the quality of its performance will directly affect the performance of optical fibre gyro, and along with the motion of carrier, light exists Propagating along two different directions in fiber optic loop, the optical path difference of formation realizes gyro by circuit digital demodulation Function, it addition, fiber optic loop is as the critical component of optical fibre gyro, its skeleton not only acts as supporting role, Also directly affecting dish dress and the overall construction design of optical system, therefore, the design of fiber optic loop skeleton is straight Connect the reliability determining fiber optic gyroscope performance, especially for high-precision optical fiber gyro, usual coiling light Fine length reaches more than 1km, along with the increase of the coiling number of turn, is ensureing overall alignment, without climbing layer, stress On the premise of Yi Zhi, bringing the biggest difficulty to coiling personnel, fiber optic loop qualification rate reduces simultaneously, cost Raise;Secondly because the increase of the coiling number of plies, the radial symmetry gradient effect of fiber optic loop increases, thus shadow Ring the temperature performance of optical fibre gyro;Finally, the design of fiber optic loop skeleton, optical fibre gyro height may be caused Increase, cause barycenter to rise, and optical fibre gyro is typically fixed by screws in base, its vibratility is produced Raw impact, therefore, it is necessary to improve.
Summary of the invention
Present invention solves the technical problem that: a kind of modular fiber optic ring skeleton for optical fibre gyro is provided, High-precision optical fiber is shared on inner fiber ring skeleton and infrared optical fiber ring skeleton around length processed, the coiling number of turn Reduce, reduce the coiling difficulty of personnel, improve qualification rate, use quadrupole symmetric fiber coiling simultaneously, Significantly reduce temperature gradient effect and impact on fiber optic gyroscope performance, improve the vibration of optical fibre gyro Performance, simple in construction, it is easy to operation.
The technical solution used in the present invention: a kind of modular fiber optic ring skeleton for optical fibre gyro, in having Fiber optic loop skeleton, infrared optical fiber ring skeleton and installing plate, described inner fiber ring skeleton and infrared optical fiber ring skeleton are equal Fixing on a mounting board for I-shaped ring structure and inner fiber ring skeleton lower surface, described inner fiber ring skeleton and The upper surface of infrared optical fiber ring skeleton is respectively fiber reel dress face I and fiber reel dress face II, and inner fiber ring bone External annulus between frame and infrared optical fiber ring skeleton upper and lower end face is respectively optical fiber coiling anchor ring I and optical fiber coiling Anchor ring II, described optical fiber coiling anchor ring I and optical fiber coiling anchor ring II are equipped with the light by quadrupole symmetrical coiling Optical fiber two optical fibre output end fine and thereon is coated with lacquer disk(-sc) and is contained on fiber reel dress face I and on fiber reel dress face II, institute State in inner fiber ring skeleton is nested in the centre bore of infrared optical fiber ring skeleton and infrared optical fiber ring skeleton lower end to be fixed on On installing plate, described fiber reel dress face I on one of them optical fibre output end and fiber reel dress face II on wherein One optical fibre output end welding and be coated with lacquer disk(-sc) in fiber reel dress face I and fiber reel dress face II on, described fiber reel fill Another optical fibre output end on face I and another optical fibre output end on fiber reel dress face II melt with optics tail optical fiber Connect and be coated with lacquer disk(-sc) on fiber reel dress face I and on fiber reel dress face II.
Wherein, described fiber reel dress face I and fiber reel dress face II cylindrical are formed respectively with symmetrical going out Fine helical flute I and fiber helical flute II, the optical fiber optical fibre output end on described fiber reel dress face I is through fiber spiral shell Being coated with lacquer disk(-sc) after wire casing I and fill on face I in fiber reel, the optical fiber optical fibre output end on described fiber reel dress face II passes Lacquer disk(-sc) optical fibre output end on fiber reel dress face II, on the right side of described fiber reel dress face I it is coated with after fiber helical flute II With the optical fibre output end welding on the left of fiber reel dress face II, the optical fibre output end on the left of described fiber reel dress face I and optical fiber Optical fibre output end on the right side of dish dress face II and optics tail optical fiber welding.
Further, described infrared optical fiber ring skeleton lower surface is shaped with screwed hole, described installing plate is shaped with The counter sink that screwed hole is corresponding, described inner fiber ring skeleton is nested in the centre bore of infrared optical fiber ring skeleton, Infrared optical fiber ring skeleton is fixed on a mounting board after screwing through counter sink and screwed hole by crossed pan head screw.
Further, described fiber reel dress face II on be shaped with prevent optical fiber depart from infrared optical fiber ring skeleton along convex Circle.
Present invention advantage compared with prior art:
1, high-precision optical fiber is shared on inner fiber ring skeleton and infrared optical fiber ring skeleton around length processed, coiling The number of turn reduces, and reduces the coiling difficulty of personnel, improves the qualification rate of fiber optic loop, and cost reduces;
2, the optical fiber coiling number of plies reduces, and the radial temperature alias of fiber optic loop reduces, and to use quadrupole right simultaneously Claim optical fiber coiling, significantly reduce temperature gradient effect and impact on fiber optic gyroscope performance;
3, this structure effectively prevent the phenomenon causing barycenter to rise due to the increase of fiber optic loop skeleton height, Thus improve the vibration performance of optical fibre gyro;
4, simple in construction, it is easy to operation.
Accompanying drawing explanation
Fig. 1 is present configuration schematic diagram;
Fig. 2 is inner fiber ring skeleton of the present invention and installing plate front perspective view;
Fig. 3 is infrared optical fiber ring skeleton Facad structure schematic diagram of the present invention;
Fig. 4 is infrared optical fiber ring skeleton side structure schematic diagram of the present invention;
Fig. 5 is inner fiber ring skeleton of the present invention and installing plate side perspective view.
Detailed description of the invention
1-5 describes a kind of embodiment of the present invention below in conjunction with the accompanying drawings.
A kind of modular fiber optic ring skeleton for optical fibre gyro, has inner fiber ring skeleton 1, infrared optical fiber ring Skeleton 2 and installing plate 3, described inner fiber ring skeleton 1 and infrared optical fiber ring skeleton 2 be I-shaped ring structure and Inner fiber ring skeleton 1 lower surface is fixed on installing plate 3, described inner fiber ring skeleton 1 and infrared optical fiber ring The upper surface of skeleton 2 is respectively fiber reel dress face I 6 and fiber reel dress face II 7, and inner fiber ring skeleton 1 With the external annulus between infrared optical fiber ring skeleton 2 upper and lower end face is respectively optical fiber coiling anchor ring I 4 and optical fiber coiling Anchor ring II 5, described optical fiber coiling anchor ring I 4 and optical fiber coiling anchor ring II 5 are equipped with by quadrupole symmetrical coiling Optical fiber 12 and 12 liang of optical fibre output ends of optical fiber thereon be coated with lacquer disk(-sc)s and be contained on fiber reel dress face I 6 and fill with fiber reel On face II 7, high-precision optical fiber is shared inner fiber ring skeleton 1 and infrared optical fiber ring skeleton 2 around length processed On, the coiling number of turn reduces, and reduces the coiling difficulty of personnel, improves the qualification rate of fiber optic loop, cost Reducing, the optical fiber 12 coiling number of plies reduces, and the radial temperature alias of fiber optic loop reduces, and uses four simultaneously Extremely symmetrical coiling, significantly reduces temperature gradient effect and impact on fiber optic gyroscope performance, described in In fiber optic loop skeleton 1 is nested in the centre bore of infrared optical fiber ring skeleton 2 and infrared optical fiber ring skeleton 2 lower end is fixed On installing plate 3, concrete, described infrared optical fiber ring skeleton 2 lower surface is shaped with screwed hole 10, described peace Being shaped with the counter sink 11 corresponding with screwed hole 10 on dress plate 3, described inner fiber ring skeleton 1 is nested in outer light In the centre bore of fine ring skeleton 2, after crossed pan head screw 14 screws through counter sink 11 and screwed hole 10 Infrared optical fiber ring skeleton 2 is fixed on installing plate 3, one of them fiber on described fiber reel dress face I 6 End and fiber reel fill one of them the optical fibre output end welding on face II 7 and are coated with lacquer disk(-sc) in fiber reel dress face I 6 and light On fine dish dress face II 7, another optical fibre output end and fiber reel on described fiber reel dress face I 6 fill on face II 7 Another optical fibre output end and optics tail optical fiber welding and be coated with lacquer disk(-sc) on fiber reel dress face I 6 and fiber reel On dress face II 7, concrete, described fiber reel dress face I 6 and fiber reel dress face II 7 cylindrical are formed respectively with Symmetrical fiber helical flute I 8 and fiber helical flute II 9, the optical fiber on described fiber reel dress face I 6 12 optical fibre output ends are coated with lacquer disk(-sc) and fill on face I 6 in fiber reel after passing fiber helical flute I 8, described fiber reel dress face Optical fiber 12 optical fibre output end on II 7 is coated with lacquer disk(-sc) and fills on face II 7 in fiber reel after passing fiber helical flute II 9, institute State the optical fibre output end on the right side of fiber reel dress face I 6 and fill the optical fibre output end welding on the left of face II 7, described light with fiber reel Optical fibre output end on the left of fine dish dress face I 6 and the optical fibre output end on the right side of fiber reel dress face II 7 melt with optics tail optical fiber Connect, described fiber reel dress face II 7 on be shaped with prevent optical fiber 12 depart from infrared optical fiber ring skeleton 2 along flange collar 13, This structure effectively prevent the phenomenon causing barycenter to rise due to the increase of fiber optic loop skeleton height, thus Improve the vibration performance of optical fibre gyro, simple in construction, it is easy to operation.
Above-described embodiment, simply presently preferred embodiments of the present invention, be not used for limiting the scope of the present invention, Therefore all with content described in the claims in the present invention done equivalence change, all should be included in right of the present invention want Within the scope of asking.

Claims (4)

1., for the modular fiber optic ring skeleton of optical fibre gyro, there is inner fiber ring skeleton (1), outer Fiber optic loop skeleton (2) and installing plate (3), it is characterised in that: described inner fiber ring skeleton (1) and outer Fiber optic loop skeleton (2) is I-shaped ring structure and inner fiber ring skeleton (1) lower surface is fixed on installing plate (3), on, the upper surface of described inner fiber ring skeleton (1) and infrared optical fiber ring skeleton (2) is respectively optical fiber Dish dress face I (6) and fiber reel fill face II (7), and inner fiber ring skeleton (1) and infrared optical fiber ring skeleton (2) external annulus between upper and lower end face is respectively optical fiber coiling anchor ring I (4) and optical fiber coiling anchor ring II (5), described optical fiber coiling anchor ring I (4) and optical fiber coiling anchor ring II (5) are equipped with by quadrupole symmetry The optical fiber (12) of coiling and optical fiber thereon (12) two optical fibre output end are coated with lacquer disk(-sc) and are contained in fiber reel dress face I (6) Upper and fiber reel fills on face II (7), and described inner fiber ring skeleton (1) is nested in infrared optical fiber ring skeleton (2) Centre bore in and infrared optical fiber ring skeleton (2) lower end be fixed on installing plate (3), described fiber reel fill One of them optical fibre output end on face I (6) and one of them optical fibre output end on fiber reel dress face II (7) melt Connect and be coated with lacquer disk(-sc) and fill on face II (7) in fiber reel dress face I (6) and fiber reel, described fiber reel dress face Another optical fibre output end and fiber reel on I (6) fill another optical fibre output end on face II (7) and optics device Part tail optical fiber welding is also coated with lacquer disk(-sc) in fiber reel dress face I (6) is upper and fiber reel fills on face II (7).
Modular fiber optic ring skeleton for optical fibre gyro the most according to claim 1, its feature exists In: it is formed respectively with symmetrically on described fiber reel dress face I (6) and fiber reel dress face II (7) cylindrical Fiber helical flute I (8) and fiber helical flute II (9), described fiber reel dress face I (6) on light Fine (12) optical fibre output end is coated with lacquer disk(-sc) afterwards through fiber helical flute I (8) and fills on face I (6) in fiber reel, Optical fiber (12) optical fibre output end on described fiber reel dress face II (7) is coated with afterwards through fiber helical flute II (9) Lacquer disk(-sc) is on fiber reel dress face II (7), and described fiber reel fills optical fibre output end and the optical fiber on right side, face I (6) Dish dress face II (7) left side optical fibre output end welding, described fiber reel dress face I (6) left side optical fibre output end and The optical fibre output end on right side, fiber reel dress face II (7) and optics tail optical fiber welding.
Modular fiber optic ring skeleton for optical fibre gyro the most according to claim 2, its feature It is: described infrared optical fiber ring skeleton (2) lower surface is shaped with screwed hole (10), on described installing plate (3) It is shaped with the counter sink (11) corresponding with screwed hole (10), outside described inner fiber ring skeleton (1) is nested in In the centre bore of fiber optic loop skeleton (2), crossed pan head screw (14) passes counter sink (11) and screw thread Infrared optical fiber ring skeleton (2) is fixed on installing plate (3) after screwing by hole (10).
4. according to the modular fiber optic ring skeleton for optical fibre gyro described in claim 1 or 2 or 3, It is characterized in that: be shaped with on described fiber reel dress face II (7) and prevent optical fiber (12) from departing from infrared optical fiber ring bone Frame (2) along flange collar (13).
CN201610458249.6A 2016-06-22 2016-06-22 Combined type fiber loop framework for fiber-optic gyroscope Pending CN105910597A (en)

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Application Number Priority Date Filing Date Title
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105928502A (en) * 2016-06-22 2016-09-07 陕西宝成航空仪表有限责任公司 Combined type optical fiber ring skeleton for optical fiber gyroscope
CN106643687A (en) * 2016-12-30 2017-05-10 陕西宝成航空仪表有限责任公司 Elliptical fiber ring skeleton for fiber gyroscope
CN116026302A (en) * 2023-03-27 2023-04-28 中国船舶集团有限公司第七〇七研究所 Tail fiber processing method of optical fiber ring assembly of optical fiber gyro
CN116182825A (en) * 2023-04-26 2023-05-30 南京开拓光电科技有限公司 Optical fiber ring for optical fiber gyroscope, processing device and processing method

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CN2655179Y (en) * 2003-11-20 2004-11-10 北京航空航天大学 Optical fiber top mechanical frame
CN101551249A (en) * 2008-11-19 2009-10-07 北京航天时代光电科技有限公司 Detachable framework and optical fiber coil preparation method realized by using the framework
CN102435210A (en) * 2011-09-23 2012-05-02 武汉长盈通光电技术有限公司 Separable demoulding skeleton for manufacturing optic fiber loop of optic fiber gyroscope
CN202350793U (en) * 2011-09-28 2012-07-25 湖南航天远望测控技术有限公司 Novel optical fiber gyroscope ring framework structure
CN102607548A (en) * 2012-02-24 2012-07-25 北京航空航天大学 Fiber-optic loop structure wound in vertically symmetrical cross manner for fiber-optic gyroscope and winding method
CN102967302A (en) * 2012-11-16 2013-03-13 中国船舶重工集团公司第七一七研究所 Framework for optical fiber gyroscope and manufacturing method thereof as well as method for packaging optical fiber ring
CN103033179A (en) * 2012-12-25 2013-04-10 北京航空航天大学 Fiber-optic gyroscope sensitive ring skeleton with inner flange
CN105928502A (en) * 2016-06-22 2016-09-07 陕西宝成航空仪表有限责任公司 Combined type optical fiber ring skeleton for optical fiber gyroscope

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4699451A (en) * 1983-09-10 1987-10-13 International Standard Electric Corp. Optical fiber coil having juxtaposed ends in same or adjacent layers for rotation rate measuring instrument
CN2655179Y (en) * 2003-11-20 2004-11-10 北京航空航天大学 Optical fiber top mechanical frame
CN101551249A (en) * 2008-11-19 2009-10-07 北京航天时代光电科技有限公司 Detachable framework and optical fiber coil preparation method realized by using the framework
CN102435210A (en) * 2011-09-23 2012-05-02 武汉长盈通光电技术有限公司 Separable demoulding skeleton for manufacturing optic fiber loop of optic fiber gyroscope
CN202350793U (en) * 2011-09-28 2012-07-25 湖南航天远望测控技术有限公司 Novel optical fiber gyroscope ring framework structure
CN102607548A (en) * 2012-02-24 2012-07-25 北京航空航天大学 Fiber-optic loop structure wound in vertically symmetrical cross manner for fiber-optic gyroscope and winding method
CN102967302A (en) * 2012-11-16 2013-03-13 中国船舶重工集团公司第七一七研究所 Framework for optical fiber gyroscope and manufacturing method thereof as well as method for packaging optical fiber ring
CN103033179A (en) * 2012-12-25 2013-04-10 北京航空航天大学 Fiber-optic gyroscope sensitive ring skeleton with inner flange
CN105928502A (en) * 2016-06-22 2016-09-07 陕西宝成航空仪表有限责任公司 Combined type optical fiber ring skeleton for optical fiber gyroscope

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105928502A (en) * 2016-06-22 2016-09-07 陕西宝成航空仪表有限责任公司 Combined type optical fiber ring skeleton for optical fiber gyroscope
CN106643687A (en) * 2016-12-30 2017-05-10 陕西宝成航空仪表有限责任公司 Elliptical fiber ring skeleton for fiber gyroscope
CN116026302A (en) * 2023-03-27 2023-04-28 中国船舶集团有限公司第七〇七研究所 Tail fiber processing method of optical fiber ring assembly of optical fiber gyro
CN116182825A (en) * 2023-04-26 2023-05-30 南京开拓光电科技有限公司 Optical fiber ring for optical fiber gyroscope, processing device and processing method
CN116182825B (en) * 2023-04-26 2023-08-11 南京开拓光电科技有限公司 Optical fiber ring for optical fiber gyroscope, processing device and processing method

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Application publication date: 20160831