JPH0320603B2 - - Google Patents

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Publication number
JPH0320603B2
JPH0320603B2 JP60037047A JP3704785A JPH0320603B2 JP H0320603 B2 JPH0320603 B2 JP H0320603B2 JP 60037047 A JP60037047 A JP 60037047A JP 3704785 A JP3704785 A JP 3704785A JP H0320603 B2 JPH0320603 B2 JP H0320603B2
Authority
JP
Japan
Prior art keywords
port
inner hole
check valve
electromagnetic
control 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.)
Expired - Lifetime
Application number
JP60037047A
Other languages
Japanese (ja)
Other versions
JPS61197803A (en
Inventor
Kazuo Niitsuma
Nobutaka Chiaki
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.)
Tokyo Keiki Inc
Original Assignee
Tokyo Keiki 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 Tokyo Keiki Co Ltd filed Critical Tokyo Keiki Co Ltd
Priority to JP3704785A priority Critical patent/JPS61197803A/en
Publication of JPS61197803A publication Critical patent/JPS61197803A/en
Publication of JPH0320603B2 publication Critical patent/JPH0320603B2/ja
Granted legal-status Critical Current

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Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は重量物を押し上げるアクチユエータ例
えばシリンダー等を制御するパイロツトチエツク
機能付方向切換弁で特に超小型で応答速度の速
い、しかも安価なパイロツトチエツク機能付方向
切換弁に関する。
[Detailed Description of the Invention] [Field of Industrial Application] The present invention is a directional control valve with a pilot check function that controls an actuator that pushes up a heavy object, such as a cylinder, and is particularly directed to an ultra-compact, fast-response, and inexpensive pilot check valve. Regarding directional valves with functions.

〔従来の技術〕[Conventional technology]

従来、この種の方向切換弁としては例えば第2
図に示すようなものがある。第2図で重量物Wは
シリンダー44で押上げられる。チエツク弁42
は外方から制御可能で、電磁ソレノイドにより駆
動されるスプール切換弁をもつ電磁方向切換弁4
1により制御される。圧力源P′からの圧油とタン
クT′の戻り油は電磁4方向切換弁43により制
御される。すなわち電磁4方向切換弁43が励磁
されると圧油は圧力源P′からチエツク弁42を通
りシリンダー44に流入し、重量物Wを押上げ
る。消磁されるとチエツク弁42の逆止力によつ
て重量物Wは現状に保持される。次に電磁方向切
換弁41が励磁されるとチエツク弁42はパイロ
ツト圧油により開き、シリンダー44の戻り油は
タンクT′に戻り重量物Wは自重で下がる。消磁
されるとチエツク弁42はチエツク状態に戻る。
このようにして重量物Wを上下に制御できる。
Conventionally, as this type of directional control valve, for example, the second
There is something like the one shown in the figure. In FIG. 2, a heavy object W is pushed up by a cylinder 44. Check valve 42
is an electromagnetic directional control valve 4 which can be controlled from the outside and has a spool control valve driven by an electromagnetic solenoid.
1. The pressure oil from the pressure source P' and the return oil from the tank T' are controlled by an electromagnetic four-way switching valve 43. That is, when the electromagnetic four-way switching valve 43 is energized, pressure oil flows from the pressure source P' into the cylinder 44 through the check valve 42 and pushes up the heavy object W. Once demagnetized, the heavy load W is held in its current state by the non-return force of the check valve 42. Next, when the electromagnetic directional control valve 41 is energized, the check valve 42 is opened by the pilot pressure oil, and the return oil from the cylinder 44 returns to the tank T' and the heavy object W is lowered by its own weight. When demagnetized, the check valve 42 returns to the checked state.
In this way, the heavy object W can be controlled up and down.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

しかしながら、このような従来のチエツク弁4
2と電磁方向切換弁41からなるパイロツトチエ
ツク機能付方向切換弁にあつては、電磁方向切換
弁がスプール型の切換弁を使用し、別置きのパイ
ロツトチエツク弁とが配管で接続されている。従
つて電磁方向切換弁41からの動作信号であるパ
イロツト圧油の流入によつてパイロツトチエツク
が作動するまでに時間がかかり、更にパイロツト
室の容積も大きく、動作信号のパイロツト圧油の
上昇に遅れがある。またスプール型の切換弁はス
プールのランド部にラツプしろを必要とするため
に応答遅れを生ずる。これらが原因となり応答速
度が遅いという欠点があつた。更にチエツク弁4
2と電磁方向切換弁41を例えば縦150mm、横100
mm、奥行60mm程度の小容積に収容され、しかも低
コストでかつ超小型のパイロツト機能付方向切換
弁の要望が極めて多く、従来の機能別に独立した
構造をもつ油圧機器の組合せでは到底満足されな
いものであつた。
However, such a conventional check valve 4
In the case of a directional control valve with a pilot check function consisting of a directional control valve 2 and an electromagnetic directional control valve 41, the electromagnetic directional control valve uses a spool type control valve, and is connected to a separate pilot check valve by piping. Therefore, it takes time for the pilot check to operate due to the inflow of the pilot pressure oil, which is the operation signal from the electromagnetic directional control valve 41, and the volume of the pilot chamber is also large, so there is a delay in the rise of the pilot pressure oil, which is the operation signal. There is. In addition, the spool-type switching valve requires a wrapping margin on the land portion of the spool, which causes a delay in response. Due to these factors, the response speed was slow. Furthermore, check valve 4
2 and the electromagnetic directional control valve 41, for example, 150 mm in length and 100 mm in width.
There is an extremely high demand for a low-cost, ultra-compact directional control valve with a pilot function that can be housed in a small volume of approximately 60 mm and depth, and cannot be satisfied by conventional combinations of hydraulic equipment with independent structures for each function. It was hot.

〔発明の目的〕[Purpose of the invention]

そこで本発明は電磁方向切換弁とパイロツトチ
エツク弁を形成する各機能部材として、スプール
をポペツトに変更し、配管は極力例えば50mm立方
程度の小形のブロツク内の油路で行うようにし、
ポペツトやパイロツト用のピストンやチエツク弁
の中心軸をいずれも上記ブロツクの内孔の中心軸
線上に一致するようにし、全ての部材を上記ブロ
ツクの内孔に集積して収容できるように小型化す
ることによつてパイロツトチエツク機能付方向切
換弁の超小型化と応答速度の高速化を行うことを
目的とする。
Therefore, in the present invention, the spools are changed to poppets as the functional members forming the electromagnetic directional control valve and the pilot check valve, and the piping is done as much as possible in the oil passage in a small block of, for example, about 50 mm cubic.
The center axes of the poppet, pilot piston, and check valve are all aligned with the center axis of the inner hole of the block, and the size is reduced so that all the members can be integrated and accommodated in the inner hole of the block. The purpose of this invention is to miniaturize a directional valve with a pilot check function and increase its response speed.

〔問題点を解決するための手段〕[Means for solving problems]

このような目的を達成するために、本発明は、
ブロツク15に、その表面には開口する圧力源用
Pポート、タンク用Tポート、接続用Aポートお
よびBポートを備えるとともに側面の中心部に円
筒状の内孔31を設け、電磁方向切換弁の電磁ソ
レノイド1と、シート10および環状のガイド1
1内の液室中に保持された球状のチエツク弁12
と、上記ソレノイド1とチエツク弁12との間に
該チエツク弁12を開閉駆動するスリーブ7の内
孔の液室に摺動自在に内蔵されたピストン9と、
該ピストン9の油室へ連通されている油路8を上
記電磁ソレノイド1の電磁駆動によりスリーブ3
の内孔を摺動させてPポートまたはTポートに切
換接続させる線接触形バランスドポペツト2と、
上記ガイド11、スリーブ7,3、シート10お
よびガイド11とを、各中心軸……が上記内孔3
1の中心軸線上に一致するように上記内孔31に
集積し一体に収納してなるパイロツトチエツク機
能付方向切換弁とした。そのために、全ての部材
の作動が同一ブロツク内で機能するのでその応答
時間を従来より1/3程度に短縮することができる。
In order to achieve such an objective, the present invention
The block 15 has a P port for a pressure source, a T port for a tank, and an A port and a B port for connection, which are open on the surface thereof, and a cylindrical inner hole 31 in the center of the side surface, and a cylindrical inner hole 31 is provided in the center of the side surface. Electromagnetic solenoid 1, seat 10 and annular guide 1
A spherical check valve 12 held in a liquid chamber within 1.
and a piston 9 slidably housed in a liquid chamber in the inner hole of the sleeve 7 that opens and closes the check valve 12 between the solenoid 1 and the check valve 12;
The oil passage 8 communicating with the oil chamber of the piston 9 is connected to the sleeve 3 by the electromagnetic drive of the electromagnetic solenoid 1.
a line contact type balanced poppet 2 that slides through the inner hole of the line contact type balanced poppet 2 to be connected to the P port or the T port;
The guide 11, the sleeves 7, 3, the seat 10, and the guide 11 are arranged so that each center axis is connected to the inner hole 3.
A directional control valve with a pilot check function is integrated and housed integrally in the inner hole 31 so as to coincide with the central axis of the valve. Therefore, since all the members operate within the same block, the response time can be reduced to about 1/3 of that of the conventional system.

〔実施例〕〔Example〕

本発明の実施例について図面を参照して詳細に
説明する。
Embodiments of the present invention will be described in detail with reference to the drawings.

第1図は本発明に係るパイロツト機能付方向切
換弁を使用して、重量物を押上げるシリンダーを
制御する一実施例を示す。
FIG. 1 shows an embodiment in which a directional control valve with a pilot function according to the present invention is used to control a cylinder that lifts up a heavy object.

第1図において、ブロツク15の表面に開口す
るポートP,T,AおよびBならびにその中心部
に円筒状の内孔31を備え、その内孔31に電磁
ソレノイド1、スリーブ3、スペーサ6、スリー
ブ7、シート10、ガイド11およびプラグ16
が順次相互に側面を接し集積収容され、 (a) 電磁ソレノイド1はその支接部を前記内孔3
1の一方端にねじ込んで固着され、 (b) スリーブ3は円周上に環状溝をもち、該環状
溝からスリーブ内孔に通ずる油路34をもち、 (c) ポペツト2は該スリーブ内孔で保持されて電
磁ソレノイド1により駆動され、またスペーサ
6に接するスリーブ3の側面のエツジ17に対
してスプリング4押圧により線接触し、ポート
Pへ油路5を介して通ずる油路34を閉じるバ
ランス型形状の凹部をもち、 (d) スペーサ6は内部に貫通孔をもち、該貫通孔
がスリーブ7に設けられる油路8および13に
開口し、また電磁ソレノイド1の作動によりポ
ペツト2がスプリング4を圧縮してスペーサ7
の端面に密着すると、油路34に開くとともに
油路13から閉ざされ、 (e) スリーブ7はスペーサ6に接する端面にスプ
リング4を保持し、シート10に接する他の端
面に開口して油路8に通ずる液室をもつ内孔を
備え、該内孔にピストン9を収容し、円周上の
2個所に環状溝をもち、これら各環状溝からピ
ストン9の駆動軸部にあたる該内孔の部分およ
び油路13にそれぞれ通ずる油路14および油
路35をもち、 (f) ピストン9はシート10に進行しチエツク弁
12のパイロツト駆動を行い、シート10の穴
の直径より大きいランド直径をもち、 (g) 2個のシート10は環状体のガイド11を介
して液室を形成し、該液室中に2個の球状のチ
エツク弁12を保持し、 (h) ガイド11は円周上に環状溝をもち、該環状
溝からチエツク弁12の位置する液室に通ずる
油路18をもち、 (i) プラグ16は前記内孔31の他端にねじ込ま
れ、プラグ16の突出部でシート10を押圧
し、 (j) ポペツト2、ピストン9およびチエツク弁1
2の中心軸は前記内孔31の中心軸上に一致す
るようにし、油路34とポートPを接続する油
路5、油路35とポートTを接続する油路3
6、油路18をポートAに接続する油路38お
よび油路14をポートBに接続する油路37を
いずれもブロツク15の中に設けるようにした
パイロツトチエツク機能付方向切換弁を有し、
かかるパイロツト機能付方向切換弁には、主流
路の圧油の流れ方を切換える電磁4方向切換弁
43をポートBに、圧力源P1およびタンクT1
をポートPとTに、シリンダー44をポートA
にそれぞれ接続するようにしたことが示されて
いる。
In FIG. 1, the block 15 has ports P, T, A, and B that open on the surface thereof, and a cylindrical inner hole 31 in the center thereof. 7, seat 10, guide 11 and plug 16
(a) The electromagnetic solenoid 1 has its support portion connected to the inner hole 3.
(b) The sleeve 3 has an annular groove on its circumference and an oil passage 34 leading from the annular groove to the inner hole of the sleeve, (c) The poppet 2 is attached to the inner hole of the sleeve. The balance is held by the electromagnetic solenoid 1 and is in line contact with the edge 17 of the side surface of the sleeve 3 in contact with the spacer 6 by the pressure of the spring 4, closing the oil passage 34 leading to the port P via the oil passage 5. (d) The spacer 6 has a through hole inside, which opens into oil passages 8 and 13 provided in the sleeve 7, and when the electromagnetic solenoid 1 is actuated, the poppet 2 is connected to the spring 4. compress and spacer 7
(e) The sleeve 7 holds the spring 4 on the end surface in contact with the spacer 6, and opens on the other end surface in contact with the sheet 10 to open the oil path. 8, the piston 9 is accommodated in the inner hole, and an annular groove is provided at two locations on the circumference. (f) The piston 9 advances to the seat 10 to pilot drive the check valve 12 and has a land diameter larger than the diameter of the hole in the seat 10. (g) The two sheets 10 form a liquid chamber through an annular guide 11, and two spherical check valves 12 are held in the liquid chamber, (h) The guide 11 is arranged on the circumference. (i) The plug 16 is screwed into the other end of the inner hole 31, and the protruding part of the plug 16 is inserted into the seat. (j) Poppet 2, piston 9 and check valve 1
The central axis of the inner hole 31 is made to coincide with the central axis of the inner hole 31, and the oil passage 5 connects the oil passage 34 and the port P, and the oil passage 3 connects the oil passage 35 and the port T.
6. It has a directional control valve with a pilot check function in which an oil passage 38 connecting the oil passage 18 to port A and an oil passage 37 connecting the oil passage 14 to port B are both provided in the block 15.
This directional control valve with a pilot function includes an electromagnetic four-way control valve 43 for switching the flow direction of pressure oil in the main flow path at port B, a pressure source P1 and a tank T1.
to ports P and T, cylinder 44 to port A
It is shown that they are connected to each other.

そして、電磁ソレノイド1については電磁ソレ
ノイドの支持部のみを示し、可動片に固着される
駆動軸と電磁コイルは図示しないが内孔31の一
方端を液密に閉じることは内孔31の他端に備え
るプラグ16においても同様である。
Regarding the electromagnetic solenoid 1, only the supporting part of the electromagnetic solenoid is shown, and the drive shaft and electromagnetic coil fixed to the movable piece are not shown. The same applies to the plug 16 prepared for use.

つぎに、本発明のパイロツト機能付方向切換弁
の作用について説明する。ポペツト2はポートP
から油路5と34を経て流入する圧油に対しては
バランス型形状の凹部で圧油による左右方向でへ
の圧力が平衡しているから静止している。図示の
状態は電磁ソレノイド1が消磁の状態で、スプリ
ング4のばね抗力により、ポペツト2は右方向に
押圧されてスリーブ3のエツジ17と線接触を行
い油路34を閉じている。油路8は油路13とス
ペーサ6の貫通孔で通じ、更に油路35と36お
よびポートTを介してタンタT1に通ずる。ピス
トン9は図示の位置へチエツク弁12の逆止圧力
により戻り、チエツク状態である。従つてポート
Aから油路38および18を介して液室に通ずる
シリンダー44の圧油は流出しないのでシリンダ
ー44は現在位置を保持する状態である。電磁ソ
レノイド1が励磁されると、ポペツト2はスリー
ブ7の端面にスプリング4を圧縮しながら密着し
てエツジ17を開くと共にこの密着により油路1
3を閉じる。ポートPからの圧油は油路5と34
を介してエツジ17の開いた通路から流入して、
油路8を通り、スリーブ7のスリーブ内孔の底部
にある液室に入り、ピストン9を左方向に押圧す
る。チエツク弁12とピストン9の圧力作用面積
には面積差が設けてあるので、ピストン9は左方
向へ移動し、ピストン9の駆動軸はシート10へ
進行してチエツク弁12を開く、シリンダー44
の圧油は重量物Wに押されてポートAと油路38
を通り更に油路14と37を介してペートBに至
り、電磁4方向切換弁43を通つてタンクT1
戻る。電磁ソレノイド1を消磁するとチエツク弁
12は最初のパイロツトチエツクの状態に戻る。
次に電磁4方向切換弁43を励磁すると、圧油は
ポートBから油路37と14を経てチエツク弁1
2を押し開いて液室に入り、更に油路18と38
を介してポートAからシリンダー44に流入し重
量物Wを押し上げる。消磁するとチエツク弁12
により現状態を保持する。
Next, the operation of the directional control valve with pilot function of the present invention will be explained. Poppet 2 is port P
With respect to the pressure oil flowing in through the oil passages 5 and 34, the pressure in the left and right direction due to the pressure oil is balanced in the balanced-shaped recess, so that it is stationary. In the illustrated state, the electromagnetic solenoid 1 is in a demagnetized state, and the poppet 2 is pushed rightward by the spring resistance of the spring 4 to make line contact with the edge 17 of the sleeve 3, thereby closing the oil passage 34. The oil passage 8 communicates with the oil passage 13 through the through hole of the spacer 6, and further communicates with the tank T1 via the oil passages 35 and 36 and the port T. The piston 9 returns to the illustrated position due to the check pressure of the check valve 12, and is in the check state. Therefore, the pressure oil in the cylinder 44 that communicates with the liquid chamber from the port A through the oil passages 38 and 18 does not flow out, so the cylinder 44 maintains its current position. When the electromagnetic solenoid 1 is energized, the poppet 2 comes into close contact with the end surface of the sleeve 7 while compressing the spring 4, opening the edge 17 and opening the oil passage 1 due to this close contact.
Close 3. Pressure oil from port P goes through oil lines 5 and 34.
Flowing in from the open passage of edge 17 through
It passes through the oil passage 8 and enters the liquid chamber at the bottom of the sleeve inner hole of the sleeve 7, and presses the piston 9 to the left. Since there is a difference between the pressure acting areas of the check valve 12 and the piston 9, the piston 9 moves to the left, and the drive shaft of the piston 9 advances to the seat 10 to open the check valve 12.
Pressure oil is pushed by the heavy object W to port A and oil passage 38.
It further reaches Pate B via oil passages 14 and 37, and returns to tank T1 through electromagnetic four-way switching valve 43. When the electromagnetic solenoid 1 is demagnetized, the check valve 12 returns to the initial pilot check state.
Next, when the electromagnetic four-way switching valve 43 is energized, the pressure oil flows from port B through oil passages 37 and 14 to check valve 1.
Push open 2 to enter the liquid chamber, and then open oil passages 18 and 38.
It flows into the cylinder 44 from the port A through the cylinder 44 and pushes up the heavy object W. When demagnetized, check valve 12
The current state is maintained by

〔発明の効果〕〔Effect of the invention〕

本発明のようなパイロツトチエツク弁とこのパ
イロツトチエツク弁を制御する電磁方向切換弁を
超小型の一つのブロツク内に集積したパイロツト
機能付方向切換弁とすることにより、パイロツト
圧油の油路の著しい短縮パイロツト圧油の液室容
積の縮少ならびにスプール弁をポペツト弁に変更
したこと等により応答時間を従来の約1/3に短縮
するとともに、パイロツト機能付方向切換弁のス
ペースを需要者の要望にかなう程度に縮小するこ
とが可能になり、従つて各部材の加工ならびに組
立作業に要する時間は短縮され、コスト低減を行
なうことができた。
By making the pilot check valve and the electromagnetic directional control valve that controls the pilot check valve into a pilot function directional control valve integrated into one ultra-compact block, it is possible to improve the pilot pressure oil passage. By reducing the volume of the pilot pressure oil chamber and changing the spool valve to a poppet valve, the response time has been shortened to approximately 1/3 of that of the conventional model, and the space for the directional control valve with pilot function has been reduced to meet customer requests. Therefore, the time required for processing and assembling each member was shortened, and costs could be reduced.

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

第1図は本発明のパイロツト機能付方向切換弁
の一実施例を示す説明図、第2図は従来装置を示
す油圧回路図である。 1…電磁ソレノイド、2…ポペツト、3,7…
スリーブ、4…スプリング、6…スペーサ、9…
ピストン、10…シート、11…ガイド、12…
チエツク弁、15…ブロツク、16…プラグ、1
7…エツジ、5,8,13,14,18,34,
35,36,37,38…油路、31…内孔、4
1…電磁方向切換弁、42…チエツク弁、43…
電磁4方向切換弁、44…シリンダー。
FIG. 1 is an explanatory view showing one embodiment of a directional control valve with a pilot function according to the present invention, and FIG. 2 is a hydraulic circuit diagram showing a conventional device. 1...Electromagnetic solenoid, 2...Poppet, 3,7...
Sleeve, 4...Spring, 6...Spacer, 9...
Piston, 10... Seat, 11... Guide, 12...
Check valve, 15...Block, 16...Plug, 1
7... Edge, 5, 8, 13, 14, 18, 34,
35, 36, 37, 38...Oil passage, 31...Inner hole, 4
1... Solenoid directional control valve, 42... Check valve, 43...
Solenoid 4-way switching valve, 44...cylinder.

Claims (1)

【特許請求の範囲】 1 ブロツク15に、その表面には開口する圧力
源用Pポート、タンク用Tポート、接続用Aポー
トおよびBポートを備えるとともに中心部に円筒
状の内孔31を設け、電磁方向切換弁の電磁ソレ
ノイド1と、 シート10および環状のガイド11内の液室中
に保持された球状のチエツク弁12と、 上記ソレノイド1とチエツク弁12との間に該
チエツク弁12を開閉駆動するスリーブ7の内孔
の液室に摺動自在に内蔵されたピストン9と、 該ピストン9の油室へ連通されている油路8を
上記電磁ソレノイド1の電磁駆動によりスリーブ
3の内孔を摺動させてPポートまたはTポートに
切換接続させる線接触形バランスドポペツト2
と、 上記ガイド11、スリーブ7ならびに3、シー
ト10およびガイド11とを、各中心軸が上記内
孔31の中心軸上に一致するように上記内孔31
に集積し一体に収納したことを特徴とするパイロ
ツトチエツク機能付方向切換弁。
[Claims] 1. The block 15 is provided with a pressure source P port, a tank T port, a connection A port and a B port that are open on its surface, and a cylindrical inner hole 31 in the center, An electromagnetic solenoid 1 of an electromagnetic directional control valve, a spherical check valve 12 held in a liquid chamber in a seat 10 and an annular guide 11, and an opening/closing mechanism for opening and closing the check valve 12 between the solenoid 1 and the check valve 12. A piston 9 is slidably built into a liquid chamber in the inner hole of the sleeve 7 to be driven, and an oil passage 8 communicating with the oil chamber of the piston 9 is connected to the inner hole of the sleeve 3 by electromagnetic driving of the electromagnetic solenoid 1. Line contact type balanced poppet 2 that can be switched and connected to P port or T port by sliding.
and the guide 11, the sleeves 7 and 3, the seat 10, and the guide 11 in the inner hole 31 so that their center axes coincide with the center axis of the inner hole 31.
A directional control valve with a pilot check function, which is integrated and housed in one piece.
JP3704785A 1985-02-26 1985-02-26 Directional changeover valve with pilot check function Granted JPS61197803A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3704785A JPS61197803A (en) 1985-02-26 1985-02-26 Directional changeover valve with pilot check function

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3704785A JPS61197803A (en) 1985-02-26 1985-02-26 Directional changeover valve with pilot check function

Publications (2)

Publication Number Publication Date
JPS61197803A JPS61197803A (en) 1986-09-02
JPH0320603B2 true JPH0320603B2 (en) 1991-03-19

Family

ID=12486672

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3704785A Granted JPS61197803A (en) 1985-02-26 1985-02-26 Directional changeover valve with pilot check function

Country Status (1)

Country Link
JP (1) JPS61197803A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61211580A (en) * 1985-03-15 1986-09-19 Tokyo Keiki Co Ltd Direction change-over valve with triple pilot checking function

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5712170A (en) * 1980-06-23 1982-01-22 Nissan Motor Co Ltd Check valve

Also Published As

Publication number Publication date
JPS61197803A (en) 1986-09-02

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