JPH01294979A - electronically controlled pump - Google Patents

electronically controlled pump

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Publication number
JPH01294979A
JPH01294979A JP63124192A JP12419288A JPH01294979A JP H01294979 A JPH01294979 A JP H01294979A JP 63124192 A JP63124192 A JP 63124192A JP 12419288 A JP12419288 A JP 12419288A JP H01294979 A JPH01294979 A JP H01294979A
Authority
JP
Japan
Prior art keywords
pressure
valve
line
discharge line
discharge
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
Application number
JP63124192A
Other languages
Japanese (ja)
Other versions
JP2560415B2 (en
Inventor
Junichi Miyagi
淳一 宮城
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.)
Daikin Industries Ltd
Original Assignee
Daikin Industries 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 Daikin Industries Ltd filed Critical Daikin Industries Ltd
Priority to JP63124192A priority Critical patent/JP2560415B2/en
Publication of JPH01294979A publication Critical patent/JPH01294979A/en
Application granted granted Critical
Publication of JP2560415B2 publication Critical patent/JP2560415B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Control Of Positive-Displacement Pumps (AREA)

Abstract

PURPOSE:To simply an surely damp serge pressure in a discharge line from a pump by connecting an inlet port to the discharge line, and by connecting a spring chamber to an orifice in a pilot line branching off from the discharge line while providing a serve absorbing valve. CONSTITUTION:An electronic controller 17 changes over a servo valve 10 so as to connect the secondary port A thereof to a pilot line 8 branching off from a discharge line 6 connected to a hydraulic cylinder 21 when a serge pressure is produced in the discharge line 6. Further, a pressure control valve 14 is changed over so as to connect its secondary port A top the secondary port A of the servo valve 10. Further, a swash plate 2 in a pump 1 is tilted toward a neutral position so as to discharge oil at a high pressure but at a low flow rate. In this arrangement, with the use of a differential pressure across an orifice 7 in the pilot line 8, the serge pressure is opened. Thereby it is possible to relieve the serge pressure from the discharge line 6 into a tank 22 even though a relief valve 13 does not open.

Description

【発明の詳細な説明】 〈産業」二の利用分野〉 本発明は、電子コントローラからの偏差信号が人力され
るサーボ弁によって斜板を傾動させ、吐出圧や吐出量を
目標値に制御する電子制御ポンプに関する。
[Detailed Description of the Invention] <Industry> 2 Field of Application The present invention is an electronic device that tilts a swash plate using a servo valve that receives a deviation signal from an electronic controller and controls the discharge pressure and discharge amount to a target value. Regarding control pumps.

〈従来の技術〉 従来、この種の電子制御ポンプとして、例えばバイアス
スプリングに抗して動作して斜板を中立方向に傾動させ
るサーボシリンダを何する可変容量形ポンプと、2次ポ
ートを上記可変容量形ポンプの吐出ラインから分岐する
パイロットラインとタンクとに切換接続ずろサーボ弁と
、上記パイロットラインに絞りを介して接続された安全
弁と、上記サーボシリンダに連通ずる2次ポートを上記
サーボ弁の2次ポートと上記パイロットラインとに上記
絞りの前後の差圧に応動して切換接続する圧力制御弁と
、上記吐出ラインに介設した圧カセンザや斜板角センサ
の検出値と吐出圧や吐出量の設定値との偏差に応じた制
御信号を上記サーボ弁に出力する電子コントローラを備
えたちのが知られている。そして、この電子制御ポンプ
は、吐出ラインが昇圧して安全弁が開成するとき、上記
絞りを流れろ圧油の前後の差圧によって圧力制御弁が切
り換わってサーボシリンダに吐出ラインの圧力を導くこ
とによって、斜板を中立位置まで傾動さけて吐出量を最
小Iこするようになっている。
<Prior Art> Conventionally, as this type of electronically controlled pump, for example, a variable displacement pump has a servo cylinder that operates against a bias spring to tilt a swash plate in a neutral direction, and a secondary port has a variable displacement pump as described above. A pilot line branched from the discharge line of the displacement pump is connected to the tank, a safety valve is connected to the pilot line via a throttle, and a secondary port communicating with the servo cylinder is connected to the servo valve. A pressure control valve is connected to the secondary port and the pilot line in response to the differential pressure before and after the throttle, and the detection values of the pressure sensor and swash plate angle sensor installed in the discharge line, as well as the discharge pressure and discharge. It is known to include an electronic controller that outputs a control signal to the servo valve according to the deviation from the set value of the amount. In this electronically controlled pump, when the pressure in the discharge line increases and the safety valve opens, the pressure control valve is switched by the differential pressure before and after the pressure oil flowing through the throttle, and the pressure in the discharge line is guided to the servo cylinder. , the swash plate is tilted to the neutral position to reduce the discharge amount to the minimum I.

〈発明が解決しようとする課題〉 一般に、油圧ポンプの吐出ラインに切換弁等を介して油
圧シリンダを接続して駆動ずろ場合、ストロークエンド
などで上記切換弁を切り換えて大流量制御から圧力制御
に移るとき、吐出ラインに大きなサージ圧力が発生ずる
ことはよく知られている。ところが、上記従来の電子制
御ポンプは、上記最高設定圧力よりら若干高い設定圧で
圧力制御弁を介して斜板を中立へ傾動させろ方式の安全
弁を備えるだけのものであるため、斜板が中立へ傾動す
る間にポンプより吐出する油かサージ圧力を発生させ、
接続ラインに別途サージ吸収弁を介設しない限り、油圧
回路の諸要素や配管に損傷を来たすという問題がある。
<Problems to be Solved by the Invention> Generally, when a hydraulic cylinder is connected to the discharge line of a hydraulic pump via a switching valve or the like and the hydraulic cylinder is driven in a staggered manner, the switching valve is switched at the end of the stroke or the like to switch from large flow rate control to pressure control. It is well known that large pressure surges are generated in the discharge line during transfer. However, the conventional electronically controlled pump described above is only equipped with a safety valve that tilts the swash plate to neutral via a pressure control valve at a set pressure slightly higher than the maximum set pressure. generates oil or surge pressure discharged from the pump while tilting to
Unless a surge absorbing valve is separately installed in the connection line, there is a problem in that various elements of the hydraulic circuit and piping are damaged.

そして、安全弁の開成に伴うベント流によって絞りの前
後に生じる差圧でしかサージ吸収弁を作動できないもの
と考えられていたため、サージ吸収弁を内蔵するコンパ
クトで有用な電子制御ポンプがなかった。
Furthermore, it was thought that the surge absorption valve could only be activated by the differential pressure created before and after the throttle by the vent flow that occurs when the safety valve opens, so there was no compact and useful electronically controlled pump with a built-in surge absorption valve.

そこで、本発明の目的は、安全弁のベント流によらずと
も吐出ラインからの圧油によって作動中るサージ吸収弁
を内蔵して、吐出ラインのザーノ圧を十分に緩和できる
新規有用な電子制御ポンプを提供することである。
SUMMARY OF THE INVENTION Therefore, an object of the present invention is to provide a new and useful electronically controlled pump that has a built-in surge absorption valve that is operated by pressure oil from the discharge line without relying on the vent flow of the safety valve, and can sufficiently alleviate the zano pressure in the discharge line. The goal is to provide the following.

〈課題を解決するための手段〉 上記目的を達成するため、本発明の第1の電子制御ポン
プは、第1図に例示するように、斜板2を傾動さt!−
ろノリンダ5を有する可変容量形ポンプlと、2次ポー
トAを上記可変容量形ポンプ1の吐出ライン6から分岐
して校り7を有するパイロットライン8とタンク9とに
切換接続ずろサーボ弁10と、上記絞り7の下流側のパ
イロットライン8に接続された安全弁13と、上記の可
変容量形ポンプlの7リンダ5に連通ずる2次ポートA
を上記サーボ弁IOの2次ポートAと」二足パイロット
ライン8とに上記絞り7,11の前後の差圧に応動して
切換接続する圧力制御弁14と、上記吐出ライン6の吐
出圧または吐出量に関する設定値と検出値の偏差に応じ
た制御信号を上記サーボ弁lOに出力する電子コントロ
ーラ17を備えたちのにおいて、上記絞り11の下流側
の圧力がバネ室に導かれ、入口ポートが上記吐出ライン
6に接続されたサージ吸収弁I8を備えたことを特徴と
する。また、本発明の第2の電子制御ポンプは、上記第
1の電子制御ポンプlの構成部材に、上記サージ吸収弁
I8のバネ室に連通ずるように設けられた油室19を加
えてなる。
<Means for Solving the Problems> In order to achieve the above object, the first electronically controlled pump of the present invention tilts the swash plate 2 t! as illustrated in FIG. −
A variable displacement pump 1 having a rotor cylinder 5, a secondary port A branched from a discharge line 6 of the variable displacement pump 1, and connected to a pilot line 8 having a calibration 7 and a tank 9 by switching and connecting a servo valve 10. , a safety valve 13 connected to the pilot line 8 on the downstream side of the throttle 7, and a secondary port A communicating with the cylinder 5 of the variable displacement pump l.
A pressure control valve 14 is connected to the secondary port A of the servo valve IO and the bipedal pilot line 8 in response to the differential pressure before and after the throttles 7 and 11, and the discharge pressure of the discharge line 6 or Equipped with an electronic controller 17 that outputs a control signal to the servo valve lO according to the deviation between the set value and the detected value regarding the discharge amount, the pressure on the downstream side of the throttle 11 is guided to the spring chamber, and the inlet port is It is characterized by comprising a surge absorption valve I8 connected to the discharge line 6. Further, the second electronically controlled pump of the present invention is formed by adding an oil chamber 19 provided in communication with the spring chamber of the surge absorption valve I8 to the components of the first electronically controlled pump I.

く作用〉 本発明の第1の電子制御ポンプの吐出ライン6に例えば
油圧シリンダ21を接続してこれを駆動する乙のとする
。例えば、油圧シリンダ21がストロークエンドになり
、大流量制御から圧力制御に自動的に制御か切り換わる
際に、吐出ライン6に大きなサージ圧が発生ずる。この
とき、サーボ弁10は、上記制御変更に伴って電子コン
トローラ17から出力される制御信号により、その2次
ポートAを吐出ライン6から分岐するパイロットライン
8に接続するように切り換わっており、圧力制御弁1・
1は、可変容量形ポンプ1のシリンダ5に連通ずる2次
ポートAを上記サーボ弁IOの2次ポートAに接続する
定常状態における位置に切り換わっている。従って、吐
出ライン6の圧油は、上記パイロットライン8.サーボ
弁10.圧力制御弁14を経て可変容量形ポンプ1のシ
リンダ5に流入して斜板2を中立方向へ傾動させ、ポン
プlからの吐出油を高圧小流量にするととしに、上記圧
油の流入に伴ってパイロットライン8の校り7の前後に
差圧が生じる。すると、上記絞り7の上流側即ち吐出ラ
イン6が入口ポートに、上記絞り7の下流側がバネ室に
夫々接続されたサージ吸収弁18は、上記差圧を受けて
開成し、吐出ライン6に発生したサージ圧をタンク22
へ逃がす。
Function> It is assumed that, for example, a hydraulic cylinder 21 is connected to the discharge line 6 of the first electronically controlled pump of the present invention and is driven. For example, when the hydraulic cylinder 21 reaches its stroke end and the control is automatically switched from large flow rate control to pressure control, a large surge pressure is generated in the discharge line 6. At this time, the servo valve 10 is switched to connect its secondary port A to the pilot line 8 branched from the discharge line 6 by a control signal output from the electronic controller 17 in conjunction with the above control change, Pressure control valve 1・
1 has been switched to a steady state position in which the secondary port A communicating with the cylinder 5 of the variable displacement pump 1 is connected to the secondary port A of the servo valve IO. Therefore, the pressure oil in the discharge line 6 is transferred to the pilot line 8. Servo valve 10. The oil flows into the cylinder 5 of the variable displacement pump 1 through the pressure control valve 14, tilts the swash plate 2 in the neutral direction, and makes the oil discharged from the pump 1 high pressure and small flow rate. As a result, a pressure difference is generated before and after the calibration 7 of the pilot line 8. Then, the surge absorption valve 18, which is connected to the inlet port on the upstream side of the throttle 7, that is, the discharge line 6, and to the spring chamber on the downstream side of the throttle 7, opens in response to the differential pressure, and the surge absorption valve 18 is opened in response to the differential pressure. The surge pressure is transferred to tank 22.
escape to

こうして、上記パイ〔1ツトライン8に接続された安全
弁13が開かなくと6、サージ吸収弁18が開いて、吐
出ライン6に発生したサージ圧力を大幅に緩和する。
In this way, if the safety valve 13 connected to the piping line 8 does not open, the surge absorption valve 18 opens and the surge pressure generated in the discharge line 6 is greatly alleviated.

本発明の第2の電子制御ポンプlで上述と同様に油圧シ
リンダ2Iを駆動する場合、吐出ライン6に同じく大き
なサージ圧が発生ずる。このとき、サーボ弁lOと圧力
制御弁14は、上述と同様に動作してポンプ1のシリン
ダ5への圧油の流入で斜板2が中立方向へ傾動するとと
もに、パイロットライン8を経る上記圧油の流入と油室
19への圧油の流入によりパイロットライン8の絞り7
゜l!の前後に差圧が生じる。すると、この差圧を受け
てサージ吸収弁18が開成し、吐出ライン6に発生した
サージ圧をタンク22へ逃がし、サージ圧が大幅に緩和
されろ。
When the hydraulic cylinder 2I is driven by the second electronically controlled pump 1 of the present invention in the same manner as described above, a large surge pressure is also generated in the discharge line 6. At this time, the servo valve lO and the pressure control valve 14 operate in the same manner as described above, and the swash plate 2 is tilted toward the neutral direction due to the inflow of pressure oil into the cylinder 5 of the pump 1, and the above pressure passing through the pilot line 8 is The throttle 7 of the pilot line 8 is caused by the inflow of oil and the inflow of pressure oil into the oil chamber 19.
゜l! A differential pressure occurs before and after. Then, the surge absorption valve 18 opens in response to this differential pressure, and the surge pressure generated in the discharge line 6 is released to the tank 22, and the surge pressure is significantly alleviated.

〈実施例〉 以下、本発明を図示の実施例により詳細に説明する。<Example> Hereinafter, the present invention will be explained in detail with reference to illustrated embodiments.

第1図は本発明の第2の電子制御ポンプの一例を示す回
路図であり、この電子制御ポンプは、斜板2を最大傾斜
角方向に傾動させるバイアススプリング3およびバイア
スシリンダ4と上記斜板を中立方向に傾動させるサーボ
シリンダ5を有する可変容量形ポンプlと、2次ポート
Aを上記ポンプ1の吐出ライン6から分岐して絞り7を
有するパイロットライン8(Pポート)とタンク9(T
ポート)とに切換接続するサーボ弁10と、上記絞り7
の下流側のパイロットライン8に絞り11を有するライ
ンI2を介して接続された安全弁13 ゛と、上記ポン
プ1のサーボシリング5に連通ずる2次ポートAを、サ
ーボ弁!0の2次ポートA(Tポート)と絞り7の下流
側のパイロットライン8(Pポート)とに上記絞り7.
11の前後(制御ポートx、y)の差圧に応動して切換
接続する圧力制御弁14を備える。
FIG. 1 is a circuit diagram showing an example of a second electronically controlled pump of the present invention, and this electronically controlled pump consists of a bias spring 3 and a bias cylinder 4 for tilting the swash plate 2 in the direction of the maximum inclination angle, and the swash plate 2. A variable displacement pump l has a servo cylinder 5 that tilts the pump in the neutral direction, a pilot line 8 (P port) whose secondary port A is branched from the discharge line 6 of the pump 1 and has a throttle 7, and a tank 9 (T
a servo valve 10 which is switchably connected to
A safety valve 13 is connected to the pilot line 8 on the downstream side of the servo valve 13 through a line I2 having a throttle 11, and a secondary port A communicating with the servo ring 5 of the pump 1 is connected to the servo valve! 0 secondary port A (T port) and the pilot line 8 (P port) on the downstream side of the throttle 7.
A pressure control valve 14 is provided which is switched and connected in response to the differential pressure between the front and rear (control ports x, y) of the pressure control valve 11.

さらに、上記電子制御ポンプは、吐出ライン6の圧力を
検出ずろ圧力センサ15と、斜板2の傾斜角即ち吐出量
を検出する斜板角センサ16と、これらのセンサl 5
.16から入力される検出値と予め人力される吐出圧と
吐出量の設定値との偏差に応じた制御信号を上記サーボ
弁10に出力する電子コントローラ17と、入口ポート
が吐出ライン6に、バネ室(制御ポートY)が絞り11
の下流側のライン12に夫々接続されたサージ吸収弁1
8と、このサージ吸収弁18のバネ室に連通ずるように
設けられた油室19と、サーボ弁10の2次ポートへと
圧力制御弁14の2次ポートAの間に設けられ、後者か
ら直音への流れを阻止するチエツク弁20を備えている
Further, the electronically controlled pump includes a drop pressure sensor 15 that detects the pressure of the discharge line 6, a swash plate angle sensor 16 that detects the inclination angle of the swash plate 2, that is, the discharge amount, and these sensors l5.
.. An electronic controller 17 outputs a control signal to the servo valve 10 according to the deviation between the detection value inputted from the servo valve 16 and the set value of the discharge pressure and discharge amount manually inputted in advance. The chamber (control port Y) is aperture 11
surge absorption valves 1 respectively connected to lines 12 on the downstream side of the
8, an oil chamber 19 provided so as to communicate with the spring chamber of this surge absorption valve 18, and a secondary port A of the pressure control valve 14 between the secondary port of the servo valve 10 and the secondary port A of the pressure control valve 14. A check valve 20 is provided to prevent the flow to direct sound.

上記サージ吸収弁I8の開成差圧は、吐出ライン6から
第1図の右のシンボル位置にあるサーボ弁10および圧
力制御弁14ならびにチエツク弁20を経てサーボシリ
ンダ5に流入する圧油によって絞り7の前後に生じる差
圧または吐出ライン6からライン12を経て油室19に
流入する圧油によって絞り7.11の前後に生じる差圧
あるいは上記両差圧の実効和になるように設定されてお
り、圧力制御弁14の開成差圧よりら高くなっている。
The opening differential pressure of the surge absorption valve I8 is created by pressure oil flowing into the servo cylinder 5 from the discharge line 6 through the servo valve 10, the pressure control valve 14, and the check valve 20 located at the symbol position on the right in FIG. The differential pressure generated before and after the throttle 7.11 due to pressure oil flowing from the discharge line 6 to the oil chamber 19 via the line 12, or the effective sum of the above two differential pressures is set. , is higher than the opening differential pressure of the pressure control valve 14.

上記構成の電子制御ポンプの動作を次に述へる。The operation of the electronically controlled pump having the above configuration will be described next.

電子制御ポンプの吐出ライン6に、油圧ンリンダ21を
接続し、これを駆動するものと唱゛る。いま、油圧ンリ
ンタ21がストロークエンドになり、大流量制御から圧
力制御に切り換わる際に、吐出ライン6に大きなサージ
圧が発生する。このとき、サーボ弁IOは、上記制御変
更に伴って電子コントローラ17から出力される制御信
号により、その2次ポートAを吐出ライン6から分岐す
るパイロットライン8(■〕ポート)に接続する図中台
のシンボル位置に切り換わっており、圧力制御弁14は
、ポンプIのザーポシリンダ5に連通ずる2次ポートへ
を上記サーボ弁IOの2次ポートA(Tポート)に接続
する図中台のノンポル位置即ち定常状態における位置に
切り換わっている。従って、サージ圧をもつ吐出ライン
6の圧油は、−1−記パイロソトライン8サーボ弁10
.圧力制御弁14ならびにヂエック弁20を経てポンプ
lのサーポンリンダ5に流入して斜板2を中立方向へ傾
動させる。また、上記サージ圧をらつ吐出ライン6の圧
油は、ライン12を経て油室I9に流入する。そのため
、吐出ライン6からザーボシリンダ5と油室19に流入
する圧油によってパイロットライン8の絞り7およびラ
イン12の絞り11の前後に所定の差圧が生じ、サージ
吸収弁18は、上記差圧を内部パイロットボー1− X
と外部パイロットポートYの間に受けて開成し、吐出ラ
イン6に発生したザーン圧力をタンク22に逃して大幅
に緩和する。
A hydraulic cylinder 21 is connected to the discharge line 6 of the electronically controlled pump and is driven. Now, when the hydraulic linter 21 reaches its stroke end and switches from large flow rate control to pressure control, a large surge pressure is generated in the discharge line 6. At this time, the servo valve IO connects its secondary port A to the pilot line 8 (■) port branched from the discharge line 6 by the control signal output from the electronic controller 17 in conjunction with the above control change. The pressure control valve 14 connects the secondary port communicating with the servo cylinder 5 of the pump I to the secondary port A (T port) of the servo valve IO. position, ie, the steady state position. Therefore, the pressure oil in the discharge line 6 having surge pressure is
.. It flows into the servo cylinder 5 of the pump 1 through the pressure control valve 14 and the check valve 20, and tilts the swash plate 2 in the neutral direction. Further, the pressure oil in the discharge line 6, which has the above-mentioned surge pressure, flows into the oil chamber I9 via the line 12. Therefore, a predetermined pressure difference is generated before and after the throttle 7 of the pilot line 8 and the throttle 11 of the line 12 due to the pressure oil flowing into the servo cylinder 5 and the oil chamber 19 from the discharge line 6, and the surge absorption valve 18 suppresses the pressure difference. Internal pilot bow 1-X
and the external pilot port Y, and the Zahn pressure generated in the discharge line 6 is released to the tank 22 and is significantly relieved.

このように、本発明では、従来、安全弁I3の開成に伴
うベント流による絞りの差圧でしか開成できないと考え
られていたサージ吸収弁18を、サーボ弁lOと圧力制
御弁14を経てサーボノリンダ5に流入する圧油または
これに加えて油室19に流入する圧油によって、パイロ
ットライン8に絞りまたはこれに加えてライン12の絞
り11の前後に生じる差圧で開成側るようにしているの
で、サージ吸収弁18を内蔵するコンバットな電子制御
ポンプによって外付けの場合のような配管等の手間を要
さず、吐出ライン6のサーノ圧力を大幅に低減すること
かできる。
As described above, in the present invention, the surge absorption valve 18, which was conventionally thought to be able to be opened only by the differential pressure across the throttle caused by the vent flow accompanying the opening of the safety valve I3, is now opened by the servo cylinder 5 via the servo valve lO and the pressure control valve 14. The pilot line 8 is throttled by the pressure oil flowing into the oil chamber 19 or the pressure oil flowing into the oil chamber 19, or in addition to this, the pressure difference generated before and after the throttle 11 of the line 12 causes the opening side to be opened. By using a combat electronically controlled pump with a built-in surge absorption valve 18, the surno pressure in the discharge line 6 can be significantly reduced without requiring the trouble of installing piping, etc., which is required when installing an external pump.

上記実施例では、絞り7の下流側のパイロットライン8
からライン12を分岐さ仕、これに絞り11を介設とと
もに、絞り11の下流側を油室19とサージ吸収弁18
の外部パイロットポートYに夫々接続しているので、油
室19へ流入する圧油による絞り11前後の差圧をもサ
ージ吸収弁18に作用せしめることができ、その分だけ
サージ圧吸収能力が向上する。
In the above embodiment, the pilot line 8 on the downstream side of the throttle 7
A line 12 is branched from the line 12, and a throttle 11 is interposed therein, and the downstream side of the throttle 11 is connected to an oil chamber 19 and a surge absorption valve 18.
Since the valves are connected to the external pilot ports Y, the differential pressure across the throttle 11 caused by the pressure oil flowing into the oil chamber 19 can be applied to the surge absorption valve 18, and the surge pressure absorption capacity is improved accordingly. do.

なお、上記実施例では、サージ吸収弁18と油室I9の
双方を設けた場合について説明したが、油室19を省略
して、吐出ライン6からサーボ弁10、圧力制御弁14
を経てサーポソリンダ5に流入する圧油による絞り7前
後の差圧のみでサージ吸収弁18を開成させることかで
きる。
In the above embodiment, the case where both the surge absorption valve 18 and the oil chamber I9 are provided has been described, but the oil chamber 19 is omitted and the discharge line 6 is connected to the servo valve 10 and the pressure control valve 14.
The surge absorption valve 18 can be opened only by the differential pressure across the throttle 7 caused by the pressure oil flowing into the servo cylinder 5 through the servo cylinder 5.

なお、本発明が」二足実施例に限られないのは勿論であ
る。
It goes without saying that the present invention is not limited to the two-legged embodiment.

〈発明の効果〉 以上の説明で明らかなように、本発明の′電子制御ポン
プは、安全弁を備え、可変容量形ポンプの吐出ラインか
ら分岐する絞りを有するパイロットラインの圧油を、電
子コントローラからの吐出圧。
<Effects of the Invention> As is clear from the above description, the electronically controlled pump of the present invention is equipped with a safety valve and allows pressure oil from the pilot line, which has a restriction branching from the discharge line of the variable displacement pump, to be supplied from the electronic controller. discharge pressure.

吐出量の制御偏差信号で動作せしめられるサーボ弁およ
び上記絞りの前後の差圧に応動する圧力制御弁を介して
上記ポンプの斜板傾動ンリンダに給。
It is supplied to the swash plate tilting cylinder of the pump through a servo valve operated by a discharge amount control deviation signal and a pressure control valve that responds to the differential pressure across the throttle.

排するしのにおいて、入口ポートが上記吐出ラインに、
バネ室が上記絞りの下流側に夫々接続されたサージ吸収
弁を備え、さらには上記バネ室に連通して設けた油室を
備えているので、安全弁のクラブキング圧よりも小さい
サージ圧が吐出ラインに生じても、この吐出ラインから
斜板傾動ノリンダや油室へ前述の如く流入する圧油によ
り上記絞りの前後に生じる差圧でサージ吸収弁を開成で
き、ザージ圧力を大幅に低減することができる。
In the discharge line, the inlet port is connected to the above discharge line,
Since the spring chamber is equipped with a surge absorption valve connected to the downstream side of each of the above-mentioned throttles, and is further equipped with an oil chamber that is connected to the above-mentioned spring chamber, a surge pressure smaller than the crab king pressure of the safety valve is discharged. Even if surge pressure is generated in the surge absorption line, the surge absorption valve can be opened by the differential pressure generated before and after the throttle due to the pressure oil flowing from this discharge line into the swash plate tilting nolinder and the oil chamber as described above, and the surge pressure can be significantly reduced. I can do it.

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

第1図は本発明の第2の電子制御ポンプの一例を示す回
路図である。 l・・可変容量形ポンプ、2 ・、斜板、訃・・サーホ
ノリング、6・・・吐出ライン、7.11・・絞り、8
・・パイロットライン、10 ・サーホ弁、I3・・安
全弁、 14 圧力制御弁、17・・電子コントローラ、I8 
・サージ吸収弁、19・油室。
FIG. 1 is a circuit diagram showing an example of the second electronically controlled pump of the present invention. l...Variable displacement pump, 2...Swash plate, butt...Surho ring, 6...Discharge line, 7.11...Aperture, 8
・・Pilot line, 10 ・Surho valve, I3・・Safety valve, 14 Pressure control valve, 17・・Electronic controller, I8
・Surge absorption valve, 19・Oil chamber.

Claims (2)

【特許請求の範囲】[Claims] (1)斜板(2)を傾動させるシリンダ(5)を有する
可変容量形ポンプ(1)と、2次ポート(A)を上記可
変容量形ポンプ(1)の吐出ライン(6)から分岐して
絞り(7)を有するパイロットライン(8)とタンク(
9)とに切換接続するサーボ弁(10)と、上記絞り(
7)の下流側のパイロットライン(8)に接続された安
全弁(13)と、上記の可変容量形ポンプ(1)のシリ
ンダ(5)に連通する2次ポート(A)を上記サーボ弁
(10)の2次ポート(A)と上記パイロットライン(
8)とに上記絞り(7、11)の前後の差圧に応動して
切換接続する圧力制御弁(14)と、上記吐出ライン(
6)の吐出圧または吐出量に関する設定値と検出値の偏
差に応じた制御信号を上記サーボ弁(10)に出力する
電子コントローラ(17)を備えた電子制御ポンプにお
いて、上記絞り(11)の下流側の圧力がバネ室に導か
れ、入口ポートが上記吐出ライン(6)に接続されたサ
ージ吸収弁(18)を備えたことを特徴とする電子制御
ポンプ。
(1) A variable displacement pump (1) having a cylinder (5) for tilting the swash plate (2), and a secondary port (A) branched from the discharge line (6) of the variable displacement pump (1). A pilot line (8) with a restriction (7) and a tank (
9) and a servo valve (10) which is switchably connected to the above-mentioned throttle (
A safety valve (13) connected to the pilot line (8) on the downstream side of the servo valve (10) and a secondary port (A) communicating with the cylinder (5) of the variable displacement pump (1) )'s secondary port (A) and the above pilot line (
8) and a pressure control valve (14) which is switched and connected in response to the differential pressure before and after the throttle (7, 11), and the discharge line (
6) in an electronically controlled pump equipped with an electronic controller (17) that outputs a control signal to the servo valve (10) in accordance with a deviation between a set value and a detected value regarding the discharge pressure or discharge amount; An electronically controlled pump characterized in that it is equipped with a surge absorption valve (18) whose downstream pressure is guided into a spring chamber and whose inlet port is connected to the discharge line (6).
(2)斜板(2)を傾動させるシリンダ(5)を有する
可変容量形ポンプ(1)と、2次ポート(A)を上記可
変容量形ポンプ(1)の吐出ライン(6)から分岐する
パイロットライン(8)とタンク(9)とに切換接続す
るサーボ弁(10)と、上記パイロットライン(8)に
絞り(11)を介して接続された安全弁(13)と、上
記可変容量形ポンプ(1)のシリンダ(5)に連通する
2次ポート(A)を上記サーボ弁(10)の2次ポート
(A)と上記パイロットライン(8)とに上記絞り(1
1)の前後の差圧に応動して切換接続する圧力制御弁(
14)と、上記吐出ライン(6)の吐出圧または吐出量
に関する設定値と検出値の偏差に応じた制御信号を上記
サーボ弁(10)に出力する電子コントローラ(17)
を備えた電子制御ポンプにおいて、 上記絞り(11)の下流側の圧力がバネ室に導かれ、入
口ポートが上記吐出ライン(6)に接続されたサージ吸
収弁(18)と、このサージ吸収弁(18)のバネ室に
連通するように設けられた油室(19)とを備えたこと
を特徴とする電子制御ポンプ。
(2) A variable displacement pump (1) having a cylinder (5) that tilts the swash plate (2), and a secondary port (A) branched from the discharge line (6) of the variable displacement pump (1). A servo valve (10) switchably connected to the pilot line (8) and the tank (9), a safety valve (13) connected to the pilot line (8) via a throttle (11), and the variable displacement pump. The secondary port (A) communicating with the cylinder (5) of (1) is connected to the secondary port (A) of the servo valve (10) and the pilot line (8).
1) Pressure control valve (
14), and an electronic controller (17) that outputs a control signal to the servo valve (10) according to the deviation between the set value and the detected value regarding the discharge pressure or discharge amount of the discharge line (6).
An electronically controlled pump equipped with a surge absorption valve (18) in which the pressure downstream of the throttle (11) is guided to a spring chamber and whose inlet port is connected to the discharge line (6); (18) An electronically controlled pump characterized by comprising an oil chamber (19) provided to communicate with the spring chamber.
JP63124192A 1988-05-20 1988-05-20 Electronically controlled pump Expired - Lifetime JP2560415B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP63124192A JP2560415B2 (en) 1988-05-20 1988-05-20 Electronically controlled pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP63124192A JP2560415B2 (en) 1988-05-20 1988-05-20 Electronically controlled pump

Publications (2)

Publication Number Publication Date
JPH01294979A true JPH01294979A (en) 1989-11-28
JP2560415B2 JP2560415B2 (en) 1996-12-04

Family

ID=14879264

Family Applications (1)

Application Number Title Priority Date Filing Date
JP63124192A Expired - Lifetime JP2560415B2 (en) 1988-05-20 1988-05-20 Electronically controlled pump

Country Status (1)

Country Link
JP (1) JP2560415B2 (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5813202A (en) * 1981-07-14 1983-01-25 Daikin Ind Ltd Flow control device with pressure compensation
JPS6255484A (en) * 1985-09-02 1987-03-11 Yuken Kogyo Kk variable displacement pump

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5813202A (en) * 1981-07-14 1983-01-25 Daikin Ind Ltd Flow control device with pressure compensation
JPS6255484A (en) * 1985-09-02 1987-03-11 Yuken Kogyo Kk variable displacement pump

Also Published As

Publication number Publication date
JP2560415B2 (en) 1996-12-04

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