JP3494858B2 - Hydraulic servo device - Google Patents
Hydraulic servo deviceInfo
- Publication number
- JP3494858B2 JP3494858B2 JP21800397A JP21800397A JP3494858B2 JP 3494858 B2 JP3494858 B2 JP 3494858B2 JP 21800397 A JP21800397 A JP 21800397A JP 21800397 A JP21800397 A JP 21800397A JP 3494858 B2 JP3494858 B2 JP 3494858B2
- Authority
- JP
- Japan
- Prior art keywords
- space
- piston
- hydraulic servo
- servo device
- oil
- 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 - Lifetime
Links
- 239000012530 fluid Substances 0.000 claims description 11
- 230000008878 coupling Effects 0.000 claims description 9
- 238000010168 coupling process Methods 0.000 claims description 9
- 238000005859 coupling reaction Methods 0.000 claims description 9
- 239000002245 particle Substances 0.000 claims description 9
- 239000003921 oil Substances 0.000 description 62
- 239000010720 hydraulic oil Substances 0.000 description 13
- 230000000740 bleeding effect Effects 0.000 description 5
- 238000006073 displacement reaction Methods 0.000 description 5
- 230000004043 responsiveness Effects 0.000 description 5
- 230000004044 response Effects 0.000 description 4
- 238000012423 maintenance Methods 0.000 description 3
- 230000006872 improvement Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B21/00—Common features of fluid actuator systems; Fluid-pressure actuator systems or details thereof, not covered by any other group of this subclass
- F15B21/04—Special measures taken in connection with the properties of the fluid
- F15B21/044—Removal or measurement of undissolved gas, e.g. de-aeration, venting or bleeding
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B11/00—Servomotor systems without provision for follow-up action; Circuits therefor
- F15B11/08—Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor
- F15B11/12—Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor providing distinct intermediate positions; with step-by-step action
- F15B11/121—Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor providing distinct intermediate positions; with step-by-step action providing distinct intermediate positions
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B9/00—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member
- F15B9/02—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type
- F15B9/08—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor
- F15B9/10—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor in which the controlling element and the servomotor each controls a separate member, these members influencing different fluid passages or the same passage
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Actuator (AREA)
Description
【0001】[0001]
【発明の属する技術分野】本発明は、小トルクの回転変
位を大負荷の直線変位に変換する油圧サーボ装置に関
し、特に、可変速流体継手における変速機構であるスク
ープチューブの駆動制御に用いて好適な油圧サーボ装置
に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a hydraulic servo device for converting a rotational displacement of a small torque into a linear displacement of a large load, and is particularly suitable for use in drive control of a scoop tube which is a speed change mechanism in a variable speed fluid coupling. Hydraulic servo device.
【0002】[0002]
【従来の技術】図11は、例えば、大容量のボイラへ給
水するために用いる給水装置の駆動部の構成を示すもの
で、入力軸121の回転が大歯車122、小歯車124
を介して駆動軸123に増速して伝達され、これはさら
に流体継手Cを介して被動軸125に伝達され、さらに
大歯車131、小歯車133を介して出力軸132に増
速して伝達される。流体継手Cは、駆動軸123に取り
付けたインペラ126及びインペラケーシング128
と、被動軸125に取り付けたランナ127とを備えて
構成され、インペラケーシング128内に作動油が導入
されると作動油の粘性によって両者が連動して回転が伝
達されるようになっている。2. Description of the Related Art FIG. 11 shows a structure of a drive unit of a water supply device used for supplying water to a large capacity boiler, for example, the rotation of an input shaft 121 being a large gear 122 and a small gear 124.
Is transmitted to the drive shaft 123 via the fluid coupling C, is further transmitted to the driven shaft 125 via the fluid coupling C, and is further transmitted to the output shaft 132 via the large gear 131 and the small gear 133. To be done. The fluid coupling C includes an impeller 126 and an impeller casing 128 attached to the drive shaft 123.
And a runner 127 attached to the driven shaft 125. When the working oil is introduced into the impeller casing 128, the viscosity of the working oil causes the two to work together to transmit the rotation.
【0003】作動油室内には、作動油の量を調整するス
クープチューブ130が配置されており、これを出し入
れすることにより、流体継手の伝達トルクが制御され
る。このような流体継手Cでは、比較的簡単な構成で、
負荷側の回転数を最低回転数から最高回転数まで無段階
に変化させることができる。A scoop tube 130 for adjusting the amount of hydraulic oil is arranged in the hydraulic oil chamber, and the transmission torque of the fluid coupling is controlled by taking it in and out. Such a fluid coupling C has a relatively simple structure,
The rotation speed on the load side can be continuously changed from the minimum rotation speed to the maximum rotation speed.
【0004】スクープチューブは、作動油から受ける力
に対抗して正確な位置決めを行う必要があり、そのた
め、その駆動装置として、例えば特開平7−20849
9号に示すような電気アクチュエータによる小力の変位
を力を増幅して伝達する油圧サーボ装置が用いられる。
これは、シリンダ内に配置したパイロット軸にピストン
を摺動自在に設け、パイロット軸の表面とピストンの内
部に油路を形成し、パイロット軸の回転をピストンの変
位に変えて出力する。このような駆動装置により、例え
ば、所定位置に設けた変位センサからの信号を基にフィ
ードバック制御してスクープチューブの位置を制御する
ようにしている。The scoop tube needs to be accurately positioned against the force received from the hydraulic oil, and therefore, as a drive device thereof, for example, Japanese Patent Laid-Open No. 7-20849.
A hydraulic servo device as shown in No. 9 is used which amplifies and transmits a displacement of a small force by an electric actuator.
In this, a piston is slidably provided on a pilot shaft arranged in a cylinder, an oil passage is formed on the surface of the pilot shaft and inside the piston, and rotation of the pilot shaft is converted into displacement of the piston for output. With such a driving device, for example, feedback control is performed based on a signal from a displacement sensor provided at a predetermined position to control the position of the scoop tube.
【0005】[0005]
【発明が解決しようとする課題】上記のような油圧サー
ボ装置は、全体のバランスから小型化を図る必要があ
り、そのためには、パイロット軸の径を小さくする必要
がある。しかしながら、パイロット軸径を小さくすると
その表面の溝状の油路の幅も小さくなり、パイロット軸
の回転を速くすると、図3(b)に示すように、ピスト
ン内部の油路から外れて制御不能になる(脱輪する)場
合がある。従って、油圧サーボ装置の制御の応答性が制
限されるという不具合があった。In the hydraulic servo system as described above, it is necessary to reduce the size in view of the overall balance, and for that purpose, it is necessary to reduce the diameter of the pilot shaft. However, if the pilot shaft diameter is made smaller, the width of the groove-shaped oil passage on the surface becomes smaller, and if the rotation of the pilot shaft is made faster, as shown in FIG. It may become Therefore, there is a problem that the control response of the hydraulic servo device is limited.
【0006】この発明は、小径のパイロット軸であって
も油路が外れにくく、小型であって充分な制御応答性を
得ることができるような油圧サーボ装置を提供すること
を目的とする。It is an object of the present invention to provide a hydraulic servo system which is small in size and has a sufficient control response even if the pilot shaft has a small diameter.
【0007】[0007]
【課題を解決するための手段】請求項1に記載の発明
は、シリンダ内に配置されたパイロット軸とピストンと
を備え、前記パイロット軸を回転させて該パイロット軸
の表面に形成された導通路を上記ピストンに形成された
油路に連通させて前記ピストンを軸方向に駆動する油圧
サーボ装置において、前記ピストンと前記パイロット軸
に、それぞれ前記ピストンを同一方向に駆動するための
前記油路とが少なくとも2対設けられており、前記複数
の導通路及び油路の対は、連通する回転角度がずれるよ
うに設けられていることを特徴とする油圧サーボ装置で
ある。これにより、個々の油路や導通路の径や幅を大き
くすることなく、しかも連通角度をより広くして「脱
輪」が生じることを防止し、より高い制御応答性を得る
ことができる。According to a first aspect of the present invention, there is provided a pilot shaft and a piston arranged in a cylinder, and the pilot shaft is rotated to form a conduction path formed on a surface of the pilot shaft. In the hydraulic servo device that drives the piston in the axial direction by communicating with the oil passage formed in the piston, the piston and the pilot shaft each have the oil passage for driving the piston in the same direction. At least two pairs are provided, and the plurality of
The rotation angle at which the communication path and the oil path of the
The hydraulic servo device is characterized by being provided as described above. Thus, without increasing the diameter or width of each oil passage or conduction passage, the communication angle can be widened to prevent "wheel derailment" from occurring, and higher control response can be obtained.
【0008】請求項2に記載の発明は、前記導通路は、
パイロット軸の回転角に対して非線形に設けられている
ことを特徴とする請求項1に記載の油圧サーボ装置であ
る。[0008] The invention described in 請 Motomeko 2, the conducting path,
The hydraulic servo device according to claim 1, wherein the hydraulic servo device is provided in a non-linear manner with respect to a rotation angle of the pilot shaft.
【0009】前記油路は、圧力作動油に繋がる給油路と
ドレンに繋がる排油路が相互に独立に配置されているも
のであってもよい。[0009] Before Kiyuro also oil discharge passage leading to the oil supply passage and a drain connected to the pressure hydraulic fluid is arranged independently of one another
May be
【0010】請求項3に記載の発明は、前記シリンダ内
の空間は前記ピストンにより圧油孔を有する第1の空間
と、該第1の空間と前記導通路を介して連通し、又は遮
断される第2の空間に区画され、該第2の空間の上部に
は、外部空間に開口するエア抜き配管が設けられている
ことを特徴とする請求項1又は2に記載の油圧サーボ装
置である。これにより、空気が逃げにくい第2の空間か
ら被圧縮性の高い空気を排除して、高い応答性を維持す
ることができる。[0010] According to a third aspect of the invention, the space pre-Symbol cylinder communicates via the conductive path of the first space, the space of the first with a pressurized oil hole by the piston, or blocks 3. The hydraulic servo device according to claim 1, wherein the hydraulic servo device is divided into a second space, and an air vent pipe that opens to an external space is provided at an upper portion of the second space. is there. Thereby, highly compressible air can be removed from the second space in which air does not easily escape, and high responsiveness can be maintained.
【0011】前記エア抜き配管にオリフィスを設けても
よい。また、前記エア抜き配管に逆止弁を設けてもよ
い。[0011] be provided with the orifice before Symbol air vent pipe
Good . In addition, even if the check valve provided in the air vent pipe
Yes .
【0012】請求項4に記載の発明は、前記シリンダ内
の空間は前記ピストンにより圧油孔を有する第1の空間
と、該第1の空間と前記導通路を介して連通し、又は遮
断される第2の空間に区画され、前記第1及び/又は第
2の空間の下部に粒子を溜める凹所を形成したことを特
徴とする請求項1又は2に記載の油圧サーボ装置であ
る。これにより、粒子が凹所に集合するので、ピストン
とシリンダの摺動部において噛み込みを生じることが防
止され、安定な作動が行われる。[0012] According to a fourth aspect of the invention, the space before Symbol cylinder communicates via the conductive path of the first space, the space of the first with a pressurized oil hole by the piston, or blocks 3. The hydraulic servo device according to claim 1, wherein the hydraulic servo device is divided into a second space, and a recess for accumulating particles is formed in a lower portion of the first and / or the second space. As a result, the particles gather in the recess, so that the sliding portion between the piston and the cylinder is prevented from being caught, and stable operation is performed.
【0013】前記凹所に溜められた粒子を排出するため
の排出穴を設けてもよい。[0013] In order to discharge the reservoir was particles before Symbol recess
May be provided with a discharge hole.
【0014】請求項5に記載の発明は、シリンダ内に配
置されたパイロット軸とピストンとを備え、前記パイロ
ット軸を回転させて該パイロット軸の表面に形成された
導通路を上記ピストンに形成された油路に連通させて前
記ピストンを軸方向に駆動する油圧サーボ装置におい
て、前記シリンダ内の空間は前記ピストンにより圧油孔
を有する第1の空間と、該第1の空間と前記導通路を介
して連通し、又は遮断される第2の空間に区画され、前
記シリンダの前記第1の空間側の外部には、前記第1の
空間側の側壁に形成されたピストン摺動孔を覆う油溜ま
りが形成されていることを特徴とする油圧サーボ装置で
ある。According to a fifth aspect of the present invention, there is provided a pilot shaft and a piston arranged in the cylinder, and the pilot shaft is rotated to form a conduction path formed on the surface of the pilot shaft in the piston. In the hydraulic servo device that drives the piston in the axial direction by communicating with the oil passage, the space in the cylinder is formed by a first space having a pressure oil hole by the piston, and the first space and the communication passage. It is partitioned into a second space that is communicated with or cut off via the first space, and the first space is outside the cylinder on the first space side .
The hydraulic servo device is characterized in that an oil reservoir is formed to cover a piston sliding hole formed in a side wall on the space side .
【0015】シリンダ内に配置されたパイロット軸とピ
ストンとを備え、前記パイロット軸を回転させて該パイ
ロット軸の表面に形成された導通路を上記ピストンに形
成された油路に連通させて前記ピストンを軸方向に駆動
する油圧サーボ装置において、前記ピストンの一方の端
面に、該ピストンを引き出すための引出工具と係合する
係合部を設けてもよい。これにより、ピストンやシリン
ダのメンテナンス、さらにはピストンに取り付けられた
被駆動部材のメンテナンスや交換が容易になる。[0015] comprising a sheet disposed pilot shaft within cylinder and the piston, the surface which is formed on the conductive passages is rotated by said pilot shaft the pilot shaft is communicated with the oil passage formed in the piston the In the hydraulic servo device that drives the piston in the axial direction, one end surface of the piston may be provided with an engaging portion that engages with a drawing tool for drawing the piston. This facilitates the maintenance of the piston and the cylinder, and the maintenance and replacement of the driven member attached to the piston.
【0016】請求項6に記載の発明は、駆動軸に取り付
けたインペラ及びインペラケーシングと、被動軸に取り
付けたランナと、請求項1ないし5のいずれか1項に記
載の油圧サーボ装置によって位置制御されるスクープチ
ューブとを有することを特徴とする流体継手である。According to a sixth aspect of the present invention, the position control is performed by the impeller and the impeller casing attached to the drive shaft, the runner attached to the driven shaft, and the hydraulic servo device according to any one of the first to fifth aspects. And a scoop tube that is formed.
【0017】[0017]
【発明の実施の形態】以下、図面を参照して本発明の一
実施の形態の油圧サーボ装置を図11の流体継手のスク
ープチューブの駆動装置として用いた例を説明する。図
1の油圧サーボ装置は、圧力容器であるシリンダ10
と、シリンダ10の基端側に設けられたパイロット駆動
装置12と、このパイロット駆動装置12から該シリン
ダ10内に突出するパイロット軸14と、シリンダ10
とパイロット軸14の間の空間に回転を規制されつつ摺
動自在に配置されたピストン16とを備えている。ピス
トン16は、基端側の大径部18と先端側の小径部20
を備え、小径部20はシリンダ10の側壁22の摺動孔
24から外部に突出しており、その先端に被駆動部材で
あるスクープチューブを取り付けるための取付部26が
設けられている。BEST MODE FOR CARRYING OUT THE INVENTION An example in which a hydraulic servo device according to an embodiment of the present invention is used as a drive device for a scoop tube of a fluid coupling shown in FIG. 11 will be described below with reference to the drawings. The hydraulic servo device shown in FIG. 1 includes a cylinder 10 which is a pressure vessel.
A pilot drive device 12 provided on the base end side of the cylinder 10; a pilot shaft 14 protruding from the pilot drive device 12 into the cylinder 10;
And a piston 16 slidably arranged in the space between the pilot shaft 14 and the rotation thereof. The piston 16 has a large diameter portion 18 on the base end side and a small diameter portion 20 on the tip end side.
The small-diameter portion 20 protrudes from the sliding hole 24 of the side wall 22 of the cylinder 10 to the outside, and the tip of the small-diameter portion 20 is provided with a mounting portion 26 for mounting a scoop tube which is a driven member.
【0018】ピストン16は、シリンダ10内の空間
を、小径部20の外側の第1の空間28と大径部18側
の第2の空間30に区画している。シリンダ10の先端
側には、第1の空間28に連通する圧油路32が形成さ
れ、また、シリンダ10の内面にはストッパとなる凸部
34が形成されてピストン16の停止位置が規制され、
その最先端の位置においても圧油路32と繋がる第1の
空間28が確保されるようになっている。The piston 16 divides the space inside the cylinder 10 into a first space 28 outside the small diameter portion 20 and a second space 30 on the large diameter portion 18 side. A pressure oil passage 32 communicating with the first space 28 is formed on the tip end side of the cylinder 10, and a convex portion 34 serving as a stopper is formed on the inner surface of the cylinder 10 to regulate the stop position of the piston 16. ,
The first space 28 connected to the pressure oil passage 32 is ensured even at the most advanced position.
【0019】小径部20にはパイロット軸14を挿通さ
せる中心孔36と、第1の空間28から径方向に延びて
中心孔36に開口する給油路38が、図2に示すように
中心に対してほぼ対称な位置に2つ設けられている。ま
た、給油路38に対してほぼ軸線を含む断面に面対称と
なる位置に排油路40が形成され、これは取付部26に
おいて開口している。排油路40と中心孔36はいずれ
も外部のドレンに繋がっている。A center hole 36 for inserting the pilot shaft 14 into the small diameter portion 20 and an oil supply passage 38 extending in the radial direction from the first space 28 and opening to the center hole 36 are provided with respect to the center as shown in FIG. Two are provided at substantially symmetrical positions. Further, an oil discharge passage 40 is formed at a position symmetrical with respect to the oil supply passage 38 in a cross section including an axis line, and the oil discharge passage 40 is opened at the attachment portion 26. Both the oil discharge passage 40 and the center hole 36 are connected to an external drain.
【0020】一方、パイロット軸14の表面には、その
回転位置に応じて給油路38と第2の空間30とを連通
する溝状の導通路42が、図2に示すように中心に対し
てほぼ対称な位置に2つ設けられている。この導通路4
2は、ピストン16のストロークに対応する長さに渡っ
てパイロット軸14をほぼ半周するような螺旋状に形成
されている。この例では、給油路38、排油路40の径
は導通路42の幅と等しく設定されている。On the other hand, on the surface of the pilot shaft 14, there is provided a groove-shaped conduction path 42 for communicating the oil supply path 38 and the second space 30 with respect to the center, as shown in FIG. Two are provided at substantially symmetrical positions. This conduction path 4
2 is formed in a spiral shape so as to extend around the pilot shaft 14 almost half over the length corresponding to the stroke of the piston 16. In this example, the diameters of the oil supply passage 38 and the oil discharge passage 40 are set to be equal to the width of the conduction passage 42.
【0021】第1の空間28におけるピストン16の受
圧面は大径部18の断面から小径部20の断面を引いた
差の部分であるが、第2の空間30における受圧面は大
径部18の断面からパイロット軸14を引いた部分であ
り、第2の空間30の受圧面の方が大きい。従って、導
通路42が給油路38と第2の空間30を連通させて第
1の空間28と第2の空間30の双方に同じ作動油圧力
が掛かった場合には、ピストン16は先端側に移動す
る。また、導通路42が排油路40と第2の空間30を
連通させて第1の空間28のみに作動油圧力が掛かった
場合には、ピストン16は基端側に移動する。The pressure receiving surface of the piston 16 in the first space 28 is the difference between the cross section of the large diameter portion 18 and the cross section of the small diameter portion 20, but the pressure receiving surface in the second space 30 is the large diameter portion 18. Is a portion obtained by subtracting the pilot shaft 14 from the cross section, and the pressure receiving surface of the second space 30 is larger. Therefore, when the conduction path 42 connects the oil supply path 38 and the second space 30 and the same hydraulic oil pressure is applied to both the first space 28 and the second space 30, the piston 16 moves toward the tip side. Moving. Further, when the fluid passage 42 connects the oil discharge passage 40 and the second space 30 and hydraulic oil pressure is applied only to the first space 28, the piston 16 moves to the base end side.
【0022】なお、この例の導通路42は、図4に示す
ように、角度に対して非直線的に形成され、これによっ
て結果的に入力(回転角度)に対する出力(ピストン1
6のストローク)の直線性を維持している。大径部18
は中空に形成され、ピストン16が最も基端側に移動し
た場合でも導通路42がピストン16によって覆われな
いようになっている。The conduction path 42 in this example is formed non-linearly with respect to the angle as shown in FIG. 4, and as a result, the output (piston 1) with respect to the input (rotation angle) is eventually obtained.
6 stroke) is maintained. Large diameter part 18
Is formed to be hollow so that the conduction path 42 is not covered by the piston 16 even when the piston 16 moves to the most proximal side.
【0023】この例では、第1の給油路38と第1の排
油路40及び第2の給油路38と第2の排油路40がそ
れぞれ重なり合うパイロット軸14の回転角度には、図
5に示すように、油路38,40の幅に対応する角度θ
を超えない程度のずれαがある。この結果、1つの給油
路38と排油路40のみの場合に比べて重なり合う角度
範囲が大きくなって(2θ+α)、双方の重なり合いが
外れて操作不能になる事態が起きにくくなる。In this example, the rotation angle of the pilot shaft 14 at which the first oil supply passage 38 and the first oil discharge passage 40 and the second oil supply passage 38 and the second oil discharge passage 40 overlap each other is as shown in FIG. , The angle θ corresponding to the width of the oil passages 38, 40
There is a deviation α that does not exceed As a result, compared with the case where only one oil supply passage 38 and one oil discharge passage 40 are provided, the overlapping angular range becomes large (2θ + α), and it becomes difficult for the situation in which both overlaps are lost and operation becomes impossible.
【0024】上記のような構成の油圧サーボ装置の作用
を説明する。パイロット軸14を、図2(a)に示す導
通路42が給油路38とも排油路40とも連通していな
い状態から矢印方向に回動すると、図2(b)に示すよ
うに、導通路42が給油路38と連通し始める。これに
より、第1の空間28の作動油圧力が給油路38、導通
路42を介して第2の空間30に伝えられ、ピストン1
6の受圧面積差からピストン16は先端側へ押される。
導通路42はパイロット軸14の稜線に対して傾斜して
いるので、ピストン16が先端側に移動すると導通路4
2と給油路38は、図2(a)に示すもとの連通しない
位置関係に戻って停止する。The operation of the hydraulic servo device having the above structure will be described. When the pilot shaft 14 is rotated in the arrow direction from the state in which the conduction path 42 shown in FIG. 2 (a) is not in communication with the oil supply passage 38 or the oil discharge passage 40, as shown in FIG. 42 starts to communicate with the oil supply passage 38. As a result, the hydraulic oil pressure in the first space 28 is transmitted to the second space 30 via the oil supply passage 38 and the conduction passage 42, and the piston 1
The piston 16 is pushed toward the tip end side due to the pressure receiving area difference of 6.
Since the conduction path 42 is inclined with respect to the ridgeline of the pilot shaft 14, when the piston 16 moves toward the tip side, the conduction path 4
2 and the oil supply passage 38 return to the original positional relationship where they do not communicate as shown in FIG.
【0025】さらに、パイロット軸14を回動して、図
2(b)に示す位置関係にすると、ピストン16は同じ
ように移動する。これを、ピストン16の軸方向位置を
検知してフィードバック制御しながら連続的に繰り返す
ことにより、ピストン16を軸方向の任意の位置に置く
ことができる。Further, when the pilot shaft 14 is rotated to bring the positional relationship shown in FIG. 2 (b), the piston 16 moves in the same manner. By continuously repeating this while detecting the axial position of the piston 16 and performing feedback control, the piston 16 can be placed at an arbitrary position in the axial direction.
【0026】ここで、負荷が大きい場合などで図2
(b)の状態でもピストン16が移動しないあるいは移
動量が小さい場合には、制御装置からさらにパイロット
駆動装置12に信号が出されてパイロット軸14が矢印
方向に回動され、図3(a)の状態に至る。この状態で
は、2つの導通路42から作動油が流入するので、ピス
トン16を駆動する力も大きくなって応答性が向上す
る。もし、制御装置からさらにパイロット駆動装置12
に回動信号が出ても、給油路38及び導通路42が連通
する回転角度範囲が広いので「脱輪」しにくい。Here, when the load is large, etc., FIG.
If the piston 16 does not move or the movement amount is small even in the state of (b), a signal is further output from the control device to the pilot drive device 12 and the pilot shaft 14 is rotated in the direction of the arrow, as shown in FIG. Reach the state of. In this state, since the hydraulic oil flows in from the two conduction paths 42, the force for driving the piston 16 is also increased and the responsiveness is improved. If the pilot drive 12
Even if a rotation signal is output to the oil supply path 38, since the rotation angle range in which the oil supply passage 38 and the conduction passage 42 communicate with each other is wide, it is difficult to "detach."
【0027】次に、ピストン16を軸方向基端側に移動
させる場合には、図2(a)に示す状態から、パイロッ
ト軸14を図2(b)とは逆の方向に回転させる。する
と、導通路42は排油路40と連通し始め、第2の空間
30がドレンと同じ低圧となる。この結果、第1の空間
28の作動油からの圧力により、ピストン16は導通路
42は排油路40が図2(a)に示す状態に戻るまで基
端側に移動する。これをフィードバック制御しながら繰
り返すことにより、ピストン16の位置が制御される。
第1の排油路40に対して、給油路38の場合と同じ位
置関係にある第2の排油路40が設けられているので、
応答性の向上及び脱輪の防止の作用は順方向への移動と
同様に維持されている。Next, when moving the piston 16 toward the base end side in the axial direction, the pilot shaft 14 is rotated in the direction opposite to that shown in FIG. 2B from the state shown in FIG. 2A. Then, the conduction path 42 starts to communicate with the oil discharge path 40, and the second space 30 has the same low pressure as the drain. As a result, the pressure from the hydraulic oil in the first space 28 causes the piston 16 to move to the base end side of the conduction path 42 until the oil discharge path 40 returns to the state shown in FIG. 2A. By repeating this while performing feedback control, the position of the piston 16 is controlled.
Since the second oil discharge passage 40 having the same positional relationship as that of the oil supply passage 38 is provided for the first oil discharge passage 40,
The functions of improving the responsiveness and preventing the wheel loss are maintained in the same manner as the forward movement.
【0028】図6は、この発明の他の実施の形態を示す
もので、シリンダ10の第2の空間30の基端側上部に
エア抜き配管44を設けたものである。このエア抜き配
管44はオリフィス46を介して適当な空間(大気圧)
に開口している。この実施の形態においては、圧油路3
2から流入する作動油中に含まれて第2の空間30に溜
まった空気は、このエア抜き配管44から放出されるの
で、このような空気が油圧サーボ装置の応答性に与える
悪影響を抑えることができる。また、微細孔を有するオ
リフィス46により、第2の空間30の圧力を維持した
ままで空気の放出を行なうことができる。FIG. 6 shows another embodiment of the present invention, in which an air bleeding pipe 44 is provided in the upper portion of the second space 30 of the cylinder 10 on the proximal end side. The air bleeding pipe 44 has an appropriate space (atmospheric pressure) through the orifice 46.
It is open to. In this embodiment, the pressure oil passage 3
The air contained in the hydraulic oil flowing in from 2 and accumulated in the second space 30 is discharged from the air bleeding pipe 44, so that the adverse effect of such air on the response of the hydraulic servo device can be suppressed. You can Further, the orifice 46 having the fine holes allows air to be discharged while maintaining the pressure in the second space 30.
【0029】図7は、この発明のさらに他の実施の形態
を示すもので、図6の実施の形態を改良したものであ
る。シリンダ10上部には、オリフィス46を介して大
気に繋がるエア抜き配管44が設けられ、さらに、シリ
ンダ10の先端側外部にシリンダ10の側壁22の摺動
孔24を覆うように油溜まり48が形成されている。こ
の油溜まり48は、シリンダ10側壁22に取り付けた
底板50及び壁52等の部材により形成され、この壁5
2には必要に応じて被駆動部材等を挿通する孔を形成す
る。油溜まりの高さはエア抜き配管44の接続位置と同
じかそれ以上であることが好ましい。FIG. 7 shows still another embodiment of the present invention, which is an improvement of the embodiment of FIG. An air vent pipe 44 connected to the atmosphere via an orifice 46 is provided above the cylinder 10, and an oil sump 48 is formed outside the tip end side of the cylinder 10 so as to cover the sliding hole 24 of the side wall 22 of the cylinder 10. Has been done. The oil sump 48 is formed by members such as a bottom plate 50 and a wall 52 attached to the side wall 22 of the cylinder 10.
A hole for inserting a driven member or the like is formed in 2 as required. The height of the oil sump is preferably equal to or higher than the connection position of the air vent pipe 44.
【0030】図6の実施の形態では、エア抜き配管44
がオリフィス46を介して大気に繋がっているために、
装置が停止していて第2の空間30に圧力が掛かってい
ない状態では第2の空間30のヘッド分の圧力により、
摺動孔とピストン16の小径部20の隙間から作動油が
滲出し、その分空気が流入して、次の始動時に動作の不
安定や応答性の低下を生じる。これに対して、図7の実
施の形態では、摺動孔の外側の空間に油溜まりを形成し
て、摺動孔と小径部20の間における作動油の滲出を防
止して安定な動作を確保することができる。In the embodiment shown in FIG. 6, the air vent pipe 44
Is connected to the atmosphere through the orifice 46,
In the state where the device is stopped and the pressure is not applied to the second space 30, due to the pressure of the head of the second space 30,
The hydraulic oil oozes out from the gap between the sliding hole and the small diameter portion 20 of the piston 16, and the air flows in as much as that amount, resulting in unstable operation and reduced responsiveness at the next start. On the other hand, in the embodiment of FIG. 7, an oil sump is formed in the space outside the sliding hole to prevent the hydraulic oil from seeping out between the sliding hole and the small-diameter portion 20 for stable operation. Can be secured.
【0031】図8は、同様に図6の実施の形態を改良し
たもので、エア抜き配管44にオリフィス46に加えて
逆止弁54を設けたものである。この逆止弁54は、装
置の運転が停止されている場合において、エア抜き配管
44より第2の空間30にエア等が流入するのを防止す
るものである。なお、逆止弁の替わりに、遠隔操作又は
自動操作可能な開閉弁を用いて、必要なときのみに開く
ようにしてもよい。FIG. 8 is also an improvement of the embodiment of FIG. 6, in which the check valve 54 is provided in the air vent pipe 44 in addition to the orifice 46. The check valve 54 prevents air and the like from flowing into the second space 30 from the air bleeding pipe 44 when the operation of the device is stopped. Instead of the check valve, an on-off valve that can be operated remotely or automatically may be used so that it can be opened only when necessary.
【0032】図9は、この発明のさらに他の実施の形態
を示すものである。この実施の形態のシリンダ10に
は、第1の空間28及び第2の空間30内でピストン1
6とシリンダ10の摺動に伴い生成された粒子を一時的
に収容する凹所56が、シリンダ10の先端側及び基端
側のそれぞれ端部に形成されている。この例ではそれぞ
れの凹所56の底部に溜まった粒子Pを排出するための
排出孔58が設けられ、これは耐圧性のある栓60によ
り塞がれている。この実施の形態では、摺動に伴い生成
した粒子Pは底面の凹所56に掻き寄せられてここに溜
まるので、摺動部分に残る確率が小さくなり、従って、
摺動部での噛み込みの発生も減少する。ある程度溜まっ
た粒子Pは、装置の不使用時に栓60を開けて作動油等
により洗浄することで排出される。FIG. 9 shows still another embodiment of the present invention. The cylinder 10 of this embodiment includes the piston 1 in the first space 28 and the second space 30.
Recesses 56 for temporarily containing particles generated by the sliding of the cylinder 6 and the cylinder 10 are formed at the ends of the cylinder 10 on the front end side and the base end side, respectively. In this example, a discharge hole 58 for discharging the particles P accumulated at the bottom of each recess 56 is provided, and this is closed by a pressure resistant plug 60. In this embodiment, the particles P generated along with the sliding are scraped by the recesses 56 on the bottom surface and accumulate there, so that the probability of remaining in the sliding portions is reduced, and therefore,
Occurrence of biting in the sliding portion is also reduced. The particles P accumulated to some extent are discharged by opening the plug 60 and washing with hydraulic oil or the like when the apparatus is not used.
【0033】図10はこの発明の他の実施の形態であ
り、油圧サーボ装置のメンテナンスの便宜を図るように
したものである。すなわち、ピストン16の大径部18
の端面に、これを引き出すための引出工具である長尺ボ
ルト62と螺合するねじ穴64が形成されている。この
実施の形態では、シリンダ10内から作動油を抜いた
後、シリンダ10の基端側の側壁22を外し、パイロッ
ト軸14を抜き出した後、長尺ボルト62をねじ穴64
に螺合して、該ボルト62によりピストン16を抜き出
す。これにより、シリンダ10自体を取り外したりする
ことなしに、ピストン16を取り出し、シリンダ10の
中やピストン16に取り付けられた被駆動部材等を容易
にメンテナンスすることができる。FIG. 10 shows another embodiment of the present invention for the convenience of maintenance of the hydraulic servo device. That is, the large diameter portion 18 of the piston 16
A threaded hole 64 is formed on the end face of the screw hole, which is screwed into a long bolt 62, which is a pull-out tool for pulling the screw. In this embodiment, after draining the hydraulic oil from the inside of the cylinder 10, the side wall 22 on the base end side of the cylinder 10 is removed, the pilot shaft 14 is pulled out, and then the long bolt 62 is screwed into the screw hole 64.
And the piston 16 is pulled out by the bolt 62. Accordingly, the piston 16 can be taken out and the driven member and the like attached to the cylinder 10 and the piston 16 can be easily maintained without removing the cylinder 10 itself.
【0034】[0034]
【発明の効果】以上説明したように、この発明の油圧サ
ーボ装置によれば、個々の油路や導通路の径や幅を大き
くすることなく、しかも連通角度をより広くして「脱
輪」が生じることを防止し、従って、小型であって充分
な制御応答性を得ることができるような油圧サーボ装置
を提供することができる。As described above, according to the hydraulic servo system of the present invention, the diameter of the individual oil passages and the connecting passages and the width of the passages are not increased, and the communication angle is widened to "derail". Therefore, it is possible to provide a hydraulic servo device which is small in size and can obtain a sufficient control responsiveness.
【図1】本発明の一実施例の油圧サーボ装置の一部を破
断して示す斜視図である。FIG. 1 is a partially cutaway perspective view of a hydraulic servo device according to an embodiment of the present invention.
【図2】図1の、(a)ある回転位置での油路と導通路
の取り合いを示す断面図、(b)別の回転位置での油路
と導通路の取り合いを示す断面図である。2A is a sectional view showing an engagement between an oil passage and a conduction passage at a certain rotation position in FIG. 1, and FIG. 2B is a sectional view showing an engagement between the oil passage and the conduction passage at another rotation position. .
【図3】図1の、(a)さらに別の回転位置での油路と
導通路の取り合いを示す断面図、(b)従来の油圧サー
ボ装置の油路と導通路の取り合いを示す断面図である。3A is a cross-sectional view showing an engagement between an oil passage and a conduction passage at another rotation position in FIG. 1, and FIG. 3B is a cross-sectional view showing an engagement between an oil passage and a conduction passage of a conventional hydraulic servo device. Is.
【図4】導通路の展開図である。FIG. 4 is a development view of a conduction path.
【図5】油路と導通路の第1の対と第2の対の連通する
回転角度を示すグラフである。FIG. 5 is a graph showing rotation angles at which the first pair and the second pair of the oil passage and the communication passage communicate with each other.
【図6】この発明の第2の実施の形態の断面図である。FIG. 6 is a sectional view of a second embodiment of the present invention.
【図7】この発明の第3の実施の形態の断面図である。FIG. 7 is a sectional view of a third embodiment of the present invention.
【図8】この発明の第4の実施の形態の断面図である。FIG. 8 is a sectional view of a fourth embodiment of the present invention.
【図9】この発明の第5の実施の形態の断面図である。FIG. 9 is a sectional view of a fifth embodiment of the present invention.
【図10】この発明の第6の実施の形態の断面図であ
る。FIG. 10 is a sectional view of a sixth embodiment of the present invention.
【図11】この発明の油圧サーボ装置が用いられる流体
継手の断面図である。FIG. 11 is a sectional view of a fluid coupling in which the hydraulic servo device according to the present invention is used.
10 シリンダ 14 パイロット軸 16 ピストン 28 第1の空間 30 第2の空間 32 圧油孔 38 給油路 40 排油路 42 導通路 44 エア抜き配管 46 オリフィス 48 油溜まり 54 逆止弁 56 凹所 58 排出穴 62 引出工具 64 係合部 P 粒子 10 cylinders 14 Pilot shaft 16 pistons 28 First Space 30 Second space 32 Pressure oil hole 38 oil supply passage 40 oil drain 42 Conducting path 44 Air bleeding pipe 46 Orifice 48 oil sump 54 Check valve 56 recess 58 discharge hole 62 Drawing tool 64 Engagement part P particles
フロントページの続き (72)発明者 服部 和男 東京都大田区羽田旭町11番1号 株式会 社 荏原製作所内 (56)参考文献 特開 平2−286901(JP,A) 特開 平7−208499(JP,A) 特開 平9−53607(JP,A) 特開 平5−118352(JP,A) 実開 昭58−132517(JP,U) (58)調査した分野(Int.Cl.7,DB名) F15B 15/14 380 F16D 33/14 F15B 9/00 F15B 21/04 Front page continuation (72) Inventor Kazuo Hattori 11-11 Haneda Asahi-cho, Ota-ku, Tokyo Inside the EBARA CORPORATION (56) References JP-A-2-286901 (JP, A) JP-A-7-208499 (JP, A) JP-A-9-53607 (JP, A) JP-A-5-118352 (JP, A) Actually developed 58-132517 (JP, U) (58) Fields investigated (Int. Cl. 7) , DB name) F15B 15/14 380 F16D 33/14 F15B 9/00 F15B 21/04
Claims (6)
ピストンとを備え、前記パイロット軸を回転させて該パ
イロット軸の表面に形成された導通路を上記ピストンに
形成された油路に連通させて前記ピストンを軸方向に駆
動する油圧サーボ装置において、 前記ピストンと前記パイロット軸に、それぞれ前記ピス
トンを同一方向に駆動するための前記油路と導通路が少
なくとも2対設けられており、 前記複数の導通路及び油路の対は、連通する回転角度が
ずれるように設けられていることを特徴とする油圧サー
ボ装置。1. A pilot shaft and a piston arranged in a cylinder, wherein the pilot shaft is rotated so that a passage formed on a surface of the pilot shaft communicates with an oil passage formed on the piston. In the hydraulic servo device that drives the piston in the axial direction, at least two pairs of the oil passage and the conduction passage for driving the piston in the same direction are provided on the piston and the pilot shaft, respectively. A hydraulic servo device, wherein a pair of a conduction path and an oil path is provided such that the rotation angles communicating with each other are deviated.
対して非線形に設けられていることを特徴とする請求項
1に記載の油圧サーボ装置。2. The hydraulic servo device according to claim 1, wherein the conduction path is provided in a non-linear manner with respect to a rotation angle of the pilot shaft.
より圧油孔を有する第1の空間と、該第1の空間と前記
導通路を介して連通し、又は遮断される第2の空間に区
画され、該第2の空間の上部には、外部空間に開口する
エア抜き配管が設けられていることを特徴とする請求項
1又は2に記載の油圧サーボ装置。Space 3. Before Symbol cylinder comprises a first space having a pressure oil bore by the piston, communicates through the conductive path with the first space, or the blocked second space are claim is partitioned in the upper portion of the second space, characterized in that the air vent pipe opening into the external space is provided
The hydraulic servo device according to 1 or 2 .
より圧油孔を有する第1の空間と、該第1の空間と前記
導通路を介して連通し、又は遮断される第2の空間に区
画され、前記第1及び/又は第2の空間の下部に粒子を
溜める凹所を形成したことを特徴とする請求項1又は2
に記載の油圧サーボ装置。Space 4. A front Symbol cylinder comprises a first space having a pressure oil bore by the piston, communicates through the conductive path with the first space, or the blocked second space are It is defined, according to claim 1 or 2, characterized by forming a recess for storing the particles at the bottom of the first and / or second space
The hydraulic servo device described in .
ピストンとを備え、前記パイロット軸を回転させて該パ
イロット軸の表面に形成された導通路を上記ピストンに
形成された油路に連通させて前記ピストンを軸方向に駆
動する油圧サーボ装置において、 前記シリンダ内の空間は前記ピストンにより圧油孔を有
する第1の空間と、該第1の空間と前記導通路を介して
連通し、又は遮断される第2の空間に区画され、前記シ
リンダの前記第1の空間側の外部には、前記第1の空間
側の側壁に形成されたピストン摺動孔を覆う油溜まりが
形成されていることを特徴とする油圧サーボ装置。5. A pilot shaft and a piston arranged in a cylinder are provided, and the pilot shaft is rotated so that a passage formed on the surface of the pilot shaft is communicated with an oil passage formed on the piston. In a hydraulic servo device that drives the piston in an axial direction, a space in the cylinder communicates with or is disconnected from a first space having a pressure oil hole by the piston and the first space via the communication path. Is formed in a second space, and an oil sump is formed outside the cylinder on the side of the first space to cover a piston sliding hole formed on a side wall of the side of the first space. A hydraulic servo device.
ラケーシングと、被動軸に取り付けたランナと、請求項
1ないし5のいずれか1項に記載の油圧サーボ装置によ
って位置制御されるスクープチューブとを有することを
特徴とする流体継手。6. An impeller and an impeller casing attached to a drive shaft, a runner attached to a driven shaft, and a scoop tube whose position is controlled by the hydraulic servo device according to claim 1. A fluid coupling characterized by the following.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP21800397A JP3494858B2 (en) | 1997-07-29 | 1997-07-29 | Hydraulic servo device |
DE69820934T DE69820934T2 (en) | 1997-07-29 | 1998-07-28 | Hydraulic servo device |
EP98114115A EP0894982B1 (en) | 1997-07-29 | 1998-07-28 | Hydraulic servo device |
CN98103096.3A CN1124418C (en) | 1997-07-29 | 1998-07-29 | Hydraulic servo device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP21800397A JP3494858B2 (en) | 1997-07-29 | 1997-07-29 | Hydraulic servo device |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH1144303A JPH1144303A (en) | 1999-02-16 |
JP3494858B2 true JP3494858B2 (en) | 2004-02-09 |
Family
ID=16713111
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP21800397A Expired - Lifetime JP3494858B2 (en) | 1997-07-29 | 1997-07-29 | Hydraulic servo device |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0894982B1 (en) |
JP (1) | JP3494858B2 (en) |
CN (1) | CN1124418C (en) |
DE (1) | DE69820934T2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20180063504A (en) * | 2016-12-02 | 2018-06-12 | 한국남부발전 주식회사 | Large capacity fluid coupling having device for controlling oil pressure scoop tube |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7249458B2 (en) * | 2005-07-22 | 2007-07-31 | Ashradn Holdings Ltd. | Self-contained hydraulic actuator system |
WO2009108273A2 (en) * | 2008-02-29 | 2009-09-03 | Cbe Global Holdings, Inc. | Single-axis drive system and method |
EP2396556B1 (en) * | 2009-02-10 | 2015-04-22 | CBE Global Holdings, Inc. | Non-linear actuator system and method |
CN103029828B (en) * | 2012-12-11 | 2016-03-23 | 江西洪都航空工业集团有限责任公司 | A kind of Mechanical rotation actuator |
GB2517459A (en) * | 2013-08-21 | 2015-02-25 | Airbus Uk Ltd | A hydraulic actuator arrangement |
CN119755174B (en) * | 2025-03-06 | 2025-05-23 | 长春一东汽车零部件制造有限责任公司 | Electric servo hydraulic cylinder |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2874542A (en) * | 1943-04-21 | 1959-02-24 | Sperry Rand Corp | Motion reproducing mechanism |
GB693504A (en) * | 1949-07-25 | 1953-07-01 | Boulton Aircraft Ltd | Improvements in and relating to servo systems |
US2926635A (en) * | 1957-12-24 | 1960-03-01 | Clark Equipment Co | Power shifting mechanism |
US3757640A (en) * | 1971-12-01 | 1973-09-11 | Avco Corp | Simplified follower servomechanism |
US4245547A (en) * | 1977-10-31 | 1981-01-20 | Commercial Shearing, Inc. | Rotary to linear servo mechanisms |
DE3374578D1 (en) * | 1982-02-26 | 1987-12-23 | Parisienne Outillage | Hydraulic directional spool valve |
JPS60256603A (en) * | 1984-06-01 | 1985-12-18 | Yukio Watanabe | Cylinder device |
JPH0729313Y2 (en) * | 1990-10-18 | 1995-07-05 | 株式会社大金製作所 | Release device for pull type clutch |
DE19537417C2 (en) * | 1995-10-07 | 1997-07-24 | Eurocopter Deutschland | Hydraulic actuator |
-
1997
- 1997-07-29 JP JP21800397A patent/JP3494858B2/en not_active Expired - Lifetime
-
1998
- 1998-07-28 DE DE69820934T patent/DE69820934T2/en not_active Expired - Lifetime
- 1998-07-28 EP EP98114115A patent/EP0894982B1/en not_active Expired - Lifetime
- 1998-07-29 CN CN98103096.3A patent/CN1124418C/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20180063504A (en) * | 2016-12-02 | 2018-06-12 | 한국남부발전 주식회사 | Large capacity fluid coupling having device for controlling oil pressure scoop tube |
KR101888053B1 (en) | 2016-12-02 | 2018-08-13 | 한국남부발전(주) | Large capacity fluid coupling having device for controlling oil pressure scoop tube |
Also Published As
Publication number | Publication date |
---|---|
DE69820934D1 (en) | 2004-02-12 |
DE69820934T2 (en) | 2004-11-04 |
EP0894982A3 (en) | 2000-05-24 |
JPH1144303A (en) | 1999-02-16 |
CN1210208A (en) | 1999-03-10 |
EP0894982A2 (en) | 1999-02-03 |
EP0894982B1 (en) | 2004-01-07 |
CN1124418C (en) | 2003-10-15 |
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