EP1781952A1 - Hydraulische steueranordnung - Google Patents
Hydraulische steueranordnungInfo
- Publication number
- EP1781952A1 EP1781952A1 EP05755620A EP05755620A EP1781952A1 EP 1781952 A1 EP1781952 A1 EP 1781952A1 EP 05755620 A EP05755620 A EP 05755620A EP 05755620 A EP05755620 A EP 05755620A EP 1781952 A1 EP1781952 A1 EP 1781952A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- pressure
- control
- pilot
- valve
- piston
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 230000001105 regulatory effect Effects 0.000 abstract 1
- 238000007789 sealing Methods 0.000 description 8
- 230000008859 change Effects 0.000 description 6
- 230000006835 compression Effects 0.000 description 6
- 238000007906 compression Methods 0.000 description 6
- 238000013016 damping Methods 0.000 description 5
- 230000007423 decrease Effects 0.000 description 5
- 238000010276 construction Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000000903 blocking effect Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000036316 preload Effects 0.000 description 2
- 235000010627 Phaseolus vulgaris Nutrition 0.000 description 1
- 244000046052 Phaseolus vulgaris Species 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
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- 230000003993 interaction Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000002040 relaxant effect Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B11/00—Servomotor systems without provision for follow-up action; Circuits therefor
- F15B11/02—Systems essentially incorporating special features for controlling the speed or actuating force of an output member
- F15B11/024—Systems essentially incorporating special features for controlling the speed or actuating force of an output member by means of differential connection of the servomotor lines, e.g. regenerative circuits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B11/00—Servomotor systems without provision for follow-up action; Circuits therefor
- F15B11/02—Systems essentially incorporating special features for controlling the speed or actuating force of an output member
- F15B11/028—Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the actuating force
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B11/00—Servomotor systems without provision for follow-up action; Circuits therefor
- F15B11/02—Systems essentially incorporating special features for controlling the speed or actuating force of an output member
- F15B11/04—Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed
- F15B11/042—Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed by means in the feed line, i.e. "meter in"
- F15B11/0423—Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed by means in the feed line, i.e. "meter in" by controlling pump output or bypass, other than to maintain constant speed
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B13/00—Details of servomotor systems ; Valves for servomotor systems
- F15B13/02—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
- F15B13/024—Pressure relief valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/30—Directional control
- F15B2211/305—Directional control characterised by the type of valves
- F15B2211/30505—Non-return valves, i.e. check valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/30—Directional control
- F15B2211/305—Directional control characterised by the type of valves
- F15B2211/30525—Directional control valves, e.g. 4/3-directional control valve
- F15B2211/3053—In combination with a pressure compensating valve
- F15B2211/30555—Inlet and outlet of the pressure compensating valve being connected to the directional control valve
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/30—Directional control
- F15B2211/31—Directional control characterised by the positions of the valve element
- F15B2211/3105—Neutral or centre positions
- F15B2211/3111—Neutral or centre positions the pump port being closed in the centre position, e.g. so-called closed centre
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/30—Directional control
- F15B2211/31—Directional control characterised by the positions of the valve element
- F15B2211/3122—Special positions other than the pump port being connected to working ports or the working ports being connected to the return line
- F15B2211/3133—Regenerative position connecting the working ports or connecting the working ports to the pump, e.g. for high-speed approach stroke
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/30—Directional control
- F15B2211/31—Directional control characterised by the positions of the valve element
- F15B2211/3144—Directional control characterised by the positions of the valve element the positions being continuously variable, e.g. as realised by proportional valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/30—Directional control
- F15B2211/315—Directional control characterised by the connections of the valve or valves in the circuit
- F15B2211/3157—Directional control characterised by the connections of the valve or valves in the circuit being connected to a pressure source, an output member and a return line
- F15B2211/31576—Directional control characterised by the connections of the valve or valves in the circuit being connected to a pressure source, an output member and a return line having a single pressure source and a single output member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/30—Directional control
- F15B2211/32—Directional control characterised by the type of actuation
- F15B2211/329—Directional control characterised by the type of actuation actuated by fluid pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/50—Pressure control
- F15B2211/505—Pressure control characterised by the type of pressure control means
- F15B2211/50509—Pressure control characterised by the type of pressure control means the pressure control means controlling a pressure upstream of the pressure control means
- F15B2211/50518—Pressure control characterised by the type of pressure control means the pressure control means controlling a pressure upstream of the pressure control means using pressure relief valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/50—Pressure control
- F15B2211/515—Pressure control characterised by the connections of the pressure control means in the circuit
- F15B2211/5159—Pressure control characterised by the connections of the pressure control means in the circuit being connected to an output member and a return line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/50—Pressure control
- F15B2211/52—Pressure control characterised by the type of actuation
- F15B2211/528—Pressure control characterised by the type of actuation actuated by fluid pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/60—Circuit components or control therefor
- F15B2211/605—Load sensing circuits
- F15B2211/6051—Load sensing circuits having valve means between output member and the load sensing circuit
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/70—Output members, e.g. hydraulic motors or cylinders or control therefor
- F15B2211/75—Control of speed of the output member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/80—Other types of control related to particular problems or conditions
- F15B2211/86—Control during or prevention of abnormal conditions
- F15B2211/8609—Control during or prevention of abnormal conditions the abnormal condition being cavitation
Definitions
- the invention relates to a hydraulic bistanord ⁇ voltage with a differential cylinder according to the preamble of claim 1 and a suitable for such Steuer ⁇ arrangement pilot operated Druckbegrenzungsven ⁇ til.
- Such control arrangements are used in particular in mobile work equipment, for example, to pivot a blade of a wheel loader.
- the blade is pivoted downwards in order, for example, to empty material received therein.
- the piston rod of the differential cylinder is retracted so that the blade pivots upward, ie, away from the ground.
- a control valve which is followed by a boost valve.
- control arrangement is designed with a pressure relief valve, via which the load pressure at the two Hydrozy- is limited.
- the pressure limiting valve is designed with a pressure switching stage, which makes it possible to limit the load pressure to a higher pressure when operating the blade alone, as it is the case when operating the boom or actuation of both hydraulic cylinders.
- overloading and kinking of the piston rod can occur under certain operating conditions due to the action of external forces. This is the case, for example, when the ground is to be pulled off and the blade is pivoted downwards and placed on the ground and the wheel loader then pulls off the ground when reversing. Runs the blade during this peeling on an obstacle, such as a boulder, so the blade holding the blade in the Abziehwolf piston rod of the differential cylinder claims to pressure bean ⁇ and can bend.
- the object of the invention is to provide a hydraulic control arrangement and a pressure relief valve, by means of which damage to a differential cylinder of the control arrangement can be prevented.
- the hydraulic control arrangement is designed with a differential cylinder. Its pressure chambers can be connected to a pump or a tank via a control valve arrangement so that a piston rod of the differential cylinder extends or retracts.
- the pressure in the effective pressure in the supporting pressure chamber is limited in the inventive solution via a pilot-operated pressure relief valve. Its pilot stage is executed with a Druckumsehalteck over which is set at low pressure in the other pressure chamber set the pressure at the pressure relief valve to the extent that an overload of the piston rod is reliably prevented.
- the differential cylinder can be actuated via the control valve arrangement in a differential circuit, in which the annular space is connected to the cylinder space when the piston rod is extended.
- the pressure changeover stage preferably has a tensioning piston which acts on a control spring of the pilot stage of the pressure limiting valve and which acts in the direction of increasing the spring preload from the pressure in the piston rod side annular space and in the direction of lowering the spring preload from the pressure in the other pressure space in the support direction (Cylinder space) is acted upon, wherein the effective in this direction control surface of the clamping piston
- the tensioning piston of the pressure changeover stage is acted upon in the direction of increasing the pretensioning of a control spring acting on a pilot control valve by a control pressure which corresponds to the pressure in the other pressure chamber, which at Ein ⁇
- a control pressure which corresponds to the pressure in the other pressure chamber, which at Ein ⁇
- An effective in the direction of a reduction of the control spring bias smaller control surface is acted upon by the pressure in the effective in the support direction pressure chamber.
- the smaller control surface is dispensed with.
- the area ratio between the control surface of the tensioning piston and the pilot valve seat surface is ⁇ 1.5 in one embodiment.
- the control arrangement can be made particularly compact if a pilot piston of the pressure limiting valve is provided with a longitudinal channel, via which control oil is led from a spring chamber of a main stage of the pressure limiting valve to the smaller control surface.
- the pilot piston is preferably designed with a projection which dips sealingly into a recess of the clamping piston.
- the end face of this recess then forms the smaller control surface, the effective size of this surface being equal to the cross-sectional area of the projection.
- the two control surfaces are formed on a pilot piston, wherein a smaller control surface acts on the pressure in the other pressure chamber (for example piston rod side) and the larger control surface on the pressure in the other pressure chamber of the consumer (for example, cylinder chamber) is - on the clamping piston can then verzich ⁇ tet.
- the pressure limiting valve is designed with an emergency opening, via which the inlet connection can be connected directly to the tank connection.
- control valve arrangement used in the control arrangement has a metering orifice, which is formed by a continuously adjustable directional control valve and is followed by a LUDV pressure compensator. It is particularly preferred if the pressure medium supply takes place via a pump whose flow rate is adjustable in dependence on the highest load pressure of the entire system - the control arrangement then represents a LUDV system.
- FIG. 1 shows a circuit diagram of a hydraulic control arrangement according to the invention
- FIG. 2 shows a longitudinal section through a pilot-controlled pressure limiting valve with clamping piston of the control arrangement from FIG. 1;
- FIG. 3 is a circuit symbol of the pressure relief valve of Figure 2;
- FIG. 4 shows a longitudinal section through a further pressure limiting valve with clamping piston
- FIG. 5 is a circuit symbol of this pressure limiting valve
- FIG. 6 a longitudinal section through an embodiment of a pressure limiting valve without tensioning piston
- FIG. 7 is a circuit symbol of this embodiment.
- FIG. 8 shows characteristic curves of the pressure limiting valves shown in FIGS. 2, 4 and 5.
- FIG. 1 shows a circuit diagram of a directional control valve element 1 of a mobile control block, via which a plurality of consumers of a mobile working device, for example a wheel loader, can be actuated.
- the directional control valve element 1 of the mobile control block shown in FIG. 1 serves to actuate an actuating cylinder 2, via which a blade mounted on a boom can be pivoted.
- the disk-type directional control valve element 1 has a pressure port P, a tank port T, two working ports Al, Bl, and two control ports al, bl, another control port x and an LS port LS.
- the control block is designed as a LUDV system, via which a load pressure-independent flow distribution is possible.
- a pump with variable delivery volume for example a variable displacement pump, is actuated as a function of the highest load pressure of the consumer.
- the LUDV directional control valve element 1 has a continuously adjustable directional control valve 4, the valve spool of which can be acted upon by a control pressure via the two control connections a1, and thus from a spring-biased central locking position into a plurality of (a) or (b ) is shiftable.
- the directional control valve 4 has at least one pressure connection P, a tank connection T, two working connections A, B as well as two further connections D and D '.
- the directional control valve 4 forms a directional part which is indicated by the two intersecting or branching arrows and a speed part which is formed by a variable metering orifice 5 which lies between the connections D and D '.
- the spring chamber is connected via a throttle with the working port Bl of Wege ⁇ ventiIelernents.
- the pilot valve 14 is biased into a blocking position and can be switched by means of an actuating piston 16 from this blocking position into a passage pitch in which the spring space of the logic valve 12 is connected via a tank control channel 17 to a tank port 18 connected to the tank port T, so that the spring chamber of the logic valve 12 is depressurized.
- the graduated valve body of the logic valve 12 can therefore be lifted at a pressure fluid flow in the return line 8 to the actuating cylinder 2 already due to a non-return function and at a flow of pressure medium from the actuating cylinder 2 to port B of the directional control valve with relief of the spring chamber of its valve seat.
- the Betschists ⁇ piston 16 is acted upon via a control branch passage 20 with the pressure at the control terminal al, wherein due to a large area of the actuating piston 16 a comparatively large force is applied to the pilot control valve 14. Since the construction of such a low-leakage valve 10 is known, further relevant embodiments are unnecessary.
- the two working ports Al, Bl of Wegeventil ⁇ elements 1 are via working lines 24, 26 with a
- the directional control valve element 1 is further penetrated by a connected to the pressure port P pump channel 32. From this branches off an inlet channel 34, which leads to the connection D of the directional control valve 4.
- the port D 1 of the directional control valve is connected via a connecting channel 36 to an input port P of a LUDV pressure compensator 38 whose pressure compensating piston is open in the opening direction by the pressure in the connecting channel 36 and in the closing direction by the force of a spring and the highest load pressure of the actuated load is applied, which is tapped via a connected to the LS port LS channel 40.
- the pressure compensator is thus acted upon in the opening direction by the pressure downstream of the metering orifice 5.
- An output port A of the pressure compensator 38 is connected via a pressure compensator channel 42 and a check valve 44 to the input port P of the directional control valve 4.
- the tank connection T is connected to the tank channel 18 by means of a drainage channel 46.
- the pressure in the return line 8 connected to the annular space 30 is limited by a secondary pressure limiting valve 48 which is arranged in a relief channel 50 which branches off from the return line 8 in the region of the pressure medium flow path between the logic valve 12 and the associated working port Bl and which is connected to the tank channel 18.
- the pressure relief of the feed line 6 connected to the cylinder space 28 takes place via a pilot-operated pressure limiting valve 52, which is arranged in a channel 54 which is likewise connected to the tank channel 18 and which in the
- the pilot operated pressure limiting valve 52 and the pressure limiting valve 48 are each designed with a secondary suction function, so that pressure medium can be sucked out of the tank channel 18 to avoid cavitation during a pulling load.
- the pilot-operated pressure relief valve 52 is / as will be explained in more detail below with reference to Figures 2 and 3, from a main stage, a Vor Kunststoffstu ⁇ Fe and a pressure change 56.
- This pressure circulation stage 56 shown schematically in FIG. 1 has a tensioning piston 58 on which a control spring 60 of the pilot control stage is supported.
- a larger control surface of the clamping piston 58 is acted upon by the pressure in a Vorêtka ⁇ channel 62, which leads to the control terminal X of Wege ⁇ valve element 1, which in turn is connected via a line 64 with the leading to the annulus 30 working line 26.
- the tensioning piston 58 acts in the flow line 6, which is tapped off via the channel 54 and via a clearance channel 66.
- the directional valve 4 is brought into one of its positions marked (a) by applying a control pressure to the control connection a.
- This control pressure can spielvati be adjusted via pressure reducing valves, which reduce the pressure in a control circuit to a suitable control pressure.
- This LUDV pressure balance 38 arranged downstream of the metering orifice 5 throttles the pressure medium volume flow so strongly that the pressure after all the metering of the system is the same and preferably corresponds to the highest load pressure or slightly above this. Ie. In the case of insufficient supply to several consumers, nothing changes at the pressure downstream of the metering orifices.
- the pump pressure is applied in the same way to all metering orifices of the system, so that the pressure difference at all metering orifices alters in the same way if the pump pressure decreases in the event of an undersupply - the flow distribution between the metering orifices is maintained (load pressure-independent flow distribution) ,
- the thus throttled pressure medium flow then flows through the pressure balance channel 42, the input port P and the working port A of the directional control valve 4 and the flow line 6 and the working line 24 to the cylinder chamber 28.
- the piston rod 68 extends, wherein the pressure medium displaced from the annular space 30 via the working line 26 and the working port Bl flows.
- the directional control valve 4 is displaced by applying a control pressure to the control port bl in one of its (b) marked positions, in which case the cylinder chamber 28 is connected to the Tank ⁇ channel 18 and the annular space 30 with the pump channel 32, so that pressure medium is conveyed into the annular space 30 and the pressure medium displaced from the cylinder space 28 flows back to the tank T.
- the pilot-operated pressure relief valve 52 used will be explained below with reference to FIGS. 2 and 3.
- FIG. 2 shows a longitudinal section of the pilot-operated pressure-limiting valve 52 according to the invention.
- this has a main stage 70, a pilot stage 72 and the pressure changeover stage 56.
- the basic structure of the main stage 70 and the pilot stage 72 is essentially from DE 100 62 427 A1, so that only the components required for understanding the invention are described here and, incidentally, this prior art publication is referred to.
- the pilot-operated pressure relief valve 52 is designed in cartridge construction and has a housing 74, on which an end-side pressure port P and a radial, formed for example by a bore star tank port T is formed.
- valve slide 76 designed with a sliding seat is guided in a valve bore 78, which is prestressed against a seat edge 82 via a weak pressure spring 80.
- the valve slide 76 is hollow, wherein in an axially projecting end face a nozzle bore 84 is formed, which inwardly towards a spring
- a sealing edge 92 is formed in the radially widened region of the valve bore 78, against which a seat body 94 inserted in a further enlarged region of the valve bore 78 rests. This is biased by means of a screwed into the housing 70 pilot housing 96 against the sealing edge 92.
- a pilot valve seat 98 is formed, against which a pilot valve cone 100 is biased by the control spring 60.
- the pilot control valve cone 100 has a collar 102 whose outer circumference is guided in a guide bore 104 of the seat body 94 provided with two longitudinal grooves. An axial projection is formed on the left end face of the seat body 94 in FIG.
- the control spring 60 is supported on the left end face of the tensioning piston 58 in FIG. 2, so that in its illustrated basic position it rests against a stop screw 122 screwed into the throughbore 114.
- the through-bore 114 opens on the right-hand end face of the pilot control housing and forms a connection X1 of the pilot-operated pressure-limiting valve 52, to which the control channel 62 shown in FIG. 1 is connected.
- the stop screw 122 is of annular design, so that the pressure at the control connection X1 also acts on the rear side of the tensioning piston 58, which forms a control surface 124 that is substantially larger in comparison to the control surface 120.
- a radial shoulder acting as a stop 126 is formed on the passage bore 114, limiting the axial travel of the tensioning piston 58 to the left (FIG. 2).
- the clamping piston 58 acts on the control spring 60, which acts on the valve spool 76 of the main stage 72 in Sch.rich ⁇ direction. In the opening direction acts on the valve spool 76, the pressure at the input port P, which also rests in the channel 54 and in the flow line 6.
- the pressure port P of the pressure relief valve 52 can be connected by hand to the tank port T. This is indicated in Figure 3 with the manually operable switching valve 128. When switching this switching valve 128 in its passage position, the input port P of the pressure relief valve 52 is relieved to the tank channel 18 out. In the concrete embodiment shown in FIG. 2, this emergency opening is formed by the interaction of the seat body 94 with the sealing edge 92.
- the seat body 94 sits firmly on the sealing edge 92 - this corresponds to the closed position of the switching valve 128 (see FIG. 3).
- the manually-accessible pilot-control housing 96 is unscrewed somewhat out of the housing 74, so that the seat body 94 lifts off from the sealing edge 92 and the spring chamber 110, in which the pressure is normally present at the inlet connection P.
- the Nachsaugring 88 is moved by the higher tank pressure to the right and running on the radial collar 86, so that the valve slide 76 is taken and the connection from the tank port T to the input port P is opened, so that pressure medium can be sucked from the tank.
- the pressure in the annular space 30 is at least as high as the pressure in the cylinder chamber 28.
- the pressure acting on the larger control surface 124 is at least equal to the pressure acting on the smaller control surface 120, which corresponds to the pressure in the cylinder chamber 28.
- the force acting in one direction on the clamping piston is the sum of the force of the control spring 60 plus the pressing force acting on the control surface 120, which is equal to the cross-sectional area of the projection 111 within the recess 112, through the spring chamber 110 prevailing pressure is generated.
- the spring force is equal to a compressive force generated by the boundary pressure on a surface containing the differential area
- the pressure in the annular space 30 decreases, if it was not already Tank ⁇ pressure while the pressure in the cylinder chamber 28 increases.
- the geometry of the clamping piston 58 is selected so that, starting from a certain pressure difference between the pressure chambers 28, 30, the clamping piston 58 lifts off from the stop 126 by the relief of the control surface 124 and is moved against the stop screw 122. This return movement is assisted by the pressure acting on the smaller control surface 120 - the bias of the control spring 60 is reduced and corresponding to the release pressure of
- the small control surface 120 of the tensioning piston 58 has the effect that, when the pressure limiting valve 52 responds, the tensioning piston 58 is acted upon in the direction of relaxing the control spring 60 by a force which is as great as that of the inlet pressure (P) on the entire seat surface of the pilot valve seat 98 is generated force.
- P inlet pressure
- a pressure limiting valve 52 having the geometric relationships shown in FIG.
- the basic structure of the exemplary embodiment shown in FIG. 4 corresponds to that of FIG. 2. Accordingly, the exemplary embodiment illustrated in FIG. 4 is also implemented with a main stage 70, a pilot stage 72 and a pressure changeover stage 56.
- the main stage 70 with the valve spool 76, the compression spring 80 arranged in the spring chamber 110, the cartridge-like housing 74 and the Nachsaugring 88 corresponds to the main stage 70 of the above-described embodiment, so that the simplicity is referred to the relevant embodiments.
- the pilot stage 72 and the switching stage 56 are substantially integrated into the pilot housing 96, which is screwed into the cartridge-shaped housing 74 and presses the seat body 94 against the sealing edge 92 (in the illustrated basic position).
- the sealing body 94 is designed with an axial projection 130 in which the blind hole 106 is formed, which opens via the radial bores 108 in the spring chamber 110.
- a damping piston 132 is axially displaceable, which via damping gaps (not shown in detail in FIG. 4) connects a pressure medium connection in the direction of the pilot valve seat 98.
- the clamping piston 58 bears against the stop screw 138 screwed into the pilot housing 96, with a radially extended thrust head 138, so that the clamping piston 58 moves in the direction of increasing the pretensioning of the control spring 60 by the pressure at the control terminal Xl (pressure in the annular space 30) is acted upon.
- the clamping piston 58 is guided along a through hole 114 of the pilot housing 96 as in the embodiment described above. This through hole 114 widens to the right (view according to FIG. 4) toward the connection X1, wherein an abutment piece 140 is supported on an annular shoulder, which in effect corresponds to the stop 126 and thus the axial stroke of the tensioning piston 58 to the left in FIG Figure 4 limited.
- the pilot control stage 72 opens when the pressure acting on the pilot valve seat 98 is sufficient to lift the pilot valve cone 100 away from the pilot valve seat 98. In the opening direction acts on the pilot valve seat 98 with the cross-sectional area A2 of the pressure at the pressure port P of the nozzle bore 84, the spring chamber 110, the radial bores 108 and limited by the damping oil 106 damping gap is tapped.
- the area ratio A2 . / A2 relatively small (for example, 1.12) carried out, so that even at a much higher pressure in the annular space 30 than in the above-described embodiment, the pilot stage 72 is open.
- the pressure limiting valve would accordingly open at a pressure of about 340 bar, ie much earlier than in the exemplary embodiment illustrated in FIG.
- This early opening is further supported by the fact that in the embodiment shown in Figure 4 is missing in the direction of relaxation of the control spring 60 effective control surface (120 in Figure 2).
- the pressure in the annular space 30 further, for example, to 110 bar, the stop head 138 comes into abutment against the stop screw 122, so that the lower limit pressure (minimum bias of Steuer ⁇ spring 60) is set.
- this minimum limit pressure then corresponds to approximately 123 bar, corresponding to the area ratio A 1 / A 2.
- the boundary pressure increases linearly in accordance with this area ratio.
- FIG. 6 shows a further simplified exemplary embodiment of a pressure limiting valve according to the invention, in which the use of a tensioning piston is dispensed with.
- the basic construction of the valve is identical to the exemplary embodiment described with reference to FIG. 2 except for the guidance and construction of the pilot valve cone 100, so that with regard to the description of the main stage 70 with the valve slide 76, the compression spring 80 and the suction ring 88 as well With regard to the seat body 94 and the pre-control housing 96 screwed into the housing 74 of the main stage 70, reference is made to the statements relating to FIG.
- the outer contour of the pilot valve cone 100 also corresponds to the embodiment shown in Figure 2, d. H.
- the cylindrical end portion 142 passes through a guide portion 144 of the pilot housing 96, which is formed by a radiallyteil ⁇ set part of the through hole 114.
- the right end face 146 of the pilot control valve 100 in FIG. 6 defines a control chamber 148, which is acted on by the control oil pressure at the control connection X1.
- the pilot valve cone 100 is pretensioned via the control spring 60 against the pilot valve seat 98, whose effective area in the
- the two limit pressures are determined by the ratio of the areas A1 / A2.
- the pressure at the control connection X1 and thus also the pressure in the control chamber 148 are approximately zero, so that the end face 146 is not subjected to a control oil pressure - the pilot valve cone 100 is thus biased against its pilot valve seat 98 solely by the force of the control spring 60, so that the lower limit pressure is set.
- both the end face 146 and the front area of the pilot valve piston 100 bounded by the pilot valve seat 98 are at the same pressure acted upon, so that this pressure on the area difference A2-A1 is effective and the upper limit pressure is set.
- the switching symbol of the pressure limiting valve 52 shown in FIG. 6 is shown in FIG. Accordingly, in this embodiment, the bias of the control spring 60 is not changed, but only on the pilot control in the opening and closing effective mena effective pressure forces, wherein a change in the pressure at the control port Xl always results in a change in the set limit pressure , If one applies this limiting pressure pg set at the pressure limiting valve 52 as a function of the pressure Px 1 present at the control connection X1 (pressure in the annular space 30), the result is
- the hydraulic control arrangement has a differential cylinder with a piston rod-side pressure chamber and a bottom-side pressure chamber, which can be connected via a control valve arrangement for actuating the differential cylinder with a pump or a tank.
- the pressure in a pressure chamber is limited by a pilot-operated pressure limiting valve, which is designed with a pressure changeover stage, via which the pressure set at the pressure limiting valve can be lowered in dependence on the pressure in the other of the pressure chambers.
- control spring 62 control channel
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Safety Valves (AREA)
- Operation Control Of Excavators (AREA)
- Fluid-Pressure Circuits (AREA)
Description
Claims
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102004035632 | 2004-07-22 | ||
| DE102005022275A DE102005022275A1 (de) | 2004-07-22 | 2005-05-10 | Hydraulische Steueranordnung |
| PCT/EP2005/006826 WO2006010419A1 (de) | 2004-07-22 | 2005-06-23 | Hydraulische steueranordnung |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1781952A1 true EP1781952A1 (de) | 2007-05-09 |
| EP1781952B1 EP1781952B1 (de) | 2011-09-07 |
Family
ID=34971312
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP05755620A Expired - Lifetime EP1781952B1 (de) | 2004-07-22 | 2005-06-23 | Hydraulische steueranordnung |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20070245889A1 (de) |
| EP (1) | EP1781952B1 (de) |
| AT (1) | ATE523697T1 (de) |
| DE (1) | DE102005022275A1 (de) |
| WO (1) | WO2006010419A1 (de) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20240108566A (ko) | 2022-01-17 | 2024-07-09 | 가와사끼 쥬고교 가부시끼 가이샤 | 릴리프 밸브 |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SE534272C2 (sv) * | 2009-06-18 | 2011-06-28 | Kurt Palmloef | Säkerhetsventil |
| ITTO20100190A1 (it) * | 2010-03-12 | 2011-09-13 | Cnh Italia Spa | Sistema idraulico |
| US9127437B2 (en) | 2010-12-15 | 2015-09-08 | Caterpillar Inc. | Flow regeneration hydraulic circuit |
| DE102011101921B4 (de) | 2011-05-18 | 2024-12-12 | Linde Hydraulics Gmbh & Co. Kg | Hydraulische Bremsventileinrichtung |
| CN102182715B (zh) * | 2011-05-20 | 2012-11-14 | 中联重科股份有限公司 | 液压控制系统及其液压控制模块及具有该系统的工程机械 |
| CH705123A1 (de) * | 2011-06-15 | 2012-12-31 | Liebherr Machines Bulle Sa | Druckbegrenzungsventil. |
| WO2013150613A1 (ja) | 2012-04-03 | 2013-10-10 | ボッシュ・レックスロス株式会社 | 油圧回路 |
| US9790964B2 (en) | 2014-09-25 | 2017-10-17 | Cnh Industrial America Llc | Hydraulic system |
| US9708796B2 (en) | 2014-09-25 | 2017-07-18 | Cnh Industrial America Llc | Hydraulic valve |
| CN108138809B (zh) * | 2015-09-25 | 2020-02-07 | Kyb株式会社 | 流体压控制装置 |
| AU2016277732B2 (en) * | 2016-12-23 | 2023-11-02 | Draeger Australia Pty Ltd | Breathing apparatus filling device |
| US11583455B2 (en) * | 2019-10-28 | 2023-02-21 | Stryker Corporation | Hydraulic valve and system |
| CN111577698B (zh) * | 2020-05-27 | 2022-06-17 | 三一汽车起重机械有限公司 | 缓冲阀、回转液压系统及起重机 |
| CN112096682B (zh) * | 2020-09-30 | 2021-11-19 | 潍柴动力股份有限公司 | 一种先导式电比例高压溢流阀 |
| CN118066334B (zh) * | 2024-04-01 | 2025-10-17 | 中国船舶集团有限公司第七零七研究所九江分部 | 一种差动复位式三位二通液动阀 |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3160076A (en) * | 1961-12-14 | 1964-12-08 | Parker Hannifin Corp | Fluid system and relief valve assembly therefor |
| JPS5730483Y2 (de) | 1976-06-10 | 1982-07-05 | ||
| DE3813020C2 (de) * | 1988-04-19 | 1996-12-19 | Bosch Gmbh Robert | Vorrichtung zur Vorschubsteuerung einer hydraulischen Stelleinrichtung |
| DE19524900C2 (de) * | 1995-07-08 | 2000-12-28 | Mannesmann Rexroth Ag | Vorgesteuertes Druckbegrenzungsventil |
| US6318079B1 (en) * | 2000-08-08 | 2001-11-20 | Husco International, Inc. | Hydraulic control valve system with pressure compensated flow control |
| DE10062428A1 (de) | 2000-12-14 | 2002-06-20 | Mannesmann Rexroth Ag | Vorgesteuertes Druck-Einspeiseventil |
| JP2003185042A (ja) * | 2001-12-17 | 2003-07-03 | Shin Caterpillar Mitsubishi Ltd | ラインリリーフ弁 |
-
2005
- 2005-05-10 DE DE102005022275A patent/DE102005022275A1/de not_active Withdrawn
- 2005-06-23 WO PCT/EP2005/006826 patent/WO2006010419A1/de not_active Ceased
- 2005-06-23 AT AT05755620T patent/ATE523697T1/de active
- 2005-06-23 US US11/631,779 patent/US20070245889A1/en not_active Abandoned
- 2005-06-23 EP EP05755620A patent/EP1781952B1/de not_active Expired - Lifetime
Non-Patent Citations (1)
| Title |
|---|
| See references of WO2006010419A1 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20240108566A (ko) | 2022-01-17 | 2024-07-09 | 가와사끼 쥬고교 가부시끼 가이샤 | 릴리프 밸브 |
Also Published As
| Publication number | Publication date |
|---|---|
| ATE523697T1 (de) | 2011-09-15 |
| US20070245889A1 (en) | 2007-10-25 |
| DE102005022275A1 (de) | 2006-02-16 |
| WO2006010419A1 (de) | 2006-02-02 |
| EP1781952B1 (de) | 2011-09-07 |
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