JPS639615B2 - - Google Patents

Info

Publication number
JPS639615B2
JPS639615B2 JP55130729A JP13072980A JPS639615B2 JP S639615 B2 JPS639615 B2 JP S639615B2 JP 55130729 A JP55130729 A JP 55130729A JP 13072980 A JP13072980 A JP 13072980A JP S639615 B2 JPS639615 B2 JP S639615B2
Authority
JP
Japan
Prior art keywords
valve
pilot
pressure
hydraulic
main
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
JP55130729A
Other languages
Japanese (ja)
Other versions
JPS5756734A (en
Inventor
Koji Fujiwara
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP55130729A priority Critical patent/JPS5756734A/en
Publication of JPS5756734A publication Critical patent/JPS5756734A/en
Publication of JPS639615B2 publication Critical patent/JPS639615B2/ja
Granted legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N3/32Investigating strength properties of solid materials by application of mechanical stress by applying repeated or pulsating forces
    • G01N3/36Investigating strength properties of solid materials by application of mechanical stress by applying repeated or pulsating forces generated by pneumatic or hydraulic means
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/003Generation of the force
    • G01N2203/0042Pneumatic or hydraulic means
    • G01N2203/0048Hydraulic means

Landscapes

  • Physics & Mathematics (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • General Physics & Mathematics (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
  • Servomotors (AREA)

Description

【発明の詳細な説明】 本発明は振動試験機、疲労試験機などの試験機
の起動制御装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a start-up control device for a testing machine such as a vibration testing machine or a fatigue testing machine.

例えば、振動試験機のような試験機においては
振動台を加振するアクチユエータを、パイロツト
弁と主弁とからなる2段増幅形のサーボ弁からの
制御圧油によつて制御している。そして、このサ
ーボ弁を構成するパイロツト弁への油圧PS1の圧
油と主弁への油圧PS2の圧油との供給は、同一の
油圧供給から分岐して供給されている。
For example, in a testing machine such as a vibration testing machine, an actuator that vibrates a vibration table is controlled by control pressure oil from a two-stage amplification type servo valve consisting of a pilot valve and a main valve. The pressure oil of hydraulic pressure P S1 to the pilot valve constituting this servo valve and the pressure oil of hydraulic pressure P S2 to the main valve are supplied by branching from the same hydraulic pressure supply.

このように構成された油圧供給系において、パ
イロツト弁駆動用の入力信号を零にして起動する
ときに、主弁のスプールが必ず中央位置にあると
は限らないことがある。このように、主弁のスプ
ールが中央よりずれた位置にある状態で起動が開
始されると、振動台は入力信号による移動以前に
予期しない移動を生じる。この移動を防止するた
めに主弁のスプール変位を入力側に帰還させる補
償手段を備えているが、起動時に振動台はたとえ
でもわずかに移動することが皆無にすることがで
きない。この振動台の予期しない移動は、振動台
上の被試験体を正規の試験前に破損させることが
ある。
In a hydraulic pressure supply system configured as described above, the spool of the main valve may not always be at the center position when the input signal for driving the pilot valve is set to zero and the system is started. In this way, if activation is started with the spool of the main valve being at a position offset from the center, the vibration table will unexpectedly move before it moves in response to the input signal. In order to prevent this movement, a compensating means is provided to return the spool displacement of the main valve to the input side, but it is impossible to completely eliminate even a slight movement of the vibration table upon startup. This unexpected movement of the shaking table may damage the test object on the shaking table before it is properly tested.

本発明は上述の事柄にもとづいてなされたもの
で、起動時に生じる被試験体の予期せぬ移動を抑
止することができる試験機の起動制御装置を提供
することを目的とする。
The present invention has been made based on the above-mentioned matters, and an object of the present invention is to provide a start-up control device for a test machine that can prevent unexpected movement of a test object that occurs during start-up.

本発明の特徴とするところは、油圧供給装置か
らの圧油をパイロツト弁と主弁とからなる2段増
幅形サーボ弁によつてアクチユエータに加え、こ
のアクチユエータによつて被試験体を加振する試
験機において、前記油圧供給装置を、パイロツト
弁へのパイロツト油圧供給系と主弁への主油圧供
給系とで構成し、これらの油圧供給系を均圧用チ
エツク弁を介して連結し、主油圧供給系の油圧源
駆動用のモータに、このモータをパイロツト油圧
供給系の油圧駆動用のモータの起動後に遅延起動
させる遅延手段及び主弁のスプールの位置を検出
する検出器からの信号によつてパイロツト弁のス
プールの位置を制御し、この制御によつて前記油
圧駆動源のモータの駆動前に主弁のスプールを中
央位置に復帰させる零位置制御手段を設けたもの
である。
The present invention is characterized in that pressure oil from a hydraulic supply system is applied to an actuator by a two-stage amplification type servo valve consisting of a pilot valve and a main valve, and the test object is vibrated by this actuator. In the test machine, the hydraulic pressure supply system consists of a pilot hydraulic pressure supply system to the pilot valve and a main hydraulic pressure supply system to the main valve, and these hydraulic pressure supply systems are connected via a pressure equalization check valve, and the main hydraulic pressure is A delay means for delaying starting of the motor for driving the hydraulic power source of the supply system after activation of the motor for driving the hydraulic pressure of the pilot hydraulic supply system, and a signal from a detector for detecting the position of the spool of the main valve. A zero position control means is provided which controls the position of the pilot valve spool and returns the main valve spool to the center position by this control before driving the motor of the hydraulic drive source.

以下図面を参照して本発明の実施例を説明す
る。
Embodiments of the present invention will be described below with reference to the drawings.

第1図は本発明の起動制御装置の一実施例を備
えた振動試験機の構成を示すもので、図において
1は振動台である。この振動台1は水平用加振機
2および垂直用加振機3によつて加振される。こ
れらの加振機2,3にはそれぞれサーボ弁4が設
けられている。また、これらの加振機2,3には
サーボ弁4を通して主油圧源系5とパイロツト油
圧源系6とからの圧油が供給される。これらの主
油圧源系5とパイロツト油圧源系6とはほぼ同様
に構成されており、電磁弁7a,7b、チエツク
弁8a,8b、圧力調整弁9a,9b、油圧ポン
プ10a,10b、フイルタ11a,11b、モ
ータ12a,12bおよびタンク13a,13b
などを備えている。この油圧源系5,6に吐出側
管路は均圧用チエツク弁14を介して接続されて
いる。さらに油圧源系5,6の吐出側管路には圧
力計15a,15bが設けられ、また主油圧源系
5の吐出側管路にはアキユムレータ16が設けら
れている。主油圧源5側のモータ12aにはパイ
ロツト油圧源6側のモータ12bが起動してか
ら、t秒後にモータ12aに起動入力信号を加え
る遅延手段17が接続されている。
FIG. 1 shows the configuration of a vibration tester equipped with an embodiment of the activation control device of the present invention, and in the figure, 1 is a vibration table. This vibration table 1 is vibrated by a horizontal vibrator 2 and a vertical vibrator 3. Each of these vibrators 2 and 3 is provided with a servo valve 4. Further, pressure oil is supplied to these vibrators 2 and 3 from a main hydraulic pressure source system 5 and a pilot hydraulic pressure source system 6 through a servo valve 4. The main hydraulic power source system 5 and the pilot hydraulic power source system 6 are constructed almost in the same way, and include electromagnetic valves 7a, 7b, check valves 8a, 8b, pressure regulating valves 9a, 9b, hydraulic pumps 10a, 10b, and a filter 11a. , 11b, motors 12a, 12b and tanks 13a, 13b
It is equipped with such things as A discharge side pipe line is connected to the hydraulic power source systems 5 and 6 via a pressure equalization check valve 14. Further, pressure gauges 15a and 15b are provided in the discharge side pipes of the hydraulic power source systems 5 and 6, and an accumulator 16 is provided in the discharge side pipe of the main hydraulic power source system 5. A delay means 17 is connected to the motor 12a on the main oil pressure source 5 side to apply a starting input signal to the motor 12a t seconds after the motor 12b on the pilot oil pressure source 6 side is started.

前述した加振機2,3およびサーボ弁4の詳細
な構成を第2図によつて説明する。第2図におい
て、第1図と同符号のものは同一部分である。1
8は主油圧源系5からの圧力PS1の圧油を圧力P1
の圧油として加振機2,3に供給制御する主弁、
19はパイロツト油圧源系6からの圧力PS2の圧
力をP1′の圧油として主弁18のパイロツト部に
供給するパイロツト弁である。パイロツト弁19
のスプール19aの一方端にはフオースモータ2
0が連結され、他方端には零調節器21が設けら
れている。フオースモータ20には入力信号E1
と検出器22からの加振機2,3の変圧信号との
偏差e1を求める加算器23、サーボアンプ24、
サーボアンプ24からの偏差信号e1と検出器25
からの主弁18aの変圧信号との偏差e2を求める
加算器26およびサーボアンプ27が順次接続さ
れている。これらの構成により電気油圧サーボ制
御機構が構成されている。
The detailed configuration of the above-mentioned vibrators 2, 3 and servo valve 4 will be explained with reference to FIG. In FIG. 2, parts with the same symbols as in FIG. 1 are the same parts. 1
8 is the pressure oil at pressure P S1 from the main hydraulic power source system 5 at pressure P 1
a main valve that controls the supply of pressure oil to the vibration exciters 2 and 3;
A pilot valve 19 supplies the pressure P S2 from the pilot oil pressure source system 6 to the pilot portion of the main valve 18 as pressure oil P1 ' . Pilot valve 19
The force motor 2 is attached to one end of the spool 19a.
0 is connected, and a zero adjuster 21 is provided at the other end. The force motor 20 receives an input signal E 1
an adder 23, a servo amplifier 24, which calculates the deviation e1 between the transformer signals of the vibrators 2 and 3 from the detector 22;
Deviation signal e1 from servo amplifier 24 and detector 25
An adder 26 and a servo amplifier 27 are connected in sequence for determining the deviation e 2 from the transformed voltage signal of the main valve 18a. These structures constitute an electro-hydraulic servo control mechanism.

次に上述した本発明の装置により振動試験機を
起動する場合を説明する。
Next, a case will be described in which a vibration testing machine is started using the above-described apparatus of the present invention.

まず、試験機を駆動するために、パイロツト油
圧源系6側のモータ12bを起動するとそのt秒
後に、主油圧源5側のモータ12aが起動する。
このとき、圧力調整弁9bは例えば30Kg/cm2程度
の低圧に設定され、また圧力調整弁9aは例えば
210Kg/cm2程度の高圧に設定されているものとす
ると、主弁18への油圧PS1とパイロツト弁19
への油圧PS2とは時間経過に伴なつて第3図に示
すように変化する。すなわち、最初、圧力PS2
圧油がパイロツト弁19に供給され、t秒後に圧
力PS1の圧油が主弁18に供給されると、均圧用
チエツク弁14によつて主油圧源系5の圧力PS1
の圧油が均圧用チエツク弁14を通してパイロツ
ト油圧源系6の吐出側管路に流入し、やがて両油
圧源系5,6の吐出側管路の圧力PS1,PS2は同じ
圧力となる。このようなことからパイロツト油圧
源系6の油圧ポンプ10bの容量は例えば10/
min程度に小さいものでよい。
First, in order to drive the test machine, the motor 12b on the pilot hydraulic power source system 6 is started, and t seconds later, the motor 12a on the main hydraulic power source 5 is started.
At this time, the pressure regulating valve 9b is set to a low pressure of, for example, 30 kg/ cm2 , and the pressure regulating valve 9a is set to, for example, a low pressure of about 30 kg/cm2.
Assuming that the pressure is set at a high pressure of about 210Kg/cm2, the hydraulic pressure P S1 to the main valve 18 and the pilot valve 19
The hydraulic pressure P S2 changes over time as shown in FIG. That is, first, pressure oil with a pressure P S2 is supplied to the pilot valve 19, and after t seconds, pressure oil with a pressure P S1 is supplied to the main valve 18. The pressure of P S1
The pressure oil flows into the discharge side pipe of the pilot hydraulic power source system 6 through the pressure equalization check valve 14, and soon the pressures P S1 and P S2 of the discharge side pipes of both the hydraulic power source systems 5 and 6 become the same pressure. For this reason, the capacity of the hydraulic pump 10b of the pilot hydraulic power source system 6 is, for example, 10/
It can be as small as min.

均圧用チエツク弁14の作用及び効果について
第1図及び第2図により更に説明する。
The function and effect of the pressure equalization check valve 14 will be further explained with reference to FIGS. 1 and 2.

パイロツト油圧源系6を起動するとその出力圧
力PS2はチエツク弁14の右側(主回路)へは流
れず、サーボ弁4のパイロツト19にだけ作用す
る。そのためパイロツト弁19によつて主弁18
のスプール18aは零位置に制御される。t秒後
に主油圧源系5を起動するとその出力圧力PS1
サーボ弁4の主弁18に作用する。そして、圧力
調整弁9によつて出力圧力PS1が上昇(通常は210
Kg/cm2まで)する。加振実験が開始され、パイロ
ツト油圧源6の流量が不足した時に、主回路側よ
りチエツク弁14を通過してパイロツト系の流量
不足を補う。
When the pilot hydraulic power source system 6 is activated, its output pressure P S2 does not flow to the right side (main circuit) of the check valve 14, but acts only on the pilot 19 of the servo valve 4. Therefore, the main valve 18 is controlled by the pilot valve 19.
The spool 18a is controlled to the zero position. When the main hydraulic power source system 5 is activated after t seconds, its output pressure P S1 acts on the main valve 18 of the servo valve 4. Then, the output pressure P S1 increases by the pressure regulating valve 9 (usually 210
up to Kg/ cm2 ). When an excitation experiment is started and the flow rate of the pilot hydraulic power source 6 is insufficient, the check valve 14 is passed from the main circuit side to compensate for the insufficient flow rate of the pilot system.

パイロツト油圧源6は小流量の能力のものであ
り、起動時だけ使用する。又、パイロツト油圧源
系6は主油圧源系5が起動したら主油圧源系5か
ら圧油が補給されるので、パイロツト油圧源系6
の役割は終了して停止する。チエツク弁14を設
けたことにより、パイロツト油圧源系6は非常に
小さな能力のものですむので、装置が安価にな
る。
The pilot hydraulic power source 6 has a small flow capacity and is used only at startup. In addition, the pilot hydraulic power source system 6 is supplied with pressure oil from the main hydraulic power source system 5 when the main hydraulic power source system 5 starts, so the pilot hydraulic power source system 6
role ends and ceases. By providing the check valve 14, the pilot hydraulic power source system 6 needs to have a very small capacity, so the device becomes inexpensive.

このような運転制御により起動時振動台1が動
かないで静止していることをさらに詳しく説明す
る。いま入力信号E1が零となつているときに、
パイロツト油圧源系6が起動されて圧力PS2の圧
油がパイロツト弁19に供給される。このパイロ
ツト弁19は、第2図に示すようにスプール19
aの両端にバネ21aを持つており、このバス力
を変える零調整用のネジ21によつて、スプール
19aの零調整を行う。そのため、フオースモー
タ20に制御電流が流れない場合は、スプール1
9aは中央の零の位置にあるため、圧油PS2は主
弁スプール18aの両端Aに流れない。一方、主
弁18のスプール18aが中央位置にない場合に
は、検出器25が主弁18のスプール18aの位
置を検出して、加算器26に帰還する。このた
め、フオースモータ20は加算器26からの偏差
信号e2により、パイロツト弁19のスプールを移
動する。これにより、一方の出力油圧(図面上、
左側の出力油圧)R1′が他方の出力油圧P1′(図面
上右側の出力油圧)より大きくなつたとすれば、
主弁18のスプール18aは図面上、右側に移動
して、このパイロツト弁19と主弁18とサーボ
アンプ27と加算器26とのサーボ系を零位置制
御する。すなわち、主弁18のスプールを中央に
位置決めする。この動作は第3図に示すt秒より
はるかに少い時間である。その後、主油圧源系が
遅延手段17により駆動するが、すでに主弁18
のスプール18aは中立位置に復帰しているの
で、振動台1は予期しない移動を起こさず停止し
ている。
The reason why the vibration table 1 does not move and remains stationary at startup due to such operation control will be explained in more detail. Now when the input signal E 1 is zero,
The pilot oil pressure source system 6 is activated and pressure oil at pressure P S2 is supplied to the pilot valve 19. This pilot valve 19 is connected to a spool 19 as shown in FIG.
The spool 19a has springs 21a at both ends of the spool 19a, and the zero adjustment of the spool 19a is performed by a zero adjustment screw 21 that changes the bus force. Therefore, if the control current does not flow to the force motor 20, the spool 1
Since 9a is at the zero position in the center, the pressure oil P S2 does not flow to both ends A of the main valve spool 18a. On the other hand, when the spool 18a of the main valve 18 is not at the center position, the detector 25 detects the position of the spool 18a of the main valve 18, and the detected position is fed back to the adder 26. Therefore, the force motor 20 moves the spool of the pilot valve 19 in response to the deviation signal e2 from the adder 26. This allows one output hydraulic pressure (on the drawing,
If the output oil pressure on the left side) R 1 ′ becomes larger than the output oil pressure on the other side P 1 ′ (the output oil pressure on the right side in the drawing), then
The spool 18a of the main valve 18 moves to the right in the drawing to control the servo system of the pilot valve 19, the main valve 18, the servo amplifier 27, and the adder 26 to the zero position. That is, the spool of the main valve 18 is positioned at the center. This operation takes much less time than the t seconds shown in FIG. Thereafter, the main hydraulic power source system is driven by the delay means 17, but the main valve 18 has already been activated.
Since the spool 18a has returned to the neutral position, the vibration table 1 is stopped without causing any unexpected movement.

以上詳述したように、本発明によれば油圧源系
の起動時に振動が動くという現象を抑止すること
ができるので、試験機の信頼性を高めることがで
きる。
As described in detail above, according to the present invention, it is possible to suppress the phenomenon of vibration movement when starting up the hydraulic power source system, and therefore, the reliability of the testing machine can be improved.

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

第1図は本発明の装置の一実施例を備えた振動
試験機の構成を示す図、第2図は本発明の装置に
用いられる電気油圧サーボ機構の構成を示す図、
第3図は本発明の装置によつて制御される主弁へ
の油圧PS1とパイロツト弁への油圧PS2との特性を
示す図である。 1……振動台、2,3……加振機、4……サー
ボ弁、5……主油圧源系、6……パイロツト油圧
源系、14……均圧用チエツク弁、17……遅延
手段、18……主弁、19……パイロツト弁、2
0……フオースモータ。
FIG. 1 is a diagram showing the configuration of a vibration testing machine equipped with an embodiment of the device of the present invention, and FIG. 2 is a diagram showing the configuration of an electro-hydraulic servo mechanism used in the device of the present invention.
FIG. 3 is a diagram showing the characteristics of the oil pressure P S1 to the main valve and the oil pressure P S2 to the pilot valve controlled by the device of the present invention. 1... Vibration table, 2, 3... Vibrator, 4... Servo valve, 5... Main hydraulic power source system, 6... Pilot hydraulic power source system, 14... Check valve for pressure equalization, 17... Delay means , 18...Main valve, 19...Pilot valve, 2
0...Force motor.

Claims (1)

【特許請求の範囲】[Claims] 1 油圧供給装置からの圧油をパイロツト弁と主
弁とからなる2段増幅形サーボ弁によつてアクチ
ユエータに加え、このアクチユエータによつて被
試験体を加振する試験機において、前記油圧供給
装置を、パイロツト弁へのパイロツト油圧供給系
と主弁への主油圧供給系とで構成し、これらの油
圧供給系を均圧用チエツク弁を介して連結し、主
油圧供給系の油圧源駆動用のモータにこのモータ
をパイロツト油圧供給系の油圧源駆動用のモータ
の起動後に遅延起動させる遅延手段、及び主弁の
スプールの位置を検出する検出器からの信号によ
つてパイロツト弁のスプールの位置を制御し、こ
の制御によつて前記油圧駆動源のモータの駆動前
に主弁のスプールを中央位置に復帰させる零位置
制御手段を設けたことを特徴とする試験機の起動
制御装置。
1. In a test machine in which pressure oil from a hydraulic supply device is applied to an actuator by a two-stage amplification type servo valve consisting of a pilot valve and a main valve, and the test object is vibrated by this actuator, the hydraulic pressure supply device The system consists of a pilot hydraulic pressure supply system to the pilot valve and a main hydraulic pressure supply system to the main valve, and these hydraulic pressure supply systems are connected via a pressure equalization check valve, and a The motor is equipped with a delay means for delaying starting of the motor after the motor for driving the hydraulic power source of the pilot hydraulic pressure supply system is started, and a signal from a detector that detects the position of the main valve spool to detect the position of the pilot valve spool. 1. A starting control device for a testing machine, characterized in that the starting control device for a test machine is provided with zero position control means for returning a spool of a main valve to a central position before driving a motor of the hydraulic drive source.
JP55130729A 1980-09-22 1980-09-22 Start controller for tester Granted JPS5756734A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP55130729A JPS5756734A (en) 1980-09-22 1980-09-22 Start controller for tester

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP55130729A JPS5756734A (en) 1980-09-22 1980-09-22 Start controller for tester

Publications (2)

Publication Number Publication Date
JPS5756734A JPS5756734A (en) 1982-04-05
JPS639615B2 true JPS639615B2 (en) 1988-03-01

Family

ID=15041229

Family Applications (1)

Application Number Title Priority Date Filing Date
JP55130729A Granted JPS5756734A (en) 1980-09-22 1980-09-22 Start controller for tester

Country Status (1)

Country Link
JP (1) JPS5756734A (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07117086B2 (en) * 1992-05-01 1995-12-18 株式会社東邦製作所 Actuator for electro-pneumatic positioner
JP6015440B2 (en) * 2012-12-28 2016-10-26 株式会社島津製作所 Material testing machine
CN103267620B (en) * 2013-05-08 2015-06-10 西北工业大学 Testing device for functional characteristic test of valve
CN106593970B (en) * 2016-12-09 2018-05-11 柳州职业技术学院 A kind of rigid material fatigue test hydraulic loading device
CN110594228B (en) * 2019-10-09 2024-06-07 山东泰丰智能控制股份有限公司 Automatic vibration table hydraulic system that buffering was switched

Also Published As

Publication number Publication date
JPS5756734A (en) 1982-04-05

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