[0001] The invention relates to a device for controlling a piloting pressure, in particular
the piloting pressure of a balance valve.
[0002] The prior art contains hydraulic activating circuits for hydraulic actuators, for
example for a cylinder of an arm of a lifting apparatus, in which a first circuit
branch connects a hydraulic distributor, in turn associated to a pump, with the chamber
of the actuator being associated to the lifting of the load and a second branch connects
the distributor with the chamber associated to the descent of the load. The circuit
is provided with a balance valve predisposed for controlling the fluid flow along
the first branch during the descent stage of the load. A piloting conduit removes
a piloting pressure from the second branch which piloting pressure acts by opening
the balance valve during the descent stage of the load.
[0003] In a circuit of this type instability and oscilation phenomena occur in the balance
valve on activation of the cylinder for the descent of the load or the inversion of
motion thereof. In particular, on lowering the load there can be a frequent succession
of blocks and free-ups of the actuator before stabilisation occurs, which causes dangerous
oscillation of the load.
[0004] To resolve the problem chokes have been placed on the piloting conduit. These chokes
determine a localised load loss by effect of which the increase in the piloting pressure
P
PIL commanding the opening of the balance valve is gradual and controlled with respect
to the increase in pressure P
B in the second branch (i.e. the branch which during the lowering stage of the load
is the delivery branch). In the diagram of figure 1 the curve S approximately represents
the progress of the piloting pressure P
PIL as a function of the pressure P
B in the second branch using a choke.
[0005] A drawback of the above-cited known solution is the delay in the activation of the
cylinder with respect to the operator's command, especially evident when the operating
liquid in the hydraulic circuit is very viscous (for example when cold). This delay
is due to the presence of the choke and can be schematised in figure 1 by observing
that the piloting pressure P
PIL reaches value P
V of opening of the balance valve (a value predetermined by the calibration of the
valve spring) when the delivery pressure P
B to the cylinder has already reached a relatively high level P
S. This means that the activation of the cylinder during the lowering stage starts
from the moment in which the pressure P
B reaches the value P
S. The time required for the pressure P
B to reached value P
S (to which value P
V of the piloting pressure P
PIL corresponds) can be relatively high, which determines the mentioned delay.
[0006] In patent
EP 1178219 the present Applicant provided a satisfactory solution to the technical problem described
above. In that solution, a check valve is located along the piloting conduit, in parallel
with the choke. The valve, normally open, enables passage of the piloting fluid up
to reaching a determined pressure downstream of the valve. On reaching the determined
pressure, the valve closes and the piloting fluid flow continues via the choke. The
presence of the check valve, located in parallel with the choke, enables a rapid increase
of the piloting pressure in the first stages of sending the piloting signal to the
balance valve. In this way, the lowering of the load begins promptly in response to
the lowering command.
[0007] The above-described solution exhibits however a not entirely satisfactory aspect.
The check valve exhibits a certain tendency to closure following pressure peaks or
flow peaks along the piloting conduit. As these pressure or flow peaks are rather
frequent, so are the closures of the check valve, which undesirably slow down the
opening of the balance valve.
[0008] The aim of the present invention is to realise a device for control of a piloting
pressure of a balance valve which enables reduction of the delay in response of the
balance valve or, more in general, of a hydraulically-piloted organ.
[0009] An advantage of the invention is that is provides a device which enables prompt and
progressive activation of the piloted organ.
[0010] A further advantage of the invention is to considerably reduce the delay in opening
of the balance valve in an activating circuit for a hydraulic actuator and to prevent
onset of instability and oscillation phenomena of the valve. Further characteristics
and advantages of the present invention will more fully emerge from the detailed description
that follows of some preferred though not exclusive embodiments, which are illustrated
purely by way of example in the accompanying figures of the drawings, in which:
figure 1 is a diagram indicating the piloting pressure PPIL according to the pressure PB in the delivery conduit during the lowering stage of the load, respectively for a
known valve (curve S) and for a valve made according to the invention (curve T);
figure 2 is a schematic illustration of an embodiment of the invention, combined to
an activating circuit for a hydraulic actuator, wherein a pressure reducer valve is
in an open configuration;
figure 3 shows the device of figure 2 in which the pressure reducer valve is in a
closed configuration;
figures 4 and 5 show a variant of the device illustrated in figures 2 and 3, wherein
the pressure reduction valve is respectively in an open and closed configuration.
Figure 2 illustrates an activating circuit for a hydraulic actuator 9 which, merely
by way of example, is constituted by a cylinder.
[0011] The hydraulic actuator 9 has a first chamber 10 and a second chamber 11 respectively
associated to the raising and lowering of a load 12.
[0012] The activating circuit comprises a hydraulic distributor 13 in turn connected to
a source of operating fluid under pressure, typically a pump. A first branch 14 connects
the distributor 13 with the first chamber 10, while a second branch 15 connects the
distributor 13 with the second chamber 11. A balance valve 16 is arranged along the
first branch 14 to regulate the flow rate of operating fluid which unloads from the
first chamber 10 during the descent stage of the load 12. A piloting conduit 17 takes
from the second branch 15 a piloting pressure which acts to open the flow rate control
valve 16.
[0013] The balance valve 16, of known type, exhibits a first connection which is connected
to the first chamber 10 and a second connection connected to the distributor 13. The
balance valve has a obturator which is mobile between the open position, in which
the first connection is set in communication with the second connection, and a closed
position, wherein the first and the second connections are not in communication with
one another. The obturator of the balance valve 16 is pushed towards the closed position
thereof by means of a spring, while it is pushed towards its open position by the
force exerted thereon by the pressure exerted by the piloting fluid removed from the
second branch 15. The balance valve comprises a single-acting valve connected in parallel
to the obturator for enabling free flow of the piloting fluid from the second to the
first connection.
[0014] The function of the balance valve 16 is to enable, during raising of the load, free
flow of the operating liquid 13 to the first chamber 10 of the actuator 9. During
the descent of the load, the balance valve 16 controls and limits the flow rate of
the operating fluid which unloads from the first chamber 10 towards the distributor
13, such as to slow down the descent of the load. The device of the present invention,
illustrated in figure 2, is predisposed to be positioned along the piloting conduit
17. It comprises a choke 8, predisposed to be interposed between a piloting fluid
source and an organ 16, in particular the balance valve 16, which is activatable by
the piloting fluid. The device further comprises a pressure reducer valve 2, arranged
in parallel with the choke 8, which is normally open and is predisposed to close when
the piloting fluid pressure reaches a determined level.
[0015] The reducer valve 2 is provided with an obturator 21 which is mobile between an open
position, in which the piloting fluid flow is enabled through the reducer valve 2,
and a closed position, in which the piloting fluid flow is not enabled through the
reducer valve 2. The obturator 21 is pushed towards the open position thereof by effect
of the thrust exerted by an elastic element 25, while it is pushed towards the closed
position thereof by effect of the thrust exerted by the piloting fluid pressure on
a thrust surface 210 of the obturator 21. The thrust surface 210 is defined by the
front section of the obturator 21, i.e. by the area of the circle delimited by the
external edge of the obturator 21.
[0016] The obturator 21 is advantageously conformed and arranged such that the thrust surface
210 is not exposed to the direct flow of the piloting liquid in inlet to the reducer
valve 2. The thrust surface 210 is exposed directly only to the piloting fluid pressure
downstream of the reducer valve 2.
[0017] The conformation of the obturator 21 and the arrangement of the thrust surface 210
are such that any peaks of flow rate and/or pressure of the piloting fluid in inlet
to the reducer valve 2 do not have the effect of nudging the obturator 21 towards
the closed position. The obturator 21 is only subject to the effect of the pressure
present downstream of the reducer valve 2, which pressure also acts on the balance
valve 16. In this way any peaks of flow rate and/or pressure of the piloting fluid
in inlet to the reducer valve 2, as they do not nudge the obturator 21 to closure,
do not slow down the flow of the piloting fluid towards the balance valve 16.
[0018] The obturator 21 is sealedly slidable along a longitudinal axis x internally of a
seating 22. The seating 22 exhibits at least an inlet opening 23, predisposed to be
connected to the piloting conduit 17, and at least an outlet opening 24 predisposed
to be connected to the balance valve 16. The obturator 21 is mobile between at least
an open position (figure 2), in which the inlet opening 23 and the outlet opening
24 are in communication and the piloting fluid can flow from the inlet opening to
the outlet opening, and at least a closed position (figure 3), in which communication
between the inlet opening and the outlet opening is prevented. An elastic element
25, preferably a helical spring possible provided with a calibrating organ 26 is predisposed
to push the obturator 21 towards the open position. Differently, the pressure downstream
of the outlet opening 24, which unloads on the thrust surface 210, pushes the obturator
21 towards the closed position.
[0019] The obturator 21 exhibits a communicating conduit 211 arranged longitudinally and
parallel to the sliding direction of the obturator 21. The communicating conduit 211
is provided with a first opening 212 and a second opening 213.
[0020] The second opening 213 is set in communication with the outlet opening 24 of the
reducer valve 2. The first opening 212, in the open position of the obturator 21,
is in communication with the inlet opening 23 of the reducer valve 2, such that the
inlet opening 23 is in communication with the outlet opening 24 via the first opening
212, the communicating conduit 211 and the second opening 213. In the closed position
of the obturator 21, the first opening 212 is not in communication with the inlet
opening 23 of the reducer valve 2. To this end, the first opening 212 is arranged
at an annular groove 214 located on the lateral surface of the obturator 21. The annular
groove 214 delimits, in cooperation with the internal wall of the seating 22, an annular
chamber into which the first opening 212 opens.
[0021] In the open position of the obturator 21, the annular chamber at least partly faces
the inlet opening 23 of the reducer valve 2, while in the closed position of the obturator
21 the annular chamber is not in communication with the inlet opening 23. The first
opening 212 develops perpendicular to the communicating conduit 211, such that the
piloting fluid coming from the inlet opening 23 of the reducer valve 2 flows internally
of the communicating conduit 211 from a transversal direction with respect to the
longitudinal development of the communicating conduit 211. In this way, the dynamic
effect due to the flow of the piloting fluid in inlet to the communicating conduit
211 is directed perpendicular to the sliding direction of the obturator 21, and the
obturator 21 is therefore not pushed to slide.
[0022] The inlet opening 23 and the first opening 212 are substantially facing in the same
direction. The outlet opening 24 and the second opening 213 are reciprocally aligned.
The directions of orientation of the inlet opening and the first opening are in turn
perpendicular to the orientation direction of the outlet opening and the second opening.
[0023] As already mentioned herein above, the special conformation of the obturator 21 is
such that the obturator 21 does not suffer from any pressure or flow rate peaks on
opening the inlet 23 of the reducer valve 2. The displacement of the obturator 21
towards the closed position is determined only by the pressure present at the outlet
opening 24 of the reducer valve 2. In this way, the reducer valve 2 does not perform
undesired and unexpected closures, but closes only when the pressure present at the
outlet opening 24 reaches a determined value, in particular a value determined by
the force exerted by the elastic element 25.
[0024] The elastic element 25 or spring is housed in a low-pressure chamber 27. In particular
the chamber 27 of the spring 25 is set in communication with the first branch 14 of
the circuit connecting the distributor 13 with the first chamber 10 of the actuator
9, which chamber 10 is associated to the raising of the load. During the stages of
supporting and lowering the load, this branch is normally at low pressure, and the
spring chamber of the reducer valve is also at low pressure. The eventual presence
of pressure in the chamber 27 would raise the calibration value of the reducer valve
2, i.e. the pressure required for determining the displacement of the obturator 21
towards the closed position. This might effectively occur by effect of a pressurised
oil flow present in the first branch 14 of the circuit during the descent. In this
condition the calibration of the reducer valve 2, i.e. the pressure required for displacing
the obturator 21 towards the closed position, would increase slightly and, consequently,
the pressure transmitted to the piloting of the balance valve would also increase,
in this way facilitating the opening of the valve. Alternatively to the connection
with the first branch 14, the chamber 27 containing the spring 25 might also be ventilated
by air.
[0025] A single-acting valve 3 can be interposed between the reducer valve 2 and the balance
valve 16, which single-acting valve 3 has a function of enabling flow of the fluid
only from the reducer valve 2 towards the piloting of the balance valve 16, while
reverse flow is prevented. In this way all unexpected back-flow of the piloting fluid
in outlet from the piloting of the balance valve 16 is prevented. This unexpected
flow might obtain in a case of a pressure drop in the second branch 15 of the circuit,
and might lead to an undesired closing of the balance valve 16.
[0026] The functioning of the reducer valve 2 and the activating circuit of the hydraulic
actuator 9 are as follows.
[0027] On starting the load lowering stage, i.e. when the distributor 13 is brought into
a configuration in which the operating fluid is sent to the second chamber 11 of the
actuator 9 through the second branch 15, the pressure P
B is in the second branch 15 is raised, and therefore also in the piloting conduit
17. The piloting pressure P
PIL on connection of piloting of the balance valve 16 reaches the predetermined value
for the opening of the valve in a relatively brief time. This pressure increases rapidly
up to the predetermined calibrated pressure of the reducer valve 2, which is normally
open. On reaching the predetermined calibrated pressure P
X of the reducer valve 2, the obturator 21 displaces into the closed position and the
piloting fluid flow proceeds through the choke 8, such that the piloting pressure
P
PIL further increases through the choke up to reaching the value P
V at which the balance valve 16 opens. Thereafter, on closure of the reducer valve
2, the piloting pressure P
PIL increases from value P
X to value P
V at a smaller inclination with respect to a situation in which the reducer valve 2
is open, as shown by the curve T of figure 1. This smaller inclination depends on
the pressure drop caused by the choke 8.
[0028] The curve S of figure 1 denotes the progress of the piloting pressure P
PIL for a control device comprising only the choke 8 but not the reducer valve 2. The
curve S clearly shows how the piloting pressure P
PIL reaches the start value P
V of the opening of the balance valve 16 when the pressure P
B in the second branch 15 is at a decidedly greater value than the curve T. This means
that, thanks to the device of the invention, the balance valve 16 opens decidedly
before, such that the lowering of the load follows very rapidly on from the operator's
descent command.
[0029] It has further been observed that the choke 8, which has the task of stabilising
the functioning of the actuator 9 during the descent stage of the load, effectively
performs this task even where the passage section is relatively large. In particular,
the choke 8 of the device of the invention can be decidedly more open with respect
to a stabilising choke in a device lacking the reducer valve 2. Consequently it can
be seen from figure 1 that the inclination of the curve S, relative to a more accentuated
choke, is less than the inclination of the second tract of the curve T, which relates
to the choke used in the present device, in which P
PIL is greater than P
X. This enables the operator to have an even more direct and immediate control of the
actuator 9, as the response of the actuator 9 is even more prompt for each positional
variation of the distributor 13.
[0030] During the descent manoeuvre it can happen that the load has to be sharply halted,
either by a command of the operator or following an eventual fault or breakage of
a tube. In order to enable rapid halting, the balance valve 16, the obturator of which
has been piloted, i.e. pushed, into the open position by the piloting fluid, has to
return to the closed position, sending at least a part of the piloting fluid in discharge.
[0031] For closure of the balance valve 16, the piloting fluid can be discharged only passing
through the choke 8, due to the presence of the single-acting valve 3. This might
cause an undesired delay in the closure of the obturator of the balance valve 16,
and therefore an excessive delay in the halting of the load.
[0032] To obviate this delay, the device of the present invention, as illustrated in figures
4 and 5, can advantageously be provided with a pressure limiter valve 4 arranged in
parallel with the choke 8 and the reducer valve 2. The limiter valve is provided with
an obturator which is mobile between an open position, in which the operating fluid
flow through the valve is enabled, and a closed position, in which the flow is not
enabled. The obturator is pushed towards the closed position by effect of the thrust
exerted by an elastic means, while it is pushed towards the open position by the piloting
fluid pressure. The limiter valve 4 enables the piloting fluid flow only from the
balance valve 16 to the second branch 15, while it prevents the reverse flow, and
enables flow only if the piloting fluid pressure rises above a determined value corresponding
to the thrust exerted by the elastic means. At least a part of the piloting fluid
can be rapidly discharge through the limiter valve 4, such as to enable the obturator
of the balance valve 16 to displace rapidly towards the closed position thereof, at
least for a considerable part of the run towards the closed position. Although the
above description relates to the use of the device in combination with a balance valve,
the device of the invention can be used for controlling the piloting pressure towards
any hydraulically-piloted organ, with the aim of having a very rapid start-up of the
piloted organ in response to an external command supplied via the piloting pressure
supply. The device obviates delays in start-up of the hydraulically-piloted organ
while at the same time preventing instability phenomena in the functioning of the
piloted organ after start-up.
1. A device for controlling a piloting pressure, comprising: a choke (8), predisposed
to be interposed between a piloting fluid source and an organ (16) activatable by
the piloting fluid; a valve (2), arranged in parallel to the choke (8), which valve
(2) is normally open and is predisposed to close when the piloting fluid pressure
reaches a determined value; characterised in that the valve (2) is a pressure reducer valve provided with an obturator (21).
2. The device of claim 1, wherein the obturator (21) is mobile between an open position,
in which a piloting fluid flow is enabled through the reducer valve (2), and a closed
position, in which the piloting fluid flow is not enabled through the reducer valve
(2), the obturator being pushed towards the open position thereof by effect of a thrust
exerted by an elastic element (25), the obturator being pushed towards the closed
position thereof by effect of the thrust exerted by the piloting fluid pressure on
a thrust surface (210) of the obturator (21).
3. The device of claim 2, wherein the obturator (21) is conformed and arranged such that
the thrust surface (210) is not exposed to a direct flow of the piloting fluid in
inlet to the reducer valve (2).
4. The device of claims 2 or 3, wherein the thrust surface (210) is directly exposed
to the direct flow of the piloting fluid in inlet to the reducer valve (2).
5. The device of one of the preceding claims, wherein the obturator (21) is sealedly
slidable along a seating (22) which exhibits at least an inlet opening (23) predisposed
to receive the piloting fluid, and at least an outlet opening (24), through which
the piloting fluid can be sent to the organ (16).
6. The device of claim 5, wherein the obturator (21) is mobile between at least an open
position, in which the inlet opening (23) and the outlet opening (24) are in mutual
communication and the piloting fluid can flow from the inlet opening to the outlet
opening, and at least a closed position, in which the communication between the inlet
opening and the outlet opening is prevented.
7. The device of claim 6, wherein: the obturator (21) exhibits a communicating conduit
(211) provided with a first opening (212) and a second opening (213); the second opening
(213) is set in communication with the outlet opening (24) of the reducer valve (2);
the first opening (212), in the open position of the obturator (21), is in communication
with the inlet opening (23), such that the inlet opening (23) is in communication
with the outlet opening (24) via the first opening (212), the communicating conduit
(211) and the second opening (213); in the closed position of the obturator (21),
the first opening (212) is not in communication with the inlet opening (23).
8. The device of claim 7, wherein: the inlet opening (23) and the first opening (212)
substantially face in a same direction; the outlet opening (24) and the second opening
(213) are aligned to one another; the orientation direction of the inlet opening (23)
and the first opening (212) are perpendicular to the alignment direction of the outlet
opening (24) and the second opening (213).
9. The device of claim 8, wherein: the first opening (212) is arranged at an annular
channel (214), afforded on the lateral surface of the obturator (21), which delimits,
in cooperation with the internal wall of the seating (22), an annular chamber in which
the first opening (212) opens; in the open position of the obturator (21), the annular
chamber at least partly faces the inlet opening (23); in the closure position of the
obturator (21) the annular chamber is not in communication with the inlet opening
(23).
10. The device of one of claims from 2 to 9, wherein the elastic element or spring (25)
is housed in a low-pressure chamber (27).
11. The device of claim 10, wherein the chamber (27) of the elastic element (25) is open
to air.
12. The device of one of the preceding claims, comprising a single-acting valve (3) arranged
downstream of the reducer valve (2), which is predisposed to enable flow of the piloting
fluid from the reducer valve (2) towards the organ to be piloted (16) and to prevent
a reverse flow.
13. The device of one of the preceding claims, comprising a pressure limiter valve (4),
arranged in parallel to the choke (8) and to the reducer valve (2), which is predisposed
to enable the piloting fluid flow in discharge from the organ (16) and to prevent
a reverse flow.
14. An activating circuit for a hydraulic actuator (9), comprising: a hydraulic cylinder
(13); a first branch (14) predisposed to connect the distributor (13) with a first
chamber (10) of the hydraulic actuator (9); a second branch (15) predisposed to connect
the distributor (13) with a second chamber (11) of the hydraulic actuator (9); a balance
valve (16), arranged along the first branch (14) in order to regulate the operating
fluid flow in outlet from the first chamber (10) during a lowering stage of the load
(12); a choke (8) interposed between the second branch (15) and the balance valve
(16); characterised in that it comprises a device for controlling the piloting pressure as in one of the preceding
claims, arranged in parallel to the choke (8) between the second branch (15) and the
balance valve (16).