JPH0257170B2 - - Google Patents

Info

Publication number
JPH0257170B2
JPH0257170B2 JP2367581A JP2367581A JPH0257170B2 JP H0257170 B2 JPH0257170 B2 JP H0257170B2 JP 2367581 A JP2367581 A JP 2367581A JP 2367581 A JP2367581 A JP 2367581A JP H0257170 B2 JPH0257170 B2 JP H0257170B2
Authority
JP
Japan
Prior art keywords
circuit
valve
hydraulic
pressure
pilot
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
JP2367581A
Other languages
Japanese (ja)
Other versions
JPS57140442A (en
Inventor
Takeshi Yamaguchi
Sotaro Tanaka
Takashi Yagyu
Yasuo Sakaki
Eiki Izumi
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.)
Hitachi Construction Machinery Co Ltd
Original Assignee
Hitachi Construction Machinery 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 Hitachi Construction Machinery Co Ltd filed Critical Hitachi Construction Machinery Co Ltd
Priority to JP2367581A priority Critical patent/JPS57140442A/en
Publication of JPS57140442A publication Critical patent/JPS57140442A/en
Publication of JPH0257170B2 publication Critical patent/JPH0257170B2/ja
Granted legal-status Critical Current

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E02HYDRAULIC ENGINEERING; FOUNDATIONS; SOIL SHIFTING
    • E02FDREDGING; SOIL-SHIFTING
    • E02F9/00Component parts of dredgers or soil-shifting machines, not restricted to one of the kinds covered by groups E02F3/00 - E02F7/00
    • E02F9/20Drives; Control devices
    • E02F9/22Hydraulic or pneumatic drives
    • E02F9/2278Hydraulic circuits
    • E02F9/2296Systems with a variable displacement pump
    • EFIXED CONSTRUCTIONS
    • E02HYDRAULIC ENGINEERING; FOUNDATIONS; SOIL SHIFTING
    • E02FDREDGING; SOIL-SHIFTING
    • E02F9/00Component parts of dredgers or soil-shifting machines, not restricted to one of the kinds covered by groups E02F3/00 - E02F7/00
    • E02F9/20Drives; Control devices
    • E02F9/22Hydraulic or pneumatic drives

Landscapes

  • Engineering & Computer Science (AREA)
  • Mining & Mineral Resources (AREA)
  • Civil Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structural Engineering (AREA)
  • Operation Control Of Excavators (AREA)

Description

【発明の詳細な説明】 本発明は、複数の原動機のそれぞれによつて駆
動される複数の油圧ポンプと、単数又は複数のア
クチユエータとが油圧閉回路で接続された油圧シ
ヨベル、油圧クレーンなどの土木・建設機械の油
圧回路に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention is applicable to civil engineering applications such as hydraulic excavators and hydraulic cranes in which a plurality of hydraulic pumps driven by a plurality of prime movers and one or more actuators are connected in a hydraulic closed circuit.・Related to hydraulic circuits of construction machinery.

大型の油圧シヨベルなどでは、二つのエンジン
によつて二つの旋回ポンプを駆動し、これら二つ
の旋回ポンプから一つ以上の旋回モータに油圧を
供給することが行なわれているが、旋回ポンプと
旋回モータとが形成する油圧回路が開回路である
と、旋回ブレーキ時のエネルギを回収できない。
このため、油圧回路を閉回路にして、旋回ブレー
キ時のエネルギを回収することが、従来既に知ら
れている。第1図は一般的な油圧シヨベルの構造
を示す。1は上部旋回体、2は下部走行体、3は
旋回輪、4はブーム、5はアーム、6はバケツ
ト、7はブームシリンダ、8はアームシリンダ、
9はバケツトシリンダである。第2図は旋回輪3
を駆動する旋回モータ10の油圧回路が閉回路に
なつている従来の油圧シヨベルの油圧回路を示
す。二つのエンジン11a,11bは歯車等から
成るポンプ駆動装置12a,12bを介して主ポ
ンプ13a,13b、14a,14b、パィロツ
トポンプ15a,15b及び両傾転の旋回ポンプ
16a,16bを回転駆動する。主ポンプ13
a,13bはチエツク弁17a,17bを経て開
回路により切換弁グループ19aに接続され、主
ポンプ14a,14bはチエツク弁18a,18
bを経て開回路により切換弁グループ19bに接
続される。切換弁グループ19a,19bは圧油
の入口及びタンクへの出口を共通にした複数の方
向切換弁19a1〜19a3,19b1〜19b2がそれ
ぞれ連設されたもので、方向切換弁19a1にはア
ームシリンダ8が、方向切換弁19a2にはバケツ
トシリンダ9が、方向切換弁19a3には左走行モ
ータ20aが、方向切換弁19b1にはブームシリ
ンダ7が、方向切換弁19b2には右走行モータ2
0bが、それぞれ接続される。各方向切換弁19
a1〜19a3及び19b1〜19b3はパイロツト圧信
号によつて圧油の方向を切り換え、また流量制御
を行なうものであるが、第2図ではこれらのパイ
ロツト圧信号回路は省略されている。旋回ポンプ
16a,16bは斜板などの吐出容量可変機構2
1a,21b及びこれらを制御するレギユレータ
22a,22bを備える。レギユレータ22a,
22bは、パイロツトポンプ15a,15bから
サーボ圧が供給されると共に、パイロツト弁23
からパイロツト圧信号が与えられる。パイロツト
弁23は操作レバー24を有する。
In large hydraulic excavators, two engines drive two swing pumps, and these two swing pumps supply hydraulic pressure to one or more swing motors. If the hydraulic circuit formed by the motor is an open circuit, energy during swing braking cannot be recovered.
For this reason, it is already known to make the hydraulic circuit a closed circuit to recover energy during swing braking. Figure 1 shows the structure of a typical hydraulic excavator. 1 is an upper rotating body, 2 is a lower traveling body, 3 is a rotating wheel, 4 is a boom, 5 is an arm, 6 is a bucket, 7 is a boom cylinder, 8 is an arm cylinder,
9 is a bucket cylinder. Figure 2 shows the turning wheel 3.
The hydraulic circuit of a conventional hydraulic shovel is shown in which the hydraulic circuit of the swing motor 10 that drives the swing motor 10 is a closed circuit. The two engines 11a, 11b rotationally drive main pumps 13a, 13b, 14a, 14b, pilot pumps 15a, 15b, and double-swivel swing pumps 16a, 16b via pump drive devices 12a, 12b consisting of gears and the like. Main pump 13
a, 13b are connected to the switching valve group 19a by an open circuit via check valves 17a, 17b, and the main pumps 14a, 14b are connected to the switching valve group 19a via check valves 17a, 17b.
b via an open circuit to the switching valve group 19b. The switching valve groups 19a and 19b are each a plurality of directional switching valves 19a 1 to 19a 3 and 19b 1 to 19b 2 connected in series, each having a common inlet for pressure oil and an outlet to a tank . The arm cylinder 8 is attached to the directional selector valve 19a2 , the left travel motor 20a is attached to the directional selector valve 19a3 , the boom cylinder 7 is attached to the directional selector valve 19b1 , and the bucket cylinder 9 is attached to the directional selector valve 19b2. right travel motor 2
0b are connected to each other. Each direction switching valve 19
a 1 to 19a 3 and 19b 1 to 19b 3 are used to switch the direction of the pressure oil and control the flow rate according to the pilot pressure signal, but these pilot pressure signal circuits are omitted in Fig. 2. . The rotating pumps 16a and 16b are equipped with a variable discharge capacity mechanism 2 such as a swash plate.
1a, 21b and regulators 22a, 22b for controlling them. regulator 22a,
22b is supplied with servo pressure from the pilot pumps 15a and 15b, and the pilot valve 23
A pilot pressure signal is given from The pilot valve 23 has an operating lever 24.

第2図においては、旋回モータ10の油圧回路
が閉回路になつているので、旋回ブレーキ時に旋
回モータ10から旋回ポンプ16a,16bに油
が戻り、旋回ポンプ16a,16bをモータとし
て駆動して、エンジン11a,11bの回転を助
け、これによつてエネルギが回収される。ところ
が、一方のエンジン11aを停止して、他方のエ
ンジン11bのみを運転する場合、あるいは一方
のエンジン11aが過負荷により停止した場合な
どには、閉回路であるために、旋回ポンプ16b
からの圧油が停止している旋回ポンプ16aに供
給されて、旋回ポンプ16aがモータ作用を行な
い、エンジン11aが回される。これによつてエ
ンジン11aが損傷するおそれがあり、また、エ
ンジン11aが予期せぬ時に始動してしまい、危
険である。
In FIG. 2, since the hydraulic circuit of the swing motor 10 is a closed circuit, oil returns from the swing motor 10 to the swing pumps 16a, 16b during swing braking, and the swing pumps 16a, 16b are driven as motors. It helps the engines 11a, 11b to rotate, thereby recovering energy. However, when one engine 11a is stopped and only the other engine 11b is operated, or when one engine 11a is stopped due to overload, the rotation pump 16b is closed because of the closed circuit.
The pressurized oil is supplied to the rotating pump 16a, which is stopped, and the rotating pump 16a performs a motor action to rotate the engine 11a. This may cause damage to the engine 11a, and the engine 11a may start unexpectedly, which is dangerous.

本発明の目的は、上述した問題点を解決し、正
常回転状態にない原動機がそれに連結された油圧
ポンプのモータ作用により回転されるのを防ぐこ
とができる土木・建設機械の油圧回路を提供する
ことである。
An object of the present invention is to provide a hydraulic circuit for civil engineering and construction machinery that solves the above-mentioned problems and can prevent a prime mover that is not in a normal rotation state from being rotated by the motor action of a hydraulic pump connected to it. That's true.

この目的を達成するために、本発明は、各レギ
ユレータのサーボ圧回路とパイロツト圧信号回路
の少なくともいずれか一方に、該回路の圧を閉止
により零にする開閉弁をそれぞれ設け、各原動機
が正常回転状態にないことを検出することによつ
て、検出対象の原動機の側に設けられた開閉弁を
閉止させる検出制御手段を備えたことを特徴とす
る。
In order to achieve this object, the present invention provides at least one of the servo pressure circuit and the pilot pressure signal circuit of each regulator with an on-off valve that closes the pressure in the circuit to zero, thereby ensuring that each prime mover is operating normally. The present invention is characterized in that it includes a detection control means that closes an on-off valve provided on the side of the prime mover to be detected by detecting that it is not in a rotating state.

以下、本発明を図示の実施例に基ずいて詳細に
説明する。
Hereinafter, the present invention will be explained in detail based on illustrated embodiments.

第3図は本発明の一実施例を示す。第2図と同
様の部分は同一符号にて示す。パイロツト弁23
からレギユレータ22a,22bに接続されてい
るパイロツト圧信号回路25a,25bの途中
に、閉止により該回路の圧を零にする開閉弁26
a,26bがそれぞれ設けられる。
FIG. 3 shows an embodiment of the invention. Components similar to those in FIG. 2 are designated by the same reference numerals. Pilot valve 23
In the middle of the pilot pressure signal circuits 25a, 25b connected to the regulators 22a, 22b, there is provided an on-off valve 26 which makes the pressure in the circuit zero by closing.
a and 26b are provided, respectively.

各エンジン11a,11bにはジエネレータ2
7a,27bが直結され、その出力は開閉弁26
a,26bのソレノイドを励磁して、開閉弁26
a,26bを開通させる。また、ジエネレータ2
7a,27bはダイオード28a,28bを経て
バツテリ29を充電する。ダイオード28a,2
8bはジエネレータ27a,27bの出力が他の
エンジンの側に設けられた開閉器26a,26b
のソレノイドを励磁するのを阻止するものであ
る。各レギユレータ22a,22bにはパイロツ
トポンプ15a,15bからサーボ圧回路30
a,30bによりサーボ圧が供給される。この実
施例においては、ジエネレータ27a,27bが
本発明の検出制御手段に相当する。
Each engine 11a, 11b has a generator 2.
7a and 27b are directly connected, and the output is from the on-off valve 26.
By energizing the solenoids a and 26b, the on-off valve 26
a and 26b are opened. Also, generator 2
7a and 27b charge a battery 29 via diodes 28a and 28b. Diode 28a, 2
8b is a switch 26a, 26b where the output of the generator 27a, 27b is provided on the other engine side.
This prevents the solenoid from being energized. Each regulator 22a, 22b is connected to a servo pressure circuit 30 from a pilot pump 15a, 15b.
Servo pressure is supplied by a and 30b. In this embodiment, the generators 27a and 27b correspond to the detection control means of the present invention.

エンジン11a,11bが正常に運転されてい
る間は、ジエネレータ27a,27bは開閉弁2
6a,26bのソレノイドを励磁するのに十分な
出力電流を出力するので、開閉弁26a,26b
は開通状態となる。したがつて、パイロツト弁2
3からパイロツト圧信号が出力されると、その大
きさに応じてレギユレータ22a,22bは吐出
容量可変機構21a,21bを変位させ、旋回ポ
ンプ16a,16bの吐出容量を変える。
While the engines 11a and 11b are operating normally, the generators 27a and 27b are operated by the on-off valve 2.
Since the output current is sufficient to excite the solenoids 6a and 26b, the on-off valves 26a and 26b
becomes open. Therefore, pilot valve 2
When a pilot pressure signal is output from the pump 3, the regulators 22a, 22b displace the variable displacement mechanisms 21a, 21b in accordance with the magnitude of the pilot pressure signal, thereby changing the displacement of the rotary pumps 16a, 16b.

例えば、一方のエンジン11aが正常回転状態
ではなくなり、停止状態又は逆転状態になつた場
合には、ジエネレータ27aの出力電流は零又は
零に近い所定値以下となるので、開閉弁26aの
ソレノイドは励磁されなくなり、開閉弁26aは
閉止状態となる。これによつてレギユレータ22
aはパイロツト弁23からしや断され、その両端
に与えられるパイロツト圧信号は零となる。した
がつて、レギユレータ22aは吐出容量零を示す
中立位置に保持され、旋回ポンプ16aは旋回ポ
ンプ16bからの圧油を受けてもモータ作用を行
なうことはない。
For example, when one engine 11a is no longer in a normal rotation state and enters a stopped or reversed state, the output current of the generator 27a becomes zero or less than a predetermined value close to zero, so the solenoid of the on-off valve 26a is energized. The opening/closing valve 26a is closed. This allows the regulator 22
A is now disconnected from the pilot valve 23, and the pilot pressure signal applied to both ends thereof becomes zero. Therefore, the regulator 22a is held at a neutral position indicating zero discharge capacity, and the swing pump 16a does not operate as a motor even if it receives pressure oil from the swing pump 16b.

第4図は本発明の他の実施例を示す。この実施
例ではジエネレータ27a,27bの代りに、エ
ンジンオイル圧力スイツチ31a,31b及びバ
ツテリ29が用いられる。これらが本発明の検出
制御手段に相当する。
FIG. 4 shows another embodiment of the invention. In this embodiment, engine oil pressure switches 31a, 31b and a battery 29 are used in place of the generators 27a, 27b. These correspond to the detection control means of the present invention.

二つのエンジン11a,11bが正常回転状態
にある場合には、エンジンオイル圧力の上昇によ
りエンジンオイル圧力スイツチ31a,31bは
ともにオンとなり、バツテリ29から開閉弁26
a,26bのソレノイドに通電され、開閉弁26
a,26bはともに開通状態となる。したがつ
て、二つの旋回ポンプ16a,16bはパイロツ
ト圧信号に応じて圧油を吐出する。
When the two engines 11a and 11b are in normal rotation, the engine oil pressure switches 31a and 31b are both turned on due to the increase in engine oil pressure, and the on-off valve 26 is turned on from the battery 29.
The solenoids a and 26b are energized, and the on-off valve 26
Both a and 26b are in an open state. Therefore, the two swing pumps 16a, 16b discharge pressure oil in response to the pilot pressure signal.

例えば、一方のエンジン11aが正常回転状態
でなくなると、エンジンオイル圧力が低下し、エ
ンジンオイル圧力スイツチ31aはオフとなり、
開閉弁26aは閉止状態となる。これによつて、
レギユレータ22aは吐出容量零を示す中立位置
に保持され、旋回ポンプ16aのモータ作用を防
ぐ。
For example, when one engine 11a is no longer in a normal rotation state, the engine oil pressure decreases and the engine oil pressure switch 31a is turned off.
The on-off valve 26a is in a closed state. By this,
The regulator 22a is held in a neutral position indicating zero displacement, thereby preventing the motor action of the swing pump 16a.

第5図は本発明の別の実施例を示す。この実施
例では、検出制御手段として、エンジンオイル圧
力が用いられ、エンジン11a,11bに設けら
れたエンジンオイル圧力取出口32a,32bが
開閉弁33a,33bの作動圧入力ポートに接続
される。
FIG. 5 shows another embodiment of the invention. In this embodiment, engine oil pressure is used as the detection control means, and engine oil pressure outlets 32a and 32b provided in engines 11a and 11b are connected to operating pressure input ports of on-off valves 33a and 33b.

二つのエンジン11a,11bが正常回転状態
にある場合には、エンジンオイル圧力が上昇する
ので、この圧力が開閉弁33a,33bに作動圧
として与えられることにより、開閉弁33a,3
3bは開通状態となり、二つの旋回ポンプ16
a,16bはパイロツト圧信号に応じて圧油を吐
出する。
When the two engines 11a and 11b are in a normal rotation state, the engine oil pressure increases, so this pressure is applied to the on-off valves 33a and 33b as operating pressure, so that the on-off valves 33a and 3
3b is in the open state, and the two rotating pumps 16
a and 16b discharge pressure oil in response to a pilot pressure signal.

例えば、一方のエンジン11aが正常回転状態
でなくなると、そのエンジンオイル圧力が開閉弁
33aの作動設定圧力より小さい値に低下するの
で、開閉弁33aは閉止状態に復帰する。したが
つて、レギユレータ22aは吐出容量零を示す中
立位置に保持され、旋回ポンプ16aのモータ作
用を防ぐ。
For example, when one engine 11a is no longer in a normal rotation state, the engine oil pressure drops to a value lower than the operating setting pressure of the on-off valve 33a, so the on-off valve 33a returns to the closed state. Therefore, the regulator 22a is held in a neutral position indicating zero displacement, thereby preventing the motor action of the swing pump 16a.

本発明は第3〜5図に示されるパイロツト圧信
号カツト方式のものに限定されるものではなく、
サーボ圧カツト方式のものをも含む。即ち、サー
ボ圧回路30a,30bの途中に、開閉弁26
a,26b,33a,33bをそれぞれ設け、エ
ンジン11a,11bが正常回転状態にないこと
が検出された時に開閉弁26a,26b,33
a,33bを閉止させて、レギユレータ22a,
22bに与えられるサーボ圧を零にするものをも
本発明は含む。
The present invention is not limited to the pilot pressure signal cut method shown in FIGS.
Including those using servo pressure cut method. That is, the on-off valve 26 is installed in the middle of the servo pressure circuits 30a and 30b.
a, 26b, 33a, 33b are respectively provided, and when it is detected that the engines 11a, 11b are not in a normal rotation state, the on/off valves 26a, 26b, 33
a, 33b are closed, and the regulators 22a, 33b are closed.
The present invention also includes a method that makes the servo pressure applied to 22b zero.

本発明は旋回ポンプの閉回路のみに適用が限定
されるものではなく、個別の原動機によつて駆動
される複数の油圧ポンプと単数又は複数のアクチ
ユエータとが閉回路を形成する油圧回路であれば
適用することができる。また二つの原動機のもの
に限らず、三つ以上の原動機のものにも適用する
ことができる。更に、パイロツト圧信号カツト方
式とサーボ圧カツト方式の両方を同時に用いるこ
ともできる。
The present invention is not limited to application to closed circuits of swing pumps, but can be applied to any hydraulic circuit in which a plurality of hydraulic pumps driven by individual prime movers and one or more actuators form a closed circuit. Can be applied. Furthermore, the present invention is not limited to two prime movers, but can also be applied to three or more prime movers. Furthermore, both the pilot pressure signal cut method and the servo pressure cut method can be used simultaneously.

以上説明したように、本発明によれば、複数の
油圧ポンプの各レギユレータのサーボ圧回路とパ
イロツト圧信号回路の少なくともいずれか一方
に、該回路の圧を閉止により零にする開閉弁をそ
れぞれ設け、原動機が正常回転状態にないことを
検出することによつて検出制御手段により開閉弁
を閉止するようにしたから、正常回転状態にない
原動機に連結された油圧ポンプのモータ作用を防
ぐことができる。したがつて、正常回転状態にな
い原動機に回転力が作用することを防止すること
ができ、それによる危性をなくすことができる。
As explained above, according to the present invention, at least one of the servo pressure circuit and the pilot pressure signal circuit of each regulator of a plurality of hydraulic pumps is provided with an on-off valve that closes the pressure of the circuit to zero. Since the opening/closing valve is closed by the detection control means by detecting that the prime mover is not in a normal rotation condition, it is possible to prevent the motor action of the hydraulic pump connected to the prime mover that is not in a normal rotation condition. . Therefore, it is possible to prevent rotational force from acting on the prime mover that is not in a normal rotation state, and the danger caused by this can be eliminated.

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

第1図は一般的な油圧シヨベルの側面図、第2
図は従来の閉回路を備えた油圧シヨベルの油圧回
路図、第3図は本発明の一実施例の回路図、第4
図は本発明の他の実施例の回路図、第5図は本発
明の別の油圧回路図である。 10……旋回モータ、11a,11b……エン
ジン、15a,15b……パイロツトポンプ、1
6a,16b……旋回ポンプ、21a,21b…
…吐出容量可変機構、22a,22b……レギユ
レータ、23……パイロツト弁、25a,25b
……パイロツト圧信号回路、26a,26b……
開閉弁、27a,27b……ジエネレータ、29
……バツテリ、30a,30b……サーボ圧回
路、31a,31b……エンジンオイル圧力スイ
ツチ、32a,32b……エンジンオイル圧力取
出口、33a,33b……開閉弁。
Figure 1 is a side view of a typical hydraulic excavator, Figure 2
The figure is a hydraulic circuit diagram of a hydraulic excavator equipped with a conventional closed circuit, FIG. 3 is a circuit diagram of an embodiment of the present invention, and FIG.
The figure is a circuit diagram of another embodiment of the present invention, and FIG. 5 is another hydraulic circuit diagram of the present invention. 10...Swivel motor, 11a, 11b...Engine, 15a, 15b...Pilot pump, 1
6a, 16b...Swivel pump, 21a, 21b...
...Variable discharge capacity mechanism, 22a, 22b...Regulator, 23...Pilot valve, 25a, 25b
...Pilot pressure signal circuit, 26a, 26b...
Opening/closing valve, 27a, 27b...generator, 29
...Battery, 30a, 30b...Servo pressure circuit, 31a, 31b...Engine oil pressure switch, 32a, 32b...Engine oil pressure outlet, 33a, 33b...Opening/closing valve.

Claims (1)

【特許請求の範囲】[Claims] 1 個別の原動機によつて駆動され、アクチユエ
ータに対して並列接続された複数の油圧ポンプ
と、該油圧ポンプに閉回路で接続されたアクチユ
エータと、サーボ圧回路によりサーボ圧を、パイ
ロツト圧信号回路によりパイロツト圧信号を、そ
れぞれ与えられて、各油圧ポンプの吐出容量可変
機構をそれぞれ制御する複数のレギユレータとを
備えた土木・建設機械の油圧回路において、各レ
ギユレータのサーボ圧回路とパイロツト圧信号回
路の少なくともいずれか一方に、該回路の圧を閉
止により零にする開閉弁をそれぞれ設け、各原動
機が正常回転状態にないことを検出することによ
つて、検出対象の原動機の側に設けられた開閉弁
を閉止させる検出制御手段を備えたことを特徴と
する土木・建設機械の油圧回路。
1 A plurality of hydraulic pumps driven by individual prime movers and connected in parallel to an actuator, an actuator connected to the hydraulic pumps in a closed circuit, servo pressure by a servo pressure circuit, and servo pressure by a pilot pressure signal circuit. In a hydraulic circuit for a civil engineering/construction machine equipped with a plurality of regulators each receiving a pilot pressure signal and controlling the variable discharge displacement mechanism of each hydraulic pump, a servo pressure circuit of each regulator and a pilot pressure signal circuit are provided. At least one of them is provided with an on-off valve that closes the pressure in the circuit to zero, and by detecting that each prime mover is not in a normal rotation state, the on-off valve provided on the side of the prime mover to be detected is A hydraulic circuit for civil engineering and construction machinery, characterized by comprising a detection control means for closing a valve.
JP2367581A 1981-02-21 1981-02-21 Oil-pressure circuit for civil and construction machinery Granted JPS57140442A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2367581A JPS57140442A (en) 1981-02-21 1981-02-21 Oil-pressure circuit for civil and construction machinery

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2367581A JPS57140442A (en) 1981-02-21 1981-02-21 Oil-pressure circuit for civil and construction machinery

Publications (2)

Publication Number Publication Date
JPS57140442A JPS57140442A (en) 1982-08-31
JPH0257170B2 true JPH0257170B2 (en) 1990-12-04

Family

ID=12117052

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2367581A Granted JPS57140442A (en) 1981-02-21 1981-02-21 Oil-pressure circuit for civil and construction machinery

Country Status (1)

Country Link
JP (1) JPS57140442A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03115070U (en) * 1990-03-06 1991-11-27

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03115070U (en) * 1990-03-06 1991-11-27

Also Published As

Publication number Publication date
JPS57140442A (en) 1982-08-31

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