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JPS6035566B2 - hydraulic control valve device - Google Patents
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JPS6035566B2 - hydraulic control valve device - Google Patents

hydraulic control valve device

Info

Publication number
JPS6035566B2
JPS6035566B2 JP12033574A JP12033574A JPS6035566B2 JP S6035566 B2 JPS6035566 B2 JP S6035566B2 JP 12033574 A JP12033574 A JP 12033574A JP 12033574 A JP12033574 A JP 12033574A JP S6035566 B2 JPS6035566 B2 JP S6035566B2
Authority
JP
Japan
Prior art keywords
pressure
pilot
valve
valve body
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
JP12033574A
Other languages
Japanese (ja)
Other versions
JPS5147626A (en
Inventor
敬之 荒川
重治 中野
正吉 真壁
一義 今井
康郎 菱沼
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.)
Yuken Kogyo Co Ltd
Original Assignee
Yuken Kogyo Co 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 Yuken Kogyo Co Ltd filed Critical Yuken Kogyo Co Ltd
Priority to JP12033574A priority Critical patent/JPS6035566B2/en
Publication of JPS5147626A publication Critical patent/JPS5147626A/en
Publication of JPS6035566B2 publication Critical patent/JPS6035566B2/en
Expired legal-status Critical Current

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  • Fluid-Pressure Circuits (AREA)

Description

【発明の詳細な説明】 この発明は、液圧回路に使用される制御された小容量の
パイロット回路の流れで大容量の主回路の流れを制御す
る液圧制御弁装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a hydraulic control valve device for controlling the flow of a large capacity main circuit with the flow of a controlled small capacity pilot circuit used in a hydraulic circuit.

従来のこの種の液圧制御弁装置は、パイロット回路の流
れを利用して主回路の流れを制御するパイロット操作方
式であるが、方向制御、圧力制御あるいは流量制御のい
ずれかの単一機能をもつものによって液圧制御回路を構
成する場合に夫々の機能をもった大容量の制御弁を組み
合わせて使用している。また、集積弁として体系化する
場合には、多種の単機能弁を用いることになるので不便
であり、その集積によって外形が大きくなる上に価格面
にも反映する欠点が避けられない。また、例えば椿開昭
48−73823号公報、特開昭48−86121号公
報、特開昭49−3074号公報に示されているように
、パイロット弁の機能に応じた作動をする大流量制御用
の多機能弁も公知である。
Conventional hydraulic control valve devices of this type are pilot-operated systems that use the flow in the pilot circuit to control the flow in the main circuit, but they also have a single function of directional control, pressure control, or flow rate control. When constructing a hydraulic control circuit, a combination of large-capacity control valves with different functions is used. Furthermore, when systematizing the valve as an integrated valve, it is inconvenient because it requires the use of many different types of single-function valves, and the disadvantage that the integration increases the external size and also affects the price is unavoidable. In addition, as shown in, for example, Tsubaki Publication No. 48-73823, Japanese Patent Application Publication No. 48-86121, and Japanese Patent Application Publication No. 49-3074, large flow control that operates according to the function of the pilot valve is also possible. Multifunction valves are also known.

これらの多機能弁では、パイロット流量検出オリフィス
の他に壬流れを制御する部分に主流れの流量を検出する
ためのオリフィスを設け、そのオリフィスに生ずる圧力
差を主制御弁にフィード・バックして流量調整を行うが
、このような方式の制御弁では、主制御流量が少ないと
オーJフィスに発生する圧力差が小さすぎて制御弁の精
度が悪くなるので小流量制御用には不向きであり、一方
、制御流量が多い場合にはオリフィスにおける圧力差が
大きくなり、制御時の最小作動圧力差つまり制御弁とし
ての圧力損失が大きくなる。そのため、小流量から大流
量まで幅広い制御流量の範囲を一合の制御弁で満足させ
ることができず、使用流量範囲に合わせて各個に設計、
調整しなければならないという欠点が避けられない。本
発明は前述の欠点を除去しようとするもので、その主目
的とするところは、パイロット操作方式で主回路の流れ
を制御する多機能形の液圧制御弁装置において、主制御
流れの流路中にパイロット流量検出用固定オリフィスを
設けることなしに小流量から大流量までの広い制御範囲
で主回路流れをパイロット流量に対応して高精度に制御
できる液圧制御弁装置を提供することにある。
In addition to the pilot flow rate detection orifice, these multi-function valves have an orifice for detecting the flow rate of the main flow in the part that controls the flow, and the pressure difference that occurs at the orifice is fed back to the main control valve. The flow rate is adjusted, but with this type of control valve, if the main control flow rate is low, the pressure difference generated in the OJ is too small and the accuracy of the control valve deteriorates, so it is not suitable for small flow rate control. On the other hand, when the controlled flow rate is large, the pressure difference at the orifice becomes large, and the minimum operating pressure difference during control, that is, the pressure loss as a control valve becomes large. Therefore, it is not possible to satisfy a wide range of control flow rates from small flow rates to large flow rates with a single control valve, so each control valve is designed individually according to the flow rate range used.
The disadvantage of having to make adjustments is unavoidable. The present invention seeks to eliminate the above-mentioned drawbacks, and its main purpose is to provide a flow path for the main control flow in a multifunctional hydraulic control valve device that controls the flow in the main circuit in a pilot-operated manner. An object of the present invention is to provide a hydraulic control valve device that can control the main circuit flow with high accuracy in response to the pilot flow rate over a wide control range from small flow rates to large flow rates without providing a fixed orifice for detecting the pilot flow rate. .

本発明の具体的な目的のひとつは、パイロット流量が小
流量のときから主弁体が感応して変位し得る前記液圧制
御弁装置を提供することである。本発明のもうひとつの
具体的な目的は、制御流量が大流量になっても弁の最低
作動圧力差が高くならず一定値となるようにして、大流
量まで制御可能な液圧制御弁装置を提供することである
。本発明のもうひとつの具体的な目的は、パイロット流
れの向きに応じて圧力補償弁両端にかける主制御口の差
圧の向きを切換える機能を主弁スプールに受けもたせず
にそれ用の別の切換弁を設けることによって主弁スプー
ルとそのまわりの弁本体側の晃造を簡略化すると共に、
該油路切換弁は圧力補償弁と同軸構造にして弁本体の大
形化を避けることである。このような目的を達成するた
めの本願第1発明の液圧制御弁装置は、弁本体内で両端
から主弁ばねで弾圧してスプリングセンタ方式にしたス
プール形式の主弁体を、パイロット流れによってパイロ
ットオリフィスの前後に生じる差圧が主弁ばねのばね力
と平衡するまで前記主弁ばねに抗して変位させてパイロ
ット操作方式で主回路の流れを制御するようにしたもの
において、パイロットボートからの液圧を一端面側に受
け、外部ボートからの液圧を他端面側に受け、これら両
端面側についてパイロット圧力に対する受圧面積が等し
くされ、一端面側にパイロット圧力を受けて一方へ変位
したときに外部ボートを弁本体の内部油室に蓮通させる
第一の主制御口と、他端面側からパイロット圧力を受け
て他方へ変位したときに外部ボートを前記内部油室に蓮
通させる第二の主制御口とを中立位置に対して対称的に
有する主弁体と、パイロット圧力が無いときに主弁体を
中立位置にすると共に、中立位置からの主弁体変位の両
方向で主弁体変位ストロークに対するばね力変化が互い
に等しい主弁ばねと、パイロットボートと外部ボートと
の間を所定閥度で運通してパイロット流れによりその前
後に差圧を生じるパイロットオリフィスと、弁本体内に
摺動可能に配置され、その中立位置からの変位について
均等なばね力が作用するように圧力補償弁ばねによって
スプリングセンタ方式で支持され、一端側に前記内部油
室の液圧を、他端側に前記外部ボートの液圧を、それぞ
れ互いに等しい受圧面積で受けるようになされ、外周部
に前記内部油室に閉口した凹溝が形成された圧力補償弁
と、一端側に前記パイロットボートの液圧を、他端側に
前記外部ボートの液圧を受けるように前記圧力補償弁の
外周部に同軸状に情動可能に緩められて圧力補償弁外周
の凹溝の両肩部と共に前記内部油室に蓮通した一対の圧
力補償制御口を形成すると共に、前記パイロットボート
の液圧を一端側に受けて一方へ変位したときは一方の前
記圧力補償制御口を圧油供給ボートに接続して他方を閉
じ、前記外部ボートの液圧を他端側に受けて他方へ変位
したときには他方の前記圧力補償制御口を排出ボートに
接続して一方を閉じるように、前記圧力補償弁体外周の
凹溝を間にして対称的に一対の切換油路閉口が設けられ
た油路切換弁、とを備え、更に前記パイロットオリフィ
スを固定オリフィスとし、前記主弁ばねをパイロット流
れが少ないうちから作用する円筒‘まねとパイロット流
れが或る程度多くなってから作用して榛みと共に1まね
力を増加する円すし、1まねとの組合せとしたことを特
徴とするものであり、これによって主制御流れの流路中
に固定オリフィスを設けずともパイロットオリフィス前
後の差圧に応じて主弁体制御口の開度を小流量から大流
量までの広い制御範囲で制御するようにし、主弁体スプ
ール形状および主弁体周囲の油通路や開孔を複雑化する
ことなく圧力補償弁によって主制御口前後の圧力差を常
に一定にするようにしてその闇度に比例して主流れを流
すことにより大流量城でも弁内の圧力損失が大きくなら
ないようにしたものである。
One of the specific objects of the present invention is to provide the above-mentioned hydraulic control valve device in which the main valve body can be displaced in response to the pilot flow rate even when the flow rate is small. Another specific object of the present invention is a hydraulic control valve device that can control up to a large flow rate by ensuring that the minimum operating pressure difference of the valve does not increase and remains a constant value even when the control flow rate becomes a large flow rate. The goal is to provide the following. Another specific object of the present invention is to provide a function for switching the direction of the differential pressure of the main control port applied to both ends of the pressure compensating valve according to the direction of the pilot flow, without requiring the main valve spool to have the function of switching the direction of the differential pressure applied to both ends of the pressure compensation valve. By providing a switching valve, the construction of the main valve spool and the valve body around it is simplified, and
The oil passage switching valve has a coaxial structure with the pressure compensating valve to avoid increasing the size of the valve body. To achieve such an object, the hydraulic control valve device of the first invention of the present application has a spool-type main valve body, which is compressed by a main valve spring from both ends within the valve body to create a spring center type, by a pilot flow. In a system in which the flow in the main circuit is controlled by a pilot operation method by displacing the main valve spring against the main valve spring until the differential pressure generated before and after the pilot orifice is balanced with the spring force of the main valve spring, from the pilot boat. One end side receives the hydraulic pressure, and the other end side receives the hydraulic pressure from the external boat, and the pressure receiving area for the pilot pressure is equal on both end sides, and one end side receives the pilot pressure and is displaced in one direction. A first main control port that allows the external boat to pass through the internal oil chamber of the valve body when the valve body is in use; The main valve body has two main control ports symmetrically with respect to the neutral position, and the main valve body can be set to the neutral position when there is no pilot pressure, and the main valve body can be moved in both directions when the main valve body is displaced from the neutral position. A main valve spring whose spring force changes with respect to the body displacement stroke are equal to each other, a pilot orifice that runs at a predetermined degree between the pilot boat and the external boat and creates a differential pressure before and after it due to the pilot flow, and a slider inside the valve body. The valve is movably arranged and supported in a spring center manner by a pressure compensating valve spring so that an equal spring force acts on displacement from its neutral position, and the hydraulic pressure of the internal oil chamber is applied to one end and the other end. A pressure compensating valve is configured to receive the hydraulic pressure of the external boat with equal pressure receiving areas, and has a concave groove closed to the internal oil chamber formed on the outer periphery, and a pressure compensating valve is configured to receive the hydraulic pressure of the pilot boat on one end side. , the other end is coaxially disposed on the outer periphery of the pressure compensating valve so as to receive the hydraulic pressure of the external boat, and is loosely attached to the inner oil chamber together with both shoulders of the concave groove on the outer periphery of the pressure compensating valve. A pair of pressure compensation control ports are formed through the pilot boat, and when one end receives the hydraulic pressure of the pilot boat and is displaced in one direction, one of the pressure compensation control ports is connected to the pressure oil supply boat and the other is closed. , a concave groove on the outer periphery of the pressure compensating valve body is arranged so that when the other end receives the hydraulic pressure of the external boat and is displaced to the other end, the other pressure compensating control port is connected to the discharge boat and one side is closed. an oil passage switching valve having a pair of switching oil passage closures symmetrically provided, the pilot orifice being a fixed orifice, and the main valve spring being a cylindrical valve that acts when the pilot flow is low. It is characterized by a combination of a circular sushi that acts after the pilot flow has increased to a certain extent and increases the 1 imitation force as it swells, and a 1 imitation force. The opening degree of the main valve body control port can be controlled in a wide control range from small flow rate to large flow rate according to the differential pressure before and after the pilot orifice without providing a fixed orifice in the main valve body spool shape and main valve body. By using a pressure compensating valve to always keep the pressure difference before and after the main control port constant without complicating the surrounding oil passages and openings, and by allowing the main flow to flow in proportion to the degree of darkness, the valve can be used even in large flow conditions. This is to prevent the pressure loss inside from becoming large.

また、本発明のさらに別の具体的な目的は、前記第1発
明において使用する円すし、ばねという特殊な部品を用
いずに、通常部品だけで構成することが可能な、しかも
パイロット流れが少しでも流れれば主弁体が感応して変
位し得る前記液圧制御弁装置を提供することであるこの
ため本願第2発明の液圧制御弁装置では、前言己パイロ
ットオリフィスを単なる固定オリフィスで構成せずに、
その上流側のパイロット圧力が或る圧力以上になったと
き開いてその後パイロット流量に応じた差圧を生じるポ
ベット弁によって構成し、且つ前記主弁ばねも、パイロ
ット圧力が前記ポベット弁のクラッキング圧力に達した
ときに主弁体制御口が丁度開き始めるように設定された
円筒ばねのみによって構成したことを特徴とするもので
、これにより円すし、ばねを用いることなくパイロット
流れの流れ始めから主流れの制御が行えるようにしたも
のである。
Further, another specific object of the present invention is to be able to be constructed with only ordinary parts without using the special parts such as the disk and spring used in the first invention, and to have a small pilot flow. Therefore, in the hydraulic control valve device of the second invention of the present application, the pilot orifice is configured with a simple fixed orifice. Without,
It is constituted by a povet valve that opens when the pilot pressure on the upstream side exceeds a certain pressure and then generates a differential pressure according to the pilot flow rate, and the main valve spring also has a povet valve whose pilot pressure reaches the cracking pressure of the povet valve. It is characterized by being constructed only with a cylindrical spring that is set so that the main valve body control port just starts to open when the main valve body reaches its final position. It is designed so that it can be controlled.

本発明ではパイロット流量が小流量でも主弁体が感応す
るから、主回路流れを小流量城から制御でき、また主流
れ流路中に余分なオリフィスを設けていないので、それ
による圧力損失もなく、大流量域まで制御可能である。
In the present invention, the main valve body responds even if the pilot flow rate is small, so the main circuit flow can be controlled from a small flow rate, and since no extra orifice is provided in the main flow path, there is no pressure loss due to it. , it is possible to control up to a large flow rate range.

さらに圧力補償弁に対して油路切換弁を組み合わせてこ
れらを主弁体と別に弁本体に配置したから主弁体周囲の
油通路や関孔が複雑化することもなく、主弁体スプール
形状も簡素なものになる。以下に本発明の好ましい実施
例について図面と共に説明する。
Furthermore, since the pressure compensation valve is combined with an oil passage switching valve and these are placed in the valve body separately from the main valve body, the oil passages and checkpoints around the main valve body are not complicated, and the main valve body spool shape It will also be simple. Preferred embodiments of the present invention will be described below with reference to the drawings.

第1図は第1発明の−実施例を示しており、この実施例
の液圧制御弁装置においては、弁本体1にパイロットボ
ート46と接続する供給ボート2、および同じくパイロ
ットボート47と接続する排出ボート3を配設し、これ
等供給および排出両ボートを中心にして同図に面して左
右対称に後述する諸部品を装備するものである。
FIG. 1 shows an embodiment of the first invention, and in the hydraulic control valve device of this embodiment, a supply boat 2 is connected to a pilot boat 46 to the valve body 1, and a supply boat 2 is also connected to a pilot boat 47. A discharge boat 3 is provided, and various parts to be described later are installed symmetrically with respect to both the supply and discharge boats as seen in the figure.

説明の便宜上、左方配備部品には図番後尾にAあるいは
Cを、右方配備のものには、BあるいはDを添字するも
のとし、特に必要がない限りにおいて左方構成について
主に詳述する。すなわち、前記弁本体外部に閉口する外
部接続ボートとしてのAボート4A(Bボート4B)に
蓮適する弁室44Aおよび43A内を沼動する主弁体5
Aを、その両端のはね室17Aおよび18A内に配設し
た夫々円筒ばね6A、円すし、はね60Cおよび円筒ば
ね7A、円すいばね7Cで両端から弾圧し、さらに該主
弁体には前記弁室44Aに閉口する弁室19Aおよび前
記弁室43Aに開□する弁室20Aを穿孔して該両弁室
を前記ばね室18Aに閉口する弁室21Aで蓮適する。
For convenience of explanation, parts installed on the left will be suffixed with A or C, and those installed on the right will be suffixed with B or D. Unless there is a particular need, the left configuration will mainly be described in detail. do. That is, the main valve body 5 moves within the valve chambers 44A and 43A, which are suitable for the A boat 4A (B boat 4B) as an external connection boat that closes to the outside of the valve body.
A is compressed from both ends by a cylindrical spring 6A, a conical spring 60C, a cylindrical spring 7A, and a conical spring 7C disposed in the spring chambers 17A and 18A at both ends, and the main valve body is also A valve chamber 19A that closes to the valve chamber 44A and a valve chamber 20A that opens to the valve chamber 43A are bored to form a valve chamber 21A that closes both valve chambers to the spring chamber 18A.

また該主弁体を囲総して前記本体弁室(内部油室)33
Aを穿削して前記弁室44A間に制御口41Aを、前記
弁室43A間に制御口42Aを形成する。ついで、前記
弁本体に沼動する油路切換弁体10Aを配設し、さらに
該切換弁体内部に圧力補償弁体8Aを超動自在に挿入し
、該補償弁体の両端周は前記弁本体と摺動係合させてば
ね室22A,23Aを形成し、該室内にはガイド11A
,12Aを挿入してその各先端を前記補償弁体両端に当
援させるとともに圧力補償弁ばね13A,14Aで弾圧
する。前記油路功換弁体の中央部には閉口30Aを穿っ
て弁室31A,32Aを経て前記弁室33Aと蓮通させ
、その両端側には油路関口38A,35Aを穿って前者
38Aは弁室37A,36Aを経て供給ボート2に、後
者35Aは弁室28A,27Aを経て排出ボート3に蓮
通させ、またその両端面の一端面を弁室25A内に位置
させて該弁室を前記圧力補償弁体のばね室23Aにその
パイロット通路24Aを介して蓮通させ、池端面を弁室
26Aに位置させて該弁室を弁本体1に配設したパイロ
ットボート45Aと前記ばね室23A,18Aを接続す
るパイロット通路15A,16Aに連結する。前記の通
路15Aは、また分岐して前記主弁体ばね室17Aに運
通してその蓮通路にダンピング絞り48Aを配設すると
ともに、前記通路16Aにパイロット絞り9Aを配設し
てある。前記圧力補償弁体の中央部には、前記油路切換
弁の関口30Aに運通して同じく油路閉口35Aとは制
御口40Aを、油路開口38Aとは制御口39Aをその
両肩部で形成する凹溝29Aを旋削し、該凹溝と前記補
償弁ばね室22Aとはパイロット通路34Aで蓮適する
。この実施例の作動を述べるために、第1図に添画した
パイロット切換弁49の回路について述べると、該弁4
9のポンプボートPにはパイロットボート46を、タン
クボートTにはパ‐イロツトポート47を、ボートAに
はパイロットボート45Aを、ボートBには同じくパイ
ロットボート458を接続している。上述した第1発明
の実施例によれば、パイロットボート45Aから流入し
たパイロット流れは、パイロット通路15A、同絞り9
A、同通路16A、ばね室18A、弁室21A,19A
,44Aを経てAボート4Aから流出して前記絞りの前
後に圧力差を発生させ、同時にパイロット通路15Aか
らダンピング絞り48Aを経てばね室17Aに流入する
In addition, the main valve chamber (internal oil chamber) 33 surrounds the main valve body.
A is drilled to form a control port 41A between the valve chambers 44A and a control port 42A between the valve chambers 43A. Next, a movable oil passage switching valve body 10A is disposed in the valve body, and a pressure compensating valve body 8A is inserted into the switching valve body so as to be super movable. Spring chambers 22A and 23A are formed by sliding engagement with the main body, and a guide 11A is provided in the chambers.
, 12A are inserted and their tips are brought into contact with both ends of the compensation valve body, and are pressed by pressure compensation valve springs 13A and 14A. A closing hole 30A is bored in the center of the oil passage switching valve body to communicate with the valve chamber 33A via the valve chambers 31A and 32A, and oil passage gates 38A and 35A are bored on both ends thereof, and the former 38A is a valve body. The latter passes through the chambers 37A and 36A to the supply boat 2, and the latter 35A passes through the valve chambers 28A and 27A to the discharge boat 3, and one end surface of both end surfaces thereof is located in the valve chamber 25A, so that the valve chamber is connected to the above-mentioned valve chamber. A pilot boat 45A, which is connected to the spring chamber 23A of the pressure compensating valve body through its pilot passage 24A, and whose end face is located in the valve chamber 26A, and the valve chamber is disposed in the valve body 1, and the spring chamber 23A, 18A to pilot passages 15A and 16A. The passage 15A is also branched to the main valve body spring chamber 17A, and a damping throttle 48A is disposed in the lotus passage, and a pilot throttle 9A is disposed in the passage 16A. In the center of the pressure compensating valve body, a control port 40A is connected to the oil passage switching valve 30A, and a control port 40A is connected to the oil passage closing port 35A, and a control port 39A is connected to the oil passage opening 38A at both shoulders. A concave groove 29A to be formed is turned, and the concave groove and the compensation valve spring chamber 22A fit together in the pilot passage 34A. In order to describe the operation of this embodiment, the circuit of the pilot switching valve 49 attached to FIG. 1 will be described.
A pilot boat 46 is connected to the pump boat P of No. 9, a pilot port 47 is connected to the tank boat T, a pilot boat 45A is connected to the boat A, and a pilot boat 458 is connected to the boat B. According to the embodiment of the first invention described above, the pilot flow flowing from the pilot boat 45A flows through the pilot passage 15A and the throttle 9.
A, same passage 16A, spring chamber 18A, valve chambers 21A, 19A
, 44A, and generates a pressure difference across the throttle, and at the same time flows from the pilot passage 15A through the damping throttle 48A into the spring chamber 17A.

主弁体5Aは、前記絞り9Aによる圧力差によってばね
室18A側に変位し、その内部のはね力と前記圧力差が
平衡する位置を占位する。該主弁体が図面に示す中立位
置にあるときは、制御口41A,42Aは閉止し、ばね
室17Aはダンピング絞り48A、パイロット通路15
Aを経て弁室26Aに通じ、また弁室44Aは、弁室1
9A,21A、ばね室18A、パイロット通路16A、
ばね室23A、パイロット通路24Aを経て弁室25A
に蓮適していて、前記圧力差によって主弁体5Aが小変
位すると同時に油路切襖弁10Aは弁室25A側に押さ
れて制御口39Aを開□する。供給ボート2の圧油は弁
室36A,37A、油路開□38A、制御口39A、弁
室29A、開口30A、弁室31A,32Aを経て内部
油室33Aに流入するが、制御口41Aは閉止している
から、圧力補償弁体8Aのパイロット通路35Aを経て
ばね室22Aに流入し、前記補償弁体をばね14Aに抗
し、ガイド12Aを介して押すので制御□39Aは閉止
する。主弁体5Aがさらに変位すると、制御口41Aが
関口して内部油室33Aの圧油が弁室44AからAボー
ト4Aに流出するから、ばね室22Aの油圧が低下して
前記補償弁体がばね14Aで押しもどされて制御口39
Aが開□し、油路閉口38Aの圧油が制御口39A、弁
室29A、閉口30A、弁室31A,32A、内部油室
33A、制御口41A、弁室44Aを経てAボート4A
に流出する。
The main valve body 5A is displaced toward the spring chamber 18A due to the pressure difference caused by the throttle 9A, and occupies a position where the internal spring force and the pressure difference are balanced. When the main valve body is in the neutral position shown in the drawing, the control ports 41A and 42A are closed, and the spring chamber 17A is closed to the damping throttle 48A and the pilot passage 15.
A communicates with the valve chamber 26A, and the valve chamber 44A communicates with the valve chamber 1.
9A, 21A, spring chamber 18A, pilot passage 16A,
Valve chamber 25A via spring chamber 23A and pilot passage 24A
The pressure difference causes a small displacement of the main valve body 5A, and at the same time, the oil passage sluice valve 10A is pushed toward the valve chamber 25A to open the control port 39A. Pressure oil in the supply boat 2 flows into the internal oil chamber 33A via the valve chambers 36A, 37A, oil passage opening □ 38A, control port 39A, valve chamber 29A, opening 30A, valve chambers 31A, 32A, but the control port 41A Since it is closed, it flows into the spring chamber 22A through the pilot passage 35A of the pressure compensation valve body 8A, and pushes the compensation valve body through the guide 12A against the spring 14A, so that the control □ 39A is closed. When the main valve body 5A is further displaced, the control port 41A is closed and the pressure oil in the internal oil chamber 33A flows out from the valve chamber 44A to the A boat 4A, so the oil pressure in the spring chamber 22A decreases and the compensation valve body The control port 39 is pushed back by the spring 14A.
A opens □, and the pressure oil in the oil passage closing port 38A passes through the control port 39A, the valve chamber 29A, the closing port 30A, the valve chambers 31A, 32A, the internal oil chamber 33A, the control port 41A, and the valve chamber 44A to the A boat 4A.
leaks to.

この際には、弁室22Aおよび23A間の圧力差がばね
14Aのばね力と前記補償弁体断面積によって決定され
る位置を占位して制御口39Aの主流れを制御する。つ
ぎに、パイロット流れを止めると、絞り9Aの圧力差が
なくなり、前記主弁体5Aがばね6A,7Aのばね力に
よって中立位置に復位して制御口41Aを遮閉し、した
がって主流れを遮断する。
At this time, the pressure difference between the valve chambers 22A and 23A occupies a position determined by the spring force of the spring 14A and the cross-sectional area of the compensation valve body, thereby controlling the main flow through the control port 39A. Next, when the pilot flow is stopped, the pressure difference across the throttle 9A disappears, and the main valve body 5A returns to the neutral position by the spring force of the springs 6A and 7A, blocking the control port 41A and thus blocking the main flow. do.

前述と逆に、Aボート4Aからパイロットボート45A
にパイロット流れを流入させると、その圧油は前述と逆
の経路を経て前記ボート45Aに流出し、またダンピン
グ絞り48Aからばね室17Aにも流入して絞り9Aに
圧力差を発生させ、該主弁体をばね室17A側に変位さ
せてばね6A,6Cのばね力と平衡する位置を占位させ
る。
Contrary to the above, from A boat 4A to pilot boat 45A
When the pilot flow is allowed to flow in, the pressure oil flows into the boat 45A through the reverse path as described above, and also flows into the spring chamber 17A from the damping throttle 48A to generate a pressure difference in the throttle 9A. The valve body is displaced toward the spring chamber 17A to occupy a position balanced with the spring force of the springs 6A and 6C.

この主弁体変位とともに、絞り9Aの圧力差によって油
路切換弁体10Aは弁室26A側に押されて制御口40
Aを閉口し、油路開□35A、弁室28A,27Aを経
て排出ボート3に接続するが、制御口42Aは閉止して
いるから、前記パイロット流れがばね室23Aにも流入
して前記補償弁体をガイド11Aを介してはね13Aに
抗して押し、したがって制御口40Aを閉止する。主弁
体5Aがさらに変位して制御口42Aを閉口すると、弁
室44Aの圧油は、弁室19A,21A,20A、該制
御口42A、内部油室33A、弁室32A,31A、開
□30A,29A、パイロット通路34Aを経てばね室
22Aに流入して前記補償弁体を押して制御口40Aを
開□するので、弁室29Aの圧油が油路開口35A、弁
室28Aを経て排出ボート3に流出する。この際にも、
ばね室22Aおよび23Aの圧力差は前記補償弁体によ
って常に制御されてばね13Aのばね力と該補償弁体断
面積によって決定される値となって圧力補償が行われる
。前述のように、パイロット流れがパイロットボート4
5AからAボート4Aに流れる場合、主流れは供給ボー
ト2からAボート4Aに流れ、逆にパイロット流れがA
ボート4Aからパイロットボート45Aに流れる場合、
Aボート4Aから排出ボート3に流れる。また、主弁体
制御口41Aあるいは42Aが開□する前に前記油路切
換弁が動いてパイロット通路34Aあるいは16Aが閉
口するので、圧力補償弁体制御口39Aあるいは40A
が閉止し、その後に前記主弁体制御口が、ついで前記補
償弁体制御口が開□して主流れの圧油を流すので、該主
弁体制御口が閉口するときには、通常流量制御弁に起る
ジャンピング現象が発生しない。また、前記補償弁体に
作用するばね13A,14Aは夫々ガイド11A,12
Aを介在させているから、相互にばね力を打ち消さず、
中立時より以上に行かない。なお、この実施例では、前
述したように諸部品を左右対称に構成しているので、上
述の作動は右側に対しても同様に成立することは詳説す
るまでもない。ついで、前述した作動の原理について説
明すれば、主弁体5Aの変位制御用ばねには、ばね定数
の小さい円筒‘まね6A,7Aおよびばね定数の大きい
円すし、ばね6C,7Cを選択し、前者ばねは予め榛み
を与えて装着して前記主弁体を中立位置にするようにし
、この中立位置では後者ばねは主弁体5Aにばね力作用
させないようにして、該主弁体が油圧力で変位して制御
口41A,42Aが閉口する直前から作用するように装
着する。
Along with this main valve body displacement, the oil passage switching valve body 10A is pushed toward the valve chamber 26A side due to the pressure difference in the throttle 9A, and the control port 40
A is closed and connected to the discharge boat 3 via the oil passage opening □ 35A and the valve chambers 28A and 27A, but since the control port 42A is closed, the pilot flow also flows into the spring chamber 23A and the compensation is performed. The valve body is pushed through the guide 11A against the spring 13A, thus closing the control port 40A. When the main valve body 5A is further displaced and the control port 42A is closed, the pressure oil in the valve chamber 44A is transferred to the valve chambers 19A, 21A, 20A, the control port 42A, the internal oil chamber 33A, the valve chambers 32A, 31A, and the open □ 30A, 29A, and the pilot passage 34A to the spring chamber 22A and press the compensation valve body to open the control port 40A, so that the pressure oil in the valve chamber 29A flows through the oil passage opening 35A and the valve chamber 28A to the discharge boat. 3. At this time too,
The pressure difference between the spring chambers 22A and 23A is always controlled by the compensating valve body to a value determined by the spring force of the spring 13A and the cross-sectional area of the compensating valve body, thereby performing pressure compensation. As mentioned above, the pilot flow
5A to A boat 4A, the main flow flows from supply boat 2 to A boat 4A, and conversely the pilot flow flows from A boat 4A to A boat 4A.
When flowing from boat 4A to pilot boat 45A,
It flows from the A boat 4A to the discharge boat 3. In addition, since the oil passage switching valve moves and the pilot passage 34A or 16A closes before the main valve body control port 41A or 42A opens, the pressure compensating valve body control port 39A or 40A
is closed, and then the main valve body control port and the compensation valve body control port open □ to allow the main flow of pressure oil to flow, so when the main valve body control port closes, the normal flow rate control valve The jumping phenomenon that occurs in Further, the springs 13A and 14A acting on the compensation valve body are connected to the guides 11A and 12, respectively.
Because A is interposed, the spring forces do not cancel each other out,
Do not go further than when neutral. In this embodiment, since the various parts are configured symmetrically as described above, it is needless to explain in detail that the above-mentioned operation also holds true for the right side. Next, to explain the above-mentioned principle of operation, the cylindrical springs 6A, 7A with a small spring constant and the round springs 6C, 7C with a large spring constant are selected as the displacement control springs of the main valve body 5A. The former spring is pre-stressed and installed so that the main valve body is in the neutral position, and in this neutral position, the latter spring is not applied with spring force to the main valve body 5A, so that the main valve body is free from oil. It is mounted so that it is displaced by pressure and starts acting immediately before the control ports 41A, 42A close.

この場合、円すし、ばね6C,7Cのばね力を操み量の
二乗に比例させるようにすることによって、総合ばね力
は第2図に図示したものとなる。すなわち、主弁体変位
を×、主弁体制御口開度をx、別記制御口の重複量をh
、円すし、ばね定数をkl、円筒ばね定数をk3とすれ
ば小さいので、主弁体に作用するばね力Fは、F=kl
・(×−h)2十2・k3・x 二kl.(×−h)2 =kl・x2 となる。
In this case, by making the spring force of the springs 6C and 7C proportional to the square of the amount of operation, the total spring force will be as shown in FIG. 2. In other words, the displacement of the main valve body is x, the opening degree of the main valve body control port is x, and the overlap amount of the control port (separately stated) is h.
, the circular spring constant is small if kl is the cylindrical spring constant, and k3 is the cylindrical spring constant, so the spring force F acting on the main valve body is F = kl
・(x-h)212・k3・x 2kl. (x-h)2=kl·x2.

パイロット回路に流量qが流れるときに絞り9Aの前後
に生じる圧力差△pは、絞り抵抗をRとすると、△p=
R・q2 であり、主弁体釣合式は、主弁体断面積をAとすれば、
A・△p=F=kl・そであるので、主弁体開度xは、 x=ノA・R/kl・q となる。
The pressure difference △p that occurs before and after the throttle 9A when the flow rate q flows through the pilot circuit is expressed as △p=
R・q2, and the main valve body balance equation is, if the main valve body cross-sectional area is A,
Since A・△p=F=kl・sleeve, the main valve body opening degree x is as follows: x=ノA・R/kl・q.

また、圧力補償弁体8Aによって圧力補償される主弁体
5Aの制御口41A,42Aの圧力差pmは、ばね13
A,14Aのはね定数をk2、前記ばねの榛み量をXs
、圧力補償弁体断面積をAcとすれば、・ △pm=k
2・Xs/Ac となって一定値に自動的に調整され、したがって、主弁
体制御口41A,42Aを流れる流量Qは、主弁体流量
定数をkfとすれば、Q=kf.xノ△pm=K●q となる。
Further, the pressure difference pm between the control ports 41A and 42A of the main valve body 5A whose pressure is compensated by the pressure compensating valve body 8A is
A, the spring constant of 14A is k2, and the amount of deflection of the spring is Xs
, if the pressure compensation valve body cross-sectional area is Ac, △pm=k
2.Xs/Ac, and is automatically adjusted to a constant value. Therefore, the flow rate Q flowing through the main valve body control ports 41A, 42A is Q=kf. xノ△pm=K●q.

ただし、Kは、K=Kf・k2・Xs/Ac・A・R/
klであって増幅率と呼ばれ、主流れ流量Qはパイロッ
ト流れ流量qに比例してK倍となる。
However, K is K=Kf・k2・Xs/Ac・A・R/
kl is called an amplification factor, and the main flow flow rate Q increases by K times in proportion to the pilot flow flow rate q.

したがって、Aボート4AあるいはBボート4Bを通過
する流量QTは、流量Qおよび流量qの和であるから(
1丁K)qとなり、パイロット回路の流量qと主回路の
流量QTが比例することになり、パイロット回路を制御
することで相似的に主回路を制御することが可能である
Therefore, since the flow rate QT passing through the A boat 4A or the B boat 4B is the sum of the flow rate Q and the flow rate q, (
The flow rate q of the pilot circuit is proportional to the flow rate QT of the main circuit, and it is possible to control the main circuit analogously by controlling the pilot circuit.

また、上述の説明は、流れが供給ポ−トからAあるいは
Bボートに、AボートあるいはBボートから排出ボート
にといずれの場合にも成立する。
Furthermore, the above explanation holds true regardless of whether the flow is from the supply port to the A or B boat, or from the A or B boat to the discharge boat.

つぎに、第3図は第2発明の実施例を示すもので、前述
の第1図に図示した実施例のパイロット絞り9Aに代え
て、パイロット通路16A間にばね弾圧したポベット弁
50A,51Aを、互いの遮断する流れを各々反対にし
て酉己設し、また円すし、ばねを設置しないで‘まね定
数の大きい円筒まね6′A,7′Aを配置している以外
は、前述実施例と全く同様に構成している。この実施例
の作動は前述の実施例と同様であるが、ポベット弁51
A,51Aがパイロット流量に応じて圧力差を発生させ
て主弁体5Aを変位させることによって主流れを制御す
るもので、パイロット流れがボート45AからAボート
4Aに流れる場合はポベット弁50Aを閉口し、逆の流
れの場合にはポベット弁51Aを閉口する。
Next, FIG. 3 shows an embodiment of the second invention, in which pobet valves 50A and 51A, which are spring-loaded between the pilot passage 16A, are used in place of the pilot throttle 9A of the embodiment shown in FIG. , except that the cylinders 6'A and 7'A with large simulating constants are arranged, with the flow to be blocked being opposite to each other, and the cylinders 6'A and 7'A with large simulating constants are arranged without installing circular cylinders or springs. It is configured in exactly the same way. The operation of this embodiment is similar to the previous embodiment, except that the povet valve 51
A, 51A controls the main flow by generating a pressure difference according to the pilot flow rate and displacing the main valve body 5A, and when the pilot flow flows from the boat 45A to the A boat 4A, the povet valve 50A is closed. However, in the case of reverse flow, the povet valve 51A is closed.

これ等の場合における前記各ポベット弁の前後の圧力差
△pは、ポベット弁クラッキング圧を△pc、定数をk
qとすれば、△p=△pc十kq・q であって勺第4図に図示したようにほぼ直線になる。
In these cases, the pressure difference △p before and after each povet valve is determined by △pc being the povet valve cracking pressure, and k being the constant.
If q, then △p=△pc1kq·q, and as shown in FIG. 4, it is almost a straight line.

前記ポベット弁50A,51Aの圧力差と円筒ばね6′
A,7′Aのばね力と平衡した位置で主弁体5Aが停止
して制御口41A,42Aを関口し、前述の実施例と同
様に主流量をパイロット流量に比例させることが可能で
ある。
The pressure difference between the povet valves 50A and 51A and the cylindrical spring 6'
The main valve body 5A stops at a position balanced with the spring forces of A and 7'A, and the control ports 41A and 42A are closed, making it possible to make the main flow rate proportional to the pilot flow rate as in the previous embodiment. .

つぎに、この発明に係る弁装置の機能をさらに使用例に
ついて説明すると、前述の第1図に図示した回路は単一
機能をもつた切換弁としての例示であって、パィ。
Next, the functions of the valve device according to the present invention will be further explained with reference to usage examples.The circuit shown in FIG. 1 is an example of a switching valve having a single function.

ット切換弁49のポンプボートPはパイロットボート4
6を経て供給ボート2に、ボートAは/ぐイロツトポー
ト45Aに、ボートBは/ぐイロツトポート45Bに、
タンクボートTはパイロットボート47を経て排出ボー
ト3に夫々接続し構成していることは前述した通りであ
る。今、前記切換弁をP−A、B−Tに切り換えると、
パイロット流れが、A側では供給ボート2、パイロット
ボート46、パイロット切換弁49、同じボート45A
、同じく通路15A、絞り9A、同じく通路16A、ば
ね室18A、弁室21A,19A,44A、Aボート4
Aの順に流れ、B側ではBボート4Bから前述の通路と
反対の順路で排出ボート3に流れて主弁体5A,5Bが
夫々変位し、主流れは、A側では供給ボート2からAボ
ート4Aに、B側ではBボート4Bから排出ボート3に
流れる。この場合パイロット回路に他の制御弁を挿入し
ていないから、パイロット流れは自由に流れ、主流れも
前述の経路を自由に流れる。また、前記切襖弁A−T、
P−Bに切り換えると、前述と同様に、主流れは、Aボ
ート4Aから排出ボート3に、供給ボート2からBボー
ト4Bに流れる。切換兼流量制御弁として回路を構成し
た第5図において、第1図に図示したパイロットボート
45Aとパイロット切襖弁49のボートA間の管路中に
パィ。ット流量制御弁52Aを、同じくB側に同流量制
御弁52Bを挿入したもので、前記切換弁をP−A、B
−Tに切り換えると、パイロット流れは、A側では供給
ボート2から図示の経路を経てAボート4Aに、B側も
Bボート4Bから図示の経路を経て排出ボート3に流れ
るが、A側ではパイロット流量制御弁52Aでパイロッ
ト流量qに制御調整されるから、王流れの流量はK・q
となり、Aボート4Aからアクチュェータへの流量は(
1十K)qとなり、B側では前記流量制御弁52Bのチ
ェック弁側をパイロット流れが自由に流れるから、主流
れもBボート4Bから排出ポ山ト3に自由に流れる。つ
いで、前記切襖弁をA−T、P−Bに切り換えると、A
側ではパイロット流れが排出ボート3に自由に流れ、B
側では前記流量制御弁52Bで前述同様に制御されてア
クチュェータへの流量は(1十K)qとなる。この際の
パイロット流量制御弁はもとにメータィンに入っている
ので、主流れをメータィンを制御しているが、前記制御
弁をメータアウトに入れてパイロット流れの排出ボート
3にもどる流量を制御することによって王流れをメータ
アウトで制御することもできる。なおさらに、第6図に
図示する功換兼減圧弁としての回路構成について説明す
ると、前述同様に第1図で例示したパイロットボート4
5Aと前記切換弁ボートA間の管路にパイロット減圧弁
53Aを挿入したもので、パイロット切換弁49をP−
A、B−Tに切換えると、A側ではAボート4Aの圧力
が前記減圧弁設定圧より低い場合、パイロット流れが供
給ボート2から図示の経路を経てAボート4Aに流れ、
主流れはパイロット流量に応じて供給ボート2からAボ
ート4Aに流れるが、前記Aボートの圧力が前記減圧弁
設定圧に近接すると前記減圧弁流量が減って主流れ流量
も減り、Aボート4Aの圧力が前記設定圧に減圧される
The pump boat P of the cut-off valve 49 is the pilot boat 4.
6 to supply boat 2, boat A to pilot port 45A, boat B to pilot port 45B,
As described above, the tank boats T are connected to the discharge boats 3 via the pilot boat 47, respectively. Now, when the switching valve is switched to P-A and B-T,
On the A side, the pilot flow is the supply boat 2, the pilot boat 46, the pilot switching valve 49, and the same boat 45A.
, the same passage 15A, the throttle 9A, the same passage 16A, the spring chamber 18A, the valve chambers 21A, 19A, 44A, the A boat 4
On the B side, the main flow flows from the B boat 4B to the discharge boat 3 in the opposite direction to the above-mentioned passage, displacing the main valve bodies 5A and 5B, respectively, and on the A side, the main flow flows from the supply boat 2 to the A boat. 4A, and from the B boat 4B to the discharge boat 3 on the B side. In this case, since no other control valve is inserted into the pilot circuit, the pilot flow flows freely and the main flow also flows freely along the aforementioned path. Moreover, the said cut-sliding valve A-T,
When switching to P-B, the main flow flows from the A boat 4A to the discharge boat 3 and from the supply boat 2 to the B boat 4B, as before. In FIG. 5, where the circuit is configured as a switching/flow rate control valve, there is a pipe in the pipeline between the pilot boat 45A and the boat A of the pilot switching valve 49 shown in FIG. The same flow rate control valve 52B is inserted into the B side, and the switching valve is connected to the P-A, B side.
- When switched to T, the pilot flow flows from the supply boat 2 on the A side to the A boat 4A via the path shown, and on the B side also flows from the B boat 4B to the discharge boat 3 via the path shown; Since the flow rate control valve 52A controls and adjusts the pilot flow rate to q, the flow rate of the royal flow is K・q
Therefore, the flow rate from A boat 4A to the actuator is (
10K)q, and since the pilot flow freely flows through the check valve side of the flow rate control valve 52B on the B side, the main flow also flows freely from the B boat 4B to the discharge port 3. Then, when the switching valve is switched to A-T and P-B, A
On the side, the pilot flow flows freely into the discharge boat 3 and B
On the other hand, the flow rate control valve 52B controls the flow rate in the same manner as described above, and the flow rate to the actuator becomes (10K)q. In this case, the pilot flow control valve is originally installed in the meter, so it controls the main flow through the meter, but the control valve is installed in the meter out to control the flow rate of the pilot flow returning to the discharge boat 3. By doing so, it is also possible to control the flow by metering out. Furthermore, to explain the circuit configuration as a functional and pressure reducing valve illustrated in FIG. 6, the pilot boat 4 illustrated in FIG.
A pilot pressure reducing valve 53A is inserted into the conduit between 5A and the switching valve boat A, and the pilot switching valve 49 is connected to P-
When switching to A, B-T, on the A side, if the pressure of the A boat 4A is lower than the pressure reducing valve setting pressure, the pilot flow flows from the supply boat 2 to the A boat 4A via the illustrated path,
The main flow flows from the supply boat 2 to the A boat 4A according to the pilot flow rate, but when the pressure of the A boat approaches the pressure reducing valve setting pressure, the pressure reducing valve flow rate decreases and the main flow rate also decreases, and the A boat 4A The pressure is reduced to the set pressure.

B側では、パイロット流れはBボート48から図示の経
路を経て排出ボート3に自由に流れるので、主流れもB
ボート4Bから排出ボート3に自由に流れる。前記切換
弁をA−T、P−Bに切換えると、AおよびB両側とも
にパイロット流れは自由流で、王流れも、Aボート4A
から排出ボート3に、供給ボート2からBボート4Bに
自由に流れる。さらにまた、第7図に図示するりリーフ
弁としての回路構成は、既に例示した第1図のパイロッ
トボート45A,45Bと前記切襖弁ボートA,B間の
夫々の管路に分岐してパイロットリリーフ弁54A,5
4Bを配置したものであって、前記切換弁の切換えによ
って第1図の図示例と同様に切換弁として作動するが、
Aボート4Aの圧力がパイロットリリーフ弁54Aの設
定より高くなると、圧油がパイロット流れとして弁室4
4A筆順路を経て前記パイロットリリーフ弁54Aから
パイロットボート47に、さらに排出ボート3にリリー
フされるから、主弁体5Aは9Aに生じる圧力差によっ
て変位し、王流れをAボート4Aから排出ボート3にリ
リーフし、また前記圧力が低下すると、パイロット流れ
が止まって主弁体5Aが円筒ばね6A、円すし、ばね6
Cで中立位置に復位して排出ボート3へりリーフ流れを
止め、Aボート4Aの圧力を前記リリーフ弁46Aの設
定圧に保持する。
On the B side, the pilot flow flows freely from the B boat 48 to the discharge boat 3 via the path shown, so that the main flow also flows from the B
Flows freely from boat 4B to discharge boat 3. When the switching valve is switched to A-T and P-B, the pilot flow is a free flow on both sides of A and B, and the king flow is also a free flow.
from the supply boat 2 to the B boat 4B. Furthermore, the circuit configuration as a releaf valve illustrated in FIG. Relief valve 54A, 5
4B, and by switching the switching valve, it operates as a switching valve in the same way as the illustrated example in FIG.
When the pressure in the A-boat 4A becomes higher than the setting of the pilot relief valve 54A, pressure oil flows into the valve chamber 4 as a pilot flow.
The main valve body 5A is displaced by the pressure difference generated at 9A, and the main valve element 5A is displaced by the pressure difference generated at 9A, and the flow is transferred from the A boat 4A to the discharge boat 3. When the pressure is relieved and the pressure decreases, the pilot flow stops and the main valve body 5A is released from the cylindrical spring 6A, the conical spring, and the spring 6.
At C, the boat returns to the neutral position, stops the reef flow to the discharge boat 3, and maintains the pressure of the A boat 4A at the set pressure of the relief valve 46A.

この作動は、B側についても成立することはいうまでも
ない。なお、さらにまた、前述の第1図に図示したパイ
ロット回路のパイロットボート45A,458とパイロ
ット切換弁49のボートA,B間の各々の管路に、前者
管路にパイロット減圧弁53A、同じく流量制御弁52
Aを、後者管路に同じくリリーフ弁54B、流量制御弁
52Bを配置した第8図においては、前記パイロット切
換弁49の中立位置ではA側は全閉であるが、B側は前
記リリーフ弁54Bが作動してBボート4Bの圧油が前
記リリーフ弁設定圧以上に上昇しない。
Needless to say, this operation also holds true for the B side. Furthermore, in each of the pipes between the pilot boats 45A and 458 of the pilot circuit and the boats A and B of the pilot switching valve 49 shown in FIG. Control valve 52
In FIG. 8, in which a relief valve 54B and a flow control valve 52B are similarly arranged in the latter pipe line, the A side is fully closed when the pilot switching valve 49 is in the neutral position, but the B side is fully closed. operates, and the pressure oil in the B boat 4B does not rise above the relief valve setting pressure.

いま、前記功換弁49をP−A、B−Tに切り換えると
、A側ではパイロット回路の流量が流量制御弁52Aで
流量qに調整されるので、供給ボート2からAボート4
Aに流量K・qが流れ、また、Aポ−ト4Aから流出す
る流量が(1十K)qよりも減少する減圧弁53Aが働
き、−Aボート4Aの圧力を前記減圧弁設定圧に減圧し
、B側ではパイロット流れがBボート4Bから流量制御
弁52Bのチェック弁を経て排出ボート3に自由に流れ
るので、王流れもBボート4Bから排出ボート3に自由
に流れる。前記切換弁をA−T、P−Bに切換えると、
A側ではパイロット流れがAボート4Aから減圧弁53
Aおよび流量制御弁52Aの各チェック弁を経て排出ボ
ート3に自由に流れるので、主流れもAボート4Aから
排出ボート3に自由に流れ、B側ではパイロット流れが
前記流量制御弁で流量qに調整されてBボート4Bに流
れるから、主流れも供給ボート2から流量K・qがBボ
ート4Bに流れ、その圧力が前記リリーフ弁54B設定
圧よりも高くなると、パイロット流量qの一部または全
量がリリーフ弁54Bから排出ボート3に放流されるか
ら、主流れの流量もそれに伴って減少してBボート4B
の圧力が前記リリーフ弁設定圧を越すことがない。また
、上述の各実施例を、第9,10図に図示するように、
弁本体101を貫いて供給ポ−ト2および排出ボート3
を設け、池弁と該弁本体を横に係合させてサポート板1
02の間で通しボルト106およびナット110で締結
した弁間接競を行い、前記弁本体側面にAボート4A、
Bボート48およびボルト孔107を設けてアクチュェ
ータに接続し、また弁本体101上面に第11図々示の
取付けボルト孔108および各パイロットボート45A
,45B.46,47を規格化して設け、その上にパイ
ロット各種弁49,103,104,105・・・を積
重して構成するか、あるいは第12図々示の前述通しボ
ルト締結に代えて各弁側面に鍔1 1 1を設けて短ボ
ルト109およびナット11川こよって弁間接縞を行っ
た上に前述の構成を行うことによって、配管あるいはマ
ニホールドを省略した弁間回路構成をしてもよい。
Now, when the switching valve 49 is switched to P-A and B-T, the flow rate of the pilot circuit on the A side is adjusted to the flow rate q by the flow rate control valve 52A, so that the flow rate is changed from the supply boat 2 to the A boat 4.
A flow rate K.q flows into A, and the pressure reducing valve 53A, which reduces the flow rate flowing out from the A port 4A to less than (10K)q, operates, and the pressure in the -A boat 4A is brought to the pressure reducing valve set pressure. The pressure is reduced, and on the B side, the pilot flow freely flows from the B boat 4B to the discharge boat 3 via the check valve of the flow control valve 52B, so the king flow also freely flows from the B boat 4B to the discharge boat 3. When the switching valve is switched to A-T and PB,
On the A side, the pilot flow flows from the A boat 4A to the pressure reducing valve 53.
Since the main flow flows freely to the discharge boat 3 through the check valves A and flow control valve 52A, the main flow also flows freely from the A boat 4A to the discharge boat 3, and on the B side, the pilot flow is controlled by the flow rate control valve to the flow rate q. Since the main flow is regulated and flows to the B boat 4B, the main flow also flows from the supply boat 2 to the B boat 4B, and when the pressure becomes higher than the set pressure of the relief valve 54B, part or all of the pilot flow q is discharged from the relief valve 54B to the discharge boat 3, the flow rate of the main flow also decreases accordingly, and the B boat 4B
The pressure does not exceed the relief valve setting pressure. Moreover, as illustrated in FIGS. 9 and 10, each of the above-mentioned embodiments is
A supply port 2 and a discharge boat 3 pass through the valve body 101.
is provided, the pond valve and the valve body are engaged laterally, and the support plate 1 is installed.
02 are fastened with through bolts 106 and nuts 110, and A boat 4A is attached to the side of the valve body.
A B boat 48 and a bolt hole 107 are provided to connect to the actuator, and a mounting bolt hole 108 and each pilot boat 45A shown in FIG. 11 are provided on the upper surface of the valve body 101.
, 45B. 46, 47 are standardized and the various pilot valves 49, 103, 104, 105, etc. are stacked on top of each other, or alternatively, instead of the aforementioned through-bolt fastening as shown in FIG. By providing the flanges 111 on the side surfaces and performing the valve joint stripes with the short bolts 109 and nuts 11, and performing the above-described configuration, an intervalve circuit configuration may be created in which piping or manifolds are omitted.

上述したように、この発明は、パイロット切換弁単独と
、あるいは他のパイロット操作弁をも組合せてパイロッ
ト回路を構成することによって、パイロット回路の機能
をすべて保有させて王流れ制御が可能であり、さらに詳
述すれば、種々の単一機能をもつ小容量のパイロット弁
を組合せて主制御回路に要求される機能をもつパイロッ
ト回路を構成し、該回路の小量流れでそのパイロット流
れの立上りから広い制御範囲にわたり、王流れの向きに
応じた圧力補償機能を伴って大容量の主制御弁を制御で
きるため、一合の主制御弁でパイロット回路のもつ機能
と同機能を満たすように主回路を制御でき、主制御弁が
一合で多機能をもち、パイロット回路のもつ機能に応じ
て機能を発揮できらから、一種類の大容量の制御弁で、
小形パイロット弁だけを機能に応じて配備すればよく、
集積弁として体系化する場合にも少数種類で構成でき、
かつ主制御弁がァクチュェータ一合に対して一合で目的
を達することができ、さらに圧力補償弁に対して油路切
換弁を組み合わせてこれらを主弁体と別に弁本体に配置
したから主弁体周囲の油通路や開孔が複雑化することも
なく、主弁体スプール形状も簡素なものになり、したが
って小形軽量で価格面においても安価である。
As described above, the present invention enables full flow control by retaining all the functions of the pilot circuit by configuring the pilot circuit with the pilot switching valve alone or in combination with other pilot operated valves. More specifically, a pilot circuit with the functions required for the main control circuit is constructed by combining small-capacity pilot valves with various single functions, and a small amount of flow in the circuit is used to control the rise of the pilot flow. Since a large-capacity main control valve can be controlled over a wide control range and with a pressure compensation function depending on the direction of flow, the main circuit can be controlled so that a single main control valve can fulfill the same functions as the pilot circuit. Since the main control valve has multiple functions in one unit and can perform functions according to the functions of the pilot circuit, one type of large-capacity control valve can
All you need to do is deploy small pilot valves according to their functions.
Even when systematized as an integrated valve, it can be configured with a small number of types.
In addition, the main control valve can achieve its purpose in combination with the actuator, and the pressure compensation valve is combined with the oil passage switching valve and these are placed in the valve body separately from the main valve body. The oil passages and openings around the body are not complicated, and the main valve body spool has a simple shape, so it is small, lightweight, and inexpensive.

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

第1図は第1発明の実施例を示す縦断面図にパイロット
切換弁回路を添画した構成説明図、第2図は円筒および
円すし、ばねのばね力および変位関係曲線図、第3図は
第2発明の実施例を示す縦断面図にパイロット切換弁回
路を添画した構成説明図、第4図はポベット弁の流量お
よび圧力特性曲線図、第5,6,7および8図は第1発
明の実施例の縦断面図に各々別のパイロット回路例を添
画した構成説明図、第9図はこの発明に係る弁装置の弁
間接続およびパイロット操作弁積重の例を示す側面図、
第10図は前図の正面図、第11図は第9図のA−A矢
視図、第12図は弁間薮競等の他の例を示す側面図であ
る。 1・・・・・・弁本体、2・・・・・・供給ボート、3
・・・・・・排出ボート、4A,4B……A,Bボート
、5A,5B・…・・主弁体、8A,8B・・・・・・
圧力補償弁体、15A,158・・・・・・パイロット
通路、9A,9B・・・・・・絞り、49・・・・・・
パイロット功換弁。 1図 第2図 第3図 第4図 第5図 第9図 第10図 第6図 第11図 第7図 第12図 第8図
Fig. 1 is a configuration explanatory diagram showing a longitudinal cross-sectional view showing an embodiment of the first invention with a pilot switching valve circuit attached, Fig. 2 is a cylinder, a circular sushi, and a spring force and displacement relationship curve diagram of a spring, Fig. 3 4 is a configuration explanatory diagram with a pilot switching valve circuit attached to a longitudinal sectional view showing an embodiment of the second invention, FIG. 4 is a flow rate and pressure characteristic curve diagram of a Pobet valve, and FIGS. FIG. 9 is a configuration explanatory diagram in which a vertical cross-sectional view of an embodiment of the invention is accompanied by different examples of pilot circuits, and FIG. ,
FIG. 10 is a front view of the previous figure, FIG. 11 is a view taken along the line A--A in FIG. 9, and FIG. 12 is a side view showing another example of the valve spacing. 1... Valve body, 2... Supply boat, 3
...Discharge boat, 4A, 4B...A, B boat, 5A, 5B...Main valve body, 8A, 8B...
Pressure compensation valve body, 15A, 158... Pilot passage, 9A, 9B... Throttle, 49...
Pilot valve. Figure 1Figure 2Figure 3Figure 4Figure 5Figure 9Figure 10Figure 6Figure 11Figure 7Figure 12Figure 8

Claims (1)

【特許請求の範囲】 1 弁本体内で両端から主弁ばねで弾圧してスプリング
センタ方式にしたスプール形式の主弁体を、パイロツト
流れによつてパイロツトオリフイスの前後に生じる差圧
が主弁ばねのばね力と平衡するまで前記主弁ばねに抗し
て変位させてパイロツト操作方式で主回路の流れを制御
するようにしたものにおいて、 パイロツトポート45
Aからの液圧を一端面側に受け、外部ポート4Aからの
液圧を他端面側に受け、これら両端面側についてパイロ
ツト圧力に対する受圧面積が等しくされ、一端面側にパ
イロツト圧力を受けて一方へ変位したときに外部ポート
4Aを弁本体1の内部油室33Aに連通させる第一の主
制御口41Aと、他端面側にパイロツト圧力を受けて他
方へ変位したときに外部ポート4Aを前記内部油室33
Aに連通させる第二の主制御口28Aとを中立位置に対
して対称的に有する主弁体5Aと、 パイロツト圧力が
無いときに主弁体5Aを中立位置にすると共に、中立位
置からの主弁体変位の両方向で主弁体変位ストロークに
対するばね力変化が互いに等しい主弁ばねと、 パイロ
ツトポート45Aと外部ポート4Aとの間を所定開度で
連通してパイロツト流れによりその前後に差圧を生じる
パイロツトオリフイスと、 弁本体1内に摺動可能に配
置され、その中立位置からの変位について均等なばね力
が作用するように圧力補償弁ばね13A,14Aによつ
てスプリングセンタ方式で支持され、一端側に前記内部
油室33Aの液圧を、他端側に前記外部ポート4Aの液
圧を、それぞれ互いに等しい受圧面積で受けるようにな
され、外周部に前記内部油室33Aに開口した凹溝29
Aが形成された圧力補償弁8Aと、 一端側に前記パイ
ロツトポート45Aの液圧を、他端側に前記外部ポート
4Aの液圧を受けるように前記圧力補償弁8Aの外周部
に同軸状に摺動可能に嵌められて圧力補償弁外周の凹溝
29Aの両肩と共に前記内部油室33Aに連通した一対
の圧力補償制御口39A,40Aを形成すると共に、前
記パイロツトポート45Aの液圧を一端側に受けて一方
へ変位したときは一方の前記圧力補償制御口39Aを圧
油供給ポート2に接続して他方40Aを閉じ、前記外部
ポート4Aの液圧を他端側に受けて他方へ変位したとき
には他方の前記圧力補償制御口40Aを排出ポート3に
接続して一方39Aを閉じるように、前記圧力補償弁体
外周の凹溝29Aを間にして対称的に一対の切換油路開
口38A,35Aが設けられた油路切換弁10A、とを
備え 更に前記パイロツトオリフイスを固定オリフイス
9Aとし、前記主弁ばねをパイロツト流れが少ないうち
から作用する円筒ばね6A,7Aとパイロツト流れが或
る程度多くなつてから作用して撓みと共にばね力を増加
する円すいばね6C,7Cとの組合せとしたことを特徴
とする液圧制御弁装置。 2 弁本体内で両端から主弁ばねで弾圧してスプリング
センタ方式にしたスプール形式の主弁体を、パイロツト
流れによつてパイロツトオリフイスの前後に生じる差圧
が主弁ばねのばね力と平衡するまで前記主弁ばねに抗し
て変位させてパイロツト操作方式で主回路の流れを制御
するようにしたものにおいて、 パイロツトポート45
Aからの液圧を一端面側に受け、外部ポート4Aからの
液圧を他端面側に受け、これら両端面側についてパイロ
ツト圧力に対する受圧面積が等しくされ、一端面側にパ
イロツト圧力を受けて一方へ変位したときに外部ポート
4Aを弁本体1の内部油室33Aに連通させる第一の主
制御口41Aと、他端面側にパイロツト圧力を受けて他
方へ変位したときに外部ポート4Aを前記内部油室33
Aに連通させる第二の主制御口42Aとを中立位置に対
して対称的に形成する主弁体5Aと、 パイロツト圧力
が無いときに主弁体5Aを中立位置にすると共に、中立
位置からの主弁体変位の両方向で主弁体変位ストローク
に対するばね力変化が互いに等しい主弁ばねと、 パイ
ロツトポート45Aと外部ポート4Aとの間を所定開度
で連通してパイロツト流れによりその前後に差圧を生じ
るパイロツトオリフイスと、 弁本体1内に摺動可能に
配置され、その中立位置からの変位について均等なばね
力が作用するように圧力補償弁ばね13A,14Aによ
つてスプリングセンタ方式で支持され、一端側に前記内
部油室33Aの液圧を、他端側に前記外部ポート4Aの
液圧を、それぞれ互いに等しい受圧面積で受けるように
なされ、外周部に前記内部油室33Aに開口した凹溝2
9Aが形成された圧力補償弁8Aと、 一端側に前記パ
イロツト45Aの液圧を、他端側に前記外部ポート4A
の液圧を受けるように前記圧力補償弁8Aの外周部に同
軸状に摺動可能に嵌められて圧力補償弁外周の凹溝29
Aの両肩部と共に前記内部油室33Aに連通した一対の
圧力補償制御口39A,40Aを形成すると共に、前記
パイロツトポート45Aの液圧を一端側に受けて一方へ
変位したときは一方の前記圧力補償制御口39Aを圧油
供給ポート2に接続して他方40Aを閉じ、前記外部ポ
ート4Aの液圧を他端側に受けて他方へ変位したときに
は他方の前記圧力補償制御口40Aを排出ポート3に接
続して一方39Aを閉じるように、前記圧力補償弁体外
周の凹溝29Aを間にして対称的に一対の切換油路開口
38A,35Aが設けられた油路切換弁10A、とを備
え、 更に前記パイロツトオリフイスを、その上流側の
パイロツト圧力が或る圧力以上になつたとき開いてその
後パイロツト流量に応じた差圧を生じるポペツト弁50
A,51Aによつて構成し、前記主弁ばねを、パイロツ
ト圧力が前記ポペツト弁のクラツキング圧力に達したと
きに主弁体の主制御口が丁度開き始めるように設定され
た円筒ばね6′A,7′Aのみによつて構成したことを
特徴とする液圧制御弁装置。
[Scope of Claims] 1. A spool-type main valve element which is made up of a spring center type by being compressed by main valve springs from both ends within the valve body, is compressed by the differential pressure generated before and after the pilot orifice due to the pilot flow. The flow of the main circuit is controlled by a pilot operation method by displacing the main valve against the spring force until it is balanced with the spring force of the pilot port 45.
The hydraulic pressure from A is received on one end side, and the hydraulic pressure from external port 4A is received on the other end side, and the pressure receiving area for the pilot pressure is equal on both end sides, and the pilot pressure is received on one end side, and the other side receives the hydraulic pressure from the external port 4A. A first main control port 41A communicates the external port 4A with the internal oil chamber 33A of the valve body 1 when the valve is displaced to the other side, and a first main control port 41A that communicates the external port 4A with the internal oil chamber 33A of the valve body 1 when the valve body is displaced to the other side. Oil chamber 33
The main valve body 5A has a second main control port 28A that communicates with the main control port 28A symmetrically with respect to the neutral position. The main valve spring, whose spring force change with respect to the main valve body displacement stroke is equal in both directions of the valve body displacement, and the pilot port 45A and the external port 4A are communicated with each other at a predetermined opening degree to create a differential pressure before and after the valve body due to the pilot flow. the resulting pilot orifice, which is slidably arranged within the valve body 1 and supported in a spring-centered manner by pressure compensating valve springs 13A, 14A so as to apply an equal spring force to its displacement from its neutral position; One end receives the hydraulic pressure of the internal oil chamber 33A, and the other end receives the hydraulic pressure of the external port 4A with equal pressure receiving areas, and a concave groove opens to the internal oil chamber 33A on the outer periphery. 29
A pressure compensating valve 8A is formed, and a pressure compensating valve 8A is coaxially arranged on the outer circumference of the pressure compensating valve 8A so that one end receives the hydraulic pressure of the pilot port 45A and the other end receives the hydraulic pressure of the external port 4A. A pair of pressure compensation control ports 39A and 40A that are slidably fitted and communicated with the internal oil chamber 33A together with both shoulders of the concave groove 29A on the outer periphery of the pressure compensation valve are formed. When the pressure compensation control port 39A is connected to the pressure oil supply port 2 and the other 40A is closed, the hydraulic pressure of the external port 4A is received at the other end and the valve is displaced to the other side. A pair of switching oil passage openings 38A are arranged symmetrically with a concave groove 29A on the outer periphery of the pressure compensating valve body in between, so that when this happens, the other pressure compensation control port 40A is connected to the discharge port 3 and one 39A is closed. and an oil passage switching valve 10A provided with an oil passage switching valve 35A; further, the pilot orifice is a fixed orifice 9A, and the main valve spring is actuated by cylindrical springs 6A and 7A that act from when the pilot flow is small, and when the pilot flow is large to a certain extent. A hydraulic control valve device characterized in that it is combined with conical springs 6C and 7C which act after bending and increase the spring force as they bend. 2. The spool-type main valve element is pressed by main valve springs from both ends within the valve body to form a spring center system, and the differential pressure generated before and after the pilot orifice due to the pilot flow balances the spring force of the main valve spring. The pilot port 45 is configured to control the flow of the main circuit by a pilot operation method by displacing the main valve against the main valve spring.
The hydraulic pressure from A is received on one end side, and the hydraulic pressure from external port 4A is received on the other end side, and the pressure receiving area for the pilot pressure is equal on both end sides, and the pilot pressure is received on one end side, and the other side receives the hydraulic pressure from the external port 4A. A first main control port 41A communicates the external port 4A with the internal oil chamber 33A of the valve body 1 when the valve is displaced to the other side, and a first main control port 41A that communicates the external port 4A with the internal oil chamber 33A of the valve body 1 when the valve body is displaced to the other side. Oil chamber 33
The main valve body 5A has a second main control port 42A that communicates with the main control port 42A, which is formed symmetrically with respect to the neutral position. The main valve spring, which has the same spring force change with respect to the main valve body displacement stroke in both directions of the main valve body displacement, and the pilot port 45A and the external port 4A are communicated with each other at a predetermined opening degree, and a differential pressure is created before and after the main valve spring by the pilot flow. a pilot orifice that generates a pressure, and a pilot orifice that is slidably disposed within the valve body 1 and supported in a spring center manner by pressure compensating valve springs 13A and 14A so that an equal spring force acts on displacement from the neutral position. , one end side receives the hydraulic pressure of the internal oil chamber 33A, the other end side receives the hydraulic pressure of the external port 4A with equal pressure receiving areas, and a recess opened to the internal oil chamber 33A on the outer periphery. Groove 2
9A is formed, the hydraulic pressure of the pilot 45A is connected to one end, and the external port 4A is connected to the other end.
A concave groove 29 on the outer periphery of the pressure compensating valve is slidably fitted coaxially to the outer periphery of the pressure compensating valve 8A so as to receive the hydraulic pressure of the pressure compensating valve 8A.
Together with both shoulders of A, a pair of pressure compensation control ports 39A and 40A are formed which communicate with the internal oil chamber 33A. The pressure compensation control port 39A is connected to the pressure oil supply port 2 and the other 40A is closed, and when the other end receives the hydraulic pressure of the external port 4A and is displaced to the other end, the other pressure compensation control port 40A is connected to the discharge port. an oil passage switching valve 10A, which is provided with a pair of switching oil passage openings 38A, 35A symmetrically with a concave groove 29A on the outer periphery of the pressure compensating valve body in between, so as to connect to the oil passage opening 38A and close one 39A; further comprising a poppet valve 50 which opens the pilot orifice when the pilot pressure on the upstream side thereof exceeds a certain pressure and thereafter generates a differential pressure according to the pilot flow rate.
A, 51A, and the main valve spring is a cylindrical spring 6'A set so that the main control port of the main valve body just starts to open when the pilot pressure reaches the cracking pressure of the poppet valve. , 7'A.
JP12033574A 1974-10-21 1974-10-21 hydraulic control valve device Expired JPS6035566B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12033574A JPS6035566B2 (en) 1974-10-21 1974-10-21 hydraulic control valve device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12033574A JPS6035566B2 (en) 1974-10-21 1974-10-21 hydraulic control valve device

Publications (2)

Publication Number Publication Date
JPS5147626A JPS5147626A (en) 1976-04-23
JPS6035566B2 true JPS6035566B2 (en) 1985-08-15

Family

ID=14783704

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12033574A Expired JPS6035566B2 (en) 1974-10-21 1974-10-21 hydraulic control valve device

Country Status (1)

Country Link
JP (1) JPS6035566B2 (en)

Also Published As

Publication number Publication date
JPS5147626A (en) 1976-04-23

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