JPS62247209A - Optical gyroscope - Google Patents

Optical gyroscope

Info

Publication number
JPS62247209A
JPS62247209A JP9154586A JP9154586A JPS62247209A JP S62247209 A JPS62247209 A JP S62247209A JP 9154586 A JP9154586 A JP 9154586A JP 9154586 A JP9154586 A JP 9154586A JP S62247209 A JPS62247209 A JP S62247209A
Authority
JP
Japan
Prior art keywords
optical
waveguide
light
waveguide path
substrate
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
JP9154586A
Other languages
Japanese (ja)
Inventor
Tsunehisa Takabayashi
高林 恒久
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.)
Furukawa Electric Co Ltd
Original Assignee
Furukawa Electric 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 Furukawa Electric Co Ltd filed Critical Furukawa Electric Co Ltd
Priority to JP9154586A priority Critical patent/JPS62247209A/en
Publication of JPS62247209A publication Critical patent/JPS62247209A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/44Mechanical structures for providing tensile strength and external protection for fibres, e.g. optical transmission cables
    • G02B6/4439Auxiliary devices
    • G02B6/4457Bobbins; Reels
    • 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

Landscapes

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

Abstract

PURPOSE:To obtain a flat and thin-type optical gyroscope, by forming a waveguide path in a spiral shape on a waveguide substrate and permitting it to be serviceable as an optical loop sensor. CONSTITUTION:A waveguide path 2 of 5-10mum thick is shaped in a spiral shape on a circular-disc waveguide path substrate established on a single waveguide path substrate 1 by installing laser-diode-originated light source 3, polarizing member 4, detector 5, light-branching members 6a, 6b and optical fiber 8 for bypass. The waveguide path 2 is so formed that, a film is formed on a silicon substrate using SiO2, TiO2 and reactive ion-etching is conducted and the etched surface is covered with SiO2 as a clad surface. A beam of light from the source 3 is transmitted to the spiral-shape waveguide path 2 via light- branching member 6a, polarizing member 4, light-branching member 6b and directed from the other end of the waveguide path 2 to the light-branching members 6b, 6b by the optical fiber 8 for bypass and reaches the detector 5.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は光ジャイロスコープに関するものであり、従来
の光フアイバジャイロのボビンに相当する部分をレコー
ドの溝のような螺旋状をした先導波路としたものである
Detailed Description of the Invention (Field of Industrial Application) The present invention relates to an optical gyroscope, in which a part corresponding to the bobbin of a conventional optical fiber gyro is formed into a spiral leading waveguide like the grooves of a record. This is what I did.

(従来技術) 従来の光フアイバジャイロは第2図のような構成になっ
ている。この光フアイバジャイロではファイバボビンに
光ファイバを巻いて光ループセンサAが形成されている
(Prior Art) A conventional fiber optic gyro has a configuration as shown in FIG. In this optical fiber gyro, an optical loop sensor A is formed by winding an optical fiber around a fiber bobbin.

コノ光フアイバジャイロはボビンに巻かれた光フアイバ
内に左右両回りに光を入射させ、その内方の光の周波数
変化や位相変化を検出することにより回転角速度を知る
ものである。
The Konohikari fiber gyro allows light to enter an optical fiber wound around a bobbin in both left and right directions, and detects the frequency change and phase change of the inner light to determine the rotational angular velocity.

(従来技術の聞届点) 従来の光フアイバジャイロは光ファイ/へを光分岐部や
位相変調器部と接続しなければならないので小型化した
り、薄くシたりするのが難しい。
(Considerations of the Prior Art) Conventional optical fiber gyros have to connect the optical fiber to the optical branching section and the phase modulator section, so it is difficult to make them smaller or thinner.

この光フアイバジャイロを小型化するにはファイバボビ
ンの大きさを小型にすればよいが、ファイバの曲げ゛ト
径の許容量−がファイノへの太さに制限されるとか、−
・ターン当たりのファイ/(lそが短かくなると巻き数
で長さを嫁せがねばならないため、ボビンを小型化する
にも限度があった。また巻き数が多くなると巻き付は張
力やファイ/くに生じるねしれにより 一様な巻きつ(
1を行なうのか難かしいという問題もある。
In order to miniaturize this optical fiber gyro, the size of the fiber bobbin can be made smaller, but the allowable bending diameter of the fiber is limited by the thickness of the fiber.
・Fi per turn/(l) As the length becomes shorter, the length must be determined by the number of windings, so there is a limit to how small the bobbin can be made. Also, as the number of windings increases, the winding becomes more difficult due to tension and fiber. / Uniform winding (
There is also the problem that it is difficult to carry out step 1.

(発明のr1的) 本発明の目的は11板状で蒔型の光ジャイロスコープを
提供することにある。
(R1 aspect of the invention) An object of the present invention is to provide an optical gyroscope having an eleven plate shape and a sock type.

(問題点を解決するための「段) 本発明の光ジャイロスコープは、導波路ノ1(板lに導
波路2を螺旋状に形成して光ループセンサとしてなるも
のである。
(Steps for Solving Problems) The optical gyroscope of the present invention is an optical loop sensor in which a waveguide 2 is spirally formed on a waveguide 1 (plate 1).

(発明の実施例) :fS1図は本発明の光ジャイロスコープの一実施例で
ある。
(Embodiment of the invention): The fS1 diagram is an embodiment of the optical gyroscope of the invention.

第1図の1は円板状の導波路基板であり、これにレコー
ド板の溝のように5〜10μmの導波路2が螺旋状に形
成されている。
Reference numeral 1 in FIG. 1 is a disk-shaped waveguide substrate, on which a waveguide 2 of 5 to 10 μm is spirally formed like the grooves on a record plate.

第1図の3はレーザダイオードによる光源、4は偏光Y
一部、5は検出器、6a、6bは光分岐部、7は位相変
調部、8はバイパス用光ファイバである。これらは一枚
の導波路基板lに設けてハイプリント化しであるが、こ
れらは導波路ノ^板1と別に外部に設けてもよい。
In Figure 1, 3 is a laser diode light source, and 4 is polarized light Y.
5 is a detector, 6a and 6b are optical branching sections, 7 is a phase modulation section, and 8 is a bypass optical fiber. Although these are provided on one waveguide substrate 1 for high printing, they may be provided externally separately from the waveguide board 1.

バイパス用光ファイバ8は先導波路を積層化して電気回
路のスルーホールのように表から裏まで先導波路を連結
するとか、導波路ノ1(板lをもう一枚作って光分岐部
と接続するなどして作る。
The bypass optical fiber 8 can be constructed by stacking the leading waveguides and connecting them from front to back like a through hole in an electric circuit, or by making another waveguide 1 (another plate 1 and connecting it to the optical branch). Make it by doing something like this.

ノリ波路2は現在はシリコン基板1−に5i02、Ti
O2を用いた膜を作り、それを反応性イオンエツチング
して作られ、その玉にCVD法により5102をつけて
クラッドとしている。しかし将来はこの導波路2もIn
PやGa Asを基板とするものに変えることにより、
光源も一緒に作製できるようになり、光ジャイロ−光I
Cジャイロとなり()る。
Currently, the Nori wave path 2 is made of 5i02 and Ti on the silicon substrate 1-.
A film using O2 is made and then subjected to reactive ion etching, and 5102 is attached to the ball using the CVD method to form a cladding. However, in the future, this waveguide 2 will also be In
By changing to a substrate made of P or GaAs,
It is now possible to create a light source at the same time, and optical gyro - optical I
It becomes C gyro().

(発明の作用) 第1図の光源3からの光は光分岐部6a、偏光T一部4
、光分岐部6bを通って螺旋状の導波路2へ伝送され、
導波路2の他端からバイパス用光ファイバ8により光分
岐部6b、6bに導かれ、検出器5に至る。
(Operation of the invention) The light from the light source 3 in FIG.
, is transmitted to the spiral waveguide 2 through the optical branching part 6b,
The light is guided from the other end of the waveguide 2 to optical branching parts 6b, 6b by a bypass optical fiber 8, and reaches the detector 5.

(発IIの効果) 本発明の光ンヤイロはスコープは次のような効果がある
(Effects of Effect II) The optical scope of the present invention has the following effects.

(1)光ループセンサがモ面化されるため、小型型化、
薄型化できる。全体の厚さが本体部分だけならば約5m
mにも薄くなる。
(1) Since the optical loop sensor is made into a mosaic surface, it becomes smaller and smaller.
Can be made thinner. If the total thickness is just the main body part, it is approximately 5m.
It becomes thinner to m.

(2)他の光部品との一体化が口r能となる。(2) Integration with other optical components becomes an advantage.

(3)導波路2の螺旋間隔を狭くすれば導波路2を長く
することができるため、導波路2を長くしても大型にな
らない。
(3) Since the waveguide 2 can be made longer by narrowing the helical interval of the waveguide 2, even if the waveguide 2 is made longer, it does not become larger.

(4) Jlt球磁気による影響を防ぐためのシールド
もし易い。
(4) It is easy to shield to prevent the influence of Jlt ball magnetism.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は未発IJIのf板型光ジャイロの一例を示すf
面図、第2図は従来の光ジヤイロの説明図である。 1は導波路基板 2は導波路 出願人 、す%11’、L:気[業株式会社代理人 ブ
r理ト 小林1治1ji i1・(、、。 1仁;・1++1 堵 1 図 $2  電”jl
Figure 1 shows an example of an unreleased IJI f-plate type optical gyro.
The top view and FIG. 2 are explanatory diagrams of a conventional optical gyro. 1 is the waveguide substrate 2 is the waveguide applicant. electric “jl”

Claims (3)

【特許請求の範囲】[Claims] (1)導波路基板に導波路を螺旋状に形成して光ループ
センサとしたことを特徴とする光ジャイロスコープ。
(1) An optical gyroscope characterized in that an optical loop sensor is formed by forming a waveguide in a spiral shape on a waveguide substrate.
(2)光ループセンサを光分岐、光変調部などと同時に
作成して、外付けの光源、検出器とハイブリット化して
なる特許請求の範囲第1項記載の光ジャイロスコープ。
(2) The optical gyroscope according to claim 1, wherein the optical loop sensor is created at the same time as the optical branching section, the optical modulating section, etc., and is hybridized with an external light source and a detector.
(3)G_dA_sやI_nPを用いた半導体基板の上
に導波路、光源、検出器を一体に製作してなる特許請求
の範囲第1項記載の光ジャイロスコープ。
(3) The optical gyroscope according to claim 1, in which a waveguide, a light source, and a detector are integrally manufactured on a semiconductor substrate using G_dA_s or I_nP.
JP9154586A 1986-04-21 1986-04-21 Optical gyroscope Pending JPS62247209A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9154586A JPS62247209A (en) 1986-04-21 1986-04-21 Optical gyroscope

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9154586A JPS62247209A (en) 1986-04-21 1986-04-21 Optical gyroscope

Publications (1)

Publication Number Publication Date
JPS62247209A true JPS62247209A (en) 1987-10-28

Family

ID=14029451

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9154586A Pending JPS62247209A (en) 1986-04-21 1986-04-21 Optical gyroscope

Country Status (1)

Country Link
JP (1) JPS62247209A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0512471A2 (en) * 1991-05-10 1992-11-11 BODENSEEWERK GERÄTETECHNIK GmbH Fibre ring resonator
FR2686411A1 (en) * 1992-01-17 1993-07-23 Commissariat Energie Atomique OPTICAL GYROMETER WITH SAGNAC EFFECT IN COMPLETELY INTEGRATED STRUCTURE.
JPH06317606A (en) * 1993-05-10 1994-11-15 Oki Electric Ind Co Ltd Semiconductor acceleration sensor and semiconductor acceleration detecting device using this sensor
CN1313802C (en) * 2001-08-28 2007-05-02 精工爱普生株式会社 Optical gyroscope and manufacturing method thereof
US10415970B2 (en) * 2016-11-01 2019-09-17 University Of Central Florida Research Foundation, Inc. Rotation sensor, rotation sensing method, and applications

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5849456B2 (en) * 1975-09-19 1983-11-04 株式会社日立製作所 Capsule Souniyu Souchi
JPS60218021A (en) * 1984-04-13 1985-10-31 Komatsu Ltd Laser gyro
JPS61184417A (en) * 1985-02-12 1986-08-18 Komatsu Ltd Laser gyroscope
JPS61233314A (en) * 1985-04-09 1986-10-17 Fujikura Ltd Optical element

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5849456B2 (en) * 1975-09-19 1983-11-04 株式会社日立製作所 Capsule Souniyu Souchi
JPS60218021A (en) * 1984-04-13 1985-10-31 Komatsu Ltd Laser gyro
JPS61184417A (en) * 1985-02-12 1986-08-18 Komatsu Ltd Laser gyroscope
JPS61233314A (en) * 1985-04-09 1986-10-17 Fujikura Ltd Optical element

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0512471A2 (en) * 1991-05-10 1992-11-11 BODENSEEWERK GERÄTETECHNIK GmbH Fibre ring resonator
FR2686411A1 (en) * 1992-01-17 1993-07-23 Commissariat Energie Atomique OPTICAL GYROMETER WITH SAGNAC EFFECT IN COMPLETELY INTEGRATED STRUCTURE.
US5555088A (en) * 1992-01-17 1996-09-10 Commissariat A L'energie Atomique Sagnac effect optical gyrometer having a fully integrated structure
JPH06317606A (en) * 1993-05-10 1994-11-15 Oki Electric Ind Co Ltd Semiconductor acceleration sensor and semiconductor acceleration detecting device using this sensor
CN1313802C (en) * 2001-08-28 2007-05-02 精工爱普生株式会社 Optical gyroscope and manufacturing method thereof
US10415970B2 (en) * 2016-11-01 2019-09-17 University Of Central Florida Research Foundation, Inc. Rotation sensor, rotation sensing method, and applications

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