JPH08327363A - Angular velocity sensor - Google Patents
Angular velocity sensorInfo
- Publication number
- JPH08327363A JPH08327363A JP7131351A JP13135195A JPH08327363A JP H08327363 A JPH08327363 A JP H08327363A JP 7131351 A JP7131351 A JP 7131351A JP 13135195 A JP13135195 A JP 13135195A JP H08327363 A JPH08327363 A JP H08327363A
- Authority
- JP
- Japan
- Prior art keywords
- angular velocity
- signal
- mechanical coupling
- velocity sensor
- output
- 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
Landscapes
- Gyroscopes (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は角速度センサに関するも
のである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an angular velocity sensor.
【0002】[0002]
【従来の技術】例えば音叉形の角速度センサは、音叉形
の駆動部の両駆動板の先端に、それとは直交する方向に
検知板を設け、前記駆動板を常時音叉駆動させた状態で
角速度が加わると、それに呼応して互いに逆方向に振動
する前記検知板からの出力で角速度を検出するものであ
った。2. Description of the Related Art For example, a tuning fork type angular velocity sensor is provided with a detection plate at the tip of both drive plates of a tuning fork type drive section in a direction orthogonal to the drive plates, and the angular velocity is kept constant while the drive plates are constantly driven. When added, the angular velocity is detected by the output from the detection plate which vibrates in the opposite directions in response thereto.
【0003】[0003]
【発明が解決しようとする課題】前記従来例において問
題となるのは、センサ起動後、特性が安定動作に達して
利用が可能かどうかを検知する機能、あるいはまた角速
度センサの取付体、例えば車が衝突する等して大きな衝
撃が加わる結果としてその一部が損傷し、正常な検知動
作ができなくなってしまっているのを検知すべき機能を
備えていないことであった。そこで本発明は角速度セン
サにおいて、その一部が損傷して正常な検知動作ができ
なくなっている状態を検出することができるようにし、
かつセンサの起動後、出力が安定するタイミングを検出
できる為、従来よりも素早い使用を可能にする事を目的
とするものである。A problem in the above-mentioned conventional example is a function of detecting whether or not the characteristics reach stable operation after the sensor is activated, or an attachment body of an angular velocity sensor, for example, a vehicle. As a result of a large impact such as a collision with a part of the part, the part is damaged and a normal detection operation cannot be performed. Therefore, the present invention makes it possible to detect a state in which a part of the angular velocity sensor is damaged and a normal detection operation cannot be performed,
Moreover, since the timing at which the output stabilizes after the activation of the sensor can be detected, the purpose is to enable quicker use than before.
【0004】[0004]
【課題を解決するための手段】そしてこの目的を達成す
る為に本発明は、振動部とこの振動部を駆動振動させる
為の駆動手段と角速度を検出する検出手段からなる検知
体と、この検知体から角速度出力を取り出す出力端子と
を備え、前記検知体から得られる角速度出力以外の機械
結合信号を検知してモニター信号とするものである。In order to achieve this object, the present invention relates to a vibrating portion, a driving means for driving and vibrating the vibrating portion, and a detection body including a detecting means for detecting an angular velocity, and this detection means. An output terminal for extracting an angular velocity output from the body is provided, and a mechanical coupling signal other than the angular velocity output obtained from the detection body is detected and used as a monitor signal.
【0005】[0005]
【作用】以上の構成とすれば、構成上必ず検知体から得
られる機械結合信号をモニター信号とすることにより、
この角速度信号が正常な検知動作ができる状態にあるの
か否かを検知することができるようになり、しかも機械
結合信号は必ず発生するものであるので、この機械結合
信号を発生させるための手段を別個に設ける必要がな
く、その分構成がきわめてシンプルで、モニターに対す
る信頼性の高いものとすることができるばかりでなく、
センサ起動後、特性が安定するタイミングを知ることが
でき、起動後、より早くセンサ出力を利用できるように
なる。With the above configuration, by using the mechanical coupling signal that is always obtained from the detector as the monitor signal in the configuration,
It becomes possible to detect whether or not this angular velocity signal is in a state in which normal detection operation is possible, and since the mechanical coupling signal is always generated, a means for generating this mechanical coupling signal should be provided. Not only it does not have to be provided separately, but its configuration is extremely simple and reliable for the monitor.
After the sensor is activated, the timing at which the characteristics become stable can be known, and the sensor output can be used sooner after the activation.
【0006】[0006]
【実施例】図1において1は樹脂製よりなる一端が開口
したケースで、このケース1の開口部に樹脂製の蓋2が
装着されることにより密封空間が形成されている。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS In FIG. 1, reference numeral 1 denotes a case made of resin and having one end opened, and a lid 2 made of resin is attached to the opening of the case 1 to form a sealed space.
【0007】この密封空間の内部には、回路基板3と、
金属製のウェイト板4が収納されている。すなわち、ケ
ース1の内部四隅には支持ピン5が植設されており、こ
の支持ピン5によりウェイト板4と回路基板3が弾性的
に支持、固定されている。ウェイト板4にはこの弾性支
持のために、四隅にゴム製のダンパー6が装着されてお
り、またこのダンパー6と回路基板3の間には樹脂製の
支持脚7が設けられ、支持ピン5は下方よりダンパー
6、支持脚7、回路基板3を貫通後、その先端が回路基
板3側に押し潰されており、これにより回路基板3、ウ
ェイト板4は弾性的に支持、固定されている。また、ウ
ェイト板4の回路基板3側には図2に示す如く、金属製
の支持ピン8が垂直方向に圧入、固定されており、この
支持ピン8の上部には水平方向に金属製の支持ピン9の
一端が圧入、固定されている。この支持ピン9の径は支
持ピン8の径の約5分の1と細く、しかも材質はピアノ
線などの様にバネ性を持つ金属材料で形成されており、
その他端に金属製の基板10がはんだにより固定されて
いる。Inside the sealed space, the circuit board 3 and
A weight plate 4 made of metal is stored. That is, the support pins 5 are planted at the four inner corners of the case 1, and the weight plate 4 and the circuit board 3 are elastically supported and fixed by the support pins 5. In order to elastically support the weight plate 4, dampers 6 made of rubber are attached to the four corners, and support legs 7 made of resin are provided between the damper 6 and the circuit board 3, and the support pins 5 are provided. Has penetrated the damper 6, the support leg 7, and the circuit board 3 from below, and its tip is crushed toward the circuit board 3 side, whereby the circuit board 3 and the weight plate 4 are elastically supported and fixed. . As shown in FIG. 2, metal support pins 8 are vertically press-fitted and fixed to the weight plate 4 on the circuit board 3 side, and metal support pins 8 are horizontally supported on the support pins 8 in the horizontal direction. One end of the pin 9 is press-fitted and fixed. The diameter of the support pin 9 is as small as about one fifth of the diameter of the support pin 8, and the material is made of a metallic material having a spring property such as a piano wire.
A metal substrate 10 is fixed to the other end by soldering.
【0008】この基板10の支持ピン8,9を挟む両側
には金属製の駆動板11,12の一端が固定され、さら
にそれらの表面には板状の圧電素子11a,12aが固
定され、これにより音叉形の駆動部が形成されている。
また、駆動板11,12の他端は図2に示す如く、圧電
素子11a,12a部とは直交する方向に折り曲げら
れ、その後延長形成された検知板13,14に板状の圧
電素子13a,14aが固定され、これにより検知部が
構成されている。One end of metal drive plates 11 and 12 is fixed on both sides of the support pin 8 and 9 of the substrate 10, and plate-shaped piezoelectric elements 11a and 12a are fixed to the surfaces thereof. Thereby forming a tuning fork-shaped drive unit.
Further, as shown in FIG. 2, the other ends of the drive plates 11 and 12 are bent in a direction orthogonal to the piezoelectric elements 11a and 12a, and then the detection plates 13 and 14 formed by extension are plate-shaped piezoelectric elements 13a and 13a. 14a is fixed, and the detector is configured by this.
【0009】図3は制御回路を示し、駆動板11の圧電
素子11aにはドライバ15から約1VP-P、1.5kH
zの交流信号が印加される。これにより、駆動板11,
12には支持ピン9に対して内外方向に音叉振動を始め
る。駆動板12の圧電素子12aは音叉振動により、印
加信号に比例した電圧が誘起され、それはカレントアン
プ16、バンドパスフィルタ17を通過し、図4のA点
信号となる。これは次に全波整流器18、AGC回路1
9を介してドライバ15にフィードバックされ、駆動信
号のAGC制御が行われている。検知部においては、圧
電素子13a,14aが角速度を検知すると、圧電素子
13a,14aは共に+Qの角速度信号を出力し、その
様子は図4のB,Cに角速度信号として示されており、
これは図3のD点において合成され、図4のDの様な角
速度信号となる。この角速度信号は次にチャージアンプ
20、バンドパスフィルタ21、同期検波22、ローパ
スフィルタ23を介して出力端子24から出力される。
その間のE点、F点、G点の信号波形は図4のE,F,
Gに角速度信号として示されている。FIG. 3 shows a control circuit, in which the piezoelectric element 11a of the driving plate 11 has a voltage of about 1 V PP , 1.5 kHz from the driver 15.
An AC signal of z is applied. As a result, the drive plate 11,
At 12, a tuning fork vibration starts inward and outward with respect to the support pin 9. A voltage proportional to the applied signal is induced in the piezoelectric element 12a of the drive plate 12 by the tuning fork vibration, which passes through the current amplifier 16 and the bandpass filter 17 and becomes the signal A in FIG. This is followed by full wave rectifier 18, AGC circuit 1
It is fed back to the driver 15 via 9, and the AGC control of the drive signal is performed. In the detection unit, when the piezoelectric elements 13a and 14a detect the angular velocity, the piezoelectric elements 13a and 14a both output an angular velocity signal of + Q, which is shown in FIGS. 4B and 4C as the angular velocity signal.
This is synthesized at point D in FIG. 3 and becomes an angular velocity signal as shown in D in FIG. This angular velocity signal is then output from the output terminal 24 via the charge amplifier 20, the bandpass filter 21, the synchronous detection 22, and the lowpass filter 23.
The signal waveforms at points E, F, and G in the meantime are E, F, and
It is shown in G as an angular velocity signal.
【0010】さて、本実施例においては、駆動板11,
12に対して検知板13,14を直交する方向に設けな
ければならないが、真にこれを直交方向とすることは実
質的に困難で、しかも圧電素子13a,14aの大きさ
やその取り付け方も全く同じものとする事ができないの
で、その結果として圧電素子13a,14aからは常時
図4のB,Cに示す機械結合信号が発生してしまう。こ
の場合圧電素子13a,14a側は検知板13,14の
同一面に貼りつけており、検知板13,14の重心が若
干圧電素子13a,14a貼付側にずれるため、駆動板
11,12が音叉振動する場合に、例えば外方に広がる
場合、圧電素子13a,14a側にたわんで広がること
になる。従ってこれらの圧電素子13a,14aに発生
する機械結合信号は図4のB,Cの如く逆相の状態とな
るので、図3のD点においてはその機械結合信号が合成
された場合には、機械結合信号は小さくなる。この機械
結合信号はチャージアンプ20、増幅器25で増幅した
後、整流器26で整流され、その後平滑器27で平滑
後、判定器28でレベル判定が行われ、モニター信号端
子29からその判定結果が出力される。図3のH,I,
J各点の出力は図4にそれぞれ示している。即ち、平滑
器27の出力Iがa,b間にある時には、モニター信号
端子29の出力は図4のJに示す如くローレベルとな
る。これに対して例えば図3に示す検知板14が破損も
しくはそのリード線などが断線した場合には図4のCに
示す如く、角速度信号も機械結合信号もゼロレベルとな
ってしまう。この結果D点においては圧電素子13aか
らだけの機械結合信号が発生することとなり、今までよ
りもはるかに大きな機械結合信号レベルとなってしま
う。従ってこの時には平滑器27の出力は図4のIに示
す如く、a点より大きくなり、この結果判定器28から
は、図4のJに示す如くハイレベルの出力が発生する事
となる。また検知板13,14両方が損傷したり、両方
のリード線が断線した場合などには平滑器27の出力は
図4のIのb点よりも小さく、この時にも判定器28の
出力はハイレベルの出力を出すことになる。そしてこの
様なハイレベルの出力が出た場合には、この角速度セン
サが故障したとして使用機器へ情報伝達をする。In the present embodiment, the drive plates 11,
Although the detection plates 13 and 14 must be provided in a direction orthogonal to the position 12, it is practically difficult to make this a true orthogonal direction, and the size of the piezoelectric elements 13a and 14a and the mounting method thereof are completely different. Since they cannot be the same, as a result, the mechanical coupling signals shown in B and C of FIG. 4 are always generated from the piezoelectric elements 13a and 14a. In this case, the piezoelectric elements 13a and 14a are attached to the same surface of the detection plates 13 and 14, and the centers of gravity of the detection plates 13 and 14 are slightly shifted to the attachment sides of the piezoelectric elements 13a and 14a, so that the drive plates 11 and 12 are tuned. When it vibrates, for example, when it spreads outward, it flexes and spreads toward the piezoelectric elements 13a and 14a. Therefore, the mechanical coupling signals generated in these piezoelectric elements 13a and 14a are in the opposite phases as shown in B and C of FIG. 4, and therefore, when the mechanical coupling signals are combined at point D of FIG. The mechanical coupling signal is small. The mechanical coupling signal is amplified by the charge amplifier 20 and the amplifier 25, rectified by the rectifier 26, smoothed by the smoother 27, and then level-determined by the determiner 28, and the determination result is output from the monitor signal terminal 29. To be done. H, I, in FIG.
The output of each J point is shown in FIG. That is, when the output I of the smoother 27 is between a and b, the output of the monitor signal terminal 29 becomes a low level as indicated by J in FIG. On the other hand, for example, when the detection plate 14 shown in FIG. 3 is damaged or its lead wire is broken, both the angular velocity signal and the mechanical coupling signal become zero level, as shown in C of FIG. As a result, at point D, a mechanical coupling signal is generated only from the piezoelectric element 13a, and the mechanical coupling signal level becomes much higher than before. Therefore, at this time, the output of the smoother 27 becomes larger than the point a as shown by I in FIG. 4, and as a result, the decision unit 28 produces a high level output as shown by J in FIG. When both the detection plates 13 and 14 are damaged or both lead wires are broken, the output of the smoother 27 is smaller than the point b of I in FIG. 4, and the output of the determiner 28 is high at this time as well. It will output the level. When such a high level output is output, it is determined that the angular velocity sensor has failed and information is transmitted to the device used.
【0011】図5は他の実施例を示し、この実施例にお
いては増幅器25と、平滑器27の間に同期検波器30
を介在させ、駆動信号のフィードバック回路のフィード
バック信号、つまり図5のA点より位相器31を介した
信号により、同期検波を行うものである。すなわち増幅
器25に流入する機械結合信号中には、角速度信号も混
入しているので、この角速度信号をキャンセルし、機械
結合信号レベルを正確な値に近づけるものである。その
為に上述の如く、図5のA点に流れる図6のAの信号を
位相器31で90度位相を遅らせ、この90度位相遅れ
のある信号で、増幅器25からの出力を同期検波すれ
ば、図6のIに示す如く角速度信号がキャンセルされ、
機械結合信号レベルを正確な値に近づける事ができるの
である。FIG. 5 shows another embodiment. In this embodiment, a synchronous detector 30 is provided between an amplifier 25 and a smoother 27.
, The synchronous detection is performed by the feedback signal of the drive signal feedback circuit, that is, the signal from the point A in FIG. That is, since the angular velocity signal is also mixed in the mechanical coupling signal flowing into the amplifier 25, this angular velocity signal is canceled to bring the mechanical coupling signal level close to an accurate value. Therefore, as described above, the signal of A in FIG. 6 flowing to the point A in FIG. 5 is delayed by 90 degrees in the phase shifter 31, and the output from the amplifier 25 is synchronously detected by the signal having the 90 degree phase delay. For example, the angular velocity signal is canceled as shown by I in FIG.
The mechanical coupling signal level can be brought close to an accurate value.
【0012】図7は他の実施例を示し、この実施例にお
いては初期設定として、圧電素子13a,14aから得
られる機械結合信号を図7のD点で加算した場合、0と
なる様にしたものである。すなわち、図3、図5に示す
ものは、この加算が0以外の状態になっていたのに対
し、この実施例においては検知板13あるいは14をト
リミングすることにより、圧電素子13a,14aから
生じる機械結合信号を加算したものを0に初期設定する
ものである。図8のDはそれを示しており、例えば検知
板14が損傷したり、リード線が外れたりするまでは機
械結合信号は発生していない。しかし、この故障以後は
圧電素子14aからの機械結合信号が発生しなくなるの
で、図8のDの如く機械結合信号が現出することにな
る。この結果、図8のJに示す如く、判定器28の出力
はハイレベルとなり、これが論理和回路32を介してモ
ニター信号端子29から図8のLに示す如く角速度セン
サが故障したことを知らせる信号が出力されることにな
る。また、本実施例においては論理和回路32に判定器
33を介して駆動信号のフィードバック信号、つまり全
波整流器18の出力を供給する様にしている。これは、
本実施例において、駆動板11,12が駆動されていな
い時にもモニター信号端子29から故障を報知できる様
にするためのものである。その為に本実施例では、駆動
信号を判定器33を介して論理和回路32へ供給するこ
とにしたものであり、判定器33はこのフィードバック
信号が0の時にハイレベルを出力し、これが論理和回路
32を介してモニター信号端子29から出力され故障を
報知することができるのである。図9は他の実施例を示
し、この実施例においても圧電素子13a,14aから
得られる機械結合信号を加算した場合0となる様に検知
板13あるいは14をトリミングして初期設定してい
る。そして圧電素子13aからの信号はチャージアンプ
20aで増幅し、また圧電素子14aの信号はチャージ
アンプ20bで増幅し、それらを加算器34で加算した
ものが、その後の処理により出力端子24から角速度出
力として取出される。また、減算器35にてチャージア
ンプ20aの出力からチャージアンプ20bの出力を減
算したものが、その後の処理により、モニター信号端子
29からモニター信号として出力される様になってい
る。なお各部の波形は図10に示している。なお上記実
施例においては、いくつかの例を示したが、増幅器2
5、整流器26、平滑器27は省いても良い。また音叉
形の角速度センサを用いて説明したが、三角柱タイプ、
円柱タイプ、音片タイプ、円筒タイプ、の角速度センサ
においても機械結合信号が必ず発生するので、この機械
結合信号を用いて故障検出をすることができる。FIG. 7 shows another embodiment. In this embodiment, as an initial setting, the mechanical coupling signals obtained from the piezoelectric elements 13a and 14a are set to 0 when added at point D in FIG. It is a thing. That is, while the addition shown in FIGS. 3 and 5 is in a state other than 0, in this embodiment, the detection plates 13 or 14 are trimmed to generate the piezoelectric elements 13a and 14a. The sum of the mechanical coupling signals is initialized to 0. FIG. 8D shows that, for example, the mechanical coupling signal is not generated until the detection plate 14 is damaged or the lead wire is disconnected. However, after this failure, the mechanical coupling signal is not generated from the piezoelectric element 14a, so that the mechanical coupling signal appears as shown in D of FIG. As a result, as shown in J of FIG. 8, the output of the determiner 28 becomes high level, and this is a signal from the monitor signal terminal 29 via the logical sum circuit 32 to inform that the angular velocity sensor has failed as shown in L of FIG. Will be output. Further, in the present embodiment, the feedback signal of the drive signal, that is, the output of the full-wave rectifier 18 is supplied to the OR circuit 32 via the determiner 33. this is,
In the present embodiment, the purpose is to notify the failure from the monitor signal terminal 29 even when the drive plates 11 and 12 are not driven. Therefore, in the present embodiment, the drive signal is supplied to the logical sum circuit 32 through the judging device 33, and the judging device 33 outputs a high level when the feedback signal is 0, which is a logical value. The failure can be notified by being output from the monitor signal terminal 29 via the summing circuit 32. FIG. 9 shows another embodiment. Also in this embodiment, the detection plate 13 or 14 is trimmed and initialized so that it becomes 0 when the mechanical coupling signals obtained from the piezoelectric elements 13a and 14a are added. The signal from the piezoelectric element 13a is amplified by the charge amplifier 20a, the signal from the piezoelectric element 14a is amplified by the charge amplifier 20b, and the signals obtained by adding them by the adder 34 are output from the output terminal 24 from the angular velocity output. Is taken out as. Further, the subtractor 35 subtracts the output of the charge amplifier 20b from the output of the charge amplifier 20a, and the subsequent processing outputs the monitor signal from the monitor signal terminal 29 as a monitor signal. The waveform of each part is shown in FIG. Although some examples have been shown in the above embodiment, the amplifier 2
5, the rectifier 26 and the smoother 27 may be omitted. Also, I explained using a tuning fork type angular velocity sensor, but it is a triangular prism type,
Since the mechanical coupling signal is always generated in the cylindrical type, the sound piece type, and the cylindrical type angular velocity sensors, the failure can be detected using the mechanical coupling signal.
【0013】[0013]
【発明の効果】以上の様に本発明は振動部とこの振動部
を駆動振動させる為の駆動手段と角速度を検出する検出
手段からなる検知体と、この検知体から角速度出力を取
り出す出力端子とを備え、前記検知体から得られる角速
度出力以外の機械結合信号を検知してモニター信号とす
るものである。そして以上の構成とすれば、構成上必ず
検知体から得られる機械結合信号をモニター信号とする
ことにより、この角速度信号が正常な検知動作ができる
状態にあるのか否かを検知することができるようにな
り、しかも機械結合信号は必ず発生するものであるの
で、この機械結合信号を発生させるための手段を別個に
設ける必要がなく、その分構成が極めてシンプルで、モ
ニターに対する信頼性の高いものとすることができる。As described above, according to the present invention, the vibrating portion, the driving means for driving and vibrating the vibrating portion, and the detecting body including the detecting means for detecting the angular velocity, and the output terminal for extracting the angular velocity output from the detecting body. And a mechanical coupling signal other than the angular velocity output obtained from the detection body is detected and used as a monitor signal. With the above configuration, it is possible to detect whether or not this angular velocity signal is in a state where normal detection operation can be performed by using the mechanical coupling signal obtained from the detection body as a monitor signal without fail in the configuration. In addition, since the mechanical coupling signal is always generated, it is not necessary to separately provide a means for generating the mechanical coupling signal, and the configuration is extremely simple for that, and the monitor is highly reliable. can do.
【図1】本発明の一実施例の分解斜視図FIG. 1 is an exploded perspective view of an embodiment of the present invention.
【図2】図1の要部の拡大斜視図FIG. 2 is an enlarged perspective view of a main part of FIG.
【図3】図1の制御回路図3 is a control circuit diagram of FIG.
【図4】図3の波形図FIG. 4 is a waveform diagram of FIG.
【図5】本発明の他の実施例の制御回路図FIG. 5 is a control circuit diagram of another embodiment of the present invention.
【図6】図5の波形図6 is a waveform diagram of FIG.
【図7】本発明の更に他の実施例の制御回路図FIG. 7 is a control circuit diagram of still another embodiment of the present invention.
【図8】図7の波形図8 is a waveform diagram of FIG. 7.
【図9】本発明の更に他の実施例の制御回路図FIG. 9 is a control circuit diagram of still another embodiment of the present invention.
【図10】図9の波形図10 is a waveform diagram of FIG.
11 駆動板 11a 圧電素子 12 駆動板 12a 圧電素子 13 検知板 13a 圧電素子 14 検知板 14a 圧電素子 24 出力端子 29 モニター信号端子 11 Drive Plate 11a Piezoelectric Element 12 Drive Plate 12a Piezoelectric Element 13 Detection Plate 13a Piezoelectric Element 14 Detection Plate 14a Piezoelectric Element 24 Output Terminal 29 Monitor Signal Terminal
Claims (12)
の駆動手段と角速度を検出する検出手段からなる検知体
と、この検知体から角速度出力を取り出す出力端子とを
備え、前記検知体から得られる角速度出力以外の機械結
合信号を検知してモニター信号とする角速度センサ。1. A detection body comprising a vibrating portion, a driving means for driving and vibrating the vibrating portion, and a detection means for detecting an angular velocity, and an output terminal for extracting an angular velocity output from the detection body. An angular velocity sensor that detects mechanical coupling signals other than the obtained angular velocity output and uses them as monitor signals.
部を構成する両方の駆動板の先端に、それとは直交する
方向に設けられた検知板とにより構成した請求項1に記
載の角速度センサ。2. The detector according to claim 1, wherein the detector is composed of a tuning fork-shaped drive portion and a detection plate provided at the tips of both drive plates constituting the drive portion in a direction orthogonal to the drive plates. Angular velocity sensor.
る請求項1記載の角速度センサ。3. The angular velocity sensor according to claim 1, wherein the vibrating portion is made of a material having piezoelectricity.
械結合に起因する機械結合信号を検知してモニター信号
とする請求項2または3に記載の角速度センサ。4. The angular velocity sensor according to claim 2, wherein a mechanical coupling signal resulting from mechanical coupling between the sensing plate and the drive plate is detected from the sensing plate and used as a monitor signal.
信号成分を検知してモニター信号とする請求項4に記載
の角速度センサ。5. The angular velocity sensor according to claim 4, wherein a mechanical coupling signal component is detected from a signal obtained from the output terminal and is used as a monitor signal.
ニター信号とする請求項1または4または5に記載の角
速度センサ。6. The angular velocity sensor according to claim 1, wherein the decrease in the level of the mechanical coupling signal is detected and used as a monitor signal.
をチャージアンプで増幅、整流、平滑後、判定回路に供
給する構成とした請求項4または5に記載の角速度セン
サ。7. The angular velocity sensor according to claim 4, wherein the mechanically coupled signals obtained from the two detectors are amplified by a charge amplifier, rectified, smoothed, and then supplied to a determination circuit.
の和を0以外の所定値に初期設定する構成とした請求項
6または7に記載の角速度センサ。8. The angular velocity sensor according to claim 6, wherein the sum of the mechanical coupling signals obtained from the two detectors is initialized to a predetermined value other than zero.
の和を0に初期設定する構成とした請求項7に記載の角
速度センサ。9. The angular velocity sensor according to claim 7, wherein the sum of mechanical coupling signals obtained from the two detection plates is initialized to 0.
出力を論理和回路に供給する構成とした請求項9に記載
の角速度センサ。10. The angular velocity sensor according to claim 9, wherein the determination circuit output of the drive section and the monitor signal output are supplied to an OR circuit.
号の和を0以外の所定値に初期設定するとともに、これ
らの検知板から得られた機械結合信号をチャージアンプ
で増幅し、このチャージアンプで増幅された機械結合信
号を駆動信号のフィードバック回路に流れるフィードバ
ック信号を90度位相器で位相変換した信号により同期
検波し平滑後、判定回路に供給する構成とした請求項4
または5または6に記載の角速度センサ。11. The sum of mechanical coupling signals obtained from two detection plates is initialized to a predetermined value other than 0, and the mechanical coupling signals obtained from these detection plates are amplified by a charge amplifier. 5. The structure in which the mechanically coupled signal amplified by the signal is synchronously detected by a signal obtained by phase-converting a feedback signal flowing through a feedback circuit of a drive signal by a 90-degree phase shifter, and smoothed, and then supplied to the determination circuit.
Or the angular velocity sensor described in 5 or 6.
号の和を0に初期設定するとともに、2つの検知板から
得られる機械結合信号をそれぞれ別のチャージアンプで
増幅し、これら別のチャージアンプの出力を引き算した
信号を整流、平滑後、判定回路に供給する構成にした請
求項4に記載の角速度センサ。12. The sum of the mechanical coupling signals obtained from the two detection plates is initialized to 0, and the mechanical coupling signals obtained from the two detection plates are amplified by different charge amplifiers, respectively, and these different charge amplifiers are amplified. The angular velocity sensor according to claim 4, wherein the signal obtained by subtracting the output of (1) is rectified and smoothed, and then supplied to the determination circuit.
Priority Applications (17)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP13135195A JP3430711B2 (en) | 1995-05-30 | 1995-05-30 | Angular velocity sensor |
EP01121470A EP1174683B1 (en) | 1995-05-30 | 1996-05-29 | Angular velocity sensor |
CN96190557.3A CN1090313C (en) | 1995-05-30 | 1996-05-29 | Angular velocity sensor |
CNB011355921A CN1160574C (en) | 1995-05-30 | 1996-05-29 | Angular-rate sensor |
PCT/JP1996/001445 WO1996038712A1 (en) | 1995-05-30 | 1996-05-29 | Angular velocity sensor |
US08/776,443 US5939630A (en) | 1995-05-30 | 1996-05-29 | Angular velocity sensor |
DE69622815T DE69622815T2 (en) | 1995-05-30 | 1996-05-29 | ROTARY SPEED SENSOR |
DE69637287T DE69637287T2 (en) | 1995-05-30 | 1996-05-29 | Angular rate sensor |
EP96919991A EP0773430B1 (en) | 1995-05-30 | 1996-05-29 | Angular velocity sensor |
CNB011355913A CN1142436C (en) | 1995-05-30 | 1996-05-29 | Angular-rate sensor |
US09/332,161 US6089091A (en) | 1995-05-30 | 1999-06-14 | Angular velocity sensor |
US09/332,162 US6244095B1 (en) | 1995-05-30 | 1999-06-14 | Angular velocity sensor |
US09/811,786 US6705151B2 (en) | 1995-05-30 | 2001-03-20 | Angular velocity sensor |
US10/300,937 US6732586B2 (en) | 1995-05-30 | 2002-11-21 | Angular velocity sensor |
US10/614,025 US6912901B1 (en) | 1995-05-30 | 2003-07-08 | Angular velocity sensor |
US10/614,026 US6959584B2 (en) | 1995-05-30 | 2003-07-08 | Angular velocity sensor |
US11/233,014 US7043988B2 (en) | 1995-05-30 | 2005-09-23 | Angular velocity sensor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP13135195A JP3430711B2 (en) | 1995-05-30 | 1995-05-30 | Angular velocity sensor |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH08327363A true JPH08327363A (en) | 1996-12-13 |
JP3430711B2 JP3430711B2 (en) | 2003-07-28 |
Family
ID=15055909
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP13135195A Expired - Fee Related JP3430711B2 (en) | 1995-05-30 | 1995-05-30 | Angular velocity sensor |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP3430711B2 (en) |
Cited By (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1999066289A1 (en) * | 1998-06-15 | 1999-12-23 | Matsushita Electric Industrial Co., Ltd. | Angular velocity sensor |
JP2002267448A (en) * | 2001-03-09 | 2002-09-18 | Matsushita Electric Ind Co Ltd | Angular velocity sensor |
WO2009122739A1 (en) * | 2008-04-04 | 2009-10-08 | パナソニック株式会社 | Sensor device |
KR100950387B1 (en) * | 2008-04-04 | 2010-03-29 | 파나소닉 주식회사 | Sensor apparatus |
JP2010107416A (en) * | 2008-10-31 | 2010-05-13 | Epson Toyocom Corp | Angular velocity detecting device and method of manufacturing the same |
US7730782B2 (en) | 2008-04-04 | 2010-06-08 | Panasonic Corporation | Sensor device |
US7746091B2 (en) | 2008-10-16 | 2010-06-29 | Panasonic Corporation | Sensor apparatus |
JP2010169408A (en) * | 2009-01-20 | 2010-08-05 | Epson Toyocom Corp | Physical quantity detection device |
JP2010169409A (en) * | 2009-01-20 | 2010-08-05 | Epson Toyocom Corp | Physical quantity detection device |
US7865284B2 (en) | 2004-04-21 | 2011-01-04 | Panasonic Corporation | Angular velocity sensor and transporting equipment |
WO2011030541A1 (en) * | 2009-09-14 | 2011-03-17 | パナソニック株式会社 | Angular velocity sensor |
US8131507B2 (en) | 2009-02-05 | 2012-03-06 | Panasonic Corporation | Sensor apparatus |
US8131508B2 (en) | 2009-02-05 | 2012-03-06 | Panasonic Corporation | Sensor apparatus |
JP2012211872A (en) * | 2011-03-31 | 2012-11-01 | Denso Corp | Sensor apparatus |
US8322214B2 (en) | 2008-04-04 | 2012-12-04 | Panasonic Corporation | Sensor device |
JP2014016356A (en) * | 2013-09-05 | 2014-01-30 | Seiko Epson Corp | Method for manufacturing angular velocity detection device |
JP2015118102A (en) * | 2015-02-16 | 2015-06-25 | セイコーエプソン株式会社 | Method for manufacturing angular velocity detection device |
US10746809B2 (en) | 2017-09-28 | 2020-08-18 | Seiko Epson Corporation | Physical quantity measurement device, electronic apparatus, and vehicle |
JP2020180785A (en) * | 2019-04-23 | 2020-11-05 | セイコーエプソン株式会社 | Physical quantity detection circuit, physical quantity sensor, electronic equipment, mobile body and failure diagnosis method of physical quantity sensor |
US11014571B2 (en) | 2017-10-31 | 2021-05-25 | Seiko Epson Corporation | Physical quantity measurement device, electronic apparatus, and vehicle |
US12031822B2 (en) | 2019-04-23 | 2024-07-09 | Seiko Epson Corporation | Physical quantity detection circuit, physical quantity sensor, electronic instrument, vehicle, and method for diagnosing failure of physical quantity sensor |
-
1995
- 1995-05-30 JP JP13135195A patent/JP3430711B2/en not_active Expired - Fee Related
Cited By (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1999066289A1 (en) * | 1998-06-15 | 1999-12-23 | Matsushita Electric Industrial Co., Ltd. | Angular velocity sensor |
US6386034B1 (en) | 1998-06-15 | 2002-05-14 | Matsushita Electric Industrial Co., Ltd. | Angular velocity sensor |
EP1394509A2 (en) * | 1998-06-15 | 2004-03-03 | Matsushita Electric Industrial Co., Ltd. | Angular velocity sensor |
EP1394509A3 (en) * | 1998-06-15 | 2011-06-29 | Panasonic Corporation | Angular velocity sensor |
JP2002267448A (en) * | 2001-03-09 | 2002-09-18 | Matsushita Electric Ind Co Ltd | Angular velocity sensor |
US7865284B2 (en) | 2004-04-21 | 2011-01-04 | Panasonic Corporation | Angular velocity sensor and transporting equipment |
US7730782B2 (en) | 2008-04-04 | 2010-06-08 | Panasonic Corporation | Sensor device |
US8322214B2 (en) | 2008-04-04 | 2012-12-04 | Panasonic Corporation | Sensor device |
US7775109B2 (en) | 2008-04-04 | 2010-08-17 | Panasonic Corporation | Sensor device |
KR100950387B1 (en) * | 2008-04-04 | 2010-03-29 | 파나소닉 주식회사 | Sensor apparatus |
WO2009122739A1 (en) * | 2008-04-04 | 2009-10-08 | パナソニック株式会社 | Sensor device |
EP2634532A1 (en) * | 2008-04-04 | 2013-09-04 | Panasonic Corporation | Sensor device with failure diagnosing circuit |
US7746091B2 (en) | 2008-10-16 | 2010-06-29 | Panasonic Corporation | Sensor apparatus |
JP2010107416A (en) * | 2008-10-31 | 2010-05-13 | Epson Toyocom Corp | Angular velocity detecting device and method of manufacturing the same |
JP2010169408A (en) * | 2009-01-20 | 2010-08-05 | Epson Toyocom Corp | Physical quantity detection device |
JP2010169409A (en) * | 2009-01-20 | 2010-08-05 | Epson Toyocom Corp | Physical quantity detection device |
US8131507B2 (en) | 2009-02-05 | 2012-03-06 | Panasonic Corporation | Sensor apparatus |
US8131508B2 (en) | 2009-02-05 | 2012-03-06 | Panasonic Corporation | Sensor apparatus |
US8939024B2 (en) | 2009-09-14 | 2015-01-27 | Panasonic Intellectual Property Management Co., Ltd. | Angular velocity sensor |
JPWO2011030541A1 (en) * | 2009-09-14 | 2013-02-04 | パナソニック株式会社 | Angular velocity sensor |
WO2011030541A1 (en) * | 2009-09-14 | 2011-03-17 | パナソニック株式会社 | Angular velocity sensor |
JP2012211872A (en) * | 2011-03-31 | 2012-11-01 | Denso Corp | Sensor apparatus |
JP2014016356A (en) * | 2013-09-05 | 2014-01-30 | Seiko Epson Corp | Method for manufacturing angular velocity detection device |
JP2015118102A (en) * | 2015-02-16 | 2015-06-25 | セイコーエプソン株式会社 | Method for manufacturing angular velocity detection device |
US10746809B2 (en) | 2017-09-28 | 2020-08-18 | Seiko Epson Corporation | Physical quantity measurement device, electronic apparatus, and vehicle |
US11014571B2 (en) | 2017-10-31 | 2021-05-25 | Seiko Epson Corporation | Physical quantity measurement device, electronic apparatus, and vehicle |
JP2020180785A (en) * | 2019-04-23 | 2020-11-05 | セイコーエプソン株式会社 | Physical quantity detection circuit, physical quantity sensor, electronic equipment, mobile body and failure diagnosis method of physical quantity sensor |
US11733045B2 (en) | 2019-04-23 | 2023-08-22 | Seiko Epson Corporation | Physical quantity detection circuit, physical quantity sensor, electronic instrument, vehicle, and method for diagnosing failure of physical quantity sensor |
US12031822B2 (en) | 2019-04-23 | 2024-07-09 | Seiko Epson Corporation | Physical quantity detection circuit, physical quantity sensor, electronic instrument, vehicle, and method for diagnosing failure of physical quantity sensor |
Also Published As
Publication number | Publication date |
---|---|
JP3430711B2 (en) | 2003-07-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP3430711B2 (en) | Angular velocity sensor | |
EP0773430B1 (en) | Angular velocity sensor | |
JP3536497B2 (en) | Vibration type angular velocity detector | |
KR101077383B1 (en) | Inertia force sensor | |
US6177756B1 (en) | Piezoelectric gyro and method of driving the piezoelectric gyro | |
JPH09281138A (en) | Angular velocity sensor | |
JPH07181042A (en) | Diagnostic unit for angular speed sensor | |
JPH0752105B2 (en) | Angular velocity sensor | |
JP3458732B2 (en) | Vibration sensor disconnection detection device | |
JPS612013A (en) | Angular velocity sensor | |
JP3360510B2 (en) | Angular velocity sensor | |
JP3191404B2 (en) | Temperature detection method for piezoelectric vibrator | |
US7987715B2 (en) | Angular speed sensor | |
JP3360500B2 (en) | Angular velocity sensor | |
JPH08114458A (en) | Angular velocity sensor | |
JPH0933260A (en) | Angular velocity sensor | |
JP3391098B2 (en) | Vibrating gyro | |
JP3307257B2 (en) | Acceleration sensor | |
JPH08178668A (en) | Vibration offset reducing device for angular velocity sensor | |
JP3343824B2 (en) | Vibration level detector | |
JP4631154B2 (en) | Vibrating gyro and electronic device using the same | |
JPH0729480Y2 (en) | Complex elastic modulus measuring device with multiple force detectors | |
JPH08201067A (en) | Angular speed sensor | |
JPH10160546A (en) | Vibrating-type level detector and its detecting method | |
JPH09113281A (en) | Angular velocity sensor |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FPAY | Renewal fee payment (event date is renewal date of database) |
Free format text: PAYMENT UNTIL: 20080523 Year of fee payment: 5 |
|
FPAY | Renewal fee payment (event date is renewal date of database) |
Free format text: PAYMENT UNTIL: 20090523 Year of fee payment: 6 |
|
FPAY | Renewal fee payment (event date is renewal date of database) |
Free format text: PAYMENT UNTIL: 20100523 Year of fee payment: 7 |
|
LAPS | Cancellation because of no payment of annual fees |