JPS6068410A - Reversible reducing valve - Google Patents

Reversible reducing valve

Info

Publication number
JPS6068410A
JPS6068410A JP58174190A JP17419083A JPS6068410A JP S6068410 A JPS6068410 A JP S6068410A JP 58174190 A JP58174190 A JP 58174190A JP 17419083 A JP17419083 A JP 17419083A JP S6068410 A JPS6068410 A JP S6068410A
Authority
JP
Japan
Prior art keywords
pressure
spool
pilot
secondary side
reducing valve
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.)
Pending
Application number
JP58174190A
Other languages
Japanese (ja)
Inventor
Nobuatsu Kasashima
笠島 信篤
Kazuo Takada
和夫 高田
Makoto Inamura
稲村 誠
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.)
Nachi Fujikoshi Corp
Original Assignee
Nachi Fujikoshi Corp
Fujikoshi KK
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 Nachi Fujikoshi Corp, Fujikoshi KK filed Critical Nachi Fujikoshi Corp
Priority to JP58174190A priority Critical patent/JPS6068410A/en
Publication of JPS6068410A publication Critical patent/JPS6068410A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D16/00Control of fluid pressure
    • G05D16/14Control of fluid pressure with auxiliary non-electric power
    • G05D16/16Control of fluid pressure with auxiliary non-electric power derived from the controlled fluid
    • G05D16/166Control of fluid pressure with auxiliary non-electric power derived from the controlled fluid using pistons within the main valve

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Power Engineering (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Fluid Pressure (AREA)

Abstract

PURPOSE:To obtain a miniature reversible valve by providing slidably a small spool to a pilot path so that an end of the spool is exposed to the pressure of the primary side and closing the pilot path by the land of the spool only when the pressure of the secondary side is higher than that of the primary side. CONSTITUTION:A miniature spool 6 is set slidably to a pilot path 8 which is led to an end face 5 of a main spool 4 from a secondary side B provided to a cover 3. The spool 6 is closed by plugs 20 and 22 and also pressed always toward the plug 22 by a spring 13. The pressure receiving surface 6' at an end of the spool 6 is exposed to the pilot pressure oil via the side B and the path 8. While the pressure receiving surface 6'' of the other end having almost the same area as the surface 6' is exposed to the pressure of a primary side B'. A sleeve part 6c which forms a land of the spool 6 cuts off a pilot oil path 8d only when the pressure P2 of the side B is higher than the pressure P1 of the side B'. Thus it is possible to obtain a miniature reversible reducing valve with which a reverse current is not limited by a decompressing action.

Description

【発明の詳細な説明】 本発明は工作機械および産業機械などに使用される流体
圧レデューシングバルブの改良に関し、特にスペース節
約型のカートリッジタイプのレデューシングバルブの改
良に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to improvements in fluid pressure reducing valves used in machine tools, industrial machinery, etc., and more particularly to improvements in space-saving cartridge-type reducing valves.

油圧装置のような流体圧装置に使用されるレデューシン
グバルブはポンプから切換弁等を通ってシリンダへ送ら
れる油路に挿入され、例えば第1図でポンプ倶jの一次
側(B′)圧力に対してシリンダ側の二次側1 (B)
圧力を減圧する。そしてこのために通常二次側からメイ
ンスプールの端部にパイロット圧油がパイロット通路(
8)を介して導かれている。
A reducing valve used in a fluid pressure device such as a hydraulic device is inserted into an oil path that is sent from a pump to a cylinder through a switching valve, etc. For example, in FIG. Secondary side 1 on the cylinder side with respect to pressure (B)
Reduce pressure. For this purpose, pilot pressure oil is usually passed from the secondary side to the end of the main spool through the pilot passage (
8).

(9)はドレン油路である。シリンダが戻されるとき、
シリンダ内の圧油は他のバルブが介されていない時は該
レデューシングパルプ(Inを通って逆流されタンクへ
戻されなければならない。即ち逆方向に二次側(B)か
ら−次側(B′)へ戻される必要がある。
(9) is a drain oil passage. When the cylinder is returned,
When no other valve is used, the pressure oil in the cylinder must flow back through the reducing pulp (In) and return to the tank, i.e. in the opposite direction from the downstream side (B) to the It needs to be returned to (B').

ところが、この”場合二次側から導かハたパイロット圧
油が同様にメインスプールの該端部を押すので、二次側
への流入圧力が設定圧力(二次1μm1圧力)ニ近いと
、レデューシングバルブは減圧作動をし、設定圧力以上
になるとメインスプールは二次側から一次側へのバルブ
内の通路を遮1tliシ、逆流しなくなることが知られ
ている。このため、一般には第1図に示すようにチェッ
クパルプ(7)がバイパスして組込まれ、逆流はこのチ
ェックバルブ(7)を通って自由流とされタンクへ戻さ
れる。しかしこのやり方では逆流量に応じた大きさのチ
ェックパルプを使用しなければならず、その分だけバル
ブが大きくなりコンパクト化が図れないしまたコスト高
になる。
However, in this case, the pilot pressure oil led from the secondary side also pushes the end of the main spool, so if the inflow pressure to the secondary side is close to the set pressure (secondary 1 μm 1 pressure), the reduction will occur. It is known that the single valve operates to reduce pressure, and when the pressure exceeds the set pressure, the main spool blocks the passage inside the valve from the secondary side to the primary side, preventing backflow. A check pulp (7) is installed as a bypass as shown in the figure, and the backflow is returned to the tank as a free flow through this check valve (7).However, in this method, a check of a size corresponding to the backflow amount is required. Pulp must be used, which increases the size of the valve, making it difficult to make it compact and increasing costs.

代替的に、第2図に示すように、ポンプからの圧油ポー
) (P)にレデューシングバルブを直結し、パイロッ
ト圧油をシリンダへの通路(B’B)よシ導くことが知
られている。しかしながらこのやり方ではバルブはコン
パクトにはなるが、二次側113)から−次III (
3’lに圧油を逆流させるとき、圧力損失で二次側圧力
ひいてはパイロット圧油の圧力が大きくなり、これが設
定圧力に近づくとレデューシングバルブ(]0は減圧作
動し逆流流量を制限し減少させる欠点がある。
Alternatively, as shown in Figure 2, it is known to connect a reducing valve directly to the pressure oil port (P) from the pump and guide the pilot pressure oil through the passage (B'B) to the cylinder. It is being However, although this approach makes the valve more compact, it does mean that from the secondary side 113) to the
When pressure oil flows backward into 3'l, the pressure on the secondary side and the pilot pressure oil increase due to pressure loss, and when this approaches the set pressure, the reducing valve (]0 operates to reduce the pressure and limit the flow rate of backflow. There are drawbacks to reducing it.

本発明は、かかる従来製品の欠点を除去した、チェック
弁をパラレルに使用することがなく、コンパクトで安価
でかつ逆流が減圧作動により制限されることのない、逆
流可能レデューシングバルブを提供することを目的とす
る。
The present invention eliminates the drawbacks of such conventional products and provides a reducing valve capable of backflow, which does not use a check valve in parallel, is compact and inexpensive, and whose backflow is not restricted by pressure reduction operation. The purpose is to

このため本発明は、−次側から二次側へ流れる圧油の二
次側の圧力を減圧するように、二次側からメインスプー
ルの端部にパイロット圧油がパイロット通路を介して導
かれたレデューシングバルブにおいて、前記パイロット
通路に、一端の受圧面を前記パイロット圧油にさらしそ
れとほぼ同面積の他端の受圧面を油路を介し一次側の圧
力にさらすようにされた小スプールが摺動可能に挿入さ
れており、該小スプールは二次側圧力が一次側圧力より
高いときにのみ小スプールのランドにより前記パイロッ
ト通路を閉じるようにされた逆流可能レデューシングバ
ルブとしたものである。かかる構成によると、二次側か
ら一次1則への逆流時には必づ二次1111圧力が一次
側圧力より高くなるので、小スプールのランドはパイロ
ット通路を閉じ、減圧作動をさせないので、逆流時に圧
力損失の影響で二次側圧力が高くなり、パイロット圧油
の圧力が設定圧力に近づき減圧作動させ、流量が制限さ
れることかなくなった。またパラレルにチェックパルプ
を使用する必要がなく、パイロット通路に小ピストンが
挿入されるだけであるから、コンパクトでかつ安価であ
る。
Therefore, in the present invention, pilot pressure oil is guided from the secondary side to the end of the main spool via the pilot passage so as to reduce the pressure on the secondary side of the pressure oil flowing from the secondary side to the secondary side. In the reducing valve, a small spool is provided in the pilot passage, the pressure receiving surface of one end of which is exposed to the pilot pressure oil, and the pressure receiving surface of the other end of approximately the same area as that of the small spool exposed to the pressure on the primary side via the oil passage. is slidably inserted therein, and the small spool is a reversible reducing valve configured to close the pilot passage by the land of the small spool only when the outlet pressure is higher than the inlet pressure. It is. According to this configuration, when there is a backflow from the secondary side to the primary one law, the secondary 1111 pressure is always higher than the primary side pressure, so the land of the small spool closes the pilot passage and does not perform a pressure reduction operation, so the pressure decreases during the backflow. The secondary side pressure increased due to the influence of the loss, and the pressure of the pilot pressure oil approached the set pressure, allowing the pressure to be reduced and the flow rate to no longer be restricted. Furthermore, since there is no need to use check pulp in parallel and only a small piston is inserted into the pilot passage, it is compact and inexpensive.

次に本発明の実施例につき図面を参照して説明する。第
3図、第4図は一実施例を示す断面構造図を示し、第5
図はその油圧J工S記号を示す。第3図において、逆流
可能レデューシングバルブはバランスピストン形のもの
で、パイロット部(2)によってメインスプール(4)
のランド(6)が(a)部で一次側(B゛)から2次側
■〕への流れを二次側から、パイロット通路(8)で導
かれたパイロット圧油がメインスプール(4)の端部(
5)K作用して減圧作用をするようにされている。かか
るバランスピストン形のレデューシングバルブの構成、
減圧作動の原理は周知であり詳細は説明しない。
Next, embodiments of the present invention will be described with reference to the drawings. 3 and 4 show cross-sectional structural views showing one embodiment, and FIG.
The figure shows the hydraulic J/S symbol. In Figure 3, the reversible reducing valve is of the balanced piston type, and the pilot part (2) connects the main spool (4) to the main spool (4).
At part (a), the land (6) of the pilot pressure oil guided from the secondary side by the pilot passage (8) flows from the primary side (B) to the secondary side ■] to the main spool (4). The end of (
5) K acts to reduce pressure. The configuration of such a balanced piston type reducing valve,
The principle of pressure reduction operation is well known and will not be described in detail.

本実施例ではカバー(3)に設けられた二次側(B)が
らメインスプール(4)の端面(5)に導かれたパイロ
ット通路(8)に、摺動可能な小スプール(6)が挿入
されている。小スプール(6)はプラグ−(ハ)によっ
て閉じられ、スプリングQ3で常時プラタン2に向けて
押圧されている。そして小スプール(6)は第5図に示
すように、小径部(6a)で連結されたポペット部(6
c)と、小スプール(6)のランドを形成するスリーブ
部(6りからなり、かつ小径部(6a)には半径方 向
寒(6d)が設けられ、スリーブ部(6つの中央孔(8
りと共にパイロット通路(8d)を形成している。ポペ
ット部(6b)内にはスプリングq4が入れられている
In this embodiment, a slidable small spool (6) is installed in a pilot passage (8) that is guided from the secondary side (B) provided on the cover (3) to the end face (5) of the main spool (4). It has been inserted. The small spool (6) is closed by a plug (c) and is constantly pressed toward the platen 2 by a spring Q3. The small spool (6) is connected to the poppet part (6a) by the small diameter part (6a) as shown in FIG.
c) and a sleeve part (6) forming the land of the small spool (6), and the small diameter part (6a) is provided with a radial hole (6d), and the sleeve part (six central holes (8)
Together with this, a pilot passage (8d) is formed. A spring q4 is inserted into the poppet portion (6b).

ポペット部(6b)の1端の受圧面(6つは、二次側(
B)とパイロット通路(8b、80.8a、(3d )
 fx介してパイロット圧油にさらされており、それと
ほぼ同面積の他端の受圧面(6“)は油路(場を介した
一次側(Bつの圧力にさらされている。
The pressure receiving surface at one end of the poppet portion (6b) (6 is the pressure receiving surface on the secondary side (
B) and pilot passage (8b, 80.8a, (3d)
The pressure receiving surface (6") at the other end, which has approximately the same area as the pilot pressure oil, is exposed to the pressure of the primary side (B) via the oil passage (field).

いま無負荷状態であるときは、メインスプール(4)ハ
メインスプリングaηに押圧され、その端面(5)をカ
バー(3)に押し付けている。そして−次側(B“)か
ら二次側(B)に圧油が流れるときは、−次側(Bりの
圧力(Pl)が二次側1■)の圧力(P2)よシ高いの
で、小スプール(6)は図示の位置にある。スプリング
a4はこの状態を確実にするためのごく弱いものであリ
、/」・スプール(6)の下方端はプラグ器と当接して
おり、パイロット通路(8b、8G、8(1,,6d、
8 )は開かれており、バルブは減圧作動をする。パイ
ロット圧油はメインスプール(4)の端部(5)に作用
し、ランド(6)次に二次倶](B)から−次側(Bつ
に圧油が逆流するときは、二次1ull (f3)の圧
力(B2)が−次側(Bつの圧力(Pl)より高いので
、小スプール(6)は上方に移動しソト圧油はメインス
プール(4)の端面(5)に作用しないので、バルブは
減圧作動をせず、メインスプール(4)のランド(6)
は(a)部で全開し、二次体幹〕から一次側(B1)へ
の流れは自由流となシ、圧力降下による二次側の圧力上
昇の影響を受けない。またパラレルにチェックバルブを
入れる必要がないので、コンパクトで安価である。小ピ
ストン(6)は小さいものでよいので、スペースの増加
はきわめて少い。
When the main spool (4) is currently under no load, the main spool (4) is pressed by the main spring aη, and its end face (5) is pressed against the cover (3). When pressure oil flows from the negative side (B'') to the secondary side (B), the pressure (Pl) on the negative side (B) is higher than the pressure (P2) on the secondary side 1. , the small spool (6) is in the position shown.The spring a4 is very weak to ensure this state./''The lower end of the spool (6) is in contact with the plug device, Pilot passage (8b, 8G, 8 (1, 6d,
8) is open and the valve operates to reduce pressure. The pilot pressure oil acts on the end (5) of the main spool (4), then the land (6), then the secondary Since the pressure (B2) of 1ull (f3) is higher than the pressure (Pl) of - next side (B), the small spool (6) moves upward and the soto pressure oil acts on the end face (5) of the main spool (4). Therefore, the valve does not operate to reduce pressure, and the land (6) of the main spool (4)
is fully opened at part (a), and the flow from the secondary trunk to the primary side (B1) is a free flow and is not affected by the pressure increase on the secondary side due to pressure drop. Also, since there is no need to install a check valve in parallel, it is compact and inexpensive. Since the small piston (6) may be small, the increase in space is extremely small.

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

第1図、第2図は従来品であるレデューシングバルブを
示し、第3図は本発明の一実施例である逆流可能レデュ
ーシング・くルブの断面構造図、第4図は第3図の部分
拡大図、第4図は第3図の油圧JIS記号を示す。 4・・・メインスプール 5・・端 而6・・・小スプ
ール 6+、6”・・・受圧面6G・・・小スプールの
ランド 6eL、8.8b、8C,8d・・・パイロット通路1
2・・・メインスプールのランド 13・・・スプリング 19・・油 路代理人 弁理士
 河 内 潤 二 手 続 補 正 書 昭和58年10月31日 特許庁長官若杉和夫殿 1、事件の表示 昭和58年特許願第174190号 2、発明の名称 逆流可能レデューシングバルブ 3、補正をする者 事件との関係 特許出願人 名称 (519) 株式会社 不 二 越4、代理人 居所 東京都港区芝公園2丁目4番1号秀和芝パークビ
ル3階 自 発 6、補正の対象 明細書の発明の詳細な説明の欄、図面 7、補正の内容 7.1 明細書第6頁第3行目「ポペット部(bcJを
「ポペット部(6b)Jに訂正する。 7.2 図面第3図を別紙の通り訂正[る。
Figures 1 and 2 show a conventional reducing valve, Figure 3 is a cross-sectional structural diagram of a reducing valve that allows backflow, which is an embodiment of the present invention, and Figure 4 is a diagram of the reducing valve shown in Figure 3. The partially enlarged view, FIG. 4, shows the hydraulic JIS symbols in FIG. 3. 4...Main spool 5...End 6...Small spool 6+, 6"...Pressure receiving surface 6G...Small spool land 6eL, 8.8b, 8C, 8d...Pilot passage 1
2...Main spool land 13...Spring 19...Oil road agent Patent attorney Jun Kawachi Second procedure Amendment Written on October 31, 1981 Mr. Kazuo Wakasugi, Commissioner of the Japan Patent Office 1, Indication of the case 1982 Patent Application No. 174190 2, name of the invention Reducing valve capable of backflow 3, relationship with the case of the person making the amendment Patent applicant name (519) Fuji Koshi Co., Ltd. 4, agent residence Shiba Koen, Minato-ku, Tokyo 2-4-1 Hidekazu Shiba Park Building, 3rd floor, Part 6, Detailed description of the invention in the specification subject to amendment, Drawing 7, Contents of amendment 7.1 Page 6 of the specification, line 3 “Poppet portion (Correct bcJ to ``Poppet part (6b) J.'' 7.2 Correct figure 3 of the drawing as shown in the attached sheet.)

Claims (1)

【特許請求の範囲】[Claims] 一次側から二次側へ流れる圧油の二次I11の圧力を減
圧するように、二次mlからメインスプールの端部にパ
イロット圧油がパイロット通路を介して導かれたレデュ
ーシングバルブにおいて、前記パイロット通路に、一端
の受圧面を前記パイロット圧油にさらしそれとほぼ同面
積の他端の受圧面を油路を介し一次側の圧力にさらすよ
うにされた小スプールが、摺動可能に挿入されており、
該小スプールは二次側圧力が一次側圧力より高いときに
のみ小スプールのランドによシ前記パイロット通路を閉
じるようにされた逆流可能レデューシングバルブ。
In a reducing valve in which pilot pressure oil is guided from the secondary ml to the end of the main spool via a pilot passage so as to reduce the pressure of the secondary I11 of pressure oil flowing from the primary side to the secondary side, A small spool having a pressure receiving surface at one end exposed to the pilot pressure oil and a pressure receiving surface at the other end having approximately the same area as the pilot pressure oil is slidably inserted into the pilot passage. has been
The small spool is configured to close the pilot passage by the land of the small spool only when the pressure on the secondary side is higher than the pressure on the primary side.
JP58174190A 1983-09-22 1983-09-22 Reversible reducing valve Pending JPS6068410A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58174190A JPS6068410A (en) 1983-09-22 1983-09-22 Reversible reducing valve

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58174190A JPS6068410A (en) 1983-09-22 1983-09-22 Reversible reducing valve

Publications (1)

Publication Number Publication Date
JPS6068410A true JPS6068410A (en) 1985-04-19

Family

ID=15974292

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58174190A Pending JPS6068410A (en) 1983-09-22 1983-09-22 Reversible reducing valve

Country Status (1)

Country Link
JP (1) JPS6068410A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62146212U (en) * 1986-03-03 1987-09-16
FR2654794A1 (en) * 1989-11-21 1991-05-24 Tilles Mecanique NEUTRALIZABLE DETENDER.
EP1188934A3 (en) * 2000-09-13 2004-01-21 Robert Bosch Gmbh Control device for an hydraulic volume flow

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62146212U (en) * 1986-03-03 1987-09-16
FR2654794A1 (en) * 1989-11-21 1991-05-24 Tilles Mecanique NEUTRALIZABLE DETENDER.
EP1188934A3 (en) * 2000-09-13 2004-01-21 Robert Bosch Gmbh Control device for an hydraulic volume flow

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