[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

EP3679254B1 - Valve - Google Patents

Valve Download PDF

Info

Publication number
EP3679254B1
EP3679254B1 EP18766189.7A EP18766189A EP3679254B1 EP 3679254 B1 EP3679254 B1 EP 3679254B1 EP 18766189 A EP18766189 A EP 18766189A EP 3679254 B1 EP3679254 B1 EP 3679254B1
Authority
EP
European Patent Office
Prior art keywords
valve
fluid
connection
control
valve housing
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.)
Active
Application number
EP18766189.7A
Other languages
German (de)
French (fr)
Other versions
EP3679254A1 (en
Inventor
Peter Bruck
Frank Schulz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hydac Fluidtechnik GmbH
Original Assignee
Hydac Fluidtechnik GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hydac Fluidtechnik GmbH filed Critical Hydac Fluidtechnik GmbH
Publication of EP3679254A1 publication Critical patent/EP3679254A1/en
Application granted granted Critical
Publication of EP3679254B1 publication Critical patent/EP3679254B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B1/00Installations or systems with accumulators; Supply reservoir or sump assemblies
    • F15B1/02Installations or systems with accumulators
    • F15B1/021Installations or systems with accumulators used for damping
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00Details of servomotor systems ; Valves for servomotor systems
    • F15B13/02Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
    • F15B13/04Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor
    • F15B13/0416Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor with means or adapted for load sensing
    • F15B13/0417Load sensing elements; Internal fluid connections therefor; Anti-saturation or pressure-compensation valves
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66FHOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F9/00Devices for lifting or lowering bulky or heavy goods for loading or unloading purposes
    • B66F9/06Devices for lifting or lowering bulky or heavy goods for loading or unloading purposes movable, with their loads, on wheels or the like, e.g. fork-lift trucks
    • B66F9/075Constructional features or details
    • B66F9/20Means for actuating or controlling masts, platforms, or forks
    • B66F9/22Hydraulic devices or systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B1/00Installations or systems with accumulators; Supply reservoir or sump assemblies
    • F15B1/02Installations or systems with accumulators
    • F15B1/027Installations or systems with accumulators having accumulator charging devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B1/00Installations or systems with accumulators; Supply reservoir or sump assemblies
    • F15B1/02Installations or systems with accumulators
    • F15B1/027Installations or systems with accumulators having accumulator charging devices
    • F15B1/033Installations or systems with accumulators having accumulator charging devices with electrical control means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B11/00Servomotor systems without provision for follow-up action; Circuits therefor
    • F15B11/02Systems essentially incorporating special features for controlling the speed or actuating force of an output member
    • F15B11/04Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed
    • F15B11/05Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed specially adapted to maintain constant speed, e.g. pressure-compensated, load-responsive
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00Details of servomotor systems ; Valves for servomotor systems
    • F15B13/02Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
    • F15B13/026Pressure compensating valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00Details of servomotor systems ; Valves for servomotor systems
    • F15B2013/002Modular valves, i.e. consisting of an assembly of interchangeable components
    • F15B2013/004Cartridge valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/50Pressure control
    • F15B2211/505Pressure control characterised by the type of pressure control means
    • F15B2211/50563Pressure control characterised by the type of pressure control means the pressure control means controlling a differential pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/50Pressure control
    • F15B2211/505Pressure control characterised by the type of pressure control means
    • F15B2211/50563Pressure control characterised by the type of pressure control means the pressure control means controlling a differential pressure
    • F15B2211/50572Pressure control characterised by the type of pressure control means the pressure control means controlling a differential pressure using a pressure compensating valve for controlling the pressure difference across a flow control valve
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/50Pressure control
    • F15B2211/57Control of a differential pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/50Pressure control
    • F15B2211/575Pilot pressure control
    • F15B2211/5753Pilot pressure control for closing a valve
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/60Circuit components or control therefor
    • F15B2211/625Accumulators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/60Circuit components or control therefor
    • F15B2211/665Methods of control using electronic components
    • F15B2211/6658Control using different modes, e.g. four-quadrant-operation, working mode and transportation mode

Definitions

  • the invention relates to a valve with the features in the preamble of claim 1.
  • the use of pressure compensators in hydraulically operating lifting devices is state of the art.
  • the document DE 102 02 607 C1 shows an example of the arrangement of a pressure compensator in a lifting device for lifting and lowering loads to influence the lowering behavior, the pressure compensator being arranged in a return line of a relevant lifting cylinder.
  • Another preferred application is the use in lifting devices that are equipped with a lifting mechanism damping that can be activated or deactivated.
  • a pressure compensator ensures that the accumulator pressure at an associated damping accumulator automatically follows the load pressure of the respective lifting mechanism cylinder, both when the lifting mechanism damping is activated and when the lifting mechanism is deactivated. This ensures that if the lifting mechanism damping is activated, after previously deactivated operation, no uncontrolled lifting or lowering of the lifting mechanism can take place.
  • valve with the features in the preamble of claim 1 with a valve housing which has a control connection and a fluid inlet and a fluid outlet, and with a Control piston arranged longitudinally displaceably in the valve housing, which, against the action of an energy store, in particular in the form of a compression spring, brings the control piston into at least one position forming a fluid-carrying connection between the fluid inlet and the fluid outlet by means of a control pressure prevailing at the control connection, or blocks this connection, in which Control piston a first orifice is arranged, which connects the control connection with a receiving space for the energy storage fluid-carrying, and wherein a second orifice is arranged in an intermediate part in the valve housing, by means of which the receiving space can be connected to a compensation space.
  • the invention is based on the object of providing a valve which is characterized by particularly favorable operating behavior as a pressure compensator for use in hydraulically operated lifting devices which are provided with lifting mechanism damping.
  • this object is achieved by a valve which has the features of claim 1 in its entirety.
  • an essential feature of the invention is that the valve is intended for use as a pressure compensator in hydraulically actuated lifting devices and that the compensation chamber is in fluid communication with the fluid outlet. Due to the arrangement of two diaphragms, which on the one hand lead from the control connection to the receiving space with the spring loading the control piston and, on the other hand, lead from the equalizing chamber leading the pressure of the fluid outlet to the receiving space, the valve represents a kind of piloted pressure compensator the two diaphragms with the spring arranged between them, the control pressure of the pressure compensator generated by the spring is increased.
  • the damping accumulator Since, due to the function of the pressure compensator, the pressure on the damping accumulator follows the load pressure on the lifting cylinder, the damping accumulator is automatically discharged when the lifting cylinder is lowered and is reloaded when it is lifted again.
  • the constant charging process which also takes place in the deactivated damping mode, i.e. with a functionless damping memory, requires pump power, which costs energy and which reduces the lifting speed.
  • an additional switching valve is used between the pump side and the pressure compensator, which blocks this connection in the deactivated damping mode and prevents the accumulator from charging in this mode.
  • the second diaphragm can be closed by means of a pilot control device which can be controlled by an actuating magnet. If an actuating magnet is used, the closing force of which is greater than the hydraulic force acting on the control piston, the pilot oil flow is prevented when the magnet is actuated and the control piston of the pressure compensator is therefore in the closed position, so that the pressure compensator is blocked.
  • a pilot control device which can be controlled by an actuating magnet. If an actuating magnet is used, the closing force of which is greater than the hydraulic force acting on the control piston, the pilot oil flow is prevented when the magnet is actuated and the control piston of the pressure compensator is therefore in the closed position, so that the pressure compensator is blocked.
  • the pilot control device has a pilot cone which interacts with a valve seat on the intermediate part and on which two energy stores, in particular in the form of compression springs, act in and against the effective direction of the actuating magnet.
  • the arrangement can advantageously be made in such a way that the compensation space is at least partially accommodated in the intermediate part, which establishes a fluid-conducting connection to a collecting space as a further part of the compensation space that is permanently connected to the fluid outlet via at least one fluid-conducting connection path Valve housing is in communication.
  • the actuation part of the actuation magnet is guided in a connection part of the actuation magnet provided for connecting the actuation magnet to the valve housing, which, at least partially, takes up one energy store of the pilot control device and connects to the intermediate part, the latter and the connection part being stationary on the valve housing are arranged.
  • control piston is designed as a hollow piston, at least in the area of the control connection and at least in the area in which, at least partially, the energy store is accommodated, with one orifice, designed as a screw-in piece, being inserted into the control piston, the two cavities of which permanently connected to each other in a fluid-carrying manner.
  • the orifice is designed as a screw-in piece, identical control pistons can be fitted with different orifices for the desired function adjustment.
  • the control piston can advantageously be provided with a stop part on the side of the intermediate part, which is in one and in the other Stop position can be brought into contact with the valve housing or with the intermediate part.
  • the arrangement can be made such that the control connection is introduced into the valve housing in the axial direction and the fluid inlet and the fluid outlet reach through the valve housing in the radial direction, the hollow piston on the outer circumference with the valve housing Limited annular space, which in the other stop position of the control piston completely passes over the fluid outlet.
  • the invention also relates to a device for damping the lifting mechanism, the device having the features of claim 10.
  • a hydraulically actuated lifting cylinder is denoted by 2, by means of whose working piston 4 a load 6 can be raised and lowered.
  • To control the lifting cylinder 2 its working spaces 8 and 10, which are separate from the working piston 4, are connected to a 4/3-way slide valve 12 which can be controlled by a relevant operator and which has a pressure supply connection P and a tank connection T leading to the tank side.
  • the lifting device is provided with a lifting mechanism damper 14, which is connected to the piston-side working space 8 via a connection point 16 and to the rod-side working space 10 of the lifting cylinder 2 via a connection point 18.
  • the lifting mechanism damping 14 has a hydropneumatic damping accumulator 20, the oil side 22 of which is connected at a connection point 24 to an accumulator line 26.
  • two electrically actuated switching valves 28 and 30 are provided, which can be switched against a mechanical restoring force into an open position to activate the lifting mechanism damping 14.
  • the switching valve 28 connects the piston-side working chamber 8 of the lifting cylinder 2 via the connection point 16 with the storage line 26.
  • the other switching valve 30 connects the rod-side working chamber 10 of the lifting cylinder 2 with a return line 32 leading to the tank side T in the open position Fig.
  • the switching valves 28 and 30 are in a switching position in the absence of electrical actuation in which the switching valve 28 with a check valve 34 blocks the fluid flow from the working chamber 8 to the storage line 26, but the fluid flow in allows reverse direction.
  • switching valve 30 blocks the fluid flow from the rod-side working chamber 10 of the lifting cylinder 2 to the return line 32 with a check valve 36, but enables the fluid flow in the opposite direction.
  • a pressure compensator 38 is inserted between the storage line 26 and the pressure supply connection P, the control connection 40 of which is connected via a control line 42 to the connection point 16, which is connected to the piston-side working chamber 8 of the lifting cylinder 2.
  • the load pressure of the working chamber 8 of the lifting cylinder 2 is therefore applied to the control connection 40 via the control line 42. Since the pressure compensator 38 is connected with its input 44 via a charging line 48 to the pressure supply connection P and with its output 46 to the accumulator line 26, the accumulator pressure of the damping accumulator 20 follows the load pressure of the working chamber 8 of the lifting cylinder 2.
  • the piston-side working chamber 8 of the lifting cylinder 2 is connected to the tank side T via the 4/3-way valve 12 during lowering operations.
  • the switching position shown of the switching valve 28 is therefore discharged via its check valve 34 during each lowering operation of the damping accumulator 20. Since the pressure of the damping accumulator 20 follows the load pressure in the working chamber 8 of the pressure cylinder 2 due to the function of the pressure compensator 38, the damping accumulator 20 is charged again via the charging line 48 with each new lifting process.
  • a switching valve 50 is inserted in the prior art in the charging line 48 between pressure compensator 38 and pressure supply connection P, which a charging current when lifting mechanism damping 14 is deactivated towards the Damping memory 20 prevents and only releases the charging line 48 when the lifting mechanism damping 14 is activated.
  • the charging line 48 is protected against a return flow in the direction of the pressure supply connection P by a check valve 52.
  • the diaphragm or throttle shown in the control line 42 and the diaphragm or throttle in the charging line 48 (each without a reference number) are used for improved control and coordination of the hydraulic circuit (likewise Fig. 3 ).
  • the Fig. 2 shows in a separate representation the design of the pressure compensator 38 according to a first embodiment of the invention.
  • the so-called cartridge design valve has a valve housing 54 with an open end 56 and an end which is closed in a pressure-tight manner by a screwed-in end piece 58.
  • the valve housing 54 can be installed in a valve block, not shown, in the manner customary for cartridge cartridges.
  • a guide cylinder 60 extends in the valve housing 54 to a spring receiving space 62 with an enlarged inner diameter of which the bores 64 closest to the open end 56 connect the fluid inlet 44 ( Fig. 1 ) and the other bores 66 the fluid outlet 46 ( Fig. 1 ) form.
  • the open housing end 56 forms the control connection 40 of the valve.
  • a control piston 68 is guided in a longitudinally displaceable manner, which is designed as a hollow piston and is loaded at its inner end by a compression spring 70 provided as an energy store.
  • the end of the compression spring 70 facing away from the control piston 68 is supported on an intermediate part 72, which on the one hand rests on a step 74 of the valve housing 54 and on the other hand rests on the end piece 58 in Is set in the axial direction and seals the spring receiving space 62 by means of a sealing device 76.
  • the in Fig. 2 As shown in the depressurized state, the control piston 68 is moved by the compression spring 70 into an end position in which the control piston 68 rests with an end stop part 78 on a housing step located at the end of the spring receiving space 62. In the other end position displaced against the force of the compression spring 70, the control piston 68 rests with the stop part 78 on the intermediate part 72.
  • the control piston 68 has an outer annular space 80 into which the fluid inlet 44 formed by the bores 64 opens and whose axially inner end forms a control edge 82.
  • the in Fig. 2 In the illustrated end position of the control piston 68, the depressurized state shown is the control edge 82 in front of the bores 66, so that the fluid outlet 46 is closed.
  • control edge 82 In the control position of the control piston 68 shifted against the force of the compression spring 70, the control edge 82 exposes the connection to the annular space 80, with the control edge 82 completely traversing the bores 66 of the fluid outlet 46 when the control piston 68 is in the right end position.
  • the control piston 68 designed as a hollow piston has, in the area adjoining the spring receiving space 62, an area tapered in internal diameter with an internal thread 84 into which a screw-in piece 86 is screwed, in which a first orifice 88 is located, which has the control input 40 the spring receiving space 62 connects.
  • a second panel 90 is formed which connects the spring receiving space 62 with a compensation space 92 located in the intermediate part 72, which in turn is connected via radial bores 94 with a collecting space 96, which is as Annular space between the outer circumference of the intermediate part 72 and the inside of the valve housing 54 is located.
  • the collecting space 96 is above inclined connecting sections 98 in the valve housing 54
  • Fluid ducts in the valve block, not shown, are connected to the fluid outlet 46 formed by the bores 66, so that the pressure of the damping accumulator 20 is effective on the second diaphragm 90 via the connecting paths 98, the collecting chamber 96 and the compensation chamber 92.
  • the combination of the two orifices 88 and 90 with the compression spring 70 in between forms a type of pilot control for the pressure compensator, the pilot oil flow flowing through the second orifice 90 increasing the control pressure generated by the compression spring 70.
  • the Fig. 3 shows how the Fig. 1 , the circuit of a hydraulically actuated lifting device, wherein the lifting mechanism damper 14 works with a pressure compensator according to a second embodiment of the valve according to the invention, which is shown in Fig. 4 is shown separately in longitudinal section.
  • the valve housing 54 of the second exemplary embodiment corresponds in construction to the first exemplary embodiment, as are the internal components, such as control piston 54 with first aperture 88, compression spring 70, intermediate part 72 as the closure of spring receiving space 62 and second aperture 90.
  • the compensation space 92 formed in the intermediate part 72 is not closed by a closed end piece 58, but is replaced by a connection part 102 screwed into the valve housing 54 for an actuating magnet 104.
  • the connection part 102 rests on the intermediate part 72 for its axial fixing.
  • the actuation magnet 104 has an axially displaceable actuation part 106 which, when the magnet 104 is energized, in Fig. 4 moves to the left.
  • the actuating part 106 which is guided displaceably in the connection part 102, extends into a chamber 108 formed in the connection part 102, which forms a continuation of the adjoining compensation space 92 in the intermediate part 72.
  • the actuating part 106 is used to control a pilot cone 110, for which a valve seat 112 is formed on the intermediate part 72. This is located on the intermediate part 72 in front of the access to the second panel 90, so that it can be closed by the pilot cone 110.
  • a third compression spring 120 is inserted between the pressure plate 118 and the intermediate part 72, the spring force of which is less than that of the other pressure spring 116 resting on the pressure plate 118.
  • the second diaphragm 90 can be closed by means of the pilot cone 110 when the magnet 104 is actuated, or can be released by means of the restoring force of the third compression spring 120 when the electromagnet 104 is not actuated.
  • the pilot oil flow is prevented, so that the control piston 68 closes the connection between the fluid inlet 44 and the fluid outlet 46.
  • the valve assumes not only the function of the pressure compensator 38 when the lifting mechanism damping 14 is activated, but also the function of the switching valve 50, which blocks the charging line 48, when the lifting mechanism damping 14 is deactivated Fig. 1 and replaces this.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • Transportation (AREA)
  • Structural Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Civil Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Safety Valves (AREA)

Description

Die Erfindung betrifft ein Ventil mit den Merkmalen im Oberbegriff von Anspruch 1.The invention relates to a valve with the features in the preamble of claim 1.

Der Einsatz von Druckwaagen bei hydraulisch arbeitenden Hubeinrichtungen ist Stand der Technik. Das Dokument DE 102 02 607 C1 zeigt beispielhaft die Anordnung einer Druckwaage bei einer Hubeinrichtung zum Anheben und Absenken von Lasten zur Beeinflussung des Senkverhaltens, wobei die Druckwaage in einer Rücklaufleitung eines betreffenden Hubzylinders angeordnet ist. Eine weitere bevorzugte Anwendung ist der Einsatz bei Hubeinrichtungen, die mit einer aktivierbaren oder deaktivierbaren Hubwerksdämpfung ausgerüstet sind. Mittels einer Druckwaage wird hierbei sichergestellt, dass der Speicherdruck an einem zugeordneten Dämpfungsspeicher sowohl bei aktivierter als auch bei deaktivierter Hubwerksdämpfung selbsttätig dem Lastdruck des betreffenden Hubwerkzylinders folgt. Dadurch ist gewährleistet, dass im Falle des Aktivierens der Hubwerksdämpfung, nach vorausgehendem deaktiviertem Betrieb, kein unkontrolliertes Heben oder Senken des Hubwerks stattfinden kann.The use of pressure compensators in hydraulically operating lifting devices is state of the art. The document DE 102 02 607 C1 shows an example of the arrangement of a pressure compensator in a lifting device for lifting and lowering loads to influence the lowering behavior, the pressure compensator being arranged in a return line of a relevant lifting cylinder. Another preferred application is the use in lifting devices that are equipped with a lifting mechanism damping that can be activated or deactivated. A pressure compensator ensures that the accumulator pressure at an associated damping accumulator automatically follows the load pressure of the respective lifting mechanism cylinder, both when the lifting mechanism damping is activated and when the lifting mechanism is deactivated. This ensures that if the lifting mechanism damping is activated, after previously deactivated operation, no uncontrolled lifting or lowering of the lifting mechanism can take place.

Die WO 2006/084576 A1 beschreibt Ventil mit den Merkmalen im Oberbegriff von Anspruch 1 mit einem Ventilgehäuse, das einen Steueranschluss sowie einen Fluideingang und einen Fluidausgang aufweist, und mit einem im Ventilgehäuse längsverfahrbar angeordneten Regelkolben, der entgegen der Wirkung eines Energiespeichers, insbesondere in Form einer Druckfeder, mittels eines am Steueranschluss herrschenden Steuerdrucks den Regelkolben in mindestens eine eine fluidführende Verbindung zwischen dem Fluideingang und dem Fluidausgang bildende Stellung bringt oder diese Verbindung sperrt, wobei in dem Regelkolben eine erste Blende angeordnet ist, die den Steueranschluss mit einem Aufnahmeraum für den Energiespeicher fluidführend verbindet, und wobei eine zweite Blende in einem Zwischenteil im Ventilgehäuse angeordnet ist, mittels deren der Aufnahmeraum mit einem Ausgleichsraum verbindbar ist.the WO 2006/084576 A1 describes valve with the features in the preamble of claim 1 with a valve housing which has a control connection and a fluid inlet and a fluid outlet, and with a Control piston arranged longitudinally displaceably in the valve housing, which, against the action of an energy store, in particular in the form of a compression spring, brings the control piston into at least one position forming a fluid-carrying connection between the fluid inlet and the fluid outlet by means of a control pressure prevailing at the control connection, or blocks this connection, in which Control piston a first orifice is arranged, which connects the control connection with a receiving space for the energy storage fluid-carrying, and wherein a second orifice is arranged in an intermediate part in the valve housing, by means of which the receiving space can be connected to a compensation space.

Weitere Ventile gehen aus der DE 36 05 980 A1 , der EP 2 698 545 A2 und der EP 3 309 644 A1 hervor.More valves go out of the DE 36 05 980 A1 , the EP 2 698 545 A2 and the EP 3 309 644 A1 emerged.

Ausgehend von diesem Stand der Technik stellt sich die Erfindung die Aufgabe, ein Ventil zur Verfügung zu stellen, das sich als Druckwaage für den Einsatz bei hydraulisch betätigten Hubeinrichtungen, die mit Hubwerksdämpfung versehen sind, durch ein besonders günstiges Betriebsverhalten auszeichnet.Based on this prior art, the invention is based on the object of providing a valve which is characterized by particularly favorable operating behavior as a pressure compensator for use in hydraulically operated lifting devices which are provided with lifting mechanism damping.

Erfindungsgemäß ist diese Aufgabe durch ein Ventil gelöst, das die Merkmale des Patentanspruchs 1 in seiner Gesamtheit aufweist.According to the invention, this object is achieved by a valve which has the features of claim 1 in its entirety.

Gemäß dem kennzeichnenden Teil des Anspruchs 1 besteht eine wesentliche Besonderheit der Erfindung darin, dass das Ventil für den Einsatz als Druckwaage bei hydraulisch betätigbaren Hubeinrichtungen vorgesehen ist und dass der Ausgleichsraum in fluidführender Verbindung mit dem Fluidausgang steht. Durch die Anordnung zweier Blenden, die einerseits vom Steueranschluss her zu dem Aufnahmeraum mit der den Regelkolben belastenden Feder führen und andererseits von dem den Druck des Fluidausgangs führenden Ausgleichsraum her zum Aufnahmeraum führen, stellt das Ventil eine Art vorgesteuerte Druckwaage dar. Durch die Kombination aus den beiden Blenden mit der dazwischen angeordneten Feder wird der von der Feder erzeugte Regeldruck der Druckwaage verstärkt. Dies begünstigt eine kompakte Bauweise mit kleindimensionierter Druckfeder in der Art eines sog. Cartridge-Ventils, das sich besonders für den Einsatz bei Hubeinrichtungen mobiler Einheiten, wie Staplern, Autokrane oder dergleichen, eignet, bei denen für die Hydraulikkomponenten ein begrenzter Einbauraum zur Verfügung steht.According to the characterizing part of claim 1, an essential feature of the invention is that the valve is intended for use as a pressure compensator in hydraulically actuated lifting devices and that the compensation chamber is in fluid communication with the fluid outlet. Due to the arrangement of two diaphragms, which on the one hand lead from the control connection to the receiving space with the spring loading the control piston and, on the other hand, lead from the equalizing chamber leading the pressure of the fluid outlet to the receiving space, the valve represents a kind of piloted pressure compensator the two diaphragms with the spring arranged between them, the control pressure of the pressure compensator generated by the spring is increased. This favors a compact design with a small compression spring in the manner of a so-called cartridge valve, which is particularly suitable for use in lifting devices of mobile units, such as forklifts, truck cranes or the like, in which there is limited installation space available for the hydraulic components.

Da aufgrund der Funktion der Druckwaage der Druck am Dämpfungsspeicher dem Lastdruck am Hubzylinder folgt, entlädt sich der Dämpfungsspeicher bei Senkvorgängen des Hubzylinders automatisch und wird bei erneuten Hubvorgängen neu geladen. Der ständige Ladeprozess, der auch im deaktivierten Dämpfungsmodus, also bei funktionslosem Dämpfungsspeicher, stattfindet, erfordert Pumpenleistung, was Energie kostet und wodurch sich die Hubgeschwindigkeit reduziert. Beim Stand der Technik wird zur Verhinderung dieses Effektes ein zusätzliches Schaltventil zwischen Pumpenseite und Druckwaage eingesetzt, das diese Verbindung im deaktivierten Dämpfungsmodus sperrt und den Ladeprozess des Speichers in diesem Modus verhindert.Since, due to the function of the pressure compensator, the pressure on the damping accumulator follows the load pressure on the lifting cylinder, the damping accumulator is automatically discharged when the lifting cylinder is lowered and is reloaded when it is lifted again. The constant charging process, which also takes place in the deactivated damping mode, i.e. with a functionless damping memory, requires pump power, which costs energy and which reduces the lifting speed. In the prior art, to prevent this effect, an additional switching valve is used between the pump side and the pressure compensator, which blocks this connection in the deactivated damping mode and prevents the accumulator from charging in this mode.

Im Hinblick auf diese Problematik ist bei einem besonders vorteilhaften Ausführungsbeispiel des erfindungsgemäßen Ventils die zweite Blende mittels einer Vorsteuereinrichtung verschließbar, die von einem Betätigungsmagneten ansteuerbar ist. Bei Einsatz eines Betätigungsmagneten, dessen Schließkraft größer ist als die auf den Regelkolben wirkende hydraulische Kraft, bleibt bei Betätigung des Magneten der Vorsteuerölstrom unterbunden und somit der Regelkolben der Druckwaage in der Schließstellung, so dass die Druckwaage gesperrt ist. Dies ermöglicht die Integration der üblicherweise vom zusätzlichen Schaltventil zur Verfügung gestellten Sperrfunktion in die Patrone der Druckwaage und ermöglicht eine entsprechende Einsparung an Bauaufwand und Bauraum der Dämpfungseinrichtung.In view of this problem, in a particularly advantageous embodiment of the valve according to the invention, the second diaphragm can be closed by means of a pilot control device which can be controlled by an actuating magnet. If an actuating magnet is used, the closing force of which is greater than the hydraulic force acting on the control piston, the pilot oil flow is prevented when the magnet is actuated and the control piston of the pressure compensator is therefore in the closed position, so that the pressure compensator is blocked. This enables the blocking function, which is usually made available by the additional switching valve, to be integrated into the cartridge of the pressure compensator and enables a corresponding saving in terms of construction effort and installation space for the damping device.

Bei vorteilhaften Ausführungsbeispielen weist die Vorsteuereinrichtung einen Vorsteuerkegel auf, der mit einem Ventilsitz am Zwischenteil zusammenwirkt und an dem in und entgegen der Wirkrichtung des Betätigungsmagneten zwei Energiespeicher, insbesondere in Form von Druckfedern, angreifen.In advantageous exemplary embodiments, the pilot control device has a pilot cone which interacts with a valve seat on the intermediate part and on which two energy stores, in particular in the form of compression springs, act in and against the effective direction of the actuating magnet.

Mit Vorteil kann die Anordnung in der Art getroffen sein, dass der Ausgleichsraum, zumindest teilweise, im Zwischenteil aufgenommen ist, das eine fluidführende Verbindung zu einem Sammelraum als einem weiteren Teil des Ausgleichsraums herstellt, der über mindestens eine fluidführende Verbindungsstrecke permanent fluidführend mit dem Fluidausgang im Ventilgehäuse in Verbindung steht.The arrangement can advantageously be made in such a way that the compensation space is at least partially accommodated in the intermediate part, which establishes a fluid-conducting connection to a collecting space as a further part of the compensation space that is permanently connected to the fluid outlet via at least one fluid-conducting connection path Valve housing is in communication.

Bei vorteilhaften Ausführungsbeispielen ist das Betätigungsteil des Betätigungsmagneten in einem für die Verbindung des Betätigungsmagneten mit dem Ventilgehäuse vorgesehenen Anschlussteil des Betätigungsmagneten geführt, das, zumindest teilweise, den einen Energiespeicher der Vorsteuereinrichtung aufnimmt und sich an das Zwischenteil anschließt, wobei Letzteres und das Anschlussteil stationär am Ventilgehäuse angeordnet sind.In advantageous exemplary embodiments, the actuation part of the actuation magnet is guided in a connection part of the actuation magnet provided for connecting the actuation magnet to the valve housing, which, at least partially, takes up one energy store of the pilot control device and connects to the intermediate part, the latter and the connection part being stationary on the valve housing are arranged.

Bei vorteilhaften Ausführungsbeispielen ist der Regelkolben, zumindest im Bereich des Steueranschlusses und zumindest im Bereich, in dem, zumindest teilweise, der eine Energiespeicher aufgenommen ist, als Hohlkolben ausgeführt, wobei die eine Blende, als Einschraubstück ausgeführt, in den Regelkolben eingesetzt, dessen beide Hohlräume permanent fluidführend miteinander verbindet. Bei der Ausbildung der Blende als Einschraubstück können baugleiche Regelkolben für die gewünschte Funktionsanpassung mit unterschiedlichen Blenden bestückt werden.In advantageous embodiments, the control piston is designed as a hollow piston, at least in the area of the control connection and at least in the area in which, at least partially, the energy store is accommodated, with one orifice, designed as a screw-in piece, being inserted into the control piston, the two cavities of which permanently connected to each other in a fluid-carrying manner. When the orifice is designed as a screw-in piece, identical control pistons can be fitted with different orifices for the desired function adjustment.

Mit Vorteil kann der Regelkolben auf der Seite des Zwischenteils mit einem Anschlagteil versehen sein, das in der einen und in der anderen Anschlagstellung in Anlage mit dem Ventilgehäuse bzw. mit dem Zwischenteil bringbar ist.The control piston can advantageously be provided with a stop part on the side of the intermediate part, which is in one and in the other Stop position can be brought into contact with the valve housing or with the intermediate part.

Für die Ausbildung des Ventils in sog. Cartridge-Bauweise kann die Anordnung so getroffen sein, dass der Steueranschluss in axialer Richtung in das Ventilgehäuse eingebracht ist und der Fluideingang und der Fluidausgang in radialer Richtung das Ventilgehäuse durchgreifen, wobei der Hohlkolben außenumfangsseitig mit dem Ventilgehäuse einen Ringraum begrenzt, der in der anderen Anschlagstellung des Regelkolbens den Fluidausgang vollständig überfährt.For the design of the valve in the so-called cartridge design, the arrangement can be made such that the control connection is introduced into the valve housing in the axial direction and the fluid inlet and the fluid outlet reach through the valve housing in the radial direction, the hollow piston on the outer circumference with the valve housing Limited annular space, which in the other stop position of the control piston completely passes over the fluid outlet.

Gegenstand der Erfindung ist auch eine Vorrichtung zur Hubwerksdämpfung, wobei die Vorrichtung die Merkmale des Patentanspruchs 10 aufweist.The invention also relates to a device for damping the lifting mechanism, the device having the features of claim 10.

Nachstehend ist die Erfindung anhand von in der Zeichnung dargestellten Ausführungsbeispielen im Einzelnen erläutert. Es zeigen:

Fig. 1
in Symboldarstellung die Schaltung einer hydraulisch betätigbaren, mit einer Hubwerksdämpfung versehenen Hubeinrichtung;
Fig. 2
einen gegenüber einer praktischen Ausführungsform etwa 3½-fach vergrößert gezeichneten Längsschnitt eines Ausführungsbeispiels des erfindungsgemäßen Ventils, das als Druckwaage bei der Hubeinrichtung von Fig. 1 eingesetzt ist;
Fig. 3
in Symboldarstellung die Schaltung einer hydraulisch betätigbaren, mit einer Hubwerksdämpfung versehenen Hubeinrichtung, die als Druckwaage ein Ventil gemäß einem zweiten Ausführungsbeispiel der Erfindung aufweist; und
Fig. 4
einen Längsschnitt des zweiten Ausführungsbeispiels des erfindungsgemäßen Ventils.
The invention is explained in detail below with reference to the exemplary embodiments shown in the drawing. Show it:
Fig. 1
In a symbolic representation, the circuit of a hydraulically actuated lifting device provided with a lifting mechanism damping;
Fig. 2
a compared to a practical embodiment enlarged approximately 3½ times drawn longitudinal section of an embodiment of the valve according to the invention, which is used as a pressure compensator in the lifting device of Fig. 1 is used;
Fig. 3
In a symbolic representation, the circuit of a hydraulically actuated lifting device provided with a lifting mechanism damping, which has a valve according to a second embodiment of the invention as a pressure compensator; and
Fig. 4
a longitudinal section of the second embodiment of the valve according to the invention.

In Fig. 1 ist ein hydraulisch betätigbarer Hubzylinder mit 2 bezeichnet, mittels dessen Arbeitskolben 4 eine Last 6 anhebbar und absenkbar ist. Zur Steuerung des Hubzylinders 2 sind dessen vom Arbeitskolben 4 getrennte Arbeitsräume 8 und 10 mit einem durch einen betreffenden Bediener ansteuerbaren 4/3-Wege-Schieberventil 12 in Verbindung, das einen Druckversorgungsanschluss P und einen zur Tankseite führenden Tankanschluss T aufweist. Die Hubeinrichtung ist mit einer Hubwerksdämpfung 14 versehen, die über eine Anschlussstelle 16 mit dem kolbenseitigen Arbeitsraum 8 und über eine Anschlussstelle 18 mit dem stangenseitigen Arbeitsraum 10 des Hubzylinders 2 verbunden ist. Die Hubwerksdämpfung 14 weist entsprechend dem Stand der Technik einen hydropneumatischen Dämpfungsspeicher 20 auf, dessen Ölseite 22 an einer Anschlussstelle 24 mit einer Speicherleitung 26 verbunden ist.In Fig. 1 a hydraulically actuated lifting cylinder is denoted by 2, by means of whose working piston 4 a load 6 can be raised and lowered. To control the lifting cylinder 2, its working spaces 8 and 10, which are separate from the working piston 4, are connected to a 4/3-way slide valve 12 which can be controlled by a relevant operator and which has a pressure supply connection P and a tank connection T leading to the tank side. The lifting device is provided with a lifting mechanism damper 14, which is connected to the piston-side working space 8 via a connection point 16 and to the rod-side working space 10 of the lifting cylinder 2 via a connection point 18. According to the prior art, the lifting mechanism damping 14 has a hydropneumatic damping accumulator 20, the oil side 22 of which is connected at a connection point 24 to an accumulator line 26.

Um die Hubeinrichtung in einen Betriebszustand mit deaktivierter Hubwerksdämpfung 14 oder einen Betriebszustand mit aktivierter Hubwerksdämpfung 14 zu bringen, sind zwei elektrisch betätigbare Schaltventile 28 und 30 vorgesehen, die gegen eine mechanische Rückstellkraft in eine Durchlassstellung zur Aktivierung der Hubwerksdämpfung 14 schaltbar sind. In der Durchlassstellung verbindet das Schaltventil 28 den kolbenseitigen Arbeitsraum 8 des Hubzylinders 2 über die Anschlussstelle 16 mit der Speicherleitung 26. Das andere Schaltventil 30 verbindet in der Durchlassstellung den stangenseitigen Arbeitsraum 10 des Hubzylinders 2 mit einer zur Tankseite T führenden Rücklaufleitung 32. In Fig. 1, bei der der Zustand der deaktivierten Hubwerksdämpfung 14 dargestellt ist, befinden sich die Schaltventile 28 und 30 bei fehlender elektrischer Betätigung in einer Schaltstellung, bei der das Schaltventil 28 mit einem Rückschlagventil 34 den Fluidstrom vom Arbeitsraum 8 zur Speicherleitung 26 sperrt, den Fluidstrom jedoch in umgekehrter Richtung ermöglicht. Das andere Schaltventil 30 sperrt bei dieser Schaltstellung mit einem Rückschlagventil 36 den Fluidstrom vom stangenseitigen Arbeitsraum 10 des Hubzylinders 2 zur Rücklaufleitung 32, ermöglicht jedoch den Fluidstrom in umgekehrter Richtung.In order to bring the lifting device into an operating state with deactivated lifting mechanism damping 14 or an operating state with activated lifting mechanism damping 14, two electrically actuated switching valves 28 and 30 are provided, which can be switched against a mechanical restoring force into an open position to activate the lifting mechanism damping 14. In the open position, the switching valve 28 connects the piston-side working chamber 8 of the lifting cylinder 2 via the connection point 16 with the storage line 26. The other switching valve 30 connects the rod-side working chamber 10 of the lifting cylinder 2 with a return line 32 leading to the tank side T in the open position Fig. 1 , in which the state of the deactivated lifting mechanism damping 14 is shown, the switching valves 28 and 30 are in a switching position in the absence of electrical actuation in which the switching valve 28 with a check valve 34 blocks the fluid flow from the working chamber 8 to the storage line 26, but the fluid flow in allows reverse direction. The other In this switching position, switching valve 30 blocks the fluid flow from the rod-side working chamber 10 of the lifting cylinder 2 to the return line 32 with a check valve 36, but enables the fluid flow in the opposite direction.

In der bei Hubwerksdämpfungen üblichen Weise ist zwischen der Speicherleitung 26 und dem Druckversorgungsanschluss P eine Druckwaage 38 eingefügt, deren Steueranschluss 40 über eine Steuerleitung 42 mit der Anschlussstelle 16 in Verbindung ist, die mit dem kolbenseitigen Arbeitsraum 8 des Hubzylinders 2 verbunden ist. Über die Steuerleitung 42 liegt daher am Steueranschluss 40 der Lastdruck des Arbeitsraums 8 des Hubzylinders 2 an. Da die Druckwaage 38 mit ihrem Eingang 44 über eine Ladeleitung 48 mit dem Druckversorgungsanschluss P und mit ihrem Ausgang 46 mit der Speicherleitung 26 in Verbindung ist, folgt der Speicherdruck des Dämpfungsspeichers 20 dem Lastdruck des Arbeitsraums 8 des Hubzylinders 2.In the usual way with lifting mechanism damping, a pressure compensator 38 is inserted between the storage line 26 and the pressure supply connection P, the control connection 40 of which is connected via a control line 42 to the connection point 16, which is connected to the piston-side working chamber 8 of the lifting cylinder 2. The load pressure of the working chamber 8 of the lifting cylinder 2 is therefore applied to the control connection 40 via the control line 42. Since the pressure compensator 38 is connected with its input 44 via a charging line 48 to the pressure supply connection P and with its output 46 to the accumulator line 26, the accumulator pressure of the damping accumulator 20 follows the load pressure of the working chamber 8 of the lifting cylinder 2.

Beim Betrieb der Hubeinrichtung mit deaktivierter Hubwerksdämpfung 14 ist bei Senkvorgängen der kolbenseitige Arbeitsraum 8 des Hubzylinders 2 über das 4/3-Wege-Ventil 12 mit der Tankseite T in Verbindung. Bei der in Fig. 1 gezeigten Schaltstellung des Schaltventils 28 findet daher über dessen Rückschlagventil 34 ein Entladevorgang des Dämpfungsspeichers 20 bei jedem Senkvorgang statt. Da durch die Funktion der Druckwaage 38 der Druck des Dämpfungsspeichers 20 dem Lastdruck im Arbeitsraum 8 des Druckzylinders 2 folgt, findet bei jedem neuen Hubvorgang über die Ladeleitung 48 ein erneuter Ladevorgang des Dämpfungsspeichers 20 statt. Um bei aufeinanderfolgenden Senk- und Hubvorgängen des Hubzylinders 2 bei deaktivierter Hubwerksdämpfung 14 die aufeinanderfolgenden Ladevorgänge des Dämpfungsspeichers 20 zu vermeiden, ist beim Stand der Technik in der Ladeleitung 48 zwischen Druckwaage 38 und Druckversorgungsanschluss P ein Schaltventil 50 eingefügt, das bei deaktivierter Hubwerksdämpfung 14 einen Ladestrom in Richtung auf den Dämpfungsspeicher 20 unterbindet und lediglich bei aktivierter Hubwerksdämpfung 14 die Ladeleitung 48 freigibt. Zusätzlich ist die Ladeleitung 48 durch ein Rückschlagventil 52 gegen einen Rückstrom in Richtung auf den Druckversorgungsanschluss P abgesichert. Die in der Fig. 1 gezeigte Blende oder Drossel in der Steuerleitung 42 sowie die Blende oder Drossel in der Ladeleitung 48 (jeweils ohne Bezugszeichen) dienen der verbesserten Ansteuerung sowie der Abstimmung des Hydraulikkreises (ebenso Fig. 3).When operating the lifting device with deactivated lifting mechanism damping 14, the piston-side working chamber 8 of the lifting cylinder 2 is connected to the tank side T via the 4/3-way valve 12 during lowering operations. At the in Fig. 1 The switching position shown of the switching valve 28 is therefore discharged via its check valve 34 during each lowering operation of the damping accumulator 20. Since the pressure of the damping accumulator 20 follows the load pressure in the working chamber 8 of the pressure cylinder 2 due to the function of the pressure compensator 38, the damping accumulator 20 is charged again via the charging line 48 with each new lifting process. In order to avoid the successive charging processes of the damping accumulator 20 during successive lowering and lifting operations of the lifting cylinder 2 with deactivated lifting mechanism damping 14, a switching valve 50 is inserted in the prior art in the charging line 48 between pressure compensator 38 and pressure supply connection P, which a charging current when lifting mechanism damping 14 is deactivated towards the Damping memory 20 prevents and only releases the charging line 48 when the lifting mechanism damping 14 is activated. In addition, the charging line 48 is protected against a return flow in the direction of the pressure supply connection P by a check valve 52. The one in the Fig. 1 The diaphragm or throttle shown in the control line 42 and the diaphragm or throttle in the charging line 48 (each without a reference number) are used for improved control and coordination of the hydraulic circuit (likewise Fig. 3 ).

Die Fig. 2 zeigt in gesonderter Darstellung die Ausbildung der Druckwaage 38 gemäß einem ersten Ausführungsbeispiel der Erfindung. Das in sog. Cartridge-Bauweise ausgeführte Ventil weist ein Ventilgehäuse 54 mit einem offenen Ende 56 und einem durch ein eingeschraubtes Endstück 58 druckdicht abgeschlossenes Ende auf. Mit seinem in Fig. 2 linksseitigen Gehäuseabschnitt ist das Ventilgehäuse 54 in bei Cartridge-Patronen üblicher Weise in einen nicht gezeigten Ventilblock einbaubar. Vom offenen Ende 56 her erstreckt sich im Ventilgehäuse 54 ein Führungszylinder 60 bis zu einem im Innendurchmesser erweiterten Feder-Aufnahmeraum 62. Im Bereich des Führungszylinders 60 weist das Ventilgehäuse 54 axial zueinander versetzte Bohrungen 64 und 66 auf, die den Zugang zum Führungszylinder 60 bilden und von denen die dem offenen Ende 56 nächstgelegenen Bohrungen 64 den Fluideingang 44 (Fig. 1) und die anderen Bohrungen 66 den Fluidausgang 46 (Fig. 1) bilden. Das offene Gehäuseende 56 bildet den Steueranschluss 40 des Ventils.the Fig. 2 shows in a separate representation the design of the pressure compensator 38 according to a first embodiment of the invention. The so-called cartridge design valve has a valve housing 54 with an open end 56 and an end which is closed in a pressure-tight manner by a screwed-in end piece 58. With his in Fig. 2 On the left-hand side of the housing section, the valve housing 54 can be installed in a valve block, not shown, in the manner customary for cartridge cartridges. From the open end 56, a guide cylinder 60 extends in the valve housing 54 to a spring receiving space 62 with an enlarged inner diameter of which the bores 64 closest to the open end 56 connect the fluid inlet 44 ( Fig. 1 ) and the other bores 66 the fluid outlet 46 ( Fig. 1 ) form. The open housing end 56 forms the control connection 40 of the valve.

Im Führungszylinder 60 ist ein Regelkolben 68 längsverfahrbar geführt, der als Hohlkolben ausgebildet ist und an seinem innenliegenden Ende durch eine als Energiespeicher vorgesehene Druckfeder 70 belastet ist. Das vom Regelkolben 68 abgewandte Ende der Druckfeder 70 stützt sich dabei an einem Zwischenteil 72 ab, das einerseits durch Anlage an einer Stufe 74 des Ventilgehäuses 54 und andererseits durch Anlage am Endstück 58 in Axialrichtung festgelegt ist und den Feder-Aufnahmeraum 62 mittels einer Dichteinrichtung 76 abdichtet.In the guide cylinder 60, a control piston 68 is guided in a longitudinally displaceable manner, which is designed as a hollow piston and is loaded at its inner end by a compression spring 70 provided as an energy store. The end of the compression spring 70 facing away from the control piston 68 is supported on an intermediate part 72, which on the one hand rests on a step 74 of the valve housing 54 and on the other hand rests on the end piece 58 in Is set in the axial direction and seals the spring receiving space 62 by means of a sealing device 76.

Bei dem in Fig. 2 gezeigten, drucklosen Zustand ist der Regelkolben 68 durch die Druckfeder 70 in eine Endstellung bewegt, in der der Regelkolben 68 mit einem endseitigen Anschlagteil 78 an einer am Ende des Feder-Aufnahmeraums 62 befindlichen Gehäusestufe anliegt. In der gegen die Kraft der Druckfeder 70 verschobenen anderen Endstellung liegt der Regelkolben 68 mit dem Anschlagteil 78 am Zwischenteil 72 an. Der Regelkolben 68 weist einen äußeren Ringraum 80 auf, in den der durch die Bohrungen 64 gebildete Fluideingang 44 einmündet und dessen axial innenliegendes Ende eine Steuerkante 82 bildet. Bei dem in Fig. 2 gezeigten, drucklosen Zustand befindet sich bei der dargestellten Endstellung des Regelkolbens 68 die Steuerkante 82 vor den Bohrungen 66, so dass der Fluidausgang 46 geschlossen ist. Bei gegen die Kraft der Druckfeder 70 verschobenen Regelpositionen des Regelkolbens 68 legt die Steuerkante 82 die Verbindung zum Ringraum 80 frei, wobei bei der in die rechte Endstellung verfahrenen Stellung des Regelkolbens 68 die Steuerkante 82 die Bohrungen 66 des Fluidausgangs 46 vollständig überfährt.The in Fig. 2 As shown in the depressurized state, the control piston 68 is moved by the compression spring 70 into an end position in which the control piston 68 rests with an end stop part 78 on a housing step located at the end of the spring receiving space 62. In the other end position displaced against the force of the compression spring 70, the control piston 68 rests with the stop part 78 on the intermediate part 72. The control piston 68 has an outer annular space 80 into which the fluid inlet 44 formed by the bores 64 opens and whose axially inner end forms a control edge 82. The in Fig. 2 In the illustrated end position of the control piston 68, the depressurized state shown is the control edge 82 in front of the bores 66, so that the fluid outlet 46 is closed. In the control position of the control piston 68 shifted against the force of the compression spring 70, the control edge 82 exposes the connection to the annular space 80, with the control edge 82 completely traversing the bores 66 of the fluid outlet 46 when the control piston 68 is in the right end position.

Der als Hohlkolben ausgeführte Regelkolben 68 weist in dem an den Feder-Aufnahmeraum 62 angrenzenden Bereich einen im Innendurchmesser verjüngten Bereich mit einem Innengewinde 84 auf, in das ein Einschraubstück 86 eingeschraubt ist, in dem sich eine erste Blende 88 befindet, die den Steuereingang 40 mit dem Feder-Aufnahmeraum 62 verbindet. In dem an den Feder-Aufnahmeraum 62 angrenzenden Zwischenteil 72 ist eine zweite Blende 90 ausgebildet, die den Feder-Aufnahmeraum 62 mit einem im Zwischenteil 72 befindlichen Ausgleichsraum 92 verbindet, der wiederum über Radialbohrungen 94 mit einem Sammelraum 96 in Verbindung ist, der sich als Ringraum zwischen dem Außenumfang des Zwischenteils 72 und der Innenseite des Ventilgehäuses 54 befindet. Über schräg verlaufende Verbindungsstrecken 98 im Ventilgehäuse 54 ist der Sammelraum 96 über Fluidführungen im nicht gezeigten Ventilblock mit dem durch die Bohrungen 66 gebildeten Fluidausgang 46 in Verbindung, so dass der Druck des Dämpfungsspeichers 20 über die Verbindungsstrecken 98, den Sammelraum 96 und den Ausgleichsraum 92 an der zweiten Blende 90 wirksam ist. Die Kombination aus den beiden Blenden 88 und 90 mit der dazwischenliegenden Druckfeder 70 bildet für die Druckwaage eine Art Vorsteuerung, wobei der über die zweite Blende 90 fließende Vorsteuerölstrom den von der Druckfeder 70 erzeugten Regeldruck verstärkt.The control piston 68 designed as a hollow piston has, in the area adjoining the spring receiving space 62, an area tapered in internal diameter with an internal thread 84 into which a screw-in piece 86 is screwed, in which a first orifice 88 is located, which has the control input 40 the spring receiving space 62 connects. In the intermediate part 72 adjoining the spring receiving space 62, a second panel 90 is formed which connects the spring receiving space 62 with a compensation space 92 located in the intermediate part 72, which in turn is connected via radial bores 94 with a collecting space 96, which is as Annular space between the outer circumference of the intermediate part 72 and the inside of the valve housing 54 is located. The collecting space 96 is above inclined connecting sections 98 in the valve housing 54 Fluid ducts in the valve block, not shown, are connected to the fluid outlet 46 formed by the bores 66, so that the pressure of the damping accumulator 20 is effective on the second diaphragm 90 via the connecting paths 98, the collecting chamber 96 and the compensation chamber 92. The combination of the two orifices 88 and 90 with the compression spring 70 in between forms a type of pilot control for the pressure compensator, the pilot oil flow flowing through the second orifice 90 increasing the control pressure generated by the compression spring 70.

Die Fig. 3 zeigt, wie die Fig. 1, die Schaltung einer hydraulisch betätigbaren Hubeinrichtung, wobei die Hubwerksdämpfung 14 mit einer Druckwaage gemäß einem zweiten Ausführungsbeispiel des erfindungsgemäßen Ventils arbeitet, das in Fig. 4 gesondert im Längsschnitt dargestellt ist. Das Ventilgehäuse 54 des zweiten Ausführungsbeispiels entspricht in der Bauweise dem ersten Ausführungsbeispiel, ebenso wie die inneren Komponenten, wie Regelkolben 54 mit erster Blende 88, Druckfeder 70, Zwischenteil 72 als Abschluss des Feder-Aufnahmeraums 62 und zweite Blende 90. Im Unterschied zum ersten Ausführungsbeispiel ist der im Zwischenteil 72 gebildete Ausgleichsraum 92 nicht durch ein geschlossenes Endstück 58 abgeschlossen, sondern ist durch ein in das Ventilgehäuse 54 eingeschraubtes Anschlussteil 102 für einen Betätigungsmagneten 104 ersetzt. Wie das Endstück 58 des ersten Ausführungsbeispiels liegt das Anschlussteil 102 am Zwischenteil 72 für dessen axiale Festlegung an.the Fig. 3 shows how the Fig. 1 , the circuit of a hydraulically actuated lifting device, wherein the lifting mechanism damper 14 works with a pressure compensator according to a second embodiment of the valve according to the invention, which is shown in Fig. 4 is shown separately in longitudinal section. The valve housing 54 of the second exemplary embodiment corresponds in construction to the first exemplary embodiment, as are the internal components, such as control piston 54 with first aperture 88, compression spring 70, intermediate part 72 as the closure of spring receiving space 62 and second aperture 90. In contrast to the first exemplary embodiment the compensation space 92 formed in the intermediate part 72 is not closed by a closed end piece 58, but is replaced by a connection part 102 screwed into the valve housing 54 for an actuating magnet 104. Like the end piece 58 of the first exemplary embodiment, the connection part 102 rests on the intermediate part 72 for its axial fixing.

Der Betätigungsmagnet 104 weist ein axial verfahrbares Betätigungsteil 106 auf, das bei Bestromung des Magneten 104 in Fig. 4 nach links verfährt. Das im Anschlussteil 102 verschiebbar geführte Betätigungsteil 106 erstreckt sich in eine im Anschlussteil 102 gebildete Kammer 108, die eine Fortsetzung des sich anschließenden Ausgleichsraums 92 im Zwischenteil 72 bildet. Das Betätigungsteil 106 dient zur Steuerung eines Vorsteuerkegels 110, für den am Zwischenteil 72 ein Ventilsitz 112 gebildet ist. Dieser befindet sich am Zwischenteil 72 vor dem Zugang zur zweiten Blende 90, so dass diese durch den Vorsteuerkegel 110 verschließbar ist. Das Betätigungsteil 106 liegt mit seinem freien Ende an einem in der Kammer 108 befindlichen Druckstück 114 an, an dem sich eine zweite Druckfeder 116 mit ihrem einen Ende abstützt, die mit ihrem anderen Ende an einem Druckteller 118 anliegt, der einen im Durchmesser erweiterten, rückwärtigen Teil des Ventilkegels 110 bildet. Für die Rückstellung des Vorsteuerkegels 110, d.h. das Abheben vom Ventilsitz 112 bei nicht bestromtem Betätigungsmagneten 104, ist zwischen dem Druckteller 118 und dem Zwischenteil 72 eine dritte Druckfeder 120 eingesetzt, deren Federkraft geringer ist als diejenige der anderen, am Druckteller 118 anliegenden Druckfeder 116.The actuation magnet 104 has an axially displaceable actuation part 106 which, when the magnet 104 is energized, in Fig. 4 moves to the left. The actuating part 106, which is guided displaceably in the connection part 102, extends into a chamber 108 formed in the connection part 102, which forms a continuation of the adjoining compensation space 92 in the intermediate part 72. The actuating part 106 is used to control a pilot cone 110, for which a valve seat 112 is formed on the intermediate part 72. This is located on the intermediate part 72 in front of the access to the second panel 90, so that it can be closed by the pilot cone 110. The free end of the actuating part 106 rests against a pressure piece 114 located in the chamber 108, on which a second compression spring 116 is supported with its one end, the other end of which rests against a pressure plate 118 which has a rearward enlarged diameter Part of the valve cone 110 forms. For resetting the pilot cone 110, that is, lifting off the valve seat 112 when the actuating magnet 104 is not energized, a third compression spring 120 is inserted between the pressure plate 118 and the intermediate part 72, the spring force of which is less than that of the other pressure spring 116 resting on the pressure plate 118.

Bei dieser Anordnung ist die zweite Blende 90 bei betätigtem Magneten 104 mittels des Vorsteuerkegels 110 verschließbar oder bei nicht betätigtem Elektromagneten 104 mittels der Rückstellkraft der dritten Druckfeder 120 freigebbar. Bei durch den Betätigungsmagneten 104 geschlossener zweiter Blende 90 ist der Vorsteuerölstrom unterbunden, so dass der Regelkolben 68 die Verbindung zwischen Fluideingang 44 und Fluidausgang 46 schließt. Bei Einsatz als Druckwaage 38 bei der Hubwerksdämpfung 14, wie in Fig. 3 gezeigt, übernimmt das Ventil nicht nur bei aktivierter Hubwerksdämpfung 14 die Funktion der Druckwaage 38, sondern bei deaktivierter Hubwerksdämpfung 14 zusätzlich die Funktion des die Ladeleitung 48 sperrenden Schaltventils 50 von Fig. 1 und ersetzt dieses.In this arrangement, the second diaphragm 90 can be closed by means of the pilot cone 110 when the magnet 104 is actuated, or can be released by means of the restoring force of the third compression spring 120 when the electromagnet 104 is not actuated. When the second diaphragm 90 is closed by the actuating magnet 104, the pilot oil flow is prevented, so that the control piston 68 closes the connection between the fluid inlet 44 and the fluid outlet 46. When used as a pressure compensator 38 in the lifting mechanism damping 14, as in Fig. 3 As shown, the valve assumes not only the function of the pressure compensator 38 when the lifting mechanism damping 14 is activated, but also the function of the switching valve 50, which blocks the charging line 48, when the lifting mechanism damping 14 is deactivated Fig. 1 and replaces this.

Claims (11)

  1. Valve with a valve housing (54), which has a control connection (40) as well as a fluid inlet (64) and a fluid outlet (66), and with a control piston (68), which is arranged so as to be longitudinally movable in the valve housing (54) and, counter to the action of an energy accumulator (70), in particular in the form of a compression spring, by means of a control pressure prevailing at the control connection (40) brings the control piston (68) into at least one position forming a fluid-conducting connection between the fluid inlet (40) and the fluid outlet (66) or blocks this connection, wherein a first orifice (88) is arranged in the control piston (68), which orifice connects the control connection (40) to a receiving chamber (62) for the energy accumulator (70) in a fluid-conducting manner, and wherein a second orifice (90) is arranged in an intermediate part (72) in the valve housing (54), by means of which the receiving space (62) can be connected to a compensating chamber (92), characterised in that the valve is provided for use as a pressure compensator (38) in hydraulically operable lifting devices (2) and in that the compensating chamber (92) is in fluid-conducting connection (98) with the fluid outlet (66).
  2. Valve according to claim 1, characterised in that the second orifice (90) can be closed by means of a pilot control device (110) which can be controlled by an actuating magnet (104).
  3. Valve according to claim 2, characterised in that the pilot control device has a pilot control cone (110) which cooperates with a valve seat (112) on the intermediate part (72) and on which two energy accumulators (116, 120), in particular in the form of compression springs, act in and contrary to the direction of action of the actuating magnet (104).
  4. Valve according to claim 1 or 2, characterised in that the compensating chamber (92) is accommodated, at least in part, in the intermediate part (72) which establishes a fluid-conducting connection (94) to a collecting chamber (96) as a further part of the compensating chamber (92), which compensating chamber is in permanent fluid-conducting communication with the fluid outlet (66) in the valve housing (54) via at least one fluid-conducting connecting path (98).
  5. Valve according to claim 3, characterised in that the actuating part (106) of the actuating magnet (104) is guided in a connection part (102) of the actuating magnet (104) which is provided for connecting the actuating magnet (104) to the valve housing (54), which connection part accommodates, at least in part, the one energy accumulator (116) of the pilot control device (110) and connects to the intermediate part (72).
  6. Valve according to claim 5, characterised in that the intermediate part (72) and the connection part (102) are arranged fixedly on the valve housing (54).
  7. Valve according to one of the preceding claims, characterised in that the control piston (68), at least in the region of the control connection (40) and at least in the region in which the one energy accumulator (70) is, at least in part, accommodated, is configured as a hollow piston, and in that the one orifice (88), configured as a screw-in piece (86) and inserted into the control piston (68), permanently connects the two cavities thereof to each other in a fluid-conducting manner.
  8. Valve according to one of the preceding claims, characterised in that the control piston (68) is provided on the side of the intermediate part (72) with a stop part (78) which in the one stop position and in the other stop position can be brought into contact with the valve housing (54) and with the intermediate part (72) respectively.
  9. Valve according to claim 7 and claim 8, characterised in that the control connection (40) is introduced into the valve housing (54) in the axial direction and the fluid inlet (64) and the fluid outlet (66) pass through the valve housing (54) in the radial direction, and in that on the outer circumference the hollow piston with the valve housing (54) delimits an annular space (80) which completely crosses over the fluid outlet (66) in the other stop position of the control piston (68).
  10. Device for damping lifting gear having a pressure supply source (P), a pressure accumulator device (20), at least one hydraulic consumer (2), in particular in the form of a hydraulic operating cylinder, and a valve according to one of the preceding claims which with a working chamber (8) of the hydraulic consumer (2) is connected in a fluid-conducting manner to the control connection (40) of the valve, the fluid inlet (64) of which is connected to the pressure supply source (P) and the fluid outlet (66) of which is connected to the pressure accumulator device (20).
  11. Valve according to claim 10, characterised in that the one working chamber (8), which is connected to the control connection (40) of the valve, is simultaneously connected via a stop valve (28) into the fluid-conducting connection (26) between the valve and the pressure accumulator device (20), and in that a further working chamber (10) of the hydraulic consumer (2) is connected via a further stop valve (30) to a return line (32) towards the tank side (T).
EP18766189.7A 2017-09-06 2018-09-05 Valve Active EP3679254B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102017008359.2A DE102017008359A1 (en) 2017-09-06 2017-09-06 Valve
PCT/EP2018/073823 WO2019048455A1 (en) 2017-09-06 2018-09-05 Valve

Publications (2)

Publication Number Publication Date
EP3679254A1 EP3679254A1 (en) 2020-07-15
EP3679254B1 true EP3679254B1 (en) 2021-11-10

Family

ID=63528748

Family Applications (1)

Application Number Title Priority Date Filing Date
EP18766189.7A Active EP3679254B1 (en) 2017-09-06 2018-09-05 Valve

Country Status (4)

Country Link
US (1) US11268544B2 (en)
EP (1) EP3679254B1 (en)
DE (1) DE102017008359A1 (en)
WO (1) WO2019048455A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11781573B2 (en) * 2020-07-23 2023-10-10 Parker-Hannifin Corporation System, valve assembly, and methods for oscillation control of a hydraulic machine
EP4160027A4 (en) * 2020-11-04 2023-11-29 Qingdao Acme Innovation Technology Co., Ltd. Unloading valve and combined-valve-type buffer oil cylinder

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3605980A1 (en) * 1985-03-05 1986-10-16 Barmag Barmer Maschinenfabrik Ag, 5630 Remscheid Proportional valve with pressure-difference balance
DE4140409A1 (en) * 1991-12-07 1993-06-09 Robert Bosch Gmbh, 7000 Stuttgart, De ELECTROHYDRAULIC CONTROL DEVICE
DE10202607C1 (en) 2002-01-24 2003-07-31 Hydac Fluidtechnik Gmbh Control device, in particular for use in hydraulically operating lifting devices
DE102005006321A1 (en) 2005-02-11 2006-08-17 Hydac Fluidtechnik Gmbh Valve, in particular proportional pressure relief valve
DE102009049548A1 (en) * 2009-10-16 2011-04-21 Hydac Fluidtechnik Gmbh valve assembly
JP5750454B2 (en) * 2011-01-06 2015-07-22 日立建機株式会社 Hydraulic drive device for working machine with crawler type traveling device
DE102012010522A1 (en) * 2012-05-25 2013-11-28 Hydac Fluidtechnik Gmbh Valve for valve arrangement
DE102012016457A1 (en) 2012-08-17 2014-02-20 Hydac System Gmbh Device for controlling the state of charge of at least one pressure accumulator
DE102016012335A1 (en) 2016-10-14 2018-04-19 Hydac Fluidtechnik Gmbh Valve device and pressure control system with such a valve device

Also Published As

Publication number Publication date
WO2019048455A1 (en) 2019-03-14
US11268544B2 (en) 2022-03-08
DE102017008359A1 (en) 2019-03-07
EP3679254A1 (en) 2020-07-15
US20200347855A1 (en) 2020-11-05

Similar Documents

Publication Publication Date Title
DE102009061003B4 (en) Adjustable damper valve device
EP3080461B1 (en) Valve assembly
DE102010063386B4 (en) Adjustable damper valve device
EP3394454B1 (en) Valve, in particular a 4/2-way slide valve
EP3005008B1 (en) Proportional pressure-regulating valve
EP2382520A2 (en) Proportional pressure control valve
EP3256742B1 (en) Pressure-limiting valve
DE3323363A1 (en) PRE-CONTROLLED PRESSURE REDUCING VALVE
DE10150238A1 (en) Pressure regulating valve, in particular proportional pressure regulating valve
DE102012220863A1 (en) Control arrangement for driving e.g. hydraulic cylinder for e.g. hydraulic excavators, has control surface of pilot or primary stage of directly or servo-controlled lowering brake valve device acted upon by return control pressure
EP3721094B1 (en) Valve device
EP3679254B1 (en) Valve
DE1750500B2 (en) HYDRAULIC CONTROL SYSTEM WITH AT LEAST ONE HYDRAULIC CYLINDER
EP2880315B1 (en) Valve, in particular pilot-operated proportional directional poppet valve
EP2880316B1 (en) Valve, in particular pilot-operated proportional directional poppet valve
WO2006105765A1 (en) Directional control valve and control system provided therewith
WO2004109124A1 (en) Proportional pressure control valve
DE102009050007A1 (en) Hydraulic valve for use as multi-way-switchover valve in hydraulic connection with base valve, has three-way region designed in seat valve technique
DE102016007754A1 (en) Valve device for influencing a media flow
WO2006092274A2 (en) Hydraulic valve
DE102014222326A1 (en) hydraulic arrangement
DE102009019068B4 (en) pressure monitoring circuit
DE19750253C2 (en) Load-holding valve arrangement
DE8508774U1 (en) Hydraulic control pressure transmitter
DE102021003039A1 (en) Valve

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: UNKNOWN

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20200406

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20210621

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1446346

Country of ref document: AT

Kind code of ref document: T

Effective date: 20211115

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502018007788

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20211110

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220210

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220310

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220310

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220210

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220211

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502018007788

Country of ref document: DE

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20220811

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20220930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220905

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220930

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220905

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20180905

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211110

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20240930

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20240715

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20240716

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20240910

Year of fee payment: 7