JPH0429884B2 - - Google Patents

Info

Publication number
JPH0429884B2
JPH0429884B2 JP59145242A JP14524284A JPH0429884B2 JP H0429884 B2 JPH0429884 B2 JP H0429884B2 JP 59145242 A JP59145242 A JP 59145242A JP 14524284 A JP14524284 A JP 14524284A JP H0429884 B2 JPH0429884 B2 JP H0429884B2
Authority
JP
Japan
Prior art keywords
pilot
directional control
oil
control valve
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
JP59145242A
Other languages
Japanese (ja)
Other versions
JPS6124886A (en
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 filed Critical
Priority to JP14524284A priority Critical patent/JPS6124886A/en
Publication of JPS6124886A publication Critical patent/JPS6124886A/en
Publication of JPH0429884B2 publication Critical patent/JPH0429884B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00Details of servomotor systems ; Valves for servomotor systems
    • F15B13/02Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
    • F15B13/04Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor
    • F15B13/042Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by fluid pressure
    • F15B13/0422Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by fluid pressure with manually-operated pilot valves, e.g. joysticks

Landscapes

  • Engineering & Computer Science (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid-Driven Valves (AREA)
  • Multiple-Way Valves (AREA)

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は油圧シヨベル等の建設機械に備えられ
るパイロツト操作回路の暖気装置に係り、特に方
向制御弁を駆動するパイロツト管路の暖気を良好
におこなうことができる暖気装置に関する。
[Detailed Description of the Invention] [Field of Industrial Application] The present invention relates to a heating device for a pilot operating circuit provided in a construction machine such as a hydraulic excavator, and in particular to a heating device for a pilot operating circuit that drives a directional control valve. Regarding a warming device that can be used.

〔従来の技術〕 第2図は従来のパイロツト操作回路の概略構成
の一例を示す回路図である。
[Prior Art] FIG. 2 is a circuit diagram showing an example of a schematic configuration of a conventional pilot operating circuit.

この第2図において、1は図示しない作業機を
駆動するアクチユエータ、2はこのアクチユエー
タ1の駆動を制御するパイロツト操作式方向制御
弁、3はこの方向制御弁2に連絡され、アクチユ
エータ1を駆動する圧油を供給する油圧ポンプで
ある。4は油圧ポンプ3の圧油を方向制御弁2に
導く吐出側回路、5はアクチユエータ1からの戻
り油を導くリターン回路で、このリターン回路5
はタンク6に連絡されている。7はリターン回路
5中に介設され、油圧ポンプ3から吐出された圧
油をろ過し、清浄化するリターンフイルタであ
る。なお、上記した方向制御弁2は移動自在なス
プール8と、このスプール8の両端に配置された
パイロツト油室9,9′と、これらのパイロツト
油室9,9′内に配置され、スプール8の端部を
付勢するスプリング10,10′とを有するとと
もに、本体2aにリターン回路5に連通する通路
11を有している。
In this FIG. 2, 1 is an actuator that drives a working machine (not shown), 2 is a pilot-operated directional control valve that controls the drive of this actuator 1, and 3 is connected to this directional control valve 2 to drive the actuator 1. This is a hydraulic pump that supplies pressure oil. 4 is a discharge side circuit that guides the pressure oil of the hydraulic pump 3 to the direction control valve 2; 5 is a return circuit that guides return oil from the actuator 1;
is being communicated to tank 6. A return filter 7 is interposed in the return circuit 5 and filters and cleans the pressure oil discharged from the hydraulic pump 3. The above-mentioned directional control valve 2 includes a movable spool 8, pilot oil chambers 9, 9' arranged at both ends of this spool 8, and arranged within these pilot oil chambers 9, 9'. It has springs 10, 10' that bias the ends of the main body 2a, and a passage 11 communicating with the return circuit 5 in the main body 2a.

12,12′は方向制御弁2を駆動するパイロ
ツト弁を構成する減圧弁、13はこれらの減圧弁
12,12′を駆動する操作レバー、14は減圧
弁12と方向制御弁2の一方のパイロツト油室9
とを連絡するパイロツト管路、14′は減圧弁1
2′と他方のパイロツト油室9′とを連絡するパイ
ロツト管路、15は減圧弁12,12′にパイロ
ツト圧を供給するパイロツトポンプ、16は減圧
弁12,12′に圧油を供給する管路、17は減
圧弁12,12′からタンク6に圧油を戻す管路、
18はパイロツトポンプ15から吐出される圧油
をろ過し、清浄化するパイロツトフイルタ、19
は減圧弁12,12′に供給する圧油の圧力を設
定するパイロツトリリーフ弁である。
Reference numerals 12 and 12' denote pressure reducing valves constituting a pilot valve for driving the directional control valve 2, 13 an operating lever for driving these pressure reducing valves 12 and 12', and 14 a pilot for one of the pressure reducing valve 12 and the directional control valve 2. Oil chamber 9
The pilot pipe 14' connects the pressure reducing valve 1.
2' and the other pilot oil chamber 9', 15 is a pilot pump that supplies pilot pressure to the pressure reducing valves 12, 12', and 16 is a pipe that supplies pressure oil to the pressure reducing valves 12, 12'. 17 is a pipe line for returning pressure oil from the pressure reducing valves 12, 12' to the tank 6;
18 is a pilot filter that filters and cleans the pressure oil discharged from the pilot pump 15; 19;
is a pilot relief valve that sets the pressure of pressure oil supplied to the pressure reducing valves 12, 12'.

このパイロツト操作回路にあつては、例えば第
2図に示す状態から操作レバー13を左方向に傾
けると、減圧弁12が作動し、パイロツトポンプ
15の圧油がパイロツトフイルタ18、管路1
6、減圧弁12、パイロツト管路14を介して方
向制御弁2の図示左側に位置するパイロツト油室
9に導かれ、これによつてスプール8がスプリン
グ10′の力に抗して右方に移動し、パイロツト
油室9の圧油とスプリング10の力とがつり合つ
た時点でスプール8が静止する。そして、油圧ポ
ンプ3の圧油が吐出側回路4、方向制御弁2を介
してアクチユエータ1に導かれ、またアクチユエ
ータ1からの戻り油は方向制御弁2の通路11、
リターン回路5、リターンフイルタ7を介してタ
ンク6に導かれ、これによつてアスチユエータ1
が駆動し、このアクチユエータ1に対応する図示
しない作業機の駆動をおこなうことができる。な
お、操作レバー13を同第2図の右方向に傾けた
場合には、ほぼ同様の作用によつてアクチユエー
タ1を上記とは逆の方向に駆動することができ
る。
In this pilot operating circuit, for example, when the operating lever 13 is tilted to the left from the state shown in FIG.
6. The oil is guided through the pressure reducing valve 12 and the pilot line 14 to the pilot oil chamber 9 located on the left side of the directional control valve 2 in the figure, thereby causing the spool 8 to move to the right against the force of the spring 10'. When the pressure oil in the pilot oil chamber 9 and the force of the spring 10 are balanced, the spool 8 comes to rest. The pressure oil of the hydraulic pump 3 is guided to the actuator 1 via the discharge side circuit 4 and the directional control valve 2, and the return oil from the actuator 1 is guided to the passage 11 of the directional control valve 2.
It is led to the tank 6 via the return circuit 5 and the return filter 7, and thereby the astuteator 1
is driven, and a working machine (not shown) corresponding to this actuator 1 can be driven. Incidentally, when the operating lever 13 is tilted to the right in FIG. 2, the actuator 1 can be driven in the opposite direction to that described above by substantially the same action.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

ところで、このように構成される従来のパイロ
ツト操作回路にあつては次に述べるような不具合
がある。
However, the conventional pilot operating circuit configured as described above has the following drawbacks.

すなわち、寒冷時には、パイロツト管路14,
14′及び方向制御弁2のパイロツト油室9,
9′等を含むパイロツト回路の油も冷却されて粘
度が高くなり、したがつて操作レバー13を操作
してもスプール8が操作レバー13の操作量に対
応した量移動するまでに時間がかかつて応答遅れ
を生じ、操作性が著しく劣化する。しかも、パイ
ロツト油室9,9′に流入した油は当該パイロツ
ト油室9,9′から外部に流出することがないの
で、操作レバー13を操作してもこれらのパイロ
ツト回路においてはスプール8の移動量に相応す
る油量しか流動せず、したがつてこのパイロツト
回路の油温がなかなか上昇せず、応答遅れを解消
させるために長い時間を要している。
That is, in cold weather, the pilot pipe 14,
14' and the pilot oil chamber 9 of the directional control valve 2,
The oil in the pilot circuit, including parts 9', etc., is also cooled and becomes more viscous, so even if the operating lever 13 is operated, it takes time for the spool 8 to move by an amount corresponding to the amount of operation of the operating lever 13. This causes a response delay and significantly deteriorates operability. Moreover, the oil that has flowed into the pilot oil chambers 9, 9' does not flow out from the pilot oil chambers 9, 9', so even if the operating lever 13 is operated, the spool 8 will not move in these pilot circuits. Only a corresponding amount of oil flows, and therefore the oil temperature in this pilot circuit does not rise easily, and it takes a long time to eliminate the response delay.

本発明はこのような従来技術における実情に鑑
みてなされたもので、その目的は、パイロツト回
路を流れる油量を多くすることができ、寒冷時に
生じる応答遅れを短時間のうちに解消できるパイ
ロツト操作回路の暖気装置を提供することにあ
る。
The present invention was made in view of the actual situation in the prior art, and its purpose is to improve the pilot operation by increasing the amount of oil flowing through the pilot circuit and quickly eliminating response delays that occur in cold weather. The purpose is to provide circuit heating equipment.

〔課題を解決するための手段〕[Means to solve the problem]

この目的を達成するために本発明は、油圧ポン
プと、この油圧ポンプから吐出する油圧によつて
駆動するアクチユエータと、このアクチユエータ
の駆動を制御するパイロツト操作式方向制御弁
と、該方向制御弁のパイロツト油室に連絡され、
該方向制御弁のスプールを作動させる減圧弁と、
この減圧弁と上記パイロツト油室とを連絡するパ
イロツト管路とを有し、上記減圧弁を、上記パイ
ロツト油室に連絡される二次側ポートとタンクに
連絡されるタンクポートとが中立時に連通するよ
うに形成してあるパイロツト操作回路に備えら
れ、上記方向制御弁に形成されたリターン回路に
連通する通路と上記パイロツト油室とを連絡する
連絡路と、この連絡路に介設され、上記パイロツ
ト油室から上記通路への油の流入を阻止する逆止
弁とを設けた構成にしてある。
To achieve this object, the present invention includes a hydraulic pump, an actuator driven by the hydraulic pressure discharged from the hydraulic pump, a pilot-operated directional control valve for controlling the drive of the actuator, and a pilot-operated directional control valve for controlling the directional control valve. The pilot oil room was contacted.
a pressure reducing valve that operates a spool of the directional control valve;
It has a pilot pipe line that connects the pressure reducing valve with the pilot oil chamber, and communicates the pressure reducing valve with a secondary side port that communicates with the pilot oil chamber and a tank port that communicates with the tank when in neutral. a communication path which is provided in the pilot operating circuit and which connects the pilot oil chamber with a passage which communicates with the return circuit formed in the directional control valve; A check valve is provided to prevent oil from flowing into the passage from the pilot oil chamber.

〔作用〕[Effect]

本発明は、上記の構成にしてあることから、減
圧弁の中立時には、油圧ポンプを駆動することに
より、油圧ポンプから吐出される油圧が方向制御
弁内に形成される通路、連絡路、及び逆止弁を介
してパイロツト管路に導かれ、このパイロツト管
路を流れる油量が多くなり、これによりパイロツ
ト管路の油温を上昇させることができ、寒冷時等
であつてもこのパイロツト操作回路を流れる圧油
の粘度を低くすることができる。
Since the present invention has the above-mentioned configuration, when the pressure reducing valve is in the neutral state, by driving the hydraulic pump, the hydraulic pressure discharged from the hydraulic pump is transferred to the passage, the communication passage, and the reverse passage formed in the direction control valve. The amount of oil that flows through the pilot line through the stop valve increases, which increases the oil temperature in the pilot line, and even in cold weather, this pilot operation circuit remains stable. The viscosity of the pressure oil flowing through can be lowered.

〔実施例〕〔Example〕

以下、本発明のパイロツト操作回路の暖気装置
を図に基づいて説明する。
DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, a warm-up device for a pilot operating circuit according to the present invention will be explained based on the drawings.

第1図は本発明の一実施例の概略構成を示す回
路図である。なおこの図において、前述した第1
図に示すものと同じものは同一符号で示してあ
る。
FIG. 1 is a circuit diagram showing a schematic configuration of an embodiment of the present invention. Note that in this figure, the first
Components that are the same as those shown in the figures are designated by the same reference numerals.

この図において、20はスプール8の図示左端
に形成した連絡路で、リターン回路5に連絡する
通路11に連絡されるとともに、図示左端のパイ
ロツト油室9に連絡可能になつている。21はこ
の連絡路20に介設され、パイロツト油室9から
通路11への油の流入を阻止する逆止弁、22は
この逆止弁21を付勢するスプリングである。な
お図示を省略したが、これらの連絡路20、逆止
弁21、スプリング22と同等のものをスプール
8の右端側にも設けてある。その他の構成は例え
ば第2図に示すものと同等である。
In this figure, reference numeral 20 denotes a communication path formed at the left end of the spool 8 in the drawing, which is connected to the passage 11 that communicates with the return circuit 5, and can also communicate with the pilot oil chamber 9 at the left end in the drawing. Reference numeral 21 designates a check valve that is interposed in this communication passage 20 and prevents oil from flowing into the passage 11 from the pilot oil chamber 9, and 22 represents a spring that biases the check valve 21. Although not shown in the drawings, the communication passage 20, check valve 21, and spring 22 are also provided on the right end side of the spool 8. The other configurations are equivalent to those shown in FIG. 2, for example.

この実施例にあつては、例えば第1図に示す状
態から操作レバー13を左方向に傾けると、従来
と同様に、パイロツト管路14を介してパイロツ
ト圧が方向制御弁2のパイロツト油室9に導か
れ、これによつてスプール8が図示右方に移動
し、油圧ポンプ3の圧油がこの方向制御弁2を介
してアクチユエータ1に導かれ、このアクチユエ
ータ1からの戻り油は方向制御弁2の通路11、
リターン回路5を経てタンク6に戻され、当該ア
クチユエータ1が作動する。また、操作レバー1
3を右方向に傾けると同様の作用によりアクチユ
エータ1が上記の作動方向とは逆方向に作動す
る。
In this embodiment, for example, when the operating lever 13 is tilted to the left from the state shown in FIG. As a result, the spool 8 moves to the right in the figure, and the pressure oil from the hydraulic pump 3 is guided to the actuator 1 via the directional control valve 2, and the return oil from the actuator 1 is returned to the directional control valve. 2 passage 11,
It is returned to the tank 6 via the return circuit 5, and the actuator 1 is activated. In addition, operation lever 1
When the actuator 3 is tilted to the right, the actuator 1 operates in the opposite direction to the above-mentioned operating direction due to a similar effect.

また、操作レバー13の中立時には、パイロツ
ト管路14,14′は、減圧弁12,12′の二次
側ポートとタンクポートを介してタンク6に連絡
されており、油の流れもないので、このパイロツ
ト管路14,14′の圧力はタンク圧に保持され
る。一方、方向制御弁2の通路11の圧力は、油
圧ポンプ3の戻り油がリターン回路5、リターン
フイルタ7等を介してタンク6に至るので、これ
らのリターン回路5、リターンフイルタ7等の圧
力損失分だけタンク圧よりも高くなつている。し
たがつて、スプリング22等の設定圧力を上述の
圧力損失分よりも若干低い圧力に設定しておけ
ば、方向制御弁2の通路11の油が連絡路20等
を介して逆止弁21部分あるいはスプール8の右
端に設けられる図示しない逆止弁部分に導かれ、
これらの逆止弁21、あるいは図示しない逆止弁
がスプリング22等の力に抗して作動し、当該油
がパイロツト油室9,9′、及びパイロツト管路
14,14′、減圧弁12,12′、管路17を経
てタンク6に導かれる。
Furthermore, when the operating lever 13 is in the neutral position, the pilot lines 14, 14' are connected to the tank 6 via the secondary ports of the pressure reducing valves 12, 12' and the tank port, and there is no oil flow. The pressure in the pilot lines 14, 14' is maintained at tank pressure. On the other hand, the pressure in the passage 11 of the directional control valve 2 is determined by the pressure loss of the return circuit 5, return filter 7, etc., since the return oil of the hydraulic pump 3 reaches the tank 6 via the return circuit 5, return filter 7, etc. The pressure is higher than the tank pressure by that amount. Therefore, if the set pressure of the spring 22, etc. is set to a pressure slightly lower than the above-mentioned pressure loss, the oil in the passage 11 of the directional control valve 2 will flow through the communication passage 20, etc. to the check valve 21 portion. Or it is guided to a check valve part (not shown) provided at the right end of the spool 8,
These check valves 21 or a check valve (not shown) operate against the force of the spring 22, etc., and the oil flows into the pilot oil chambers 9, 9', the pilot pipes 14, 14', the pressure reducing valve 12, 12' and is led to the tank 6 via a conduit 17.

このように構成した一実施例にあつては、上記
したように操作レバー13を中立状態にしておい
て油圧ポンプ3を駆動することにより、この油圧
ポンプ3の圧油が方向制御弁2の通路11、連絡
路20を介してパイロツト管路14,14′の双
方に流れるので、これらのパイロツト管路14,
14′等を流れる油量が多くなり、当該パイロツ
ト管路14,14′等の油温が上昇し、したがつ
て仮に寒冷時にあつてもこのパイロツト回路を流
れる圧油の粘度を容易に低くすることができ、パ
イロツト管路14,14′内の圧油の円滑な流れ
を実現でき、方向制御弁2に対する応答遅れを短
時間のうちに解消できる。
In one embodiment configured in this manner, as described above, by driving the hydraulic pump 3 with the operation lever 13 in the neutral state, the pressure oil of the hydraulic pump 3 flows into the passage of the directional control valve 2. 11. Since it flows to both the pilot pipes 14 and 14' via the communication line 20, these pilot pipes 14,
The amount of oil flowing through the pilot circuits 14, 14', etc. increases, and the oil temperature in the pilot pipes 14, 14', etc. increases, so that even in cold weather, the viscosity of the pressure oil flowing through the pilot circuits can be easily lowered. This makes it possible to realize a smooth flow of pressure oil in the pilot pipes 14, 14', and to eliminate the delay in response to the directional control valve 2 in a short time.

なお、上記実施例では、方向制御弁2のスプー
ル8の両端部に逆止弁21等、スプリング22等
を設けたが、本発明はこれに限られず、例えば第
1図に示すスプール8の左端側の逆止弁21とス
プリング22、及びスプール8の右端側の図示し
ない逆止弁とスプリングを除き、連絡路20を通
路11に対して直接には連絡不能となるように形
成し、すなわちパイロツト油室9にのみ連絡され
るように形成するとともに、方向制御弁2の本体
2aに、上記の通路11に連通し、しかも上述の
連絡路20に連通可能な分岐流路を形成し、この
分岐流路に通路11側への圧油の流入を阻止する
逆止弁と、この逆止弁を付勢するスプリングとを
設け、同様の組合せをスプール8の右端側に設け
る構成とすることもできる。このように構成して
も上記の実施例と同じ作用効果を奏する。
In the above embodiment, the check valve 21, etc., the spring 22, etc. are provided at both ends of the spool 8 of the directional control valve 2, but the present invention is not limited to this. For example, the left end of the spool 8 shown in FIG. Except for the check valve 21 and spring 22 on the side, and the check valve and spring (not shown) on the right end side of the spool 8, the communication passage 20 is formed so that it cannot communicate directly with the passage 11. The main body 2a of the directional control valve 2 is formed to communicate only with the oil chamber 9, and a branch flow path is formed in the main body 2a of the directional control valve 2, which communicates with the above-mentioned passage 11 and which can communicate with the above-mentioned communication passage 20. It is also possible to provide a check valve that prevents pressure oil from flowing into the passage 11 side in the flow path and a spring that biases the check valve, and to provide a similar combination on the right end side of the spool 8. . Even with this configuration, the same effects as in the above embodiment can be achieved.

〔発明の効果〕〔Effect of the invention〕

本発明のパイロツト操作回路の暖気装置は以上
のように構成してあることから、パイロツト回路
を流れる油量を従来に比べて多くすることがで
き、またパイロツト回路を流れる圧油の粘度を容
易に低くすることができることから、応答遅れを
短時間のうちに解消でき、操作性が向上する効果
がある。
Since the warm-up device for the pilot operating circuit of the present invention is constructed as described above, the amount of oil flowing through the pilot circuit can be increased compared to the conventional system, and the viscosity of the pressure oil flowing through the pilot circuit can be easily adjusted. Since the response time can be lowered, response delays can be eliminated within a short period of time, which has the effect of improving operability.

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

第1図は本発明のパイロツト操作回路の暖気装
置の一実施例の概略構成を示す回路図、第2図は
従来のパイロツト操作回路の概略構成の一例を示
す回路図である。 1……アクチユエータ、2……パイロツト操作
式方向制御弁、2a……本体、3……油圧ポン
プ、5……リターン回路、6……タンク、7……
リターンフイルタ、8…スプール、9,9′……
パイロツト油室、10,10′……スプリング、
11……通路、12,12′……減圧弁、13…
…操作レバー、14,14′……パイロツト管路、
15……パイロツトポンプ、16,17……管
路、18……パイロツトフイルタ、20……連絡
路、21……逆止弁、22……スプリング。
FIG. 1 is a circuit diagram showing a schematic configuration of an embodiment of a warm-up device for a pilot operating circuit according to the present invention, and FIG. 2 is a circuit diagram showing an example of a schematic configuration of a conventional pilot operating circuit. DESCRIPTION OF SYMBOLS 1... Actuator, 2... Pilot operated directional control valve, 2a... Body, 3... Hydraulic pump, 5... Return circuit, 6... Tank, 7...
Return filter, 8...spool, 9,9'...
Pilot oil chamber, 10, 10'...spring,
11... Passage, 12, 12'... Pressure reducing valve, 13...
...Operation lever, 14, 14'...Pilot conduit,
15...Pilot pump, 16, 17...Pipeline, 18...Pilot filter, 20...Connection path, 21...Check valve, 22...Spring.

Claims (1)

【特許請求の範囲】[Claims] 1 油圧ポンプと、この油圧ポンプから吐出する
油圧によつて駆動するアクチユエータと、このア
クチユエータの駆動を制御するパイロツト操作式
方向制御弁と、該方向制御弁のパイロツト油室に
連絡され、該方向制御弁のスプールを作動させる
減圧弁と、この減圧弁と上記パイロツト油室とを
連絡するパイロツト管路とを有し、上記減圧弁
を、上記パイロツト油室に連絡される二次側ポー
トとタンクに連絡されるタンクポートとが中立時
に連通するように形成してあるパイロツト操作回
路に備えられ、上記方向制御弁に形成されたリタ
ーン回路に連通する通路と上記パイロツト油室と
を連絡する連絡路と、この連絡路に介設され、上
記パイロツト油室から上記通路への油の流入を阻
止する逆止弁とを設けたことを特徴とするパイロ
ツト操作回路の暖気装置。
1 A hydraulic pump, an actuator driven by hydraulic pressure discharged from the hydraulic pump, a pilot-operated directional control valve that controls the drive of the actuator, and a pilot-operated directional control valve that is connected to the pilot oil chamber of the directional control valve and that controls the directional control. It has a pressure reducing valve that operates a spool of the valve, and a pilot pipe line that communicates the pressure reducing valve with the pilot oil chamber, and connects the pressure reducing valve to a secondary port connected to the pilot oil chamber and a tank. A communication path is provided in a pilot operation circuit formed to communicate with a tank port to be communicated when in neutral, and communicates a passage communicating with a return circuit formed in the directional control valve and the pilot oil chamber. A heating device for a pilot operating circuit, characterized in that a check valve is provided in the communication passage to prevent oil from flowing into the passage from the pilot oil chamber.
JP14524284A 1984-07-14 1984-07-14 Warmup device for pilot operating circuit Granted JPS6124886A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14524284A JPS6124886A (en) 1984-07-14 1984-07-14 Warmup device for pilot operating circuit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14524284A JPS6124886A (en) 1984-07-14 1984-07-14 Warmup device for pilot operating circuit

Publications (2)

Publication Number Publication Date
JPS6124886A JPS6124886A (en) 1986-02-03
JPH0429884B2 true JPH0429884B2 (en) 1992-05-20

Family

ID=15380606

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14524284A Granted JPS6124886A (en) 1984-07-14 1984-07-14 Warmup device for pilot operating circuit

Country Status (1)

Country Link
JP (1) JPS6124886A (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1988002071A1 (en) * 1986-09-09 1988-03-24 Hitachi Construction Machinary Co., Ltd Valve device
JPH0198983U (en) * 1987-12-24 1989-07-03
JPH04105274U (en) * 1991-02-15 1992-09-10 矢崎総業株式会社 Shutoff valve drive system
JPH0784023A (en) * 1993-06-30 1995-03-31 Shigemi:Kk Sample tube for nuclear magnetic resonance apparatus
JP6012806B1 (en) * 2015-04-15 2016-10-25 Kyb株式会社 Valve device and fluid pressure control device
CN105650047B (en) * 2016-02-26 2017-11-10 常熟华威履带有限公司 A kind of hydraulicdirectional control valve device and the engineering machinery for carrying the device

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6119110B2 (en) * 1981-04-06 1986-05-15 Nippon Denshin Denwa Kk

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6119110U (en) * 1984-07-09 1986-02-04 株式会社神戸製鋼所 Hydraulic operating circuit

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6119110B2 (en) * 1981-04-06 1986-05-15 Nippon Denshin Denwa Kk

Also Published As

Publication number Publication date
JPS6124886A (en) 1986-02-03

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