Information
-
Patent Grant
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6250202
-
Patent Number
6,250,202
-
Date Filed
Friday, October 1, 199925 years ago
-
Date Issued
Tuesday, June 26, 200123 years ago
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Inventors
-
Original Assignees
-
Examiners
- Look; Edward K.
- Leslie; Michael
Agents
-
CPC
-
US Classifications
Field of Search
US
- 091 444
- 091 448
- 091 451
- 091 459
- 060 399
- 060 403
- 060 406
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International Classifications
-
Abstract
A hydraulic control arrangement which has a directional control valve, a hydraulic pump and a two-way cartridge valve constructed as a seat valve. The directional control valve is connected to an inlet line and to a discharge line leading to a tank. Leading off from it is a load line leading to a hydraulic load. The hydraulic pump draws pressure medium from a tank and discharges it into the inlet line. The two-way cartridge valve is arranged in the inlet line and, in a closed position, isolates a second inlet line section leading off from the latter to the directional control valve from a first inlet line section running between the two-way valve and the hydraulic pump. A control piston of the two-way cartridge valve has an annular opening surface exposed to the pressure in the first inlet line section, a central circular opening surface exposed to the pressure in the second inlet line section, and a closing surface, which can be subjected to the pressure in the first inlet line section via a pilot valve in a first position of the latter and can be relieved from the pressure to the tank via the pilot valve in a second position of the latter. The two-way cartridge valve closes when an emergency off facility is triggered. To satisfy particularly high safety requirements, the invention makes provision for the second inlet line section to be relieved to the tank via the pilot valve in the first position of the latter.
Description
FIELD AND BACKGROUND OF THE INVENTION
The invention relates to a hydraulic control arrangement.
A hydraulic control arrangement known, for example, from DE 196 19 860 A1. This document describes a hydraulic control arrangement which is used on a die-casting machine and in which a directional control valve is used to shut off a load line leading from the latter to a pressure space of a hydraulic cylinder, to connect it to a discharge line leading to a tank or connect it to an inlet line. The inlet line is fed by a hydraulic pump which draws pressure medium from the tank. Arranged in the inlet line is a two-way cartridge valve designed as a seat valve, which allows a first inlet line section running between the hydraulic pump and the two-way cartridge valve to be isolated from a second inlet line section leading off from the two-way cartridge valve to the directional control valve. When the control piston of the two-way cartridge valve is seated on its seat, the two inlet line sections are isolated from one another. The valve used is a conventional two-way cartridge valve with a directional control function, the control piston of which has two opening surfaces acting in the opening direction, one of which is situated centrally on the control piston, corresponds in diameter to the seat diameter and is exposed to the pressure in the second inlet line section. The second opening surface is an annular surface, the inside diameter of which corresponds to the seat diameter and the outside diameter of which corresponds to the guiding diameter of the control piston and which can be subjected to the pressure in the first inlet line section. On the control piston there is also a closing surface which acts in the closing direction and which is exposed to the pressure in a rearward control space of the two-way cartridge valve. Together, the two opening surfaces are as large as the closing surface.
In a rest position, which it assumes under the action of a compression spring, a pilot valve connects the rearward control space to the first inlet line section. In this position of the pilot valve, the two-way cartridge valve, the control piston of which is usually additionally acted upon in the closing direction by a spring, cannot be opened by the pressure in the first inlet line section and by the pressure in the second inlet line section, which is normally not greater than the pressure in the first inlet line section. By energizing an electromagnet, the pilot valve can be switched to a position in which it connects the rearward control space at the control piston to the tank. The pressure prevailing in the first inlet line section and acting on the annular surface of the control piston can now raise the control piston from the seat against the, generally weak, closing spring and open the two-way cartridge valve.
It is possible to implement an emergency off facility with the valve described. In normal operation, the electromagnet of the pilot valve is excited and the two-way cartridge valve is open. If an emergency occurs, an electric switch can be actuated, for example, interrupting the power supply to the electrical systems, with the result that the electromagnet of the pilot valve is also separated from the power supply. The pilot valve moves into its rest position by virtue of the compression spring and connects the rearward control space at the control piston to the first inlet line section, with the result that the two-way cartridge valve closes and interrupts the flow of pressure medium to the directional control valve in a leak-free manner.
DE 44 20 459 A1 has disclosed a hydraulic control arrangement, based on the load-sensing principle, which, for emergencies, likewise has a valve by means of which a second inlet line section can be isolated from a first inlet line section. The isolating valve, which can be controlled by means of an electromagnetically actuable pilot valve, is clearly a spool valve which, in the rest position of the pilot valve, not only separates the two inlet line sections from one another but also connects the load-indicating line to the tank and hence relieves it. The pressure in the second inlet line section is also dissipated via the load-indicating line if the load-sensing directional control valve is in a working position to the side of its central position in which there is an aperture cross section between the second inlet line section and the load-indicating line.
DE 43 24 177 A1 has disclosed a hydraulic control arrangement, based on the load-sensing principle, in which, after an emergency-off signal has been triggered, an isolating valve isolates two inlet line sections from one another, shuts off the load-indicating line and connects a load-indicating port on the regulator of the variable-displacement pump to the tank. The isolating valve is again a spool valve.
SUMMARY OF THE INVENTION
It is the object of the invention to develop a hydraulic control arrangement of the above type in such a way that high safety requirements are met by simple means.
According to the invention, this object is achieved by virtue of the fact that, in a hydraulic control arrangement of the above type wherein the second inlet line section can be relieved to the tank via the pilot valve in the first position of the latter. This ensures that, once an emergency-off signal has been triggered, there is no longer any pressure in the second inlet line section in each position of the directional control valve. A force acting on the second opening surface, which attempts to raise the control piston from its seat, thus disappears, with the result that the control piston is pressed onto its seat by a large excess force and closes very tightly. No pressure medium is trapped in the second inlet line section, pressure which in adverse circumstances could be relieved to a load and lead to a dangerous small movement of the hydraulic load.
The increasing relief of the second opening surface from pressure with increasing closing displacement of the control piston leads to particularly rapid closure of the two-way cartridge valve and hence to an immediate stoppage of the flow of pressure medium to the directional control valve.
A hydraulic control arrangement according to the invention is particularly advantageous if, the directional control valve is hydraulically actuable and the control oil for actuation is taken from the second inlet line section. The pressure relief of the second inlet line section causes the control pressure to fall and there is thus nothing to oppose the return of the spool of the directional control valve into its rest position. Given electrohydraulic actuation of the directional control valve, there is no need to switch off the electric pilot control valves.
BRIEF DESCRIPTION OF THE DRAWINGS
A number of embodiment examples of a hydraulic control arrangement according to the invention are illustrated in the form of circuit diagrams in the drawings. The invention will now be explained in greater detail with reference to the figures in these drawings, in which
FIG. 1
shows a first embodiment example, which is based on the load-sensing principle, the source of pressure medium being in the form of a constant-displacement pump with a pressure compensator under load-sensing control in the bypass to the tank,
FIG. 2
shows a variable-displacement pump with a load-sensing controller, which can be used instead of the constant-displacement pump and the bypass pressure compensator shown in
FIG. 1
, and
FIG. 3
shows a second embodiment example with a constant-displacement pump as the source of pressure medium and six-way directional control valves with a circulation passage.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
In the embodiment shown in
FIG. 1
, a control block
10
contains two directional control valve sections
11
and
12
, each of which has a directional control valve
13
with an inlet chamber
14
, to which pressure medium can flow from a hydraulic pump
18
, a discharge chamber
15
, which is connected to a tank
19
, and two load chambers
16
and
17
, which are connected by load lines to a double-acting hydraulic load, e.g. a differential cylinder, which is not shown specifically. The spool
27
of a directional control valve
13
can be displaced in opposite directions from a central position, in which the inlet chamber, the discharge chamber and the two load chambers are shut off from one another, into working positions in which a metering restrictor
20
between the inlet chamber
14
and load chamber
16
or load chamber
17
is open and the other load chamber respectively is connected to the discharge chamber
15
. Connected upstream of the inlet chamber
14
are a load-holding valve
21
and an individual pressure compensator
22
, the control piston of which is adjoined by two control spaces
23
and
24
. Control space
23
is connected to a load-indicating chamber
25
of the directional control valve
13
, and control space
24
is connected via the load-holding valve to the inlet chamber
14
. In the central position of the spool
27
, the load-indicating chamber
25
is relieved to the tank and, in a lateral working position, is in each case connected to the load chamber to which pressure medium is fed via the metering restrictor
20
. The control piston of the pressure compensator
22
is loaded in the opening direction by a compression spring
26
and by the pressure prevailing in control space
23
and loaded in the closing direction by the pressure prevailing in control space
24
.
A series of changeover valves
30
is used to apply the highest pressure prevailing in a control space
23
, i.e. the highest load pressure in each case, to an output LS of the control block
10
and indicate it via a load-indicating line
31
, in which there is a restrictor
32
, to a bypass pressure compensator
33
which in each case allows enough of the pressure medium delivered by the hydraulic pump
18
to flow off to the tank
19
to ensure that the pump pressure established in an inlet-line section
34
which starts from the hydraulic pump
18
and via which pressure medium can be fed to the inlet chambers
14
of the directional control valves
13
, is more than the indicated highest load pressure by a certain pressure difference.
The two directional control valves
13
can each be actuated electrohydraulically, for which purpose two electromagnetically operated pilot control valves
40
are integrated into each directional control valve section
11
and
12
respectively. In the rest position of a valve
40
, an associated control space on the spool
27
of a directional control valve
13
is relieved to a leakage-oil passage
41
which passes through directional control valve sections
11
and
12
.
By excitation of an electromagnet, one control space is connected to a control-pressure line
42
, which likewise passes through directional control valve sections
11
and
12
. The control oil is taken by means of a pressure-reducing valve
43
contained in an end plate
44
mounted on directional control valve section
12
from a passage which passes through the two directional control valve sections
11
and
12
and into the end plate
44
and which forms a second inlet line section
60
together with branch lines each connected to the inlets of the pressure compensator
22
. The pressure-reducing valve
43
is, for example, set to a control pressure of 20 bar.
Connected to directional control valve section
11
is a safety block
51
, which has a two-way cartridge valve
52
, an associated pilot valve
53
and a series of pressure-medium passages. The control piston
54
of the two-way cartridge valve
52
is a differential piston which is guided axially by means of a piston section
55
and can come to rest axially on a seat
57
by means of a piston section
56
of smaller diameter in order to close an axial outlet
58
. The first inlet line section
34
is connected to the radial inlet
59
and hence to the annular space around piston section
56
. The second inlet line section
60
, which is continued in directional control valve sections
11
and
12
as a through passage, starts from the axial outlet
58
. The control piston
54
is acted upon in the closing direction by a force which is produced by a control pressure in a rearward control space
61
at a closing surface
62
equal in area to the cross-sectional area of the large piston section
55
, and by the force of a relatively weak closing spring
63
. A pressure in the first inlet line section
34
acts in the opening direction of the control piston
54
on an annular surface
64
and a pressure in the second inlet line section
60
acts on a circular surface
65
equal in area to the cross-sectional area of the small piston section
56
in the opening direction of control piston
54
. The sum of the two areas
64
and
65
is equal to the size of surface
62
.
The pilot valve
53
is a 4/2-way valve which, under the action of a compression spring
69
, assumes a rest position, in which it connects the rearward control space
61
at the control piston
54
to the first inlet line section
34
and relieves the second inlet line section
60
to the tank
19
via a passage
70
. By activation of an electromagnet
71
, the pilot valve
53
can be switched to a position in which it connects a rearward control space
61
to the passage
70
, i.e. relieves it to the tank and, since it is a standard component, connects the first inlet line section
34
to the second inlet line section
60
.
In normal operation, the electromagnet
71
is excited, with the result that the pilot valve
53
assumes the second position. Since tank pressure prevails in the rearward control space
61
, the pump pressure acting on the annular surface
64
is able to raise the control piston
54
from the seat, allowing pressure medium to pass from the first inlet line section
34
to the second inlet line section
60
virtually without loss of pressure. If all the directional control valves
13
are in their central position, tank pressure prevails in the load-indicating line
31
and the pressure compensator
33
adjusts the pressure in the inlet line sections to, for example, 20 bar, which is equivalent to the force of a compression spring
35
acting on the control piston of the pressure compensator in the closing direction together with the pressure prevailing in the load-indicating line
31
. If one directional control valve is now switched to a working position, the load pressure is indicated to the pressure compensator
33
, which closes the bypass to the tank
19
to such an extent that a pump pressure that is 20 bar above the load pressure builds up in the inlet line
34
,
60
. If both directional control valves are actuated, the highest load pressure is indicated to the pressure compensator
33
.
The intention is that it should be possible, in a dangerous situation, to interrupt the flow of pressure medium from the hydraulic pump
18
to the directional control valves
13
from one or more points on a machine equipped with the hydraulic control arrangement shown, e.g. a multi-bucket vehicle. For this purpose, electrical switches (not shown specifically) are mounted at said points, these switches allowing connection of the electromagnet
71
of the pilot valve
53
to a power supply network in a rest position. The power supply to the electromagnet
71
is interrupted by operating one of the electrical switches, with the result that the pilot valve
53
moves into its rest position under the action of the compression spring
69
. As a result, the rearward control space
61
is subjected to the pressure prevailing in the first inlet line section
34
, causing the cartridge valve
52
to close. The second inlet line section
60
is relieved to the tank, and the pressure on the opening surface
65
thus falls rapidly during the closing operation. This leads to a rapid closing operation. Since the opening surface
65
is finally completely relieved of pressure, a large excess force in the closing direction acts on the control piston
54
and the control piston
54
thus rests firmly on its seat and shuts off the second inlet line section
60
from the first inlet line section
34
in a leak-free manner. Relieving the second inlet line section
60
also allows the control pressure in the control-pressure line
42
to fall, and the directional control valves thus return to the central position even if one pilot control valve
40
remains active.
In the central position of the directional control valve
13
, the load-indicating line
31
is relieved to the tank, and the pump
18
thus delivers to the tank via the pressure compensator
33
at a low pressure of 20 bar.
In the embodiment shown in
FIG. 2
, a variable-displacement pump
75
with a load-sensing controller
76
is used instead of a constant-displacement pump
18
and a bypass pressure compensator
33
. All the other components are the same as those in FIG.
1
and it is thus unnecessary to describe the embodiment in
FIG. 2
further.
The embodiment shown in
FIG. 3
also has a control block
10
with two directional control valve sections
11
and
12
and an end plate
44
. Here, each directional control valve section
11
contains a
6
-way throttle valve
80
of a commonly known type of construction with a circulation passage and a load-holding valve
81
. The directional control valves
80
can be activated electrohydraulically with the aid of pilot control valves
40
. Control oil is taken by the pressure-reducing valve
43
accommodated in the end plate
44
from an inlet passage which extends through the directional control valve sections
11
and is part of the second inlet line section
60
and discharged into a control-pressure passage
42
. To enable a control pressure to be built up at all starting from the central position of the directional control valve
80
, the circulation passage is subjected to a preload by means of a nonreturn valve
82
.
The same safety block
51
as in the embodiment shown in
FIG. 1
is attached to directional control valve section
11
and attention is therefore drawn to the relevant description of FIG.
1
.
A constant-displacement pump
18
protected by a pressure relief valve
83
is used as the source of pressure medium. The pump
18
draws pressure medium from a tank
19
and discharges it into a first inlet line section
34
, which is connected to the radial inlet
59
of the cartridge valve
52
. The second inlet line section
60
once again starts from axial outlet
58
of the cartridge valve
52
.
In normal operation, the cartridge valve
52
is open, with the result that the pressure medium delivered by the hydraulic pump
18
is either fed back completely to the tank via the circulation passage or, after actuation of a directional control valve, passes completely or in part to a hydraulic load. In an emergency, the electromagnet
71
is de-energized by actuation of an electric switch, causing the pilot valve
53
to assume its rest position and the cartridge valve
52
to close. The second inlet line section
60
is isolated from the first inlet line section
34
and relieved to the tank. As in the case of the embodiment example shown in
FIG. 1
, the control pressure collapses. The directional control valves
80
move into their central position.
Claims
- 1. A hydraulic control arrangement with a directional control valve (13, 80) which is connected to an inlet line (34, 60) and to a discharge line leading to a tank (19) and from which a load line leads off to a hydraulic load, with a hydraulic pump (18, 75), by which pressure medium can be drawn from the tank (19) and discharged into the inlet line (34, 60), and with a two-way cartridge valve (52), which is constructed as a seat valve, is arranged in the inlet line (34, 60) and, in a closed position, isolates a second inlet line section (60) leading off from it to the directional control valve (13, 80) from a first inlet line section (34) running between it and the hydraulic pump (18, 75) and which has a control piston (54), with an annular opening surface (64) exposed to the pressure in the first inlet line section (34), with a central annular opening surface (65) exposed to the pressure in the second inlet line section (60), and with a closing surface (62), which can be subjected to the pressure in the first inlet line section (34) via a pilot valve (53) in a first position of the latter and can be relieved to the tank (19) via the pilot valve (53) in a second position of the latter, and wherein the second inlet line section (60) can be relieved to the tank (19) via the pilot valve (53) in the first position of the latter.
- 2. The hydraulic control arrangement as claimed in claim 1, wherein the directional control valve (13, 80) is hydraulically actuatable and the control oil for actuation is taken from the second inlet line section (60).
Priority Claims (1)
Number |
Date |
Country |
Kind |
197 14 141 |
Apr 1997 |
DE |
|
PCT Information
Filing Document |
Filing Date |
Country |
Kind |
102e Date |
371c Date |
PCT/EP98/01809 |
|
WO |
00 |
10/1/1999 |
10/1/1999 |
Publishing Document |
Publishing Date |
Country |
Kind |
WO98/45603 |
10/15/1998 |
WO |
A |
US Referenced Citations (2)
Foreign Referenced Citations (8)
Number |
Date |
Country |
3605113 |
Aug 1987 |
DE |
3710699 |
Aug 1988 |
DE |
4226893 |
Feb 1994 |
DE |
4324177 |
Feb 1994 |
DE |
4239109 |
Jun 1994 |
DE |
4320490 |
Dec 1994 |
DE |
4420459 |
Jan 1995 |
DE |
196 19 860 |
Dec 1996 |
DE |