JPH04191501A - Hydromechanical actuator for construction machinery - Google Patents

Hydromechanical actuator for construction machinery

Info

Publication number
JPH04191501A
JPH04191501A JP31805890A JP31805890A JPH04191501A JP H04191501 A JPH04191501 A JP H04191501A JP 31805890 A JP31805890 A JP 31805890A JP 31805890 A JP31805890 A JP 31805890A JP H04191501 A JPH04191501 A JP H04191501A
Authority
JP
Japan
Prior art keywords
valve
passage
pilot valve
throttle
pressure
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.)
Granted
Application number
JP31805890A
Other languages
Japanese (ja)
Other versions
JP2986904B2 (en
Inventor
Yusaku Nozawa
勇作 野沢
Kazuyuki Ino
和幸 猪野
Kinya Takahashi
欣也 高橋
Eiji Yonetani
栄二 米谷
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 JP2318058A priority Critical patent/JP2986904B2/en
Publication of JPH04191501A publication Critical patent/JPH04191501A/en
Application granted granted Critical
Publication of JP2986904B2 publication Critical patent/JP2986904B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Operation Control Of Excavators (AREA)
  • Fluid-Pressure Circuits (AREA)

Abstract

PURPOSE:To suppress excessive oil and prevent it from circulating into a tank by forming a passage in a valve chamber arranged oppositely to a driving part of a pilot valve for introducing a negative load pressure of an actuator thereto, providing a first throttle on the passage, and providing a second throttle on a passage which communicates the valve chamber with the tank. CONSTITUTION:A passage 32 is formed in a valve chamber 30 arranged oppositely to a driving part of a pilot valve 6 for introducing a negative load pressure Pa of a hydraulic motor 2 thereto. A first throttle 20 is provided on the passage 31, while a second throttle 21 is provided on a passage which communicates the valve chamber 30 with a tank. When the pilot valve 6 is operated abruptly and pressure pulses are generated, displacement of the pilot valve 6 is restricted through applying of a large pressure to the valve chamber 30 of the pilot valve 6. An opening rate of a proportional seat valve 4 is restricted accordingly, and controlling is carried out so as to decrease an amount of oil to be supplied to the hydraulic motor. Generation of oscillations is thus suppressed.

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明は油圧ショベルなどの大きな慣性体を有する建設
機械の油圧駆動装置に関する。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a hydraulic drive system for a construction machine having a large inertial body, such as a hydraulic excavator.

[従来の技術] 第5図は、この種の油圧駆動装置の一例を示す回路図で
ある。この従来例は、油圧源すなわち可変容量油圧ポン
プ3と、この油圧ポンプ3がら供給される圧油によって
駆動し、慣性体1を作動させるアクチュエータ、例えば
油圧モータ2と、油圧ポンプ3から油圧モータ2に供給
される圧油の流量を制御し、周側にスリット5を有する
比例シート弁4と、この比例シート弁4の駆動を制御す
るパイロット弁6とを備えている。なお、この従来例で
は、比例シート弁4の前後差圧を一定に保つ調整手段3
Aを備えている。また、パイロット弁6の駆動部に外力
を与え、ばね9の力に抗して移動させて開口させると、
比例シート弁4の背圧室から管路7を介してパイロット
弁6の開口部に圧油が流れ、さらにこの圧油が管路8を
介して比例シート弁4の下流に合流し、これによりパイ
ロット弁6の開口量に比例した量だけ比例シート弁4が
開口する。これに伴って油圧ポンプ3の圧油が比例シー
ト弁4を介して油圧モータ2に供給される。また、パイ
ロット弁6の上下端は油通路10によって連絡され、こ
れにより油圧バランスが保たれている。上述のよ、うに
してパイロット弁6に応じて駆動する比例シート弁4は
公知である。
[Prior Art] FIG. 5 is a circuit diagram showing an example of this type of hydraulic drive device. This conventional example includes a hydraulic source, that is, a variable displacement hydraulic pump 3, an actuator, such as a hydraulic motor 2, which is driven by pressure oil supplied from the hydraulic pump 3 and operates an inertial body 1, and a hydraulic motor 2 from the hydraulic pump 3. The proportional seat valve 4 has a slit 5 on the circumferential side, and a pilot valve 6 controls the drive of the proportional seat valve 4. In addition, in this conventional example, the adjusting means 3 that keeps the differential pressure across the proportional seat valve 4 constant
It has A. Also, if an external force is applied to the driving part of the pilot valve 6 and it is moved against the force of the spring 9 to open it,
Pressure oil flows from the back pressure chamber of the proportional seat valve 4 to the opening of the pilot valve 6 via the conduit 7, and further this pressure oil flows downstream of the proportional seat valve 4 via the conduit 8. The proportional seat valve 4 opens by an amount proportional to the opening amount of the pilot valve 6. Accordingly, pressure oil from the hydraulic pump 3 is supplied to the hydraulic motor 2 via the proportional seat valve 4. Further, the upper and lower ends of the pilot valve 6 are connected by an oil passage 10, thereby maintaining hydraulic balance. As mentioned above, proportional seat valves 4 which are actuated in response to pilot valves 6 are known.

上述した慣性体1を有する油圧駆動装置でパイロット弁
6を急操作した場合、油の圧縮性に起因して圧力脈動を
生じ、これに伴って油圧モータ2の回転速度が過度的に
微小変化をくり返し、振動状態になることがある。この
ような振動を抑制するために、同第5図に示すように、
油圧モータ2に連絡される管路をタンクに接続する管路
11や油圧モータ2をタンクに接続する管路12を設け
、これらの管路11.12中にリリーフ弁等を設け、回
路圧が大きくなったときリークさせることが知られてい
る。例えば、この辺の事情について[油圧化設計] (
発行所:日刊工業新聞社、発行年月:1965、第4巻
、第8号、P、33〜p) 38)に実験的に詳しく記
載されている。
When the pilot valve 6 is suddenly operated in a hydraulic drive system having the above-mentioned inertial body 1, pressure pulsations occur due to the compressibility of oil, and the rotational speed of the hydraulic motor 2 accordingly causes a slight change. Repeated vibrations may occur. In order to suppress such vibrations, as shown in Figure 5,
A pipe line 11 connecting the pipe line connected to the hydraulic motor 2 to the tank and a pipe line 12 connecting the hydraulic motor 2 to the tank are provided, and a relief valve or the like is provided in these pipe lines 11 and 12 to reduce the circuit pressure. It is known that it leaks when it becomes large. For example, regarding this situation [hydraulic design] (
Publisher: Nikkan Kogyo Shimbun, Publication date: 1965, Volume 4, No. 8, P, 33-p) 38).

[発明が解決しようとする課題] しかしながら、上記した従来技術では、慣性体1の急操
作時に生じる振動をリリーフ弁等を介して余剰流をタン
クに戻して抑制するようにしであることから、その余剰
流に相応するエネルギー損失を生じ、経済的でない。
[Problems to be Solved by the Invention] However, in the above-mentioned prior art, the vibration that occurs when the inertial body 1 is suddenly operated is suppressed by returning excess flow to the tank via a relief valve or the like. This causes energy loss corresponding to the surplus flow, which is not economical.

本発明は、上記した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、慣性体の急操作時に生じる振
動を、余剰流をタンクに還流させることなく抑制するこ
とができる建設機械の油圧駆動装置を提供することにあ
る。
The present invention has been made in view of the above-mentioned actual situation in the prior art, and its purpose is to suppress vibrations that occur during sudden operation of an inertial body without causing excess flow to flow back into the tank. The purpose of the present invention is to provide a driving device.

[課題を解決するための手段] この目的を達成するために、本発明は、油圧源と、この
油圧源から供給される圧油によって駆動し、慣性体を作
動させるアクチュエータと、油圧源からアクチュエータ
に供給される圧油の流量を制御する比例シート弁と、こ
の比例シート弁の駆動を制御するパイロット弁とを備え
た建設機械の油圧駆動装置において、上記パイロット弁
の駆動部と反対側に位置する弁室に上記アクチュエータ
の負荷圧を導、く通路を設けるとともに、この通路中に
第1の絞りを設け、上記弁室とタンクとを連絡する通路
に第2の絞りを設けた構成にしである。
[Means for Solving the Problems] In order to achieve this object, the present invention provides a hydraulic source, an actuator that is driven by pressure oil supplied from the hydraulic source and operates an inertial body, and an actuator that operates from the hydraulic source. In a hydraulic drive system for construction machinery, which is equipped with a proportional seat valve that controls the flow rate of pressure oil supplied to the valve, and a pilot valve that controls the drive of the proportional seat valve, the valve is located on the opposite side from the drive section of the pilot valve. A passage is provided in the valve chamber for introducing the load pressure of the actuator, a first restriction is provided in the passage, and a second restriction is provided in the passage connecting the valve chamber and the tank. be.

[作用] 本発明は、上記の構成にしであることから、慣性体の急
操作に伴ってアクチュエータの負荷圧が上昇すると、当
該負荷圧が第1の絞りを介してパイロット弁の駆動部と
反対側に位置する弁室に与えられ、このパイロット弁の
開口量が負荷圧の大きさに応じて小さくなるように制限
され、これに伴って比例シート弁の開口量が小さくなる
ように制限され、アクチュエータに供給される流量が少
なくなるように制限される。すなわち、上記弁室に導か
れる負荷圧と流量特性との関係を上記弁室に連なるよう
に設けられる第1の絞り、第2の絞りの開口面積の比に
依存させることができ、これらの絞りの開口面積の比を
適宜に設定することにより、アクチュエータに供給され
る流量を制限して圧力脈動を抑え、この圧力脈動によっ
て生じる振動を抑制することができる。
[Function] Since the present invention has the above configuration, when the load pressure of the actuator increases due to sudden operation of the inertial body, the load pressure is opposed to the drive part of the pilot valve via the first throttle. is applied to a valve chamber located on the side, and the opening amount of this pilot valve is limited so that it becomes small according to the magnitude of the load pressure, and the opening amount of the proportional seat valve is accordingly limited so that it becomes small, The flow rate supplied to the actuator is limited to less. That is, the relationship between the load pressure introduced into the valve chamber and the flow rate characteristics can be made to depend on the ratio of the opening areas of the first throttle and the second throttle, which are provided so as to be continuous with the valve chamber, and these throttles By appropriately setting the ratio of the opening areas, it is possible to limit the flow rate supplied to the actuator, suppress pressure pulsations, and suppress vibrations caused by the pressure pulsations.

[実施例] 以下、本発明の建設機械の油圧駆動装置の一実施例を図
に基づいて説明する。
[Embodiment] Hereinafter, one embodiment of the hydraulic drive device for construction machinery of the present invention will be described based on the drawings.

□ワ 第1図は本発明の一実施例を示す回路図で、前述した第
5図に対応させて描いである。すなわち、この実施例も
前述した第5図に示すものと同等の油圧源すなわち可変
容量油圧ポンプ3と、慣性体1を作動させるアクチュエ
ータ、例えば油圧モータ2と、周側にスリット5を有す
る比例シート弁4と、パイロット弁6と、比例シート弁
4の前後差圧を一定に保つ調整手段3Aと、比例シート
弁4の背圧室とパイロット弁6の上流側を連絡する管路
7と、パイロット弁6の下流側と比例シート弁4の下流
側を連絡する管路と、パイロット弁6の上下端を連絡す
る油通路10とを備えている。
□W FIG. 1 is a circuit diagram showing one embodiment of the present invention, and is drawn in correspondence with FIG. 5 described above. That is, this embodiment also includes a hydraulic power source, that is, a variable displacement hydraulic pump 3, similar to that shown in FIG. The valve 4, the pilot valve 6, the adjusting means 3A for keeping the differential pressure across the proportional seat valve 4 constant, the pipe line 7 that connects the back pressure chamber of the proportional seat valve 4 with the upstream side of the pilot valve 6, and the pilot valve 4. It includes a pipe line that connects the downstream side of the valve 6 and the downstream side of the proportional seat valve 4, and an oil passage 10 that connects the upper and lower ends of the pilot valve 6.

そして特に、この実施例では、パイロット弁6の駆動部
と反対側に位置する弁室30に油圧モータ2の負荷圧P
aを導く通路31を設けるとともに、この通路31に第
1の絞り20を設け、弁室30とタンクとを連絡する通
路に第2の絞り21を設けた構成にしである。
In particular, in this embodiment, the load pressure P of the hydraulic motor 2 is applied to the valve chamber 30 located on the opposite side from the driving part of the pilot valve 6.
In addition to providing a passage 31 for guiding the air, a first throttle 20 is provided in this passage 31, and a second throttle 21 is provided in a passage connecting the valve chamber 30 and the tank.

この実施例では、外力Fによるパイロット弁6の変位に
応じて比例シート弁4の開口量が制御されるから、通路
31を介してパイロット弁6の弁室30に油圧モータ2
の駆動圧すなわち負荷圧Paが導かれ、この負荷圧Pa
に応じてパイロット弁6の変位が減じると、その減じら
れたパイロット弁6の変位に対応して比例シート弁4を
通過する油量も減る。
In this embodiment, since the opening amount of the proportional seat valve 4 is controlled according to the displacement of the pilot valve 6 due to the external force F, the hydraulic motor 2 is connected to the valve chamber 30 of the pilot valve 6 via the passage 31.
A driving pressure, that is, a load pressure Pa is introduced, and this load pressure Pa
When the displacement of the pilot valve 6 is reduced in accordance with the reduced displacement of the pilot valve 6, the amount of oil passing through the proportional seat valve 4 is also reduced in accordance with the reduced displacement of the pilot valve 6.

なお、ここで上記した構成とは別に、パイロット弁6に
負荷圧Paを与えてその変位を減じるという考え方から
、第2図に示すようにパイロット弁6の下端部を段付と
してより簡単な構成とし、その段付は部の面積差(d、
”−d2”)  ・π/4をパイロット弁6の制御に活
用することが可能であるかどうか検討すると、以下のよ
うになる。
In addition, in addition to the configuration described above, based on the concept of applying load pressure Pa to the pilot valve 6 to reduce its displacement, a simpler configuration is adopted in which the lower end of the pilot valve 6 is stepped as shown in FIG. The step is determined by the area difference (d,
"-d2") ・If we consider whether it is possible to utilize π/4 to control the pilot valve 6, we will find the following.

今仮に、d1=4[mm]、外力Fはdlに20 [K
g/cm2]相当の油圧が作用したとき最大値となり、
パイロット弁6はフルストロークするものとすると、 Fmax=(π/4) X0142X20=2.51 
[Kg]となる。そして、負荷圧Paが100 [Kg
/cm2]のとき、無負荷時の90%の流量に減少する
ように意図すると、 2、51X0.1=0.251 [Kg]が負荷圧Pa
によって発生すれば良いことになる。
Now, suppose d1=4 [mm], and the external force F is 20 [K
g/cm2] reaches its maximum value when a hydraulic pressure equivalent to
Assuming that the pilot valve 6 is fully stroked, Fmax=(π/4) X0142X20=2.51
[Kg]. Then, the load pressure Pa is 100 [Kg
/cm2], if the flow rate is intended to decrease to 90% of the no-load state, then 2,51X0.1=0.251 [Kg] is the load pressure Pa
It is a good thing if it occurs because of this.

すなわち、 (π/4) X −(0,42Xd2”) X100=
0.251 [Kg]であり、これから、 d2=  0.42−0.251/ (π/4) X1
00=0.396 となる。したがって、d1=4 [mm]に対して、d
 2 = 3.96 [mm] となり、直径差は40
[μ] となる。
That is, (π/4) X − (0,42Xd2”) X100=
0.251 [Kg], and from this, d2= 0.42-0.251/ (π/4) X1
00=0.396. Therefore, for d1=4 [mm], d
2 = 3.96 [mm], and the diameter difference is 40
[μ] becomes.

この40[μ]の段差をdl、d2の公差を考慮して製
作管理することは現実にはかなり困難であり、したがっ
てこのような段付は構成が簡単であるものの実用性には
乏しいことになる。
In reality, it is quite difficult to manufacture and manage this 40 [μ] step by taking into account the tolerances of dl and d2, and therefore, although such a step is simple in configuration, it is impractical. Become.

このようなことも考慮して、本実施例では、上述したよ
うに第1の絞り20と第2の絞り21を設け、これらの
間の信号圧を利用しているが、その作用は以下のとおり
である。
Taking this into consideration, in this embodiment, the first diaphragm 20 and the second diaphragm 21 are provided as described above, and the signal pressure between them is utilized, but the effect is as follows. That's right.

今、第1の絞り20の上流圧(負荷圧)をPa、下流圧
(弁室30内の圧)をPc、第1の絞り20の    
 ′開口面積をal、第2の絞り21の下流圧をPt、
第2の絞り21の開口面積をa2とすると、第1の絞り
20、第2の絞り21を通過する流量は、q =C+ 
’ at ” F冴ア−Y Fh:民=c2Ha2m 
F厘77f■:■ の関係があり、流量係数Cl #C2とすれば、a、z
 (Pa−Pc)= a2”(Pc −Pt)(at2
+a22) PC=a+2Pa+a22Ptが成立する
。これをPcについて求めると、Pc=Pa/ (1+
(a2/a+) 2)、+(a2/at)2・Pt/ 
(1+(a2/a+)2)    、(1)となる。
Now, the upstream pressure (load pressure) of the first throttle 20 is Pa, the downstream pressure (pressure inside the valve chamber 30) is Pc, and the pressure of the first throttle 20 is Pc.
'The opening area is al, the downstream pressure of the second throttle 21 is Pt,
If the opening area of the second diaphragm 21 is a2, the flow rate passing through the first diaphragm 20 and the second diaphragm 21 is q = C+
'at' FSaeA-Y Fh:People=c2Ha2m
There is a relationship of F77f■:■, and if the flow coefficient Cl #C2, then a, z
(Pa-Pc)=a2''(Pc-Pt)(at2
+a22) PC=a+2Pa+a22Pt holds true. If we calculate this for Pc, Pc=Pa/ (1+
(a2/a+) 2), +(a2/at)2・Pt/
(1+(a2/a+)2), (1).

ここで、パイロット弁6の受圧面積をapとすると、 
[a、 ・Pc −a、 ・Pt]の力が外力Fに対抗
する力、例えば前述したf、=0.251 [Kg]に
なれば良い。
Here, if the pressure receiving area of the pilot valve 6 is ap, then
It is sufficient if the force [a, .Pc -a, .Pt] becomes a force that opposes the external force F, for example, the aforementioned f, = 0.251 [Kg].

上記した(1)式から、 a、 ・Pc −a、 ・Pt =a、・Pa/ (1+(a2/a+)2)+a、・P
t [(az/a+)2/ (1+(a2/a+)2)
 −1]=a、 ・(Pa−Pt) /1+ (a2+
a+)2=f となる。この式をさらに整理すると、 1−  (1+(a2/a+)2)  =f/a、 ・
 (Pa−Pt)1+(a2/a+)2=ap・(Pa
−Pt)/fa2/a+=  a、・Pa −Pt  
f−1(2)f=a、・(Pa−Pt)/ (1+(a
2/a+)2)  (3)となる。すなわち、負荷圧P
aそのものでなく、(Pa−Pt)がパイロット弁6に
作用する。
From the above equation (1), a, ・Pc −a, ・Pt = a, ・Pa/ (1+(a2/a+)2)+a, ・P
t [(az/a+)2/ (1+(a2/a+)2)
−1]=a, ・(Pa−Pt) /1+ (a2+
a+)2=f. Rearranging this formula further, 1- (1+(a2/a+)2) = f/a, ・
(Pa-Pt)1+(a2/a+)2=ap・(Pa
-Pt)/fa2/a+= a,・Pa -Pt
f-1(2)f=a, ・(Pa-Pt)/(1+(a
2/a+)2) (3). That is, the load pressure P
Instead of a itself, (Pa-Pt) acts on the pilot valve 6.

上記(2)式においてpt=oとして上述の各数値を代
入してみると、 a2/a+=  (71:/4) Xo、42刈001
0.251−1=7.0 となる。また、上記の(2)式においてPt=10とし
て上述の各数値を代入してみると、 a2/a!−(77:/4) Xo、42X(100−
10)10.251−1=6.64 となる。すなわち、f =0.251 [Kg] 、P
a=100[Kg/cm2]の条件でa2/a1を求め
ると、pt=○で7゜0、Pt=10で6.64となる
。つまり、a2/a、をほぼ7にするように、第1の絞
り20の開口面積a1と第2の絞り21の開口面積a2
との比を設定すると、上記した所望の機能が得られ、ま
たこのような開口面積a1、a2を有する第1の絞り2
0、第2の絞り21を設けること−は容易である。
Substituting each of the above numerical values as pt=o in the above equation (2), a2/a+= (71:/4) Xo, 42Kari001
0.251-1=7.0. Moreover, when we substitute each of the above-mentioned numerical values into the above equation (2) with Pt=10, we get a2/a! -(77:/4) Xo, 42X(100-
10) 10.251-1=6.64. That is, f =0.251 [Kg], P
When a2/a1 is calculated under the condition of a=100 [Kg/cm2], it is 7°0 when pt=○ and 6.64 when Pt=10. In other words, the aperture area a1 of the first aperture 20 and the aperture area a2 of the second aperture 21 are adjusted so that a2/a is approximately 7.
The desired function described above can be obtained by setting the ratio of
0. Providing the second diaphragm 21 is easy.

このように構成した実施例にあっては、パイロット弁6
を急操作して圧力脈動を生じたとき、大きな圧力が上述
のようにパイロット弁6の弁室30に作用することによ
りパイロット弁6の変位が制限され、これにより比例シ
ート弁4の開口量が制限されて、油圧モータ2に供給さ
れる油量が少なくなるように制御され、これにより振動
の発生を抑制できるとともに、エネルギー損失をほとん
ど生じることがなく、経済性に富む。
In the embodiment configured in this way, the pilot valve 6
When a pressure pulsation occurs due to sudden operation of the valve, the large pressure acts on the valve chamber 30 of the pilot valve 6 as described above, which limits the displacement of the pilot valve 6, thereby reducing the opening amount of the proportional seat valve 4. As a result, the amount of oil supplied to the hydraulic motor 2 is controlled to be small, thereby suppressing the occurrence of vibrations and causing almost no energy loss, which is highly economical.

また、負荷圧Paと流量特性の関係は、第1の絞り20
.第2の絞り21の開口面積の比a 2/ a +に依
存させることができるので、この比a2/a1を適宜変
更することにより、容易に所望の特性に変更できる。
Also, the relationship between the load pressure Pa and the flow rate characteristics is
.. Since it can be made to depend on the ratio a2/a+ of the aperture area of the second diaphragm 21, desired characteristics can be easily changed by appropriately changing the ratio a2/a1.

第3図、第4図は、第1の絞りの別の例を示す図で、第
3図に示す例は、パイロット弁6内に第1の絞り20A
を設けてあ賑第4図に示す例は、パイロット弁6の摺動
クリアランスを第1の絞り20Bとしてあり、さらにこ
れらの第1の絞り20A120Bは、弁室30に負荷圧
Paを導く通路を兼ねている。このように第1の絞りを
設けたものにあっては、上述の実施例1と同様の作用効
果を奏する他、従来のパイロット弁6の構造をほとんど
変えることなく実現でき、製作がより簡単で、製作費が
安くて済む。
3 and 4 are diagrams showing other examples of the first throttle, and the example shown in FIG. 3 has a first throttle 20A inside the pilot valve 6.
In the example shown in FIG. 4, the sliding clearance of the pilot valve 6 is set as the first throttle 20B, and these first throttles 20A and 120B provide a passage for introducing the load pressure Pa into the valve chamber 30. Also serves as. In addition to achieving the same effects as in the first embodiment described above, the first throttle provided in this manner can be realized without changing the structure of the conventional pilot valve 6, and is easier to manufacture. , production costs are low.

[発明の効果] 本発明の建設機械の油圧駆動装置は、以上のように構成
しであることから、慣性体の急操作時に生じる振動を、
余剰流をタンクに還流させることなく抑制することがで
き、従来に比べてエネルギ損失を抑え、経済性に富む効
果がある。また、負荷圧と流量特性との関係は、第1の
絞り、第2の絞りの開口面積の比に依存するので、この
比を適宜変更することにより容易に所望の特性に変更す
ることができる。
[Effects of the Invention] Since the hydraulic drive system for construction machinery of the present invention is configured as described above, vibrations generated when the inertial body is suddenly operated can be suppressed.
Surplus flow can be suppressed without being returned to the tank, reducing energy loss and being highly economical compared to conventional methods. Furthermore, since the relationship between the load pressure and the flow rate characteristics depends on the ratio of the opening areas of the first throttle and the second throttle, desired characteristics can be easily changed by appropriately changing this ratio. .

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

第1図は本発明の建設機械の油圧駆動装置の一実施例を
示す回路図、第2図は本発明の前段階として考えられる
技術を説明する図、第3図、第4図はそれぞれ本発明に
具備される第1の絞りの別の例を示す図、第5図は従来
の建設機械の油圧駆動装置の一例を示す回路図である。 1・・・慣性体、2・・・油圧モータ(アクチュエータ
)、3・・・可変容量油圧ポンプ(油圧源)、3A・・
・調整手段、4・・・比例シート弁、5・・・スリット
、6・・・パイロット弁、7.8・・・管路、9・・・
ばね、10・・・油通路、11.12・・・管路、20
.20A120B・・・第1の絞り、30・・・弁室、
31・・・通路。 第4図
Fig. 1 is a circuit diagram showing an embodiment of the hydraulic drive system for construction machinery of the present invention, Fig. 2 is a diagram illustrating a technology considered as a preliminary stage of the present invention, and Figs. FIG. 5 is a circuit diagram showing an example of a conventional hydraulic drive device for construction machinery. 1... Inertia body, 2... Hydraulic motor (actuator), 3... Variable displacement hydraulic pump (hydraulic source), 3A...
- Adjustment means, 4... Proportional seat valve, 5... Slit, 6... Pilot valve, 7.8... Pipe line, 9...
Spring, 10...Oil passage, 11.12...Pipe line, 20
.. 20A120B...first throttle, 30...valve chamber,
31...Aisle. Figure 4

Claims (1)

【特許請求の範囲】[Claims] (1)油圧源と、この油圧源から供給される圧油によっ
て駆動し、慣性体を作動させるアクチュエータと、油圧
源からアクチュエータに供給される圧油の流量を制御す
る比例シート弁と、この比例シート弁の駆動を制御する
パイロット弁とを備えた建設機械の油圧、駆動装置にお
いて、上記パイロット弁の駆動部と反対側に位置する弁
室に上記アクチュエータの負荷圧を導く通路を設けると
ともに、この通路中に第1の絞りを設け、上記弁室とタ
ンクとを連絡する通路に第2の絞りを設けたことを特徴
とする建設機械の油圧駆動装置。
(1) A hydraulic source, an actuator that is driven by pressure oil supplied from the hydraulic source and operates an inertial body, a proportional seat valve that controls the flow rate of the pressure oil supplied from the hydraulic source to the actuator, and a proportional seat valve that controls the flow rate of the pressure oil supplied from the hydraulic source to the actuator. In a hydraulic and drive device for construction machinery that is equipped with a pilot valve that controls the drive of a seat valve, a passage is provided for guiding the load pressure of the actuator to a valve chamber located on the opposite side of the drive section of the pilot valve, and A hydraulic drive device for construction machinery, characterized in that a first throttle is provided in the passage, and a second throttle is provided in the passage communicating the valve chamber and the tank.
JP2318058A 1990-11-26 1990-11-26 Hydraulic drive for construction machinery Expired - Fee Related JP2986904B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2318058A JP2986904B2 (en) 1990-11-26 1990-11-26 Hydraulic drive for construction machinery

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2318058A JP2986904B2 (en) 1990-11-26 1990-11-26 Hydraulic drive for construction machinery

Publications (2)

Publication Number Publication Date
JPH04191501A true JPH04191501A (en) 1992-07-09
JP2986904B2 JP2986904B2 (en) 1999-12-06

Family

ID=18095015

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2318058A Expired - Fee Related JP2986904B2 (en) 1990-11-26 1990-11-26 Hydraulic drive for construction machinery

Country Status (1)

Country Link
JP (1) JP2986904B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2000257601A (en) * 1999-03-05 2000-09-19 Hitachi Constr Mach Co Ltd Hydraulic circuit device
US6438952B1 (en) 1999-03-04 2002-08-27 Hitachi Construction Machinery Co., Ltd. Hydraulic circuit device
US8314995B2 (en) 2010-09-27 2012-11-20 Hoya Corporation Variable power optical system and imaging apparatus

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6438952B1 (en) 1999-03-04 2002-08-27 Hitachi Construction Machinery Co., Ltd. Hydraulic circuit device
JP2000257601A (en) * 1999-03-05 2000-09-19 Hitachi Constr Mach Co Ltd Hydraulic circuit device
US8314995B2 (en) 2010-09-27 2012-11-20 Hoya Corporation Variable power optical system and imaging apparatus

Also Published As

Publication number Publication date
JP2986904B2 (en) 1999-12-06

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