JPS6349013B2 - - Google Patents
Info
- Publication number
- JPS6349013B2 JPS6349013B2 JP858181A JP858181A JPS6349013B2 JP S6349013 B2 JPS6349013 B2 JP S6349013B2 JP 858181 A JP858181 A JP 858181A JP 858181 A JP858181 A JP 858181A JP S6349013 B2 JPS6349013 B2 JP S6349013B2
- Authority
- JP
- Japan
- Prior art keywords
- pressure
- pilot
- circuit
- pump
- hydraulic
- 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
Links
- 230000007246 mechanism Effects 0.000 claims description 7
- 238000010276 construction Methods 0.000 claims description 4
- 238000000034 method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 230000007935 neutral effect Effects 0.000 description 2
- 238000001514 detection method Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B11/00—Servomotor systems without provision for follow-up action; Circuits therefor
- F15B11/16—Servomotor systems without provision for follow-up action; Circuits therefor with two or more servomotors
- F15B11/17—Servomotor systems without provision for follow-up action; Circuits therefor with two or more servomotors using two or more pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/20—Fluid pressure source, e.g. accumulator or variable axial piston pump
- F15B2211/205—Systems with pumps
- F15B2211/2053—Type of pump
- F15B2211/20538—Type of pump constant capacity
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/20—Fluid pressure source, e.g. accumulator or variable axial piston pump
- F15B2211/205—Systems with pumps
- F15B2211/2053—Type of pump
- F15B2211/20546—Type of pump variable capacity
- F15B2211/20553—Type of pump variable capacity with pilot circuit, e.g. for controlling a swash plate
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/20—Fluid pressure source, e.g. accumulator or variable axial piston pump
- F15B2211/205—Systems with pumps
- F15B2211/20576—Systems with pumps with multiple pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/60—Circuit components or control therefor
- F15B2211/635—Circuits providing pilot pressure to pilot pressure-controlled fluid circuit elements
- F15B2211/6355—Circuits providing pilot pressure to pilot pressure-controlled fluid circuit elements having valve means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/60—Circuit components or control therefor
- F15B2211/67—Methods for controlling pilot pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/70—Output members, e.g. hydraulic motors or cylinders or control therefor
- F15B2211/705—Output members, e.g. hydraulic motors or cylinders or control therefor characterised by the type of output members or actuators
- F15B2211/7058—Rotary output members
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/70—Output members, e.g. hydraulic motors or cylinders or control therefor
- F15B2211/71—Multiple output members, e.g. multiple hydraulic motors or cylinders
- F15B2211/7135—Combinations of output members of different types, e.g. single-acting cylinders with rotary motors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/70—Output members, e.g. hydraulic motors or cylinders or control therefor
- F15B2211/71—Multiple output members, e.g. multiple hydraulic motors or cylinders
- F15B2211/7142—Multiple output members, e.g. multiple hydraulic motors or cylinders the output members being arranged in multiple groups
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Operation Control Of Excavators (AREA)
- Fluid-Pressure Circuits (AREA)
Description
【発明の詳細な説明】
本発明は複数のエンジンによつて駆動される複
数の油圧ポンプと単数または複数のアクチユエー
タとが油圧閉回路を形成する油圧シヨベル、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 provides hydraulic power for civil engineering and construction machinery such as hydraulic excavators and hydraulic cranes in which a plurality of hydraulic pumps driven by a plurality of engines and one or more actuators form a hydraulic closed circuit. Regarding circuits.
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などを駆動し、これら
二つの旋回ポンプから一つ以上の旋回モータに圧
油を供給することが行われているが、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は、従来既に
知られている。第1回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、パイ
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1
3a,13bはチエツクバルブ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はチエツクバルブ1
8a,18b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,1
9bは、圧油の入口及び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
20bが、それぞれ接続される。各方向切換弁1
9a1〜19a3及び19b1〜19b2はパイロツト圧
信号によつて切り換えられ、流量制御を行うもの
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,16
bは旋回モータ10に閉回路により接続される。
旋回ポンプ16a,16bは斜板などの吐出量可
変機構21a,21b及び吐出量可変機構21
a,21bを制御するレギユレータ22a,22
b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、パイロツトバルブ23からパイ
ロツト圧信号が与えられる。パイロツトバルブ2
3は操作レバー24を有する。この種のレギユレ
ータは一般に油圧サーボ機構を有し、油圧サーボ
機構は、油圧ポンプの吐出量可変機構を作動させ
るサーボシリンダと、サーボシリンダへ供給され
る圧油の量及び方向を制御するサーボ弁とから成
つている。そして、サーボ圧とは、サーボ弁を介
してサーボシリンダへ供給される圧油を意味し、
パイロツト圧信号とは、サーボ弁のスプール移動
量を制御する油圧を意味する。 In large hydraulic excavators, two engines drive two swing pumps, and these two swing pumps supply pressure oil to one or more swing motors. If the hydraulic circuit formed by the swing motor and the swing motor is an open circuit, energy during swing braking cannot be recovered. For this reason, it is already known that the hydraulic circuit is made into a closed circuit to recover energy during swing braking. The first part shows the structure of a typical hydraulic excavator. 1 is an upper rotating body, 2 is a lower traveling body,
3 is a swing ring, 4 is a boom, 5 is an arm, 6 is a bucket, 7 is a boom cylinder, 8 is an arm cylinder, and 9 is a bucket cylinder. FIG. 2 shows a hydraulic circuit of a conventional hydraulic excavator in which the hydraulic circuit of the swing motor 10 that drives the swing wheel 3 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 1
3a, 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 check valve 1
8a and 18b, it is connected to the switching valve group 19b by an open circuit. Switching valve group 19a, 1
Reference numeral 9b denotes a plurality of directional switching valves 19a 1 to 19a 3 , 19b 1 to 19b 2 that share a common inlet and outlet for pressure oil, and are connected to each other, and the directional switching valve 19a 1 has an arm cylinder 8, The directional switching valve 19a 2 has a bucket cylinder 9, the directional switching valve 19a 3 has a left traveling motor 20a, the directional switching valve 19b 1 has a boom cylinder 7, and the directional switching valve 19b 2 has a right traveling motor 20b. , are connected respectively. Each direction switching valve 1
9a 1 to 19a 3 and 19b 1 to 19b 2 are switched by a pilot pressure signal to control the flow rate, but these pilot pressure signal circuits are omitted in FIG. Rotating pump 16a, 16
b is connected to the swing motor 10 through a closed circuit.
The rotating pumps 16a and 16b are equipped with variable discharge mechanisms 21a and 21b such as swash plates, and variable discharge mechanism 21.
regulators 22a and 22 that control a and 21b;
b. The regulators 22a, 22b are supplied with servo pressure from the pilot pumps 15a, 15b, and are also given a pilot pressure signal from the pilot valve 23. Pilot valve 2
3 has an operating lever 24. This type of regulator generally has a hydraulic servo mechanism, which includes a servo cylinder that operates a variable discharge amount mechanism of a hydraulic pump, and a servo valve that controls the amount and direction of pressure oil supplied to the servo cylinder. It consists of And, servo pressure means pressure oil supplied to the servo cylinder via the servo valve,
The pilot pressure signal means the oil pressure that controls the amount of spool movement of the servo valve.
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、出力を下げて用いるために、片方のエンジン
11bを止め、一つのエンジン11aのみを回わ
すことがあるが、この場合に、閉回路であるため
に、旋回ポンプ16aからの圧油が停止している
旋回ポンプ16bに供給されて、旋回ポンプ16
bはモータ作用を行い、エンジン11bが回わさ
れる。これによつてエンジン11bが損傷するお
それがあり、また、エンジン11bが予期せぬ時
にかかつてしまい、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, in order to reduce the output and use it, one of the engines 11b is sometimes stopped and only one engine 11a is turned, but in this case, since the circuit is closed, the pressure oil from the swing pump 16a stops. The rotating pump 16b is supplied to the rotating pump 16b.
b performs a motor action, and the engine 11b is rotated. This may cause damage to the engine 11b, and may cause the engine 11b to crash at an unexpected time, which is dangerous.
本発明の目的は、上述の問題点を解決し、個別
のエンジンによつて駆動される複数の油圧ポンプ
のうち、停止している油圧ポンプが作動している
油圧ポンプからの圧油によりモータ作用を行うの
を防ぐことができ、停止中のエンジンが回わるこ
とによる危険性をなくすことができる土木、建設
機械の油圧回路を提供することである。 It is an object of the present invention to solve the above-mentioned problems, so that among a plurality of hydraulic pumps driven by individual engines, a stopped hydraulic pump is activated by pressure oil from an operating hydraulic pump. To provide a hydraulic circuit for civil engineering and construction machinery that can prevent the engine from rotating during a stopped state and eliminate the danger caused by the rotation of a stopped engine.
この目的を達成するために、本発明は、一つの
閉回路内の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、同一エンジン側のパイロツト
ポンプの吐出圧がない時に前記サーボ圧回路或い
はパイロツト圧信号回路の圧を零にする開閉弁を
それぞれ設け、各パイロツトポンプの吐出側に、
他のパイロツトポンプからの圧油が流入するのを
防ぐバルブをそれぞれ設けたことを特徴とする。 In order to achieve this object, the present invention provides a method for transmitting the discharge pressure of the pilot pump on the same engine side to at least one of the servo pressure circuit and the pilot pressure signal circuit of each regulator of a plurality of hydraulic pumps in one closed circuit. An on-off valve is provided on the discharge side of each pilot pump to make the pressure in the servo pressure circuit or pilot pressure signal circuit zero when there is no pressure.
It is characterized in that each pilot pump is provided with a valve that prevents pressure oil from flowing in from other pilot pumps.
以下、本発明を図示の実施例にもとずいて詳細
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であるサーボ圧カツ
ト方式のものを示す。第2図と同様の部分は同一
符号にて示す。パイロツトポンプ15a,15b
からレギユレータ22a,22bにつながるサー
ボ圧回路25a,25bには開閉弁26a,26
bがそれぞれ設けられる。開閉弁26a,26b
の作動圧は同一エンジン側のパイロツトポンプ1
5a,15bからそれぞれとつている。開閉弁2
6a,26bは第3図に示される閉路状態ではサ
ーボ回路25a,25bをタンク27a,27b
に接続して、回路圧を零にする。 FIG. 3 shows a servo pressure cut method according to an embodiment of the present invention. Components similar to those in FIG. 2 are designated by the same reference numerals. Pilot pump 15a, 15b
On-off valves 26a, 26 are connected to the servo pressure circuits 25a, 25b connected to the regulators 22a, 22b.
b are provided respectively. Opening/closing valves 26a, 26b
The working pressure of pilot pump 1 on the same engine side is
5a and 15b, respectively. Open/close valve 2
6a, 26b connect the servo circuits 25a, 25b to the tanks 27a, 27b in the closed circuit state shown in FIG.
Connect to to bring the circuit pressure to zero.
パイロツトポンプ15a,15bの吐出側と共
通接続点Aとの間には、チエツクバルブ28a,
28bがそれぞれ設けられ、互いに他のパイロツ
トポンプからの圧油が流入するのを防いでいる。 A check valve 28a,
28b are provided respectively to prevent pressure oil from flowing into each other from other pilot pumps.
なお、旋回ポンプ16a,16bが本発明にお
ける個別のエンジンによつて駆動さる複数の油圧
ポンプに相当し、旋回モータ10が本発明のアク
チユエータに相当し、旋回ポンプ16a,16b
と旋回モータ10とは閉回路で接続されている。
また、開閉弁26a,26bが本発明の開閉弁
に、チエツクバルブ28a,28bが圧油流入防
止のためのバルブに、それぞれ相当する。 Note that the swing pumps 16a, 16b correspond to a plurality of hydraulic pumps driven by separate engines in the present invention, the swing motor 10 corresponds to an actuator in the present invention, and the swing pumps 16a, 16b correspond to a plurality of hydraulic pumps driven by separate engines in the present invention.
and the swing motor 10 are connected in a closed circuit.
Further, the on-off valves 26a and 26b correspond to on-off valves of the present invention, and the check valves 28a and 28b correspond to valves for preventing inflow of pressure oil, respectively.
今、エンジン11aが回転し、エンジン11b
が停止しているとすると、旋回ポンプ16a及び
パイロツトポンプ15aは駆動され、旋回ポンプ
16b及びパイロツトポンプ15bは停止してい
る。パイロツトポンプ15aの吐出圧はチエツク
バルブ28aを経てパイロツトバルブ23に作動
圧として供給されると共に、開閉弁26aに作動
圧として作用し、開閉弁26aはスプリングに抗
して開路状態に切り換わり、パイロツトポンプ1
5aの吐出圧がサーボ圧としてレギユレータ22
aに供給される。これによつて、パイロツトバル
ブ23の操作レバー24が操作されると、パイロ
ツト圧信号がレギユレータ22aに与えられ、旋
回ポンプ16aは油を吐出し、旋回モータ10が
回転する。 Now, engine 11a is rotating, engine 11b
If the pump 16a and the pilot pump 15a are stopped, the swing pump 16a and the pilot pump 15a are driven, and the swing pump 16b and the pilot pump 15b are stopped. The discharge pressure of the pilot pump 15a is supplied as operating pressure to the pilot valve 23 via the check valve 28a, and also acts as operating pressure on the on-off valve 26a, which resists the spring and switches to the open state. pump 1
The discharge pressure of 5a is used as servo pressure by the regulator 22.
supplied to a. As a result, when the operating lever 24 of the pilot valve 23 is operated, a pilot pressure signal is applied to the regulator 22a, the swing pump 16a discharges oil, and the swing motor 10 rotates.
パイロツトポンプ15bは吐出せず、また、パ
イロツトポンプ15aの吐出圧はチエツクバルブ
28bによりしや断されので、開閉弁26bは閉
路状態であり、サーボ圧回路25bはタンク27
bに接続されて、回路圧は零になる。即ち、レギ
ユレータ22bのサーボ圧は零になり、したがつ
て、レギユレータ22bにパイロツト圧信号が与
えられても、レギユレータ22bは作動せず、吐
出量可変機構21bは吐出量零を示す中立位置に
保持される。そのため、旋回ポンプ16bは旋回
ポンプ16aからの吐出圧を受けても回転しな
い。 The pilot pump 15b does not discharge, and the discharge pressure of the pilot pump 15a is cut off by the check valve 28b, so the on-off valve 26b is in a closed state, and the servo pressure circuit 25b is connected to the tank 27.
b, the circuit pressure becomes zero. That is, the servo pressure of the regulator 22b becomes zero, and therefore, even if a pilot pressure signal is applied to the regulator 22b, the regulator 22b does not operate, and the variable discharge amount mechanism 21b is held at a neutral position indicating a zero discharge amount. be done. Therefore, the orbiting pump 16b does not rotate even if it receives the discharge pressure from the orbiting pump 16a.
第4図は本発明の他の実施例であるパイロツト
圧信号カツト方式のものを示す。第3図と同様の
部分は同一符号にて示す。パイロツトバルブ23
の一方の出力ボートからレギユレータ22aを通
り、他方の出力ボートに戻るパイロツト圧信号回
路29aには、開閉弁30aが設けられ、同様に
パイロツト圧信号回路29bには開閉弁30bが
設けられる。開閉弁30a,30bの作動圧は同
一エンジン側のパイロツトポンプ15a,15b
からそれぞれとつている。開閉弁30a,30b
は本発明の開閉弁に相当するもので、第4図に示
される閉路状態ではパイロツト圧信号回路29
a,29bを短絡して、レギユレータ22a,2
2bの両端に与えられる回路圧を零にする。 FIG. 4 shows another embodiment of the present invention, which uses a pilot pressure signal cut method. Components similar to those in FIG. 3 are designated by the same reference numerals. Pilot valve 23
The pilot pressure signal circuit 29a which passes from one output boat through the regulator 22a and returns to the other output boat is provided with an on-off valve 30a, and similarly the pilot pressure signal circuit 29b is provided with an on-off valve 30b. The operating pressure of the on-off valves 30a, 30b is the same as that of the pilot pumps 15a, 15b on the same engine side.
They are taken from each. On-off valves 30a, 30b
corresponds to the on-off valve of the present invention, and in the closed state shown in FIG. 4, the pilot pressure signal circuit 29
a, 29b are short-circuited, and the regulators 22a, 2
The circuit pressure applied to both ends of 2b is made zero.
今、エンジン11aが回転し、エンジン11b
が停止しているとすると、パイロツトポンプ15
aの吐出圧により開閉弁30aが開路状態とな
り、パイロツトバルブ23のパイロツト圧信号は
パイロツト圧信号回路29aによりレギユレータ
22aに送られ、旋回ポンプ16aは油を吐出す
る。一方、パイロツトポンプ15bの吐出圧はな
いので、開閉弁30bは閉路状態となり、パイロ
ツト圧信号回路29bはしや断され、レギユレー
タ22bに与えられるパイロツト圧信号は零とな
る。これによつて、レギユレータ22bは吐出量
零を示す中立位置に保持され、旋回ポンプ16b
は旋回ポンプ16aからの圧油を受けても回転し
ない。 Now, engine 11a is rotating, engine 11b
is stopped, pilot pump 15
The opening/closing valve 30a is opened by the discharge pressure a, the pilot pressure signal of the pilot valve 23 is sent to the regulator 22a by the pilot pressure signal circuit 29a, and the orbiting pump 16a discharges oil. On the other hand, since there is no discharge pressure from the pilot pump 15b, the on-off valve 30b is closed, the pilot pressure signal circuit 29b is immediately cut off, and the pilot pressure signal given to the regulator 22b becomes zero. As a result, the regulator 22b is held at the neutral position where the discharge amount is zero, and the rotating pump 16b
does not rotate even if it receives pressure oil from the swing pump 16a.
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、個別のエンジンによつて駆
動される複数の油圧ポンプと一つ以上のアクチユ
エータとが形成する閉回路であれば適用すること
ができる。複数のアクチユエータを用いる場合に
は、油圧ポンプに対して複数のアクチユエータを
並列に接続する。また2エンジンのものには限ら
ず、3エンジン以上のものにも適用することがで
きる。 The present invention is not limited to the closed circuit of a swing pump, but can be applied to any closed circuit formed by a plurality of hydraulic pumps driven by individual engines and one or more actuators. Can be done. When using a plurality of actuators, the plurality of actuators are connected in parallel to the hydraulic pump. Further, the present invention is not limited to two engines, but can also be applied to three or more engines.
更に、サーボ圧カツト方式とパイロツト圧信号
カツト方式の両方を同時に用いることもできる。 Furthermore, both the servo pressure cut method and the pilot pressure signal cut method can be used simultaneously.
以上説明したように、本発明によれば、一つの
閉回路内の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、同一エンジン側のパイロツト
ポンプの吐出圧がない時に前記サーボ圧回路或い
はパイロツト圧信号回路の圧を零にする開閉弁を
それぞれ設け、各パイロツトポンプの吐出側に、
他のパイロツトポンプからの圧油が流入するのを
防ぐバルブをそれぞれ設けたから、個別のエンジ
ンによつて駆動される複数の油圧ポンプのうち、
停止している油圧ポンプが作動している油圧ポン
プからの圧油を受けてモータ作用を行うのを防ぐ
ことができ、停止中のエンジンが回わることによ
る危険性を防ぐことができる。更に、パイロツト
ポンプの吐出圧がないことによつてエンジンの停
止を検出するようにしたため、検出手段を別に設
ける必要がなく、流量の小さい、したがつて小形
の開閉弁及び圧油流入防止のためのバルブを設け
るのみで済むから、コストを低くすることができ
る。 As explained above, according to the present invention, the discharge pressure of the pilot pump on the same engine is connected to at least one of the servo pressure circuit and the pilot pressure signal circuit of each regulator of a plurality of hydraulic pumps in one closed circuit. An on-off valve is provided on the discharge side of each pilot pump to make the pressure in the servo pressure circuit or pilot pressure signal circuit zero when there is no pressure.
Since each pilot pump is equipped with a valve that prevents pressure oil from flowing in, one of the multiple hydraulic pumps driven by an individual engine can
It is possible to prevent a stopped hydraulic pump from receiving pressurized oil from an operating hydraulic pump to operate a motor, and to prevent a danger caused by a stopped engine rotating. Furthermore, since engine stoppage is detected based on the absence of discharge pressure from the pilot pump, there is no need to provide a separate detection means. Since only one valve is required, costs can be reduced.
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油圧回路図、
第4図は本発明の他の実施例の油圧回路図であ
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…
…吐出量可変機構、22a,22b……レギユレ
ータ、23……パイロツトバルブ、25a,25
b……サーボ圧回路、26a,26b……開閉
弁、28a,28b……チエツクバルブ、29
a,29b……パイロツト圧信号回路、30a,
30b……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, and FIG. 3 is a hydraulic circuit diagram of an embodiment of the present invention.
FIG. 4 is a hydraulic circuit diagram of another embodiment of the present invention. 10...Swivel motor, 11a, 11b...Engine, 15a, 15b...Pilot pump, 1
6a, 16b...Swivel pump, 21a, 21b...
...Variable discharge amount mechanism, 22a, 22b...Regulator, 23...Pilot valve, 25a, 25
b... Servo pressure circuit, 26a, 26b... Open/close valve, 28a, 28b... Check valve, 29
a, 29b...Pilot pressure signal circuit, 30a,
30b...Opening/closing valve.
Claims (1)
圧ポンプと、該油圧ポンプからの圧油の供給によ
り作動するアクチユエータとを、閉回路で接続
し、複数の油圧ポンプの吐出量可変機構を制御す
る各レギユレータに、前記各エンジンによつてそ
れぞれ駆動されるパイロツトポンプから、レギユ
レータを作動させるサーボ圧を供給すると共に、
すべてのパイロツトポンプを作動圧源とするパイ
ロツトバルブから、レギユレータの作動量を制御
するパイロツト圧信号を与えるようにした土木、
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、同一エンジン側のパイロツト
ポンプの吐出圧がない時に前記サーボ圧回路或い
はパイロツト圧信号回路の圧を零にする開閉弁を
それぞれ設け、各パイロツトポンプの吐出側に、
他のパイロツトポンプからの圧油が流入するのを
防ぐバルブをそれぞれ設け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 engines and an actuator operated by supply of pressure oil from the hydraulic pumps are connected in a closed circuit to control the variable discharge amount mechanism of the plurality of hydraulic pumps. Supplying servo pressure for operating the regulator to each regulator from a pilot pump driven by each of the engines, and
A civil engineering project in which pilot valves, which use all pilot pumps as operating pressure sources, give pilot pressure signals that control the operating amount of regulators.
In a hydraulic circuit of a construction machine, when there is no discharge pressure of a pilot pump on the same engine in at least one of the servo pressure circuit and the pilot pressure signal circuit of each regulator, the pressure in the servo pressure circuit or the pilot pressure signal circuit is zeroed. On the discharge side of each pilot pump,
A hydraulic circuit for civil engineering and construction machinery, characterized in that each pilot pump is provided with a valve that prevents pressure oil from flowing in from another pilot pump.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP858181A JPS57123332A (en) | 1981-01-24 | 1981-01-24 | Oil pressure circuit for civil engineering and construction machinery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP858181A JPS57123332A (en) | 1981-01-24 | 1981-01-24 | Oil pressure circuit for civil engineering and construction machinery |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS57123332A JPS57123332A (en) | 1982-07-31 |
| JPS6349013B2 true JPS6349013B2 (en) | 1988-10-03 |
Family
ID=11696975
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP858181A Granted JPS57123332A (en) | 1981-01-24 | 1981-01-24 | Oil pressure circuit for civil engineering and construction machinery |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS57123332A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP6710150B2 (en) * | 2016-11-24 | 2020-06-17 | 日立建機株式会社 | Construction machinery |
-
1981
- 1981-01-24 JP JP858181A patent/JPS57123332A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS57123332A (en) | 1982-07-31 |
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