JP2001184130A - Method and device for controlling pressure - Google Patents

Abstract

PROBLEM TO BE SOLVED: To improve the stability of pressure control. SOLUTION: A pilot spool 54 for controlling a pilot flow rate and a main flow rate controlling main poppet 41 for executing pilot operation by the pilot spool 54 are arranged in a valve housing 21. A load pressure feedback mechanism for feeding back the load pressure Pload of a main flow rate to the pilot spool 54 is formed by a passage 79, a load pressure sensing part 77, etc. The feedback mechanism displaces the spool 54 in a pilot flow rate reducing direction by the increment of the load pressure Pload and reduces the load pressure Pload by controlling the main poppet 41 in a main flow rate reducing direction. Thus the variation of the load pressure Pload is suppressed and the stability of pressure control is secured.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

The present invention relates to a pressure control method and a pressure control device using a pilot valve and a main valve.

[0002]

2. Description of the Related Art FIG. 15 shows a meter-in / meter-out type control circuit provided in a conventional construction machine such as a hydraulic excavator.
Cylinder type hydraulic actuator 2 for driving load W
Between them, there is provided a bridge circuit 3 including two meter-in valves A1IMV and A2IMV and two meter-out valves A3IMV and A4IMV.

Further, a load hold check valve 4 is provided in a passage between the pump 1 and the bridge circuit 3, and a drift preventing leak is provided in two passages between the bridge circuit 3 and the hydraulic actuator 2. Reduction valves (pilot-operated check valves) 5 are provided.

[0004] A bridge circuit (not shown) for controlling another fluid pressure actuator (not shown) is similarly connected to the discharge port of the pump 1 through a passage 6.

Further, between the discharge port of the pump 1 and the tank 7, one common bypass valve 8, which is controlled in conjunction with the control of the bridge circuit 3 of the plurality of fluid pressure actuators 2, and a pump, A main relief valve 9 for setting the discharge pressure is provided.

Meter-in valves A1IMV, A2IMV, meter-out valves A3IMV, A4IMV and common bypass valve 8
Is an open / close valve with a middle throttle notch of a spool valve type. The spool valve stroke is controlled by a push solenoid operated by an electric signal output from a controller (not shown) according to the operation amount of an operation lever. Is done.

In this circuit, for example, when the fluid pressure actuator 2 is extended against the load W, the drift reducing valve 5 is opened, the meter-in valve A1IMV and the meter-out valve A4IMV are closed, and the variable displacement pump is closed. 1, the control is performed so that the common bypass valve 8 is gradually closed, and the meter-in valve A2IMV and the meter-out valve A3IMV are gradually opened.

On the other hand, when the fluid pressure actuator 2 is contracted, the discharge amount of the variable displacement pump 1 is gradually increased while the drift-in valve 5 is opened and the meter-in valve A2IMV and the meter-out valve A3IMV are closed. At the same time, control is performed such that the common bypass valve 8 is gradually closed, and the meter-in valve A1IMV and the meter-out valve A4IMV are gradually opened. Such control is performed by an operation lever (not shown) via a controller.

As shown in FIG. 16, conventionally, a load pressure of a fluid pressure actuator 2 is detected by a pressure sensor 10A, and a meter-in valve A is electrically controlled by a controller 10B.
The control valve such as 2IMV is controlled (the opening area is reduced) so that the load pressure controlled by the control valve does not exceed a preset pressure.

[0010]

However, there is a risk that the control system may become unstable due to a delay in the calculation of the feedback, and there is a problem that it takes time until the control system is stabilized.

The present invention has been made in view of the above points, and has as its object to improve stability in pressure control.

[0012]

According to the first aspect of the present invention, a main valve for controlling a main flow rate is pilot-operated by controlling a pilot flow rate by a pilot valve, and a load pressure of the main flow rate is applied to the pilot valve. This is a pressure control method of feeding back, displacing a pilot valve in a pilot flow decreasing direction by increasing the load pressure, and controlling a main valve in a main flow decreasing direction by decreasing the pilot flow to reduce the load pressure.

When the load pressure increases, the load pressure is directly fed back to the pilot valve, and the pilot valve is displaced in the pilot flow decreasing direction by the feedback force, and the main valve is controlled in the main flow decreasing direction by the pilot valve displacement. Since the load pressure decreases with a good response, high-load driving is prevented, fluctuations in the load pressure are suppressed, and instability due to a delay in feedback calculation does not occur.

According to a second aspect of the present invention, in the pressure control method according to the first aspect, by controlling an external thrust acting on the pilot valve from a direction opposite to the load pressure fed back to the pilot valve. This is a pressure control method for adjusting the load pressure.

Then, by adjusting the thrust against the load pressure, the load pressure to be driven is adjusted.

According to a third aspect of the present invention, there is provided the pressure control method according to the second aspect, wherein the thrust is temporarily reduced from the feedback force due to the load pressure when the external thrust is raised. .

When the thrust against the load pressure rises, the thrust is temporarily reduced from the feedback force due to the load pressure, so that the pilot valve returns to the neutral position with good response and stabilizes the control system.

According to a fourth aspect of the present invention, there is provided a pilot valve for controlling a pilot flow rate, a main valve for controlling a main flow rate operated by the pilot valve, and a load pressure of the main flow rate fed back to the pilot valve. A pressure control device comprising a load pressure feedback mechanism for displacing a pilot valve in a pilot flow decreasing direction by increasing pressure and controlling a main valve in a main flow decreasing direction to reduce a load pressure.

When the load pressure increases, the load pressure is directly fed back to the pilot valve by the load pressure feedback mechanism, and the pilot valve is displaced in the pilot flow decreasing direction by the feedback force, whereby the main valve moves in the main flow decreasing direction. To reduce the load pressure with good response, preventing high-load driving and
Suppress fluctuations in load pressure to ensure stability.

According to a fifth aspect of the present invention, in the pressure control device of the fourth aspect, the load pressure is controlled by controlling the thrust acting on the pilot valve from a direction opposite to the load pressure fed back to the pilot valve. It is a pressure control device provided with a driving means for adjusting.

By controlling the driving means of the pilot valve, the thrust of the driving means against the load pressure is adjusted to adjust the load pressure to be driven.

According to a sixth aspect of the present invention, there is provided a pressure control apparatus as set forth in the fifth aspect, further comprising a controller for temporarily reducing the thrust from the feedback force due to the load pressure when the thrust of the driving means is raised. It is a control device.

When the thrust of the driving means is raised by the controller, the thrust of the driving means is temporarily reduced from the feedback force due to the load pressure, whereby the pilot valve is returned to the neutral position in a responsive manner by the load pressure. And stabilize the control system.

[0024]

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS One embodiment of the present invention will be described below with reference to FIGS.

First, an embodiment shown in FIGS. 1 and 2 will be described. The same parts as those of the conventional control circuit shown in FIG.

FIG. 2 shows a meter-in valve as a control valve.
A1IMV, A2IMV and meter-out valve as control valve
A meter-in / meter-out type control circuit is constituted by a bridge circuit 3 in which A3IMV and A4IMV are combined. Pump discharge is performed to the discharge port of a variable displacement pump 1 capable of variably controlling a discharge flow rate by a pump swash plate 1a. A passage 11 is connected to the pump discharge passage 11 and communicates with two meter-in valves A1IMV and A2IMV of one bridge circuit 3 for controlling one fluid pressure actuator 2.
12 and 13 are connected, and in the pump discharge passage 11,
A passage 6 communicating with another bridge circuit 3a for controlling another fluid pressure actuator 2a is also connected.

Further, the pump 1 has a discharge port
A common bypass valve 8 for controlling the supply amount of the working fluid discharged from each of the bridge circuits 3 and 3a and a main relief valve 9 for setting an upper limit of the pump discharge pressure are common to the plurality of bridge circuits 3 and 3a. It is provided in.

To explain one bridge circuit 3, two meter-in valves A1IMV and A2IMV are connected to a pump discharge passage 11 via passages 12 and 13, respectively. These meter-in valves A1IMV and A2IMV are connected to a fluid pressure actuator. Two meter-out valves A3IMV and A4IMV for controlling between the passages 14 and 15 to the tank 2 and the tank passages 16 and 17 are connected respectively, and the tank passages 16 and 17 are connected to the tank 7.

Further, a meter-in valve A1IMV and a meter-out valve A3 shown above the bridge circuit 3 are shown.
The passage 14a drawn through the IMV is connected to a chamber (hereinafter, referred to as a chamber) on the rod side of the piston 2p of the fluid pressure actuator 2.
"Rod side chamber 2r"), and the meter-in valve A2IMV and meter-out valve
The passage 15a drawn through the A4IMV is connected to a chamber (hereinafter, referred to as "head side chamber 2h") located closer to the head than the piston 2p of the fluid pressure actuator 2.

Referring to FIGS. 1 and 2, each of the meter-out valves A3IMV and A4IMV will be described. A pilot flow amplification type main poppet 22 as a main valve provided in a valve housing 21 is mainly arranged. And a valve chamber 23 formed in the valve housing 21 respectively.
Each of the main poppets 22 is provided so as to be displaceable in the axial direction, and return passages 14a and 15a from the fluid pressure actuator 2 are connected to the respective valve chambers 23.

The main poppet on the meter-out side
Variable slots 25 whose opening areas are proportionally enlarged and changed as the axial displacement of each main poppet 22 is increased are formed in the side surface portion of each of the 22 in the axial direction.

The variable slots 25 are provided with springs formed in the valve housing 21 in a state in which the drain flow control portions 26 formed on the opposite ends of the main poppets 22 are seated on the seat 27. It has a slight opening 25a communicating with the chamber 28. The respective seats 27 are communicated with the tank 7 by tank passages 16 and 17, respectively.

The main poppet on the meter-out side
Each of the spring chambers 28 with respect to 22 has a built-in compression coil-shaped return spring 29 that presses the drain flow control unit 26 toward the sheet 27, that is, in the closing direction.

As means for controlling the opening degree of each main poppet 22, passages 31 and 32 which can communicate with each other through the seat 30 from each spring chamber 28 to each tank passage 16 and 17 are provided.
The pilot spool 33 as a pilot valve is interposed in each passage 31, 32, respectively.
These pilot spools 33 perform drain control of each spring chamber 28 in response to an electric signal from a controller (not shown), and return springs in the spring chambers 24 that urge each pilot spool 33 to a neutral position (closed position). And a push solenoid 35 as drive means for driving the pilot spool 33 against these return springs 34, respectively.

When the displacement of the pilot spool 33 is a minute displacement equal to or less than a dead band near the neutral position, the passing flow rate through the seat 30 becomes zero.

The pilot spools 33 of the meter-out valves A3IMV and A4IMV communicate with return passages 14a and 15a from the fluid pressure actuator 2 by passages 36, respectively, and have a relief function to be described later against an excessive load pressure. .

As shown in FIG. 1, the push solenoid 35 comprises an exciting coil 35a and a movable core 35b integrated on the upper part of the pilot spool 33.

The pilot spool 33 of each of the meter-out valves A3IMV and A4IMV has a large load pressure sensing portion 38 formed therein, and a load pressure chamber 39 formed above the load pressure sensing portion 38, respectively. Load pressure chamber 39
The return passages 14a and 15a from the fluid pressure actuator 2 are connected to each other by a passage 36.

A passage 36 for introducing the load pressure, a load pressure chamber 39
The load pressure sensing mechanism 38 of the pilot spool 33 that receives the load pressure forms a load pressure feedback mechanism.

Accordingly, when an excessive load pressure is generated in the return passages 14a and 15a from the fluid pressure actuator 2,
The load pressure is guided to the load pressure chamber 39 and presses the load pressure sensing unit 38 downward in the figure, so that the seat 30 is opened,
By reducing the pressure in the spring chamber 28 and lifting the main poppet 22, the valve chamber 23 has a relief function of communicating with the tank 7.

Above the push solenoid 35, a displacement sensor 40 for detecting an axial stroke of the pilot spool 33 is mounted. In this displacement sensor 40, a coil 40a is mounted on a push solenoid 35 by a sensor mounting cylinder 40.
The core 40c, which moves integrally with the movable iron core 35b, is fitted inside the sensor mounting tubular member 40b, and the axial displacement amount of the core 40c, that is, the pilot spool is moved by the coil 40a. 33 axial displacements are detected.

The pilot spool 33, the movable iron core 35b and the core 40c are provided with drain holes 37 for discharging working fluid over the entire length.

In each of the meter-out valves A3IMV and A4IMV thus configured, a part of the return flow Q from the fluid pressure actuator 2 flows into the spring chamber 28 through the opening 25a of the pilot variable slot 25. . The stroke control of the main poppet 22 is achieved by controlling the opening degree of the seat 30 communicating with the spring chamber 28 by the pilot spool 33, and the flow rate passing through the pilot spool 33 is q.

By controlling the stroke of the main poppet 22 on the meter-out side, the drain flow controller 26
, The main flow rate LQ is controlled, and the main flow rate LQ is controlled as if the pilot spool 33
The pilot flow q controlled by the above appears in an amplified state.

On the other hand, when the pilot spool 33 is closed and both the flow rate q and the main flow rate LQ are zero,
The return pressure of the return passages 14a and 15a from the fluid pressure actuator 2 increases, the force acting on the load pressure sensing portion 38 of the pilot spool 33 via the passage 36, and the push solenoid
When the sum with the thrust of 35 overcomes the biasing force of the return spring 34,
The pilot spool 33 is displaced to open the seat 30, the pilot flow q starts to flow, and a differential pressure is generated around the opening 25a of the variable slot 25 of the main poppet 22 on the meter-out side. Go to sheet 27
Is opened and the main flow rate LQ is generated, so that the return pressure of the return passage 14a or 15a from the fluid pressure actuator 2 is prevented from rising abnormally, and the pilot spool 33
Has a relief valve function to settle at a constant pressure value set by the thrust of a return spring 34 in the form of a compression coil and a push solenoid 35 acting on the spring.

Next, the meter-in valves A1IMV, A2IM
To explain V, a pilot flow amplification type main poppet as a main valve provided inside the valve housing 21 is described.
The main poppet 41 is constructed mainly of the main poppet 41 and the pilot control means thereof is different from those of the meter-out valves A3IMV and A4IMV.

Since the structures of the meter-in valves A1IMV and A2IMV are the same, a detailed description will be given of the meter-in valve A2IMV on the cylinder head side as an example.

As shown in FIG. 2, the main poppet 41 on the meter-in side has a shuttle valve 42 as a high-pressure selecting means inside, and a passage 43 formed on one inlet side of the shuttle valve 42 has a An opening is formed in a passage 13 that communicates with a discharge port of the pump 1 via a pump discharge passage 11, guides pump discharge pressure to a shuttle valve 42, and a passage 44 formed on the other inlet side of the shuttle valve 42 includes: An annular space 45 communicated with the head side chamber 2h of the fluid pressure actuator 2 through the passage 15
And a shuttle valve for controlling the pressure supplied to the hydraulic actuator 2 or the load pressure of the hydraulic actuator 2
Guided to 42, shuttle valve 42 selects the high pressure side of these pressures.

A passage 46 in the main poppet 41 formed on the output side of the shuttle valve 42 communicates with a variable slot 47 formed in the peripheral surface of the main poppet 41 in the axial direction. The opening area of the variable slot 47 increases in accordance with the movement stroke of the main poppet 41.

The variable slot 47 is provided with a main poppet 41.
When the flow control unit 48 is seated on the seat 49, a spring chamber 51 as a pressure chamber formed in the valve housing 21 is provided.
It has a slight opening 47a communicating with the opening.

In a spring chamber 51 for the main poppet 41, there is provided a compression coil-shaped return spring 52 for pressing a flow control unit 48 of the main poppet 41 against a sheet 49.
51 is connected to a pilot spool 54 as a pilot valve by a passage 53.

As shown in FIG. 1, the pilot spool 54 has a fitting hole formed in the valve housing 21.
A seat 56 that is slidably fitted to the fitting 55 and that is opened and closed by a pilot spool 54 is provided at the tip of the fitting hole 55.

The stroke of the pilot spool 54 is controlled by a push solenoid 57 as an external driving means. This push solenoid 57 is a valve housing
The pilot spool 5 is installed in the coil 57a
The movable iron core 57b integrated with the upper end in the figure of FIG. 4 is movably fitted, and when the coil 57a is energized, the pilot spool 54 is pushed into the valve housing 21 (opens from the seat 56). Direction) can be obtained.

The illustrated lower end of the pilot spool 54 is inserted into a spring chamber 61 formed in the valve housing 21.
A compression coil-shaped return spring 62 provided in the spring chamber 61.
As a result, an urging force for returning the pilot spool 54 upward in the drawing is applied.

The spring chamber 61 communicates with the check valve 64 via a passage 63 and further communicates with the passage 15 via a passage 65.

At a relatively lower portion of the pilot spool 54,
A land 68 and a poppet 69 are formed via the circumferential groove 66, and the poppet 69 is locked to the seat 56 at a neutral position.

When the displacement of the pilot spool 54 is a minute displacement equal to or less than the dead band near the neutral position, the passing flow rate through the seat 56 becomes zero.

The fitting hole 55 is formed with an annular groove 71 which is always open to the circumferential groove 66, and the spring chamber 51 of the main poppet 41 on the meter-in side communicates with the annular groove 71 through the passage 53.

A relatively large load pressure sensor 77 is formed at a relatively upper portion of the pilot spool 54. A lower portion of the load pressure sensor 77 shown in FIG. The load pressure chamber 78 is formed by the hole.
A passage 78 communicates with the passage 65 through a passage 79. The upper part of the load pressure sensor 77 is connected to the tank 7 by a passage 81.

The passage 79 for introducing the load pressure, the load pressure chamber 78
A load pressure feedback mechanism is formed by the load pressure sensor 77 of the pilot spool 54 that receives the load pressure.

The pilot spool 54 is provided with a displacement sensor 82 as opening area monitoring means for monitoring the opening area of the pilot spool 54 by detecting its operation stroke.

This displacement sensor 82 is a push solenoid
A coil 82a is mounted on the cylinder 57 via a sensor mounting cylinder 82b, and the movable iron core 57a is mounted inside the sensor mounting cylinder 82b.
The core 82c, which moves integrally with b, is fitted, and the coil 82a detects the axial displacement of the core 82c, that is, the axial displacement of the pilot spool 54.

Further, the pilot spool 54 and the movable iron core
A drain hole 83 for discharging the working fluid is formed through the entire length of the core 57c and the core 82c.

The main poppet 22 and the pilot spool 33 constitute one control valve, and the main poppet 41 and the pilot spool 54 constitute the other control valve.

The meter-in valve A1 constructed as described above
In IMV and A2IMV, the push solenoid 57 is excited and the pilot spool 54 is pressed against the spring force of the return spring 62.
When the is moved in the pushing direction, the poppet portion 69 of the pilot spool 54 opens the sheet 56, so that the spring chamber 51 of the main poppet 41 has a passage 53, an annular groove 71, a circumferential groove 66,
Seat 56, spring chamber 61 of pilot spool 54, passage 63,
Through a check valve 64 and a passage 65, the passage 15 is communicated with the passage 15 to the fluid pressure actuator 2, and the spring chamber 51 is depressurized and controlled according to the displacement amount of the pilot spool 54.
The stroke is controlled so that the opening 41 is opened, and the main flow that flows from the passage 13 to the passage 15 through the seat 49 has an appearance in which the pilot flow controlled by the pilot spool 54 is amplified.

As shown in FIG. 2, reference numeral 86 denotes a controller mounted on a construction machine such as a hydraulic shovel.
An operation lever 87 for issuing a command signal for 2a, a pump pressure sensor 88 provided in the pump discharge passage 11 for detecting a pump discharge pressure, and meter-in valves A1IMV and A2IMV
Displacement sensor 82 and meter-out valve A3IMV, A4IM
V displacement sensors 40 are connected respectively, and the push-in solenoids 57 of the meter-in valves A1IMV and A2IMV and the meter-out valve A3IMV
, A4IMV push solenoids 35 are connected to each other, and the command signal input from the operation lever 87 is processed by the controller 86, and the meter-in valves A1IMV, A2IMV
V and the meter-out valves A3IMV and A4IMV are controlled under optimum conditions as described below.

FIG. 3 is a block diagram showing a combined pressure / flow control system for the meter-in valve A2IMV for supplying hydraulic oil from the pump 1 to the head side chamber 2h of the fluid pressure actuator 2, and the control system comprises an operating lever. 87 lever operation amount L
And a three-dimensional map 91 showing the relationship between the flow rate Q controlled by the main poppet 41, ie, the actuator speed, and the load pressure P, ie, the actuator operating force.

In this three-dimensional map 91, the corresponding flow rate Q can be obtained by inputting the lever operation amount L and the load pressure P, and can be obtained by inputting the lever operation amount L and the flow rate Q. , The corresponding load pressure P can be determined.

The curve on the LQ plane shows the flow rate characteristic when no load is applied, that is, the velocity modulation characteristic.
The curve on the LP plane shows a pressure characteristic, that is, a force modulation characteristic in a stall state in which the fluid pressure actuator 2 cannot move due to a load. The flow rate Q is used.

The solid line drawn from the three-dimensional map 91 indicates the flow rate Q, and the dotted line indicates the load pressure P.

This control system is provided with a load pressure calculating device 92 for estimating the load pressure P _load of the fluid pressure actuator 2 without using a pressure sensor. As will be described later in detail, the load pressure calculating device 92 mainly includes a driving current I supplied to the push solenoid 57 of the pilot spool 54 on the meter-in side and a displacement amount X detected by the displacement sensor 82 or a meter-out side. The load pressure P _load is estimated from the drive current I supplied to the push solenoid 35 of the pilot spool 33 and the displacement X detected by the displacement sensor 40.

The flow rate Q controlled by the main poppet 41 can be expressed by the following equation (1).

[0073]

[Equation 1] Q = α · A · (P _P −P _load ) ^1/2 where α is a constant, and A is a flow control unit of the main poppet 41.
Open area between 48 and seat 49, _PP is pump pressure sensor 88
Is the pump discharge pressure, and P _load is the load pressure.

From the formula 1, the opening area A of the main poppet 41 is obtained.
Is represented by the following equation 2.

[0075]

[Equation 2] A = Q / {α · (P _P −P _load ) ^1/2 } Therefore, by inputting the lever operation amount L with the operation lever 87, the required flow rate value output from the three-dimensional map 91 Given a Q, a pump discharge pressure P _P which is detected by the pump pressure sensor 88, by the load pressure P _load in which the load pressure calculating unit 92 is estimated with high accuracy, by calculating the opening area a of the main poppet 41 Can be.

The opening area A of the main poppet 41 and the displacement X _P of the main poppet 41 have a predetermined relationship designed in advance, and when the relationship is expressed by a function, X _P = f (A). FIG. 3 shows a function 93.

[0077] When the displacement amount X _P of the main poppet 41 is determined, the flow rate value Q, the pump delivery pressure P _P, while taking into consideration the load pressure P _load, the pilot spool 54 to achieve the displacement X _P of the main poppet 41 of the displacement X _C, X _C = f
It can be obtained by a function 94 represented by (X _P ).

Using this displacement amount X _C as a target value, an error between the actual displacement amount X of the pilot spool 54 detected by the displacement sensor 82 is calculated by a comparator 95, and two kinds of variable adjustments can be made to the error. Are multiplied by the gain K _i and the gain K _P and input to the adder 96.

[0079] The gain K _i and the gain K _P to variably adjust a gain adjustment device 97, by adjusting the current value I supplied to the push solenoid 57 by the gain adjustment, the relative pilot spool 54 The spring constant of the return spring 62 can be arbitrarily changed according to the load pressure P _load .

That is, the push solenoid 57 and the return bar
The spring 62 acts on the pilot spool 54 in the opposite direction.
Therefore, for example, when it is necessary to strengthen the return spring 62
Is connected to the push solenoid 57 by the gain adjustment device 97.
Gain K for determining current value I _iAnd gain K_PSmaller
To reduce the thrust of the push solenoid 57.
The spring constant of the return spring 62 is relatively reduced by reducing
The same effect can be obtained as when it is increased and increased.

[0081] Gain adjustment device 97 functions to directly adjust the gain K _i and the gain K _P of the flow control system, which allows for balancing the pressure control system, such as the following of the pressure control device 98 There is also.

The adder 96 includes a pressure control device 98.
Also, a signal passed through the feed forward controller 99 is input.

The pressure control device 98 includes a pressure feedback controller 101 and a work load estimating device 102.

The pressure feedback controller 101
By controlling the current value supplied to the push solenoid 57 in relation to the load pressure P _load estimated by the load pressure calculation device 92, for example, pressure control is performed so that the load pressure P _load does not exceed the set pressure. Thus, the stability of the control system can be improved.

The work load estimating device 102 estimates the load pressure of the boom cylinder or the like when the front working device of the hydraulic shovel is operating, for example. _load is, not only the pure work load (static load of the load), the assumption that the influence of the inertia load of the front work device is intended to be received, by removing the influence of the inertia load, in the bucket The work load is estimated with high accuracy.

The feed forward controller 99 is provided to improve the possibility that the control system becomes unstable due to a delay in calculation of the feedback control system.

Next, the operation of the embodiment shown in FIGS. 1 and 2 will be described.

When the operation lever 87 is operated, a command electric signal transmitted from the operation lever 87 is transmitted to the controller 86.
The common bypass valve 8 is gradually closed by an electric signal such as a current value output from the controller 86, and the pump discharge amount is gradually increased by controlling the pump swash plate 1a.

At the same time, the push solenoid 57 of the meter-in valves A1IMV and A2IMV or the push solenoid 35 of the meter-out valves A3IMV and A4IMV is transmitted from the controller 86.
A command signal (current) corresponding to the operation lever amount is supplied to the push solenoids 57 and 35 to which the current is supplied, and a thrust is generated.
Pilot flow is generated by displacement against the spring force of 2, 34.

Thus, the pressure in the spring chamber 51 or the spring chamber 28 is reduced, the main poppet 41 on the meter-in side or the main poppet 22 on the meter-out side is lifted, and the rod side chamber 2r and the head side chamber 2h of the fluid pressure actuator 2 are moved from the pump 1. The hydraulic oil supplied to one of the valves and discharged from the other to the tank 7 is supplied to two meter-in valves A1IMV and A2.
It is controlled by a bridge circuit 3 formed by IMV and two meter-out valves A3IMV and A4IMV.

For example, meter-in valves A1IMV, A2IMV
The pilot spool 54 by the push solenoid 57
Is displaced against the return spring 62 and the sheet 56 is opened, whereby the passages 13, 43, 46 and the opening 47 of the variable slot 47 are opened.
a, spring chamber 51, passage 53, seat 56, spring chamber 61, passage 63,
When the pilot flow to the passage 15 via the check valve 64 and the passage 65 occurs, a pressure difference is generated around the opening 47a of the variable slot 47, and the main poppet 41 is returned by the return spring 52 due to the pressure difference.
, The seat 49 of the main poppet 41 is opened, and the working fluid (pressure oil) passing from the passage 11 through the passage 13 and the passage 15 is supplied to the head side chamber 2h of the fluid pressure actuator 2, and the load pressure P _load Occurs.

During the operation, when the load pressure P _load in the head side chamber 2h increases, the lower step portion of the load pressure sensor 77 facing the load pressure chamber 78 of the pilot spool 54 receives the increased load pressure P _load . The pilot spool
54 is displaced toward the neutral position above in the figure, and the opening degree of the poppet portion 69 with respect to the sheet 56 decreases.

Thus, the spring chamber on the main poppet 41
The inside of the main poppet 41 is pressurized, and the difference between the pressures acting on the upper and lower surfaces of the main poppet 41, that is, the differential pressure is reduced.
41 acts in the closing direction due to the restoring force of the return spring 52, preventing high-load driving. Even if the load pressure P _load rises sharply due to a sudden input operation of the operation lever 87, the feedback is fed back to the load pressure chamber 78. The pilot spool 54 is immediately returned to the neutral position side by the load pressure P _load , and accordingly, the main poppet 41 is immediately returned to the neutral position side.
Since the load pressure decreases in a responsive manner, fluctuations in the load pressure can be suppressed. This pressure control will be further described later.

On the other hand, meter-out valves A3IMV, A4IMV
The pilot spool 33 by the push solenoid 35
Is displaced against the return spring 34, and the seat 30 is opened, thereby opening the passage 15a, the opening 25a of the variable slot 25, the spring chamber 28, the passage 31, the seat 30, the spring chamber 24, the passage 32, and the tank passage 17. When the pilot flow to the tank 7 occurs, a differential pressure is generated around the opening 25a of the variable slot 25, and the differential pressure causes the main poppet 22 to be displaced against the return spring 29 and the seat 27 of the main poppet 22 to be displaced. The passage 15a and the seat 27 are opened from the head side chamber 2h of the fluid pressure actuator 2.
The working fluid (pressure oil) that has passed through the tank passage 17 and the tank 7
Is discharged to

During the operation, when the load pressure P _load in the head side chamber 2h increases, the upper step portion of the load pressure sensing portion 38 facing the load pressure chamber 39 of the pilot spool 33 receives the increased load pressure P _load. , Pilot spool
33 is displaced in a direction away from the sheet 30.

Thus, the spring chamber on the main poppet 22 is
28, the pressure difference acting on the upper and lower surfaces of the main poppet 22 increases, and the main poppet 22 returns to the return spring 29.
Acts in the opening direction against the restoring force of the load lever, and communicates the passage 15a with the tank 7. Therefore, even if the load pressure P _load rises rapidly due to a sudden input operation of the operation lever 87, the load pressure sensing unit
The load pressure P _load automatically decreases with a good response by the feedback of the load pressure to 38, so that this load pressure P _load
Can be suppressed.

The function of reducing the leak of the meter-in valves A1IMV and A2IMV will be described. The operation lever 87 is in the neutral position, and the command (current value) is transmitted to each push solenoid 57.
, The pilot spool 54 is in the neutral position as shown in FIG. Also, since the common bypass valve 8 is open and the pump discharge amount from the variable displacement pump 1 is also minimal, the pressure in the passage 13 is low.

In this case, the load pressure P equal to or higher than the pressure of the passage 13 is applied to the head side chamber 2h of the cylinder type hydraulic actuator 2.
If there is a _load , the high pressure is selected from the passage 15 by the shuttle valve 42, and the load pressure P _load is changed to the opening 47 of the variable slot 47.
a, the main poppet 41 on the meter-in side is pressed against the sheet 49 together with the spring force of the return spring 52, so that no leak from the passage 15 to the passage 13 occurs.

The load-hold check valve function of the meter-in valves A1IMV and A2IMV will be described. The operation lever 87 is operated, the common bypass valve 8 is closed, the pump discharge amount is increased, and the push solenoid 57 is operated. When a command (current value) is supplied from the controller 86 and acts in a direction to push the pilot spool 54, the poppet unit 69 opens the sheet 56.

At this time, if the load pressure P _{load of the} passage 15 is still higher than the pressure of the passage 13, the spring chamber 51 of the main poppet 41 is equal to the pressure of the passage 15 on the high pressure side, and the main poppet 41 is closed. As a result, this functions as a load hold check valve.

Further, when the common bypass valve 8 is closed and the pump discharge amount increases, the pump discharge pressure of the passage 13 eventually becomes higher than the load pressure P _load of the passage 15.

At this time, the high pressure of the passage 13 is selected by the shuttle valve 42 and acts on the poppet portion 69 of the pilot spool 54 from the spring chamber 51 of the main poppet 41, and this pressure is applied to the pressure of the passage 65 (= the passage 15). ), A pilot flow is generated from the passage 53 to the passage 65 through the seat 56, the spring chamber 61 and the check valve 64.

The main poppet 41 on the meter-in side is
Since it has a pilot flow amplification function, the pressure in the spring chamber 51 decreases as the pilot flow increases, and the flow control unit 48 of the main poppet 41 lifts from the seat 49,
Passage 15 from passage 13 due to the gradual increase in the opening area at the valve tip
, The main flow rate is controlled, and the cylinder type hydraulic actuator 2 is slowly extended.

Next, each part of the control system shown in FIG. 3 will be described together with its function.

(1) Load pressure estimation function In the bridge circuit 3 in which the supply side (meter-in side) pilot spool 54 and the discharge side (meter-out side) pilot spool 33 are independent, the pilot spool 54
When driving the pilot spool 33, the pilot spool 33 is on the non-drive side.When driving the pilot spool 33, the pilot spool 54 is on the non-drive side. The load pressure P _load is estimated by making a small displacement in a dead zone (dead band) near the neutral position that remains at zero.

For example, when the pilot spool 54 on the meter-in side is the non-drive side, the pilot spool 54 is slightly displaced downward. In this case, when the pilot spool 54 is displaced slightly downward by the displacement amount X, , FIG.
The upward acting force is the reaction force m · d ² X / dt when the pilot spool 54 having the mass m moves at the acceleration d ² X / dt ^2.
2 , viscous resistance C · dX / dt (C is a damping constant related to viscous resistance) when the pilot spool 54 moves in oil,
The repulsive force K · X (K is a spring constant) based on the compression amount X of the return spring 62, the mounting load R of the return spring 62, and the passage 15 to the passage 6
The load pressure P _load fed back to the load pressure chamber 78 in the shape of a donut area via 5, 79 is the pilot spool.
The force P _load · A _rea acting on the lower pressure receiving area A _rea of the load pressure sensor 77 of the 54 is a force acting downward in the figure when the current I flows through the push solenoid 57. And a tank line pressure Pt generated from a structure in which hydraulic oil is discharged from the plurality of bridge circuits 3 and 3a to the common tank 7 in the load pressure sensing unit 77.
The sequence by the force Pt · A _rea acting against the upper pressure receiving area A _rea, since the dead zone (dead band) around the neutral position of the pilot spool 54 is passing flow between the seat 56 and the poppet portion 69 does not occur It is not necessary to consider the flow force generated with this passing flow rate, and the upward force and the downward force are balanced, so that the following expression 3 is established.

[0107]

[Equation 3] m · d ² X / dt ² + C · dX / dt + K · X + R + P _load
A _rea = F + Pt · _{Area When} rewritten, the following equation 4 is obtained.

[0108]

[Equation 4] P _load = ΔF− (m · d ² X / dt ² + C · dX / dt + K
In · X + R) + Pt · A rea} / A re a This equation 4, m, C, K, R and A _rea are known constants, X, dX / dt and d ² X / dt ² is the displacement sensor 82 can be measured or calculated from the measured values,
F can be calculated from the solenoid current I and the tank line pressure P
Since t can be detected by a common pressure sensor, the load pressure P _load can be estimated by the above equation.

FIG. 4 is a block diagram of a load pressure calculator 92 for estimating and calculating such a load pressure.
The current I to the push solenoid 57 is converted into a pressing force F by a function 112. Since the pressing force F includes noise, the noise is removed by a noise filter 113. Then, each numerical value such as the pressing force F is input to the calculation unit 114, and the load pressure P _load is obtained by calculation.

Further, the load pressure calculating device 92 calculates the displacement X, speed dX / dt and acceleration d ² X of the pilot spool 54.
A noise filter 115 for removing noise from / dt ² is provided.

On the other hand, when the pilot spool 33 in the passage 15 on the meter-out side is the non-drive side, the load pressure P _load is similarly estimated by _slightly displacing the pilot spool 33 within the dead band. be able to.

As described above, the load pressure P is applied to the load pressure sensing portions 38, 77 formed stepwise on the pilot spools 33, 54.
_load by feeding back a load pressure calculating unit 92 is formed to estimate the load pressure P _load from the balance relationship between such thrust of the feedback force and the pilot spool 33,54.

In short, the load pressure calculating device 92 includes a supply side (pump side) pilot valve and a discharge side (tank side).
In the dead band near the neutral position where the flow rate of the pilot valve on the non-drive side becomes zero, the pilot valve on the non-drive side is slightly displaced to reduce the flow rate The load pressure P _load is taken into account without considering the flow force generated with the load and without using a pressure sensor for detecting the load pressure.
Can be estimated with high accuracy.

[0114] In (2) the flow rate control function the formula 1 Q = α · A · ( P P -P load) 1/2, the pump discharge pressure P _P is detected by the pump pressure sensor 88, the load pressure P _load in the load since it can be calculated by the pressure calculating unit 92, and supplies a drive current to push the solenoid 57 by the lever operation, by feedback-controlling the displacement X _C of the pilot spool 54 which is calculated by the function 93 and 94, previously described So that the displacement of the main poppet 41 is controlled
By controlling the opening area A of the 41, the flow rate Q at the main poppet 41 is realized, and the operating speed of the fluid pressure actuator 2 is controlled.

(3) Pressure control function For example, when the load pressure P _load in the head side chamber 2h of the fluid pressure actuator 2 increases, the pilot spool
The lower step portion of the load pressure sensor 77 facing the load pressure chamber 78 of 54 receives the load pressure P _load and receives the pilot pressure.
Is displaced upward in the figure. As a result, the degree of opening of the poppet portion 69 with respect to the seat 56 is reduced, and high-load driving is prevented.

Even when the discharge pressure from the pump 1 is higher than the load pressure to be driven, even when the poppet portion 69 is open, the pilot spool 54 is in the neutral position (the closed position shown in the figure) even when the poppet 69 is open. When the poppet unit 69 closes the sheet 56, the load pressure P _load
Can be prevented from rising to the pump discharge pressure.

Further, the load pressure is fed back to the load pressure sensor 77 provided in the pilot spool 54 in a stepped shape, and the load pressure is applied to the flow control mechanism of the main poppet 41 controlled by the pilot spool 54. A load pressure feedback mechanism for feeding back is formed, and the load pressure can be controlled to a set value by the main poppet 41.

Referring to FIG. 5, when the actual load pressure suddenly rises and protrudes in response to the step input of the operation lever 87, the pilot spool 54 moves the load pressure as shown in the characteristic curve of the actual pilot spool displacement. It is returned to the neutral position side by the load pressure feedback mechanism such as the sensing unit 77. Along with this, the main poppet 41 is also returned to the neutral position side as shown in the characteristic curve of the actual main poppet displacement, and the actual load pressure decreases with a good response, so that the fluctuation of the load pressure can be suppressed.

At this time, the load pressure P to be driven
_{The load} is adjusted by the thrust of the push solenoid 57, that is, the drive current.

That is, since the load pressure P _load can be estimated by the load pressure calculating device 92, the pilot spool
The thrust against the load pressure P _load is adjusted by using a push solenoid 57 connected to 54.

For example, when the pressure feedback controller 101 raises the thrust of the push solenoid 57, the thrust is applied to the feedback force by the opposing load pressure P _load (acts on the lower pressure receiving surface of the load pressure sensing unit 77). By temporarily reducing the pressure slightly (upward force), the pilot spool 54 can be returned to the neutral position with good response, and the load pressure can be controlled so as not to exceed the set pressure.

This is indicated by a solid line in FIG.
When the thrust of the push solenoid 57 rises in response to the step input of 87, the input current value to the push solenoid 57 is temporarily reduced immediately after the rise, and the thrust is reduced from the feedback force by the load pressure P _load. By operating the pilot spool 54 in the closing direction and temporarily increasing the pressure in the spring chamber 51 of the main poppet 41 to suppress the opening operation of the main poppet 41, the load pressure P _load does not overshoot the set pressure. By controlling the pressure as described above, the stability of the control system can be improved. The dotted line indicates an overshoot state.

As described above, without using a pressure control valve such as a relief valve for each fluid pressure actuator and without using a pressure sensor for detecting a load pressure,
By controlling the thrust of the push solenoid 57, that is, the drive current, the main poppet which is also a flow control means
The load pressure P _load can be adjusted by 41.

Conventionally, a method of measuring the load pressure using a pressure sensor or the like and electrically controlling the throttle of the pilot spool to control the load pressure so as not to exceed a preset pressure is also available. However, there is a problem that the control system becomes unstable due to a delay in calculation of feedback.

(4) Return Spring Force Adjustment Function To explain with the meter-in valve A2IMV, a gain adjustment device
According to 97, the load pressure P _loadAccording to pilot spool
Controls the value of the current supplied to the 54 push solenoid 57
Increase or decrease the thrust of the push solenoid 57
The spring force of the return spring 62 (spring constant)
Number) is substantially adjusted.

For example, in a region where the load pressure P _load is high,
That is, in a region where the feedback force to the load pressure sensing unit 77 is large, the gain of the current value supplied to the push solenoid 57 by the gain adjusting device 97 is reduced, and the thrust of the push solenoid 57 is reduced, whereby the spring of the return spring 62 is reduced. The force (spring constant) is corrected to be relatively large. As a result, displacement of the pilot spool 54 due to a change in load pressure is suppressed, and the stability of the control system is improved.

On the other hand, in the region where the load pressure P _load is low, the gain of the current value supplied to the push solenoid 57 by the gain adjusting device 97 is increased, and the push solenoid 57
Is increased so that the spring force (spring constant) of the return spring 62 is relatively reduced. As a result, even a small change in load pressure is feedback-sensed with high sensitivity, control accuracy is improved, and responsiveness of pressure control is improved.

In particular, the load pressure P
_{When the load} is fed back and the load pressure is estimated by the load pressure calculating device 92 from the balance between the thrust acting on the pilot spool 54, the spring force, and the feedback force, the load pressure can be estimated by using this gain adjustment method. Accuracy can be improved.

As described above, by controlling the current value gain supplied to the push solenoid 57 by the gain adjusting device 97 in accordance with the load pressure P _load estimated by the load pressure calculating device 92, the thrust can be controlled. For example, the spring constant of the return spring 62 of the pilot spool 54 can be substantially variably controlled, the stability of the control system, control accuracy and responsiveness can be improved, and smooth operability can be obtained.

This spring force adjustment is performed by the meter-out valve A3.
For example, in the meter-out valve A4IMV, in a region where the load pressure P _load is high, that is, in a region where the load pressure P _load fed back from the passage 36 to the load pressure sensing unit 38 is large, the return spring is used. The gain of the current value supplied to the push solenoid 35 by the gain adjusting device (corresponding to 97 but not shown) is reduced so that the thrust of the push solenoid 35 is increased so that the spring force (spring constant) of the push solenoid 35 becomes relatively large. , The displacement of the spool with respect to the fluctuation of the load pressure is suppressed, and the stability of the control system is improved.

On the other hand, in the region where the load pressure P _load is low, the push solenoid is operated by the gain adjusting device so that the spring force (spring constant) of the return spring 34 becomes relatively small.
By increasing the gain of the current value supplied to 35 and correcting so as to increase the thrust of the push solenoid 35, even a slight change in load pressure can be feedback sensed with high sensitivity,
Control accuracy and load pressure estimation accuracy are improved, and pressure control response is improved.

(5) Workload Estimating Function of Construction Machine As shown in FIG. 7, a hydraulic shovel as a working machine has a working arm as a movable body (hereinafter, this working arm is referred to as a front working device FL). The front working device FL is rotatably supported in a vertical direction. The front working device FL includes a hydraulic actuator (hereinafter, this hydraulic actuator is connected to a boom cylinder 2).
BM).

[0133] The workload estimator 102, in such loading operation by the hydraulic excavator, to estimate bucket load as a working load (sediment load) W _L as follows.

[0134] often during work it is moving boom cylinder 2BM, since the load pressure P _load generated on the head side of the boom cylinder 2BM affected by inertial loads, in order to precisely estimate the bucket load W _L Must remove the effects of inertial loading.

Therefore, first, the time series data of the load pressure P _load of the boom cylinder 2BM is indirectly measured by the load pressure calculating device 92 as the load pressure measuring means, and continuously as shown in FIG. from the time-series data of the measured load pressure P _load, subtracted by extracting a predetermined range of frequency components is affected by inertial loads (ω ₀ ~ω _1), with a load pressure P _load after the deduction bucket to estimate the internal load W _L.

A predetermined range of frequency components (ω
_{0 ~ω 1)} extracts by passing predetermined time the time-series data of the load pressure P _{lo ad} measured to the band-pass filter 121, the frequency component of the extracted predetermined range (omega ₀
To ω ₁ ) is subtracted from the time-series data of the measured load pressure P _load by the subtractor 122 as a predetermined frequency removal operation unit, thereby removing the influence of the inertial load.

The reason why the band-pass filter 121 is used only for a certain period of time is to improve the follow-up performance thereafter.

In this case, the band width (ω _{0 to} ω ₁ ) of the band-pass filter 121 is adjusted to the natural frequency of the front working device FL. Thereby, the inertial load due to the natural vibration of the front working device FL can be effectively removed.

As shown in FIG. 9, the band-pass filter 121 cuts frequencies below ω ₀ by the differential element 123 and cuts frequencies above ω ₁ by the low-pass filter 124 so that the frequency (Ω ₀ ~
ω ₁ ).

The frequency component (ω ₀
~ Ω ₁ ) is subtracted from the load pressure P _load to the workload calculation unit 1
Type 25, estimated by workload i.e. calculating the bucket load W _L is within leading bucket of the front working mechanism FL.

That is, in the workload calculation unit 125,
Measuring the attitude of the front working mechanism FL at rotation angle detector provided in each rotation shaft portion of the front working mechanism FL to seek (X, Z) coordinates of the bucket in the load W _L, the impact of the inertial load a load pressure P _load in the head side chamber of the boom cylinder 2BM excluding preparative, in the load W _L bucket (X, Z) from the coordinate values, the bucket load _{W L, W L = f (} P load, X,
Z).

[0142] The bucket load W _L, by integrating computed for each task, for example, the total weight loading, such as earth and sand for transportation vehicles easily calculated, without using a special load sensor, the permissible weight Excess can be prevented.

FIG. 10 shows the time series data of the load pressure P _load affected by the inertial load by the dotted line, and the frequency components (ω ₀ to ω ₀ ) of the predetermined range extracted through the band-pass filter 121 by the solid line. ω ₁ ), the time series data of the load pressure P _load removed, that is, the front working device
4 shows time-series data of a load pressure P _{load from} which the influence of an inertial load on FL has been removed.

As described above, even during the operation of loading the hydraulic excavator and the like, the influence of the inertial load of the front working device FL is eliminated while the boom cylinder 2BM is operating.
The load pressure P _{load of the} cylinder is accurately estimated, and from the load pressure P _{load of the} cylinder and the attitude of the front working device FL,
The bucket load W _L can be determined quickly and accurately.

Next, the load pressure of the boom cylinder 2BM estimated with high accuracy by eliminating the influence of the inertial load by the work load estimating device 102 is taken into the pressure feedback controller 101 and used for pressure control. Simulation results of the control are shown in FIGS.

(Simulation conditions) (1) Initial cylinder load: 0 Pa (assuming a situation where the bucket is placed on the ground) (2) Initial pump load: 20 × 9.81 × 10 ⁴ Pa, provided that the pump discharge pressure after lever operation It is assumed that the main relief valve 9 is controlled so as to be higher than the actual cylinder load pressure by 20 × 9.81 × 10 ⁴ Pa or more.

(3) Lever input: Start simulation
Step input (100%) 0.2 seconds later, provided that lever input is passed through a secondary low-pass filter of 20 Hz.

(4) Cylinder load pressure: 100 × 9.81 × 10 ⁴
Pa, provided that the cylinder load pressure is generated immediately after the cylinder starts moving.

FIG. 11 is a step response characteristic diagram showing simulation results of the actual main poppet displacement, the required main poppet displacement, the actual pilot spool displacement, and the required pilot spool displacement with respect to the step input of the operating lever to the pressure control system. .

A: Operation lever position B: Actual main poppet displacement C: Requested main poppet displacement D: Actual pilot spool displacement E: Requested pilot spool displacement ・ FIG. 12 shows an actual cylinder in response to a step input of the operating lever to the pressure control system. FIG. 9 is a step response characteristic diagram showing simulation results of speed and actual cylinder displacement.

F: Actual cylinder speed G: Actual cylinder displacement ・ FIG. 13 shows each of actual main poppet displacement, required main poppet displacement, actual pilot spool displacement, and required pilot spool displacement in response to the step input of the operating lever to the flow control system. It is a step response characteristic diagram showing a simulation result.

A ': Operation lever position B': Actual main poppet displacement C ': Required main poppet displacement D': Actual pilot spool displacement E ': Required pilot spool displacement ・ FIG. 14 shows the operation lever operation to the flow control system. FIG. 9 is a step response characteristic diagram showing simulation results of an actual cylinder speed and an actual cylinder displacement with respect to a step input.

F ': Actual cylinder speed G': Actual cylinder displacement (Simulation result) When comparing the simulation result of FIG. 11 with the simulation result of FIG. 13, the fluctuation of the load pressure is smaller in the pressure control than in the flow control. Moreover, it can be seen that the convergence is quick. This is because when the load pressure is high, the pilot spool 54 is in the neutral position (closed position).
This is because the opening of the main poppet 41 is reduced, and the load pressure is thereby reduced.

Further, comparing the simulation result of FIG. 12 with the simulation result of FIG. 14, the cylinder speed change is smoother in the pressure control than in the flow control.
The fluid pressure actuator 2 can be operated smoothly.

[0155]

According to the first aspect of the present invention, when the load pressure increases, the load pressure is directly fed back to the pilot valve, and the pilot valve is displaced by the feedback force in the pilot flow decreasing direction. Because the main valve is controlled in the main flow decreasing direction, and the load pressure decreases in a responsive manner, high load driving can be prevented without detecting the load pressure using a pressure sensor,
It is possible to suppress the fluctuation of the load pressure and to ensure the stability, prevent the instability due to the calculation delay when feeding back the load pressure from the conventional pressure sensor via the calculation system, and control the pressure to converge in a short time. .

According to the second aspect of the present invention, the load pressure to be driven can be adjusted by adjusting the external thrust against the load pressure.

According to the third aspect of the present invention, when the thrust against the load pressure is raised, the thrust is temporarily reduced from the feedback force due to the load pressure, thereby returning the pilot valve to the neutral position with good response. And the stability of the control system can be improved.

According to the fourth aspect of the invention, when the load pressure increases, the load pressure is directly fed back to the pilot valve by the load pressure feedback mechanism, and the pilot valve is displaced in a pilot flow decreasing direction by the feedback force. As a result, the main valve is displaced in the main flow rate decreasing direction to reduce the load pressure with a good response, so that it is possible to provide a pressure control device that can prevent high load driving, suppress fluctuations in the load pressure, and ensure stability.

According to the fifth aspect of the present invention, there is provided a pressure control device capable of adjusting the load pressure to be driven by controlling the driving means of the pilot valve to adjust the thrust of the driving means against the load pressure. it can.

According to the sixth aspect of the present invention, when the thrust of the driving means is raised by the controller, the thrust of the driving means is temporarily reduced from the feedback force due to the load pressure, so that the pilot valve is operated by the load pressure. It is possible to provide a pressure control device that can return to the neutral position with good response and improve the stability of the control system.

[Brief description of the drawings]

FIG. 1 is a sectional view showing an embodiment of a pilot valve and a main valve according to a pressure control device of the present invention.

FIG. 2 is a fluid pressure circuit diagram showing an embodiment of a bridge circuit according to the pressure control device.

FIG. 3 is a block diagram showing an embodiment of a combined pressure-flow rate control system according to the pressure control device.

FIG. 4 is a block diagram showing an example of a load pressure calculating device according to the pressure control device.

FIG. 5 is a characteristic diagram showing an operation example of a load pressure feedback mechanism according to the pressure control device.

FIG. 6 is a characteristic diagram illustrating an example of a pressure control method according to the pressure control device.

FIG. 7 is an explanatory diagram for explaining a function of a workload estimation device according to the pressure control device.

FIG. 8 is a block diagram showing an example of the workload estimation device.

FIG. 9 is a block diagram illustrating an example of a bandpass filter in the workload estimation device.

FIG. 10 is a characteristic diagram illustrating an example of a function of removing an influence of an inertial load by the work load estimation device.

FIG. 11 is a step response characteristic diagram showing simulation results of main poppet displacement and pilot spool displacement with respect to a step input of an operation lever to a pressure control system.

FIG. 12 is a step response characteristic diagram showing a simulation result of a cylinder speed and a cylinder displacement with respect to a step input of an operation lever to a pressure control system.

FIG. 13 is a step response characteristic diagram showing simulation results of main poppet displacement and pilot spool displacement with respect to a step input of an operation lever to a flow control system.

FIG. 14 is a step response characteristic diagram showing a simulation result of a cylinder speed and a cylinder displacement with respect to a step input of an operation lever to a flow control system.

FIG. 15 is a circuit diagram showing a hydraulic actuator control circuit including a bridge circuit.

FIG. 16 is a circuit diagram showing a load pressure feedback mechanism using a conventional pressure sensor.

[Explanation of symbols]

22, 41 Main poppet as main valve 33, 54 Pilot spool as pilot valve 35, 57 Push solenoid as driving means 36, 79 Passage of load pressure feedback mechanism 38, 77 Load pressure sensing unit of load pressure feedback mechanism 86 Controller

 ──────────────────────────────────────────────────続 き Continued on the front page F term (reference) 2D003 AA01 AB03 AC09 BA01 DA03 DA04 DB01 DB02 DB05 DC02 DC03 DC05 5H316 AA09 AA18 BB09 CC08 DD01 EE02 EE10 EE12 ES02 ES05 ES06 FF01 FF37 GG03 HH04 HH08 HH10 KK03 KK03 KK03

Claims (6)

[Claims] 1. A main valve for controlling a main flow rate is pilot-operated by controlling a pilot flow rate by a pilot valve, a load pressure of the main flow rate is fed back to the pilot valve, and a pilot flow rate is reduced by increasing the load pressure. A pressure control method characterized in that the main valve is controlled in the main flow decreasing direction by decreasing the pilot flow to reduce the load pressure. 2. The pressure control method according to claim 1, wherein the load pressure is adjusted by controlling an external thrust acting on the pilot valve from a direction opposite to the load pressure fed back to the pilot valve. . 3. The pressure control method according to claim 2, wherein the thrust is temporarily reduced from the feedback force due to the load pressure when the external thrust is raised. 4. A pilot valve for controlling a pilot flow rate, a main valve for controlling a main flow rate pilot-operated by the pilot valve, and a load pressure of the main flow rate being fed back to the pilot valve to increase the load pressure so that the pilot valve is controlled. A pressure control device, comprising: a load pressure feedback mechanism for reducing a load pressure by controlling a main valve in a main flow decreasing direction by displacing in a flow decreasing direction. 5. The pressure as set forth in claim 4, further comprising driving means for adjusting the load pressure by controlling the thrust acting on the pilot valve from a direction opposite to the load pressure fed back to the pilot valve. Control device. 6. The pressure control device according to claim 5, further comprising a controller for temporarily reducing the thrust of the driving means from the feedback force due to the load pressure when the thrust of the driving means is started.