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JPS6257213B2 - - Google Patents
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JPS6257213B2 - - Google Patents

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Publication number
JPS6257213B2
JPS6257213B2 JP12816282A JP12816282A JPS6257213B2 JP S6257213 B2 JPS6257213 B2 JP S6257213B2 JP 12816282 A JP12816282 A JP 12816282A JP 12816282 A JP12816282 A JP 12816282A JP S6257213 B2 JPS6257213 B2 JP S6257213B2
Authority
JP
Japan
Prior art keywords
rectifier circuit
circuit group
component
signal
synchronous rectifier
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP12816282A
Other languages
Japanese (ja)
Other versions
JPS5918433A (en
Inventor
Yoshio Kawamori
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.)
Shimadzu Corp
Original Assignee
Shimadzu Corp
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 Shimadzu Corp filed Critical Shimadzu Corp
Priority to JP12816282A priority Critical patent/JPS5918433A/en
Publication of JPS5918433A publication Critical patent/JPS5918433A/en
Publication of JPS6257213B2 publication Critical patent/JPS6257213B2/ja
Granted legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00Testing static or dynamic balance of machines or structures
    • G01M1/14Determining imbalance
    • G01M1/16Determining imbalance by oscillating or rotating the body to be tested
    • G01M1/22Determining imbalance by oscillating or rotating the body to be tested and converting vibrations due to imbalance into electric variables
    • G01M1/225Determining imbalance by oscillating or rotating the body to be tested and converting vibrations due to imbalance into electric variables for vehicle wheels
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00Testing static or dynamic balance of machines or structures
    • G01M1/14Determining imbalance
    • G01M1/16Determining imbalance by oscillating or rotating the body to be tested
    • G01M1/22Determining imbalance by oscillating or rotating the body to be tested and converting vibrations due to imbalance into electric variables

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Balance (AREA)
  • Rectifiers (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

本発明は動釣合試験機における不釣合信号を同
期整流する為の回路に関する。 一般に、動釣合試験機においては、試験回転数
と同期した交流の不釣合検出信号から、不釣合の
90゜分力成分に相当する直流信号を抽出する為
に、同期整流回路が用いられる。従来のこの種回
路では、不釣合信号に含まれているノイズのう
ち、偶数高調波は除去されるが、奇数高調波が次
数の逆数の割合で混入する欠点があつた。その
為、その奇数高調波を除去する為に、整流回路の
前にフイルタを設け、しかもこのフイルタの遮断
周波数も入力基本周波数(試験機の回転周波数)
に対応して同調させる必要があつて、複雑な回路
構成となる欠点があつた。 本発明は上記欠点を解消する為になされたもの
で、特に影響の大きな第3高調波を整流回路で除
去し、整流回路の前に設けるフイルタがラフな固
定遮断周波数のものでも、充分高精度な不釣合の
90゜分力成分に相当する直流信号を得ることので
きる動釣合試験機の同期整流回路の提供を目的と
する。 本発明の特徴は、試験機の回転に同期して、そ
の回路の周期の半周期に亘つて不釣合信号を同期
整流する互いに60゜の位相差を持つ3つの同期整
流回路で偶数高調波を除去し、その3つの同期整
流回路出力を加算して擬似基本波を合成し、次に
同じく試験機の回転と同期して、その回転の周期
の1/3に亘つて上述の擬似基本波を同期整流する
互いに120゜の位相差を持つた2つの同期整流回
路で第3高調波を除去し、更にこの2つの同期整
流回路の出力を演算して不釣合の90゜分力成分に
相当する直流信号を得るよう構成したことにあ
る。 以下、本発明の実施例を図面に基づいて説明す
る。 第1図は本発明の実施例の回路構成図である。 不釣合信号は、試験機の回転に同期し、互いに
60゜の位相差を持ち、それぞれ上記回転の周期の
半周期に亘つて同期整流する3つの同期整流回路
からなる第1の整流回路群Aに導入される。この
第1の整流回路群Aを構成する3つの同期整流回
路は、それぞれ抵抗1a,1b,1c、スイツチ
2a,2b,2c,3a,3b,3c、およびコ
ンデンサ4a,4b,4c,5a,5b,5cと
から構成されている。それぞれの同期整流回路に
おいて、スイツチ2aと3a,2bと3b,2c
と3cは互いに逆位相で開閉を繰り返し、その開
又は閉の時間は試験機の回転の周期の1/2の時間
であり、スイツチ2a,2b,2c(および3
a,3b,3c)の開閉動作は互いに60゜の位相
差を持つている。このスイツチ2a,2b,2
c,3a,3b,3cの開閉タイミングは、例え
ば試験体上のマーク等を検出する基準位相記号か
ら、その周波数と同じ周波数を持ち、かつ、その
周期の1/2のパルス幅を持つ方形波パルス信号で
あつて、基準位相信号に対して0゜,60゜,120
゜,180゜,240゜,300゜の位相差を持つパルス
を発生することによつて制御することができる。
3つの同期整流回路の出力は加算器6に導入され
た後、試験機の回転に同期し、互いに120゜の位
相差を持ち、その回転の周期の1/3の周期にわた
つて同期整流をする2つの同期整流回路からなる
第2の整流回路群Bに導入される。この第2の整
流回路群Bを構成する2つの同期整流回路は、そ
れぞれ抵抗7a,7b、スイツチ8a,8bおよ
び積分器9a,9bから構成されている。それぞ
れの同期整流回路のスイツチ8aおよび8bは、
互いに120゜の位相差を持ち、それぞれ試験機の
回転の周期の1/3の時間だけ閉じられる。またス
イツチ8aの位相は第1の整流回路群におけるス
イツチ2aの位相と同位相になるよう制御されて
いる。このスイツチ8aおよび8bの開閉タイミ
ングも上述の第1の整流回路群内のスイツチ2a
等と同様なる手段で制御することができる。この
2つの同期整流回路の出力のうち積分器9aから
出力されたものは抵抗10を介して演算増幅器1
2へ入力され、積分器9bから出力されたものは
抵抗11を介して演算増幅器12へ入力されると
ともに、不釣合の90゜分力成分に相当する直流信
号の一方の成分(Y成分)の出力端子へ接続され
ている。また、他方の成分(X成分)の出力端子
には演算増幅器12の出力が接続されている。抵
抗10,11および演算増幅器12は、積分器9
aおよび9bの出力から不釣合のX成分を抽出す
る為に設けられたもので、抵抗10,11および
演算増幅器12の帰還抵抗13の抵抗値をそれぞ
れR1,R2およびR3とすると、次の式を満足する
ような関係を持つている。 R2=2R1 ……(1) 次に、第2図、第3図および第4図に示す出力
波形図に基づいて作用を説明する。 第2図は不釣合検出信号のうち、基本周波数成
分が第1の整流回路群Aおよび加算器6によつて
凝似基本波に変化されるまでを説明する波形図で
ある。第2図aは不釣合検出信号の基本周波数成
分の波形図であり、その周期T=2π/ω、時間t, 振幅A、基準位相信号に対する位相差θとする
と、 =A sin(ωt+θ) ……(3) で表される。第2図b,c,dは、それぞれスイ
ツチ2a,2b,2cの開閉タイミングを示す図
でONを高レベル、OFFを低レベルで示してい
る。なおスイツチ3a,3b,3cはそれぞれ第
2図b,c,dと逆位相で制御されているので図
示を略す。第2図e,f,gはそれぞれスイツチ
2aと3a,2bと3b,2cと3cの出力コモ
ン端子における出力波形図であり、第2図aの基
本周波数成分は第1の整流回路群Aを通過してこ
のような信号となつて加算器6に入力される。加
算器6は、これら信号を加算して第2図hの如
く、擬似基本波を作る。この擬似基本波の各部の
振幅I1,I2,I3、およびI4は、第2図e,f,gに
おけるそれぞれの振幅をI5,I6,I7とすれば、 I1=I5+I6+I7 ……(4) I2=I5+I6−I7 ……(5) I3=I5−I6+I7 ……(6) I4=−I5−I6−I7=−I1 ……(7) で表され、また、各I5,I6,I7は(3)より、 であるので、(4),(5),(6),(7),(8),(9),(10)より I1=2A/π(√3sinθ+cosθ) ……(11) I2=4A/πcosθ ……(12) I3=2A/π(−√3sinθ+cosθ)……(13) I4=−2A/π(√3sinθ+cosθ)……(14) と表すことができる。 第3図は不釣合検出信号に含まれる雑音のう
ち、第3高調波が第1の整流回路群Aおよび加算
器6にて変化される過程を示す波形図である。第
3図aは基本周波数の第3高調波を示す波形図、
第3図b,c,dは第2図b,c,dを再掲する
図、第3図e,f,gはそれぞれ第1の整流回路
群Aを通過した第3高調波の信号であり、加算器
6はこれらを加算して第3図hの各部における振
幅I8,I9,I10は、第3図e,f,gにおけるそれ
ぞれの振幅I11,I12,I13、とすると、 I8=I11+I12+I13 ……(15) I9=I11+I12−I13 ……(16) I10=I11−I12−I13 ……(17) で表され、第3高調波を g(3ωt)=Bsin(3ωt+α) ……(18) とすれば、 であるので、(15),(16),(17),(18),(19)

(20),(21)より I8=−I9=I10 ……(22) となる。 第4図は第1の整流回路群Aおよび加算器6を
通過した基本周波数成分とその第3高調波成分が
第2の整流回路群Bによつて変化される過程を示
す波形図である。第4図aおよびbはそれぞれ第
2図hおよび第3図hを再掲する図、第4図c,
dは第2の整流回路群Bにおけるスイツチ8a,
8bの開閉タイミングを示す図である。第4図a
に示す擬似基本波は、第2の整流回路群Bの一方
の同期整流回路を構成する積分器9aから第4図
eに示す直流信号に、またもう一方の同期整流回
路を構成する積分器9bからは第4図fに示す直
流信号に変換されて出力される。この第4図eお
よびfの信号の電圧I14およびI15は、kを定数と
すれば、 I14=k(I1+I2)/2 ……(24) I15=k(I3+I4)/2 ……(25) と表され、(11),(12),(13),(14)より となる。また3高調波成分の第2の整流回路群B
の各積分器9a,9bからの出力波形は、第4図
g,hに示す如く、その電圧をI16,I17とすれば
(22)より I16=I8+I9=0 ……(28) I17=I10+I9=0 ……(29) となつて完全に除去される。上述の擬似基本波を
第2の整流回路群Bで同期整流して得られた2つ
の直流信号のうち、積分器9bから出力される
I15なる電圧を持つ直流信号は、(27)より明らか
なように、 とおけば、 Y=C1sinθ ……(31) となつて、不釣合の90゜分力成分に相当する一方
の直流成分(Y成分)として用いることができ
る。また、積分器9aから出力されるI14なる電
圧を持つ直流信号と、このI15なる電圧を持つ直
流信号によつて不釣合の90゜分力成分に相当する
もう一方の直流成分(X成分)すなわち、 X=C1cosθ ……(32) を得るには、 α×I14+β×I15=C1cosθ ……(33) とおけば、(26),(27)より、 この(34)が恒等的に成立するには、 α/2−β=0…(35),
The present invention relates to a circuit for synchronously rectifying an unbalance signal in a dynamic balance tester. Generally, in a dynamic balance tester, the unbalance is determined from an AC unbalance detection signal synchronized with the test rotation speed.
A synchronous rectifier circuit is used to extract the DC signal corresponding to the 90° force component. In conventional circuits of this type, even harmonics are removed from the noise contained in the unbalanced signal, but there is a drawback that odd harmonics are mixed in at a rate that is the reciprocal of the order. Therefore, in order to remove the odd harmonics, a filter is installed in front of the rectifier circuit, and the cutoff frequency of this filter is also the input fundamental frequency (rotational frequency of the testing machine).
The disadvantage was that it required tuning in accordance with the , resulting in a complicated circuit configuration. The present invention was made in order to eliminate the above-mentioned drawbacks.The third harmonic, which has a particularly large influence, is removed by a rectifier circuit, and even if the filter installed in front of the rectifier circuit has a rough fixed cutoff frequency, the accuracy is sufficiently high. disproportionate
The purpose of this invention is to provide a synchronous rectifier circuit for a dynamic balance tester that can obtain a DC signal corresponding to a 90° force component. The feature of the present invention is that the unbalanced signal is synchronously rectified over half the cycle of the circuit in synchronization with the rotation of the test machine, and even harmonics are removed using three synchronous rectifier circuits with a phase difference of 60 degrees from each other. Then, add the outputs of the three synchronous rectifier circuits to synthesize a pseudo fundamental wave, and then synchronize with the rotation of the test machine and synchronize the above pseudo fundamental wave over 1/3 of the rotation period. The third harmonic is removed using two synchronous rectifier circuits with a phase difference of 120° from each other, and the outputs of these two synchronous rectifiers are calculated to generate a DC signal corresponding to the unbalanced 90° component of the force. The reason is that it is configured to obtain the following. Embodiments of the present invention will be described below based on the drawings. FIG. 1 is a circuit diagram of an embodiment of the present invention. The unbalance signals are synchronized with the rotation of the test machine and
It is introduced into a first rectifier circuit group A consisting of three synchronous rectifier circuits having a phase difference of 60 degrees and performing synchronous rectification over a half period of the rotation period. The three synchronous rectifier circuits constituting this first rectifier circuit group A each include resistors 1a, 1b, 1c, switches 2a, 2b, 2c, 3a, 3b, 3c, and capacitors 4a, 4b, 4c, 5a, 5b. , 5c. In each synchronous rectifier circuit, switches 2a and 3a, 2b and 3b, 2c
and 3c repeat opening and closing in opposite phases to each other, and the opening or closing time is 1/2 of the rotation period of the testing machine.
The opening/closing operations of a, 3b, and 3c) have a phase difference of 60° from each other. This switch 2a, 2b, 2
The opening/closing timing of c, 3a, 3b, and 3c is, for example, based on the reference phase symbol for detecting a mark on the test object, and is a square wave having the same frequency as that frequency and a pulse width of 1/2 of the period. Pulse signal, 0°, 60°, 120° with respect to the reference phase signal
Control can be achieved by generating pulses with phase differences of °, 180°, 240°, and 300°.
After the outputs of the three synchronous rectifier circuits are introduced into the adder 6, they are synchronized with the rotation of the test machine, have a phase difference of 120 degrees from each other, and are synchronously rectified over a period of 1/3 of the rotation period. The second rectifier circuit group B consists of two synchronous rectifier circuits. The two synchronous rectifier circuits constituting the second rectifier circuit group B are each comprised of resistors 7a, 7b, switches 8a, 8b, and integrators 9a, 9b. Switches 8a and 8b of each synchronous rectifier circuit are
They have a phase difference of 120° from each other and are closed for 1/3 of the rotation period of the testing machine. Further, the phase of the switch 8a is controlled to be in the same phase as the phase of the switch 2a in the first rectifier circuit group. The opening/closing timing of the switches 8a and 8b is also the same as that of the switch 2a in the first rectifier circuit group.
It can be controlled by means similar to the above. Of the outputs of these two synchronous rectifier circuits, the one output from the integrator 9a is passed through a resistor 10 to the operational amplifier 1.
2 and output from the integrator 9b is input to the operational amplifier 12 via the resistor 11, and outputs one component (Y component) of the DC signal corresponding to the unbalanced 90° component force component. connected to the terminal. Furthermore, the output of the operational amplifier 12 is connected to the output terminal of the other component (X component). Resistors 10 and 11 and operational amplifier 12 are connected to integrator 9
This is provided to extract the unbalanced X component from the outputs of a and 9b.If the resistance values of the resistors 10 and 11 and the feedback resistor 13 of the operational amplifier 12 are R 1 , R 2 and R 3 respectively, then It has a relationship that satisfies the equation. R 2 = 2R 1 ……(1) Next, the operation will be explained based on the output waveform diagrams shown in FIGS. 2, 3, and 4. FIG. 2 is a waveform diagram illustrating how the fundamental frequency component of the unbalance detection signal is changed into a condensed fundamental wave by the first rectifier circuit group A and the adder 6. Figure 2a is a waveform diagram of the fundamental frequency component of the unbalance detection signal, and assuming that its period T = 2π/ω, time t, amplitude A, and phase difference θ with respect to the reference phase signal, =A sin (ωt + θ)... (3) FIGS. 2b, 2c, and d are diagrams showing the opening/closing timing of the switches 2a, 2b, and 2c, respectively, and show ON as a high level and OFF as a low level. Note that the switches 3a, 3b, and 3c are controlled in opposite phases to those in FIG. 2b, c, and d, respectively, and are therefore not shown. Figure 2 e, f, and g are output waveform diagrams at the output common terminals of switches 2a and 3a, 2b and 3b, and 2c and 3c, respectively. The signal passes through and becomes such a signal and is input to the adder 6. The adder 6 adds these signals to create a pseudo fundamental wave as shown in FIG. 2h. The amplitudes I 1 , I 2 , I 3 , and I 4 of each part of this pseudo fundamental wave are I 1 = I 1 = I 5 +I 6 +I 7 ……(4) I 2 =I 5 +I 6 −I 7 ……(5) I 3 =I 5 −I 6 +I 7 ……(6) I 4 =−I 5 −I 6 −I 7 = −I 1 ...(7), and each I 5 , I 6 , I 7 is expressed as (3), Therefore, from (4), (5), (6), (7), (8), (9), (10), I 1 = 2A/π (√3 sin θ + cos θ) ... (11) I 2 = 4A/πcosθ...(12) I3 =2A/π(-√3sinθ+cosθ)...(13) I4 =-2A/π(√3sinθ+cosθ)...(14) FIG. 3 is a waveform diagram showing a process in which the third harmonic of the noise included in the unbalance detection signal is changed by the first rectifier circuit group A and the adder 6. Figure 3a is a waveform diagram showing the third harmonic of the fundamental frequency;
Figure 3 b, c, and d are reproductions of Figure 2 b, c, and d, and Figure 3 e, f, and g are the third harmonic signals that have passed through the first rectifier circuit group A, respectively. , the adder 6 adds these , and the amplitudes I 8 , I 9 , I 10 at each part in FIG. Then, I 8 = I 11 + I 12 + I 13 ……(15) I 9 = I 11 + I 12 − I 13 ……(16) I 10 = I 11 − I 12 − I 13 ……(17) , if the third harmonic is g(3ωt)=Bsin(3ωt+α)...(18), Therefore, (15), (16), (17), (18), (19)

From (20) and (21), I 8 = −I 9 = I 10 ...(22). FIG. 4 is a waveform diagram showing a process in which the fundamental frequency component and its third harmonic component that have passed through the first rectifier circuit group A and the adder 6 are changed by the second rectifier circuit group B. Figures 4a and b are reproductions of Figures 2h and 3h, Figure 4c,
d is the switch 8a in the second rectifier circuit group B;
8b is a diagram showing the opening/closing timing of 8b. Figure 4a
The pseudo fundamental wave shown in FIG. 4 is transmitted to the DC signal shown in FIG. is converted into a DC signal shown in FIG. 4f and output. The voltages I 14 and I 15 of the signals e and f in FIG . 4 )/2 ...(25) is expressed as (11), (12), (13), and (14). becomes. Also, the second rectifier circuit group B for the third harmonic component
The output waveforms from the integrators 9a and 9b are as shown in Figure 4g and h.If the voltages are I 16 and I 17 , then from (22) I 16 = I 8 + I 9 = 0...( 28) I 17 = I 10 + I 9 = 0 ...(29) and is completely removed. Of the two DC signals obtained by synchronously rectifying the above-mentioned pseudo fundamental wave in the second rectifier circuit group B, the signal is output from the integrator 9b.
As is clearer from (27), a DC signal with a voltage of I 15 is Then, Y=C 1 sinθ (31), which can be used as one DC component (Y component) corresponding to the unbalanced 90° component of force. In addition, the other DC component (X component) corresponding to the unbalanced 90° force component is generated by the DC signal with the voltage I 14 output from the integrator 9a and the DC signal with the voltage I 15 . In other words , to obtain In order for this (34) to hold true, α/2−β=0…(35),

【式】 (36)を(35)に代入して、【formula】 Substituting (36) into (35),

【式】【formula】

【式】 であればよく、従つてI14とI15を用いて、抵抗1
0,11および演算増幅器12の帰還抵抗13の
関係を前述した(1),(2)の如く構成すれば(32)の
Xを得ることができる。 なお、第1の整流回路群Aを第5図に示す如
く、スイツチ3a,3b,3cおよびコンデンサ
5a,5b,5cを無くし、加算器6と第2整流
回路群Bとの間に直流カツト用コンデンサ14を
設けても同様な効果を得ることができる。 以上説明したように、本発明によれば、同期整
流回路内にて、第3高調波を完全に除去すること
ができるので、従来装置のように入力基本周波数
と同調するフイルタを同期整流回路の前に設ける
必要がなく、固定遮断周波数のフイルタを設ける
だけで充分高精度なX,Y成分を得ることができ
る。
[Formula] Therefore, using I 14 and I 15 , the resistance 1
If the relationship between 0 and 11 and the feedback resistor 13 of the operational amplifier 12 is configured as in (1) and (2) above, X of (32) can be obtained. In addition, as shown in FIG. 5, the first rectifier circuit group A has switches 3a, 3b, 3c and capacitors 5a, 5b, 5c removed, and a direct current cut circuit is installed between the adder 6 and the second rectifier circuit group B. A similar effect can be obtained even if the capacitor 14 is provided. As explained above, according to the present invention, it is possible to completely remove the third harmonic within the synchronous rectifier circuit. It is not necessary to provide a filter in front of the filter, and it is possible to obtain sufficiently accurate X and Y components by simply providing a filter with a fixed cutoff frequency.

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

第1図は本発明実施例の回路構成図、第2図、
第3図および第4図はその各部における出力波形
にて示す作用説明図、第5図は本発明の他の実施
例の要部を示す回路構成図である。 2a,2b,2c……スイツチ、3a,3b,
3c……スイツチ、4a,4b,4c……コンデ
ンサ、5a,5b,5c……コンデンサ、6……
加算器、8a,8b……スイツチ、9a,9b…
…積分器、10,11……抵抗、12……演算増
幅器、13……帰還抵抗、14……直流カツト用
コンデンサ、A……第1の整流回路群、B……第
2の整流回路群。
FIG. 1 is a circuit configuration diagram of an embodiment of the present invention, FIG.
3 and 4 are action explanatory diagrams showing the output waveforms of each part, and FIG. 5 is a circuit configuration diagram showing the main part of another embodiment of the present invention. 2a, 2b, 2c... switch, 3a, 3b,
3c...Switch, 4a, 4b, 4c...Capacitor, 5a, 5b, 5c...Capacitor, 6...
Adder, 8a, 8b...Switch, 9a, 9b...
... Integrator, 10, 11 ... Resistor, 12 ... Operational amplifier, 13 ... Feedback resistor, 14 ... DC cut capacitor, A ... First rectifier circuit group, B ... Second rectifier circuit group .

Claims (1)

【特許請求の範囲】[Claims] 1 試験機の回転に同期し、互いに60゜の位相差
を持ち、それぞれ上記回転の周期の半周期に亘つ
て不釣合信号を同期整流する3つの同期整流回路
からなる第1の整流回路群と、その第1の整流回
路群の各同期整流回路出力を加算する加算回路
と、上記回転に同期し、互いに120゜の位相差を
持ち、それぞれ上記回転の周期の1/3周期に亘つ
て上記加算回路出力を同期整流する2つの同期整
流回路からなる第2の整流回路群と、その第2の
整流回路群の出力から不釣合の90゜分力成分に相
当する直流信号を抽出する演算回路を備えた動釣
合試験機の同期整流回路。
1. A first rectifier circuit group consisting of three synchronous rectifier circuits that are synchronized with the rotation of the testing machine, have a phase difference of 60 degrees from each other, and each synchronously rectify an unbalanced signal over a half period of the rotation period; an adder circuit that adds the outputs of each synchronous rectifier circuit of the first rectifier circuit group; A second rectifier circuit group consisting of two synchronous rectifier circuits that synchronously rectify the circuit output, and an arithmetic circuit that extracts a DC signal corresponding to an unbalanced 90° component of force from the output of the second rectifier circuit group. Synchronous rectifier circuit for dynamic balance tester.
JP12816282A 1982-07-21 1982-07-21 Synchronous rectifier circuit for dynamic balance tester Granted JPS5918433A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12816282A JPS5918433A (en) 1982-07-21 1982-07-21 Synchronous rectifier circuit for dynamic balance tester

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12816282A JPS5918433A (en) 1982-07-21 1982-07-21 Synchronous rectifier circuit for dynamic balance tester

Publications (2)

Publication Number Publication Date
JPS5918433A JPS5918433A (en) 1984-01-30
JPS6257213B2 true JPS6257213B2 (en) 1987-11-30

Family

ID=14977916

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12816282A Granted JPS5918433A (en) 1982-07-21 1982-07-21 Synchronous rectifier circuit for dynamic balance tester

Country Status (1)

Country Link
JP (1) JPS5918433A (en)

Also Published As

Publication number Publication date
JPS5918433A (en) 1984-01-30

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