JPH08313270A - Fiber Optic Gyro Structure - Google Patents
Fiber Optic Gyro StructureInfo
- Publication number
- JPH08313270A JPH08313270A JP11972995A JP11972995A JPH08313270A JP H08313270 A JPH08313270 A JP H08313270A JP 11972995 A JP11972995 A JP 11972995A JP 11972995 A JP11972995 A JP 11972995A JP H08313270 A JPH08313270 A JP H08313270A
- Authority
- JP
- Japan
- Prior art keywords
- optical fiber
- substrate
- bobbin
- flange
- fiber gyro
- 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.)
- Granted
Links
- 239000000835 fiber Substances 0.000 title description 2
- 239000013307 optical fiber Substances 0.000 claims abstract description 43
- 239000000758 substrate Substances 0.000 claims abstract description 43
- 239000011261 inert gas Substances 0.000 claims abstract description 5
- 230000002093 peripheral effect Effects 0.000 claims abstract description 5
- 239000002184 metal Substances 0.000 claims abstract description 3
- 229910052751 metal Inorganic materials 0.000 claims abstract description 3
- 238000007789 sealing Methods 0.000 claims abstract description 3
- 238000001816 cooling Methods 0.000 claims abstract 2
- 230000017525 heat dissipation Effects 0.000 claims description 2
- 230000003287 optical effect Effects 0.000 description 9
- 125000006850 spacer group Chemical group 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 229910052745 lead Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
Landscapes
- Gyroscopes (AREA)
Abstract
(57)【要約】
【目的】 光ファイバコイルの温度勾配を小さくして角
速度誤差を小さくする。
【構成】 光ファイバコイル（円筒部と上鍔及び下鍔よ
り成る糸巻状のボビン４ａに光ファイバが巻回されてい
る）４が金属製の基板８上にほぼ直角に取付けられる。
ボビン４ａの円筒部に囲まれた基板の上面に、光ファイ
バジャイロの光源を冷却する部材（例えばペルチェ素
子）１１の放熱部が取付けられる。この発明では、ボビ
ン円筒部の高さＨｂ（Ｈｂ＞Ｈ／２；Ｈはボビンの高
さ）の内周面より一体にフランジ２１が突設され、その
フランジを支持する支持円筒２２が基板上にほぼ直角に
突設される。基板８とボビンの下鍔との間に寸法Δの空
隙が形成される。基板８に密閉用カバー９が被され、内
部に不活性ガスが封入される。
(57) [Summary] [Purpose] To reduce the angular velocity error by reducing the temperature gradient of the optical fiber coil. [Structure] An optical fiber coil (an optical fiber is wound around a bobbin 4a having a cylindrical portion and a bobbin 4a composed of an upper collar and a lower collar) 4 is mounted on a metal substrate 8 at a substantially right angle.
A heat radiating portion of a member (for example, a Peltier element) 11 for cooling the light source of the optical fiber gyro is attached to the upper surface of the substrate surrounded by the cylindrical portion of the bobbin 4a. In the present invention, the flange 21 is integrally projected from the inner peripheral surface of the height Hb of the bobbin cylindrical portion (Hb> H / 2; H is the height of the bobbin), and the support cylinder 22 supporting the flange is provided on the substrate. Is projected almost at a right angle. A space of size Δ is formed between the substrate 8 and the lower flange of the bobbin. The substrate 8 is covered with a sealing cover 9, and an inert gas is sealed inside.
Description
【０００１】[0001]
【産業上の利用分野】光ファイバジャイロの構造に関
し、特に光ファイバコイル内の温度分布の均一化に関す
る。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a structure of an optical fiber gyro, and more particularly to uniforming temperature distribution in an optical fiber coil.
【０００２】[0002]
【従来の技術】光ファイバジャイロは航空機、ロケット
等に搭載され、角速度を検出するのに用いられる。その
ブロック構成の一例を図２に示す。光源１の光は光カプ
ラ２，３を順次通って光ファイバコイル４に入射する。
光ファイバコイル４に入射した右回り光ＬR は光ファイ
バコイル４を通り光変調器５で位相変調された後、光カ
プラ３から光カプラ２へ戻される。一方光ファイバ４に
入射した左回り光ＬL は光変調器５で変調された後光フ
ァイバコイル４を通り、光カプラ３から光カプラ２に戻
される。光カプラ２に戻された右回り光ＬR と左回り光
ＬL との干渉光（その位相は入力角速度に対応する）が
光電変換器６で検出され、電気信号に変換される。その
電気信号Ｓａは信号処理回路７で処理されて入力角速度
に対応した信号Ｓｂが得られる。2. Description of the Related Art An optical fiber gyro is mounted on an aircraft, a rocket or the like and used to detect an angular velocity. An example of the block configuration is shown in FIG. The light from the light source 1 sequentially passes through the optical couplers 2 and 3 and enters the optical fiber coil 4.
The clockwise light L R incident on the optical fiber coil 4 passes through the optical fiber coil 4, is phase-modulated by the optical modulator 5, and is then returned from the optical coupler 3 to the optical coupler 2. On the other hand, the counterclockwise light L L incident on the optical fiber 4 is modulated by the optical modulator 5, passes through the optical fiber coil 4, and is returned from the optical coupler 3 to the optical coupler 2. The interference light (the phase of which corresponds to the input angular velocity) of the clockwise light L R and the counterclockwise light L L returned to the optical coupler 2 is detected by the photoelectric converter 6 and converted into an electric signal. The electric signal Sa is processed by the signal processing circuit 7 to obtain a signal Sb corresponding to the input angular velocity.
【０００３】図２の光ファイバジャイロは、図３に示す
ように、基板８上に実装され、カバー９で密封される。
基板８上の最大の部品は光ファイバコイル４であり、円
筒部と上鍔及び下鍔より成る糸巻状のボビン４ａに巻回
され、そのボビン４ａがリング状のスペーサ１０を介し
て、基板８上に取付けられる。光ファイバコイル４以外
の部品は、概ねボビン４ａの円筒部で囲まれた基板上に
直接或いは取付具を用いて中空部に立体的に取付けられ
る。光源は高温環境下では特性が劣化するのでペルチェ
素子１１で冷却される。該素子の放熱部は基板８に対接
されている。ペルチェ素子で奪った熱はその放熱部から
基板８を通って、基板８を取付ける機体１３に逃すよう
にしている。しかしペルチェ素子１１の放熱部は一般に
高温となっている。The optical fiber gyro of FIG. 2 is mounted on a substrate 8 and sealed by a cover 9 as shown in FIG.
The largest component on the substrate 8 is the optical fiber coil 4, which is wound around a bobbin 4a having a cylindrical portion and an upper collar and a lower collar, and the bobbin 4a is interposed via a ring-shaped spacer 10 Mounted on. Components other than the optical fiber coil 4 are three-dimensionally mounted on the substrate surrounded by the cylindrical portion of the bobbin 4a directly or in the hollow portion using a mounting tool. Since the characteristics of the light source deteriorate in a high temperature environment, the light source is cooled by the Peltier element 11. The heat dissipation portion of the device is in contact with the substrate 8. The heat taken by the Peltier element passes through the heat radiating portion through the substrate 8 and escapes to the machine body 13 to which the substrate 8 is attached. However, the heat radiation part of the Peltier element 11 is generally hot.
【０００４】[0004]
【発明が解決しようとする課題】外部環境の変化によっ
て、光ファイバジャイロを取付けている機体１３の温度
が上昇した場合、ペルチェ素子１１より基板８を伝導し
て機体１３に放散される熱の量が少くなり、基板８の温
度が著しく上昇する。そのとき、基板８の熱にスペーサ
１０からボビン４ａに伝導し、更に、光ファイバコイル
４に伝導して行く。その時光ファイバコイル４の基板８
に近い下側のＰｂ点の温度に対して基板８より遠い上側
のＰａ点の温度が低く、両点の間に大きな温度勾配が発
生する。When the temperature of the machine body 13 to which the optical fiber gyro is attached rises due to changes in the external environment, the amount of heat conducted from the Peltier element 11 through the substrate 8 and dissipated to the machine body 13. And the temperature of the substrate 8 rises significantly. At that time, the heat of the substrate 8 is conducted from the spacer 10 to the bobbin 4a, and further conducted to the optical fiber coil 4. At that time, the substrate 8 of the optical fiber coil 4
The temperature at the point Pb on the lower side close to the temperature is lower than the temperature at the point Pa on the upper side far from the substrate 8, and a large temperature gradient is generated between both points.
【０００５】このような温度勾配が光ファイバコイル４
内に発生すると、光ファイバコイルの右回り光と左回り
光との間に速度差が生じ、干渉光の位相が変化し、結果
として角速度の検出値に誤差を生ずる。この発明の目的
は、上記従来の問題を解決して、光ファイバ内の温度勾
配を小さくして、角速度の検出誤差を低減しようとする
ものである。Such temperature gradient causes the optical fiber coil 4
When it occurs inside the optical fiber coil, a velocity difference occurs between the clockwise light and the counterclockwise light of the optical fiber coil, the phase of the interference light changes, and as a result, an error occurs in the detected value of the angular velocity. An object of the present invention is to solve the above-mentioned conventional problems, reduce the temperature gradient in the optical fiber, and reduce the angular velocity detection error.
【０００６】[0006]
（１）請求項１の発明では、ボビン円筒部の高さＨｂ
（Ｈｂ＞Ｈ／２；Ｈはボビンの高さ）の内周面より一体
にフランジ２１が突設され、そのフランジを支持する支
持筒２２が基板上にほぼ直角に突設され、基板とボビン
の下鍔との間に空隙が形成される。(1) In the invention of claim 1, the height Hb of the bobbin cylindrical portion is
(Hb> H / 2; where H is the height of the bobbin), a flange 21 is integrally projected from the inner peripheral surface of the bobbin, and a support cylinder 22 for supporting the flange is projected substantially at a right angle on the substrate. A void is formed between the lower brim and the lower brim.
【０００７】（２）請求項２の発明では、前記（１）に
おいて、基板が熱伝導の良好な金属製とされる。 （３）請求項３の発明では、前記（１）において、支持
筒が基板と一体に形成されている。 （４）請求項４の発明では、前記（１）において、基板
に密閉用カバーが被せられ、その内部に不活性ガスが封
入されている。(2) In the invention of claim 2, in the above (1), the substrate is made of a metal having good heat conduction. (3) In the invention of claim 3, in (1), the support cylinder is formed integrally with the substrate. (4) In the invention of claim 4, in the above (1), the substrate is covered with a sealing cover, and an inert gas is sealed in the inside thereof.
【０００８】（５）請求項５の発明では、前記（１）に
おいて、基板の形状がほぼ円形とされる。(5) In the invention of claim 5, in the above (1), the shape of the substrate is substantially circular.
【０００９】[0009]
【実施例】光ファイバコイル４内の温度勾配を小さくす
るために、この発明を得る前の段階で初めに考えられた
光ファイバジャイロの構造を図１Ｂに、図３と対応する
部分に同じ符号を付けて示し、重複説明を省略する。図
１Ｂの場合には、ボビン４ａの円筒部の軸線方向のほぼ
真中にその内周面より一体にリング状のフランジ２１が
突設される。一方、基板８の上面より一体に（又は別部
材にて）、支持（円）筒２２が、ボビンの中心孔内に同
軸心状に、ほぼ直角に突設され、その上端とフランジ２
１の底面とが互いに固定され、光ファイバコイル４が支
持（円）筒２２で支持される。支持筒２２の基板８から
の高さＨａは、 Ｈａ≒Ｈ／２＋Δ−ｔ／２ …（１） に設定される。Ｈはボビン４ａの高さ、Δは基板８とボ
ビン４ａの下鍔との間に設定される空隙の寸法、ｔはフ
ランジ２１の厚さである。BEST MODE FOR CARRYING OUT THE INVENTION In order to reduce the temperature gradient in the optical fiber coil 4, the structure of an optical fiber gyro first considered in the stage before obtaining the present invention is shown in FIG. Are shown and the duplicate description is omitted. In the case of FIG. 1B, a ring-shaped flange 21 is integrally projecting from the inner peripheral surface of the cylindrical portion of the bobbin 4a at substantially the center in the axial direction. On the other hand, a support (circular) tube 22 is integrally (or separately) provided on the upper surface of the substrate 8 and is coaxially and coaxially projected in the center hole of the bobbin at a substantially right angle.
The bottom surface of 1 is fixed to each other, and the optical fiber coil 4 is supported by the supporting (circular) tube 22. The height Ha of the support cylinder 22 from the substrate 8 is set to Ha≈H / 2 + Δ−t / 2 (1). H is the height of the bobbin 4a, Δ is the size of the gap set between the substrate 8 and the lower flange of the bobbin 4a, and t is the thickness of the flange 21.
【００１０】このようにすると、ペルチェ素子１１で発
生した熱の一部は、基板８−支持筒２２−フランジ２１
−ボビン４ａ−コイル４の第１の経路で光ファイバコイ
ル４に伝導する。フランジ２１をボビン４ａの高さのほ
ぼ真中に設けた理由は、コイルの上側の点Ｐａと下側の
点Ｐｂとをフランジ２１よりほぼ等距離にすることによ
って、両点の温度上昇をほぼ同じにしようとしたためで
ある。By doing so, a part of the heat generated in the Peltier element 11 is part of the substrate 8-support cylinder 22-flange 21.
-Bobbin 4a-conducts to the fiber optic coil 4 in the first path of the coil 4. The reason why the flange 21 is provided approximately in the middle of the height of the bobbin 4a is that the temperature Pa at both points is substantially the same by making the upper point Pa and the lower point Pb of the coil substantially equidistant from the flange 21. Because I tried to
【００１１】図１Ｂの光ファイバジャイロを実験した結
果、従来の図３のものに比べればコイル内の温度勾配は
小さくなったが、しかし、なおかなり存在することが分
った。その原因の１つは、光ファイバジャイロの寸法を
小型にしなければならないため、基板８とボビン４ａと
の間の空隙の寸法Δをあまり大きくできないためであ
る。基板８の熱で、空隙（寸法Δ）の不活性ガスが高温
とされ、ボビン４ａの下鍔が熱くなり、下鍔と接する下
側のコイルに熱が伝導して行く（この熱の伝導経路を第
２の経路と呼ぶ）。このためどうしてもコイルのＰｂ点
の方がＰａ点より温度が高くなる。As a result of experimenting with the optical fiber gyro of FIG. 1B, it was found that the temperature gradient in the coil was smaller than that of the conventional one of FIG. 3, but it was still present. One of the causes is that the size of the optical fiber gyro has to be made small, and therefore the size Δ of the gap between the substrate 8 and the bobbin 4a cannot be made too large. The heat of the substrate 8 raises the temperature of the inert gas in the air gap (size Δ) to heat the lower flange of the bobbin 4a, and the heat is conducted to the lower coil in contact with the lower flange (this heat conduction path). Is called the second route). Temperature than the Pa point towards the point Pb of the order really coil increases.
【００１２】そこでこの発明では、ボビンのフランジ２
１の高さＨｂはＨｂ＞Ｈ／２に設定される。従来はＨｂ
≒Ｈ／２である。フランジ２１の基板８からの高さＨａ
は、 Ｈａ＝Ｈｂ＋Δ−ｔ／２ …（２） このようにすると、フランジ２１の位置がコイルの上側
のＰａ点に近づき下側のＰｂ点からは遠くなる。従っ
て、基板８−支持筒２２−フランジ２１−ボビン４ａ−
コイル４の第１の経路の熱伝導によって生ずるコイルの
温度上昇はＰａ点の方がＰｂ点より高くされる。Therefore, in this invention, the flange 2 of the bobbin is used.
The height Hb of 1 is set to Hb> H / 2. Conventionally Hb
≈H / 2. Height Ha of the flange 21 from the substrate 8
Ha = Hb + Δ−t / 2 (2) In this way, the position of the flange 21 approaches the Pa point on the upper side of the coil and becomes far from the Pb point on the lower side. Therefore, the board 8-support cylinder 22-flange 21-bobbin 4a-
The temperature rise of the coil caused by the heat conduction of the first path of the coil 4 is made higher at the point Pa than at the point Pb.
【００１３】従って、図１Ｂの例で述べた、基板８−空
隙（Δ）−ボビン（主に下鍔）４ａ−コイル４の第２の
経路の熱伝導による温度上昇とは逆の温度勾配となる。
従って、第１の経路と第２の経路の熱伝導の重畳によっ
てＰａ点とＰｂ点の温度上昇はほぼ同じとなり、コイル
内の温度勾配をほとんど無くすことができる。基板８に
は熱伝導のよい金属材料を用いるのが望ましい（請求項
２）。支持筒２２は温度上昇が繰返され、形状の歪が経
年的に増加する傾向にある。しかし支持筒２２を基板８
と同一材料で一体に形成することによって、その歪を軽
減することができる（請求項３）。しかし、場合によっ
ては、ねじ、接着剤等によって締結、一体化してもよ
い。カバー９内に不活性ガスを封入して内部の湿度を下
げ、部品の経年変化を抑え、光ファイバジャイロの寿命
を延ばすことができる（請求項４）。基板８の形状を光
ファイバコイル４と同心の円形にすると占有スペースが
節約できて望ましい（請求項５）。Therefore, a temperature gradient opposite to the temperature rise due to heat conduction in the second path of the substrate 8-gap (Δ) -bobbin (mainly lower collar) 4a-coil 4 described in the example of FIG. 1B is obtained. Become.
Therefore, the temperature rises at points Pa and Pb become almost the same due to the superposition of the heat conduction in the first and second paths, and the temperature gradient in the coil can be almost eliminated. It is desirable to use a metal material having good thermal conductivity for the substrate 8 (claim 2). The temperature of the support cylinder 22 is repeatedly increased, and the distortion of the shape tends to increase over time. However, the support cylinder 22 is attached to the substrate 8
The strain can be reduced by integrally forming the same material as the above (claim 3). However, depending on the case, they may be fastened and integrated with a screw, an adhesive, or the like. By enclosing an inert gas in the cover 9 to reduce the internal humidity, it is possible to suppress the secular change of components and extend the life of the optical fiber gyro (claim 4). It is desirable that the substrate 8 has a circular shape that is concentric with the optical fiber coil 4 because the occupied space can be saved (claim 5).
【００１４】[0014]
【発明の効果】この発明では、光ファイバコイル４の円
筒状ボビンの内周面にリング状のフランジ２１が突設さ
れ、その高さＨｂはボビンの高さＨの半分より大きく設
定され、そのフランジ２１を支持する支持筒２２が基板
８上に突設され、基板８とボビン４ａの下鍔との間に空
隙（寸法Δ）が設けられる。According to the present invention, the ring-shaped flange 21 is provided on the inner peripheral surface of the cylindrical bobbin of the optical fiber coil 4, and the height Hb thereof is set to be larger than half the height H of the bobbin. A support cylinder 22 that supports the flange 21 is provided on the substrate 8 in a protruding manner, and a space (size Δ) is provided between the substrate 8 and the lower flange of the bobbin 4a.
【００１５】基板８−支持筒２２−フランジ２１−ボビ
ン４ａ−コイル４の第１の経路と、基板８−空隙（Δ）
−ボビン（下鍔）４ａ−光コイル４の第２の経路とによ
ってそれぞれ生ずるコイルの上部と下部との間の温度勾
配が互いに逆になって、全体として温度勾配がほとんど
ないコイルが得られる。これにより光ファイバジャイロ
の角速度の温度勾配による誤差を大幅に低減することが
可能である。Substrate 8-support tube 22-flange 21-bobbin 4a-first path of coil 4, substrate 8-gap (Δ)
The temperature gradient between the upper part and the lower part of the coil, which are respectively caused by the bobbin (lower collar) 4a and the second path of the optical coil 4, are opposite to each other, so that a coil having almost no temperature gradient as a whole is obtained. This makes it possible to significantly reduce the error due to the temperature gradient of the angular velocity of the optical fiber gyro.
【図１】Ａはこの発明の実施例を示す断面図、Ｂはこの
発明を得る前の段階で提案された光ファイバジャイロの
断面図。1A is a sectional view showing an embodiment of the present invention, and FIG. 1B is a sectional view of an optical fiber gyro proposed in a stage before obtaining the present invention.
【図２】光ファイバジャイロのブロック図。FIG. 2 is a block diagram of an optical fiber gyro.
【図３】従来の光ファイバジャイロの断面図。FIG. 3 is a sectional view of a conventional optical fiber gyro.
Claims (5)
の両端の上鍔及び下鍔とより成る糸巻状のボビンに光フ
ァイバが巻回されている）が、基板上にほぼ直角に取付
けられ、前記円筒部に囲まれた前記基板の上面に、光フ
ァイバジャイロの光源を冷却する部材の放熱部が取付け
られている光ファイバジャイロの構造において、 前記円筒部の高さＨｂ（Ｈｂ＞Ｈ／２；Ｈはボビンの高
さ）の内周面より一体にフランジ（２１）が突設され、 そのフランジを支持する支持筒（２２）が前記基板上に
ほぼ直角に突設され、 前記基板とボビンの下鍔との間に空隙が形成されている
ことを特徴とする、 光ファイバジャイロの構造。1. A cylindrical optical fiber coil (an optical fiber is wound around a bobbin having a bobbin shape consisting of a cylindrical portion and upper and lower flanges at both ends thereof) is mounted on a substrate at a substantially right angle. In the structure of the optical fiber gyro in which the heat dissipation portion of the member for cooling the light source of the optical fiber gyro is attached to the upper surface of the substrate surrounded by the cylindrical portion, the height Hb of the cylindrical portion (Hb> H / 2; H is the height of the bobbin), a flange (21) is integrally projecting from the inner peripheral surface of the bobbin, and a support cylinder (22) for supporting the flange is projecting substantially orthogonally on the substrate, A structure of an optical fiber gyro, characterized in that an air gap is formed between the bobbin and the lower collar.
良好な金属製であることを特徴とする光ファイバジャイ
ロの構造。2. The structure of an optical fiber gyro according to claim 1, wherein the substrate is made of metal having good heat conduction.
板と一体に形成されていることを特徴とする光ファイバ
ジャイロの構造。3. The structure of an optical fiber gyro according to claim 1, wherein the support cylinder is formed integrally with the substrate.
バーが被せられ、その内部に不活性ガスが封入されてい
ることを特徴とする光ファイバジャイロの構造。4. The structure of an optical fiber gyro according to claim 1, wherein the substrate is covered with a sealing cover, and an inert gas is sealed inside the cover.
ぼ円形であることを特徴とする光ファイバジャイロの構
造。5. The structure of an optical fiber gyro according to claim 1, wherein the substrate has a substantially circular shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11972995A JP2838123B2 (en) | 1995-05-18 | 1995-05-18 | Optical fiber gyro structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11972995A JP2838123B2 (en) | 1995-05-18 | 1995-05-18 | Optical fiber gyro structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH08313270A true JPH08313270A (en) | 1996-11-29 |
| JP2838123B2 JP2838123B2 (en) | 1998-12-16 |
Family
ID=14768684
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP11972995A Expired - Lifetime JP2838123B2 (en) | 1995-05-18 | 1995-05-18 | Optical fiber gyro structure |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2838123B2 (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2363639B (en) * | 1999-03-24 | 2003-07-23 | Bookham Technology Plc | A sealed fibre optic gyroscope assembly |
| 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 |
| CN103115621A (en) * | 2013-01-17 | 2013-05-22 | 北京航空航天大学 | Optical fiber gyroscope sensing ring device for petroleum gradiograph |
| CN103674004A (en) * | 2012-09-07 | 2014-03-26 | 中国航空工业第六一八研究所 | Triaxial fiber gyroscope assembly and mounting bracket thereof |
-
1995
- 1995-05-18 JP JP11972995A patent/JP2838123B2/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2363639B (en) * | 1999-03-24 | 2003-07-23 | Bookham Technology Plc | A sealed fibre optic gyroscope assembly |
| CN103674004A (en) * | 2012-09-07 | 2014-03-26 | 中国航空工业第六一八研究所 | Triaxial fiber gyroscope assembly and mounting bracket thereof |
| 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 |
| CN103115621A (en) * | 2013-01-17 | 2013-05-22 | 北京航空航天大学 | Optical fiber gyroscope sensing ring device for petroleum gradiograph |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2838123B2 (en) | 1998-12-16 |
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