EP0828945B1 - Pilot controlled servo-valve - Google Patents

Pilot controlled servo-valve Download PDF

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Publication number
EP0828945B1
EP0828945B1 EP95937068A EP95937068A EP0828945B1 EP 0828945 B1 EP0828945 B1 EP 0828945B1 EP 95937068 A EP95937068 A EP 95937068A EP 95937068 A EP95937068 A EP 95937068A EP 0828945 B1 EP0828945 B1 EP 0828945B1
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EP
European Patent Office
Prior art keywords
main
spring
main control
control piston
control
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.)
Expired - Lifetime
Application number
EP95937068A
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German (de)
French (fr)
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EP0828945A1 (en
Inventor
Arsène Bourkel
Bernd Lanfermann
Karl Tratberger
Karl-Heinz Post
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Hydrolux SARL
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Hydrolux SARL
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Publication of EP0828945A1 publication Critical patent/EP0828945A1/en
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    • 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
    • F15B13/0401Valve members; Fluid interconnections therefor
    • F15B13/0402Valve members; Fluid interconnections therefor for linearly sliding valves, e.g. spool valves
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/8593Systems
    • Y10T137/86493Multi-way valve unit
    • Y10T137/86574Supply and exhaust
    • Y10T137/86582Pilot-actuated
    • Y10T137/86606Common to plural valve motor chambers
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/8593Systems
    • Y10T137/86493Multi-way valve unit
    • Y10T137/86574Supply and exhaust
    • Y10T137/86582Pilot-actuated
    • Y10T137/86614Electric

Definitions

  • the invention relates to a pilot operated servo valve with four Power terminals.
  • Pilot operated electrohydraulic servo valves in two or more stages Version with four main power connections are used as 4-way valves Control of position, speed and force in cylinders for Linear movements, respectively position, speed and torque at Hydraulic motors for rotary movements. They are known in the Design as a panel-mounted valve, which means that they have one prismatic valve housing for mounting on a connection surface of a Hydraulic blocks on.
  • the four main power connections of the valve are in one planar connection surface of the valve housing and its openings in the
  • the guide bore of a main control piston is symmetrical. Control chambers are arranged in end caps on both sides of the Valve housing are flanged. These tax chambers are over Control holes connected to a pilot servo valve.
  • the hydraulic The symmetrical main spool is actuated by Pressurization of its two end faces in the front Control chambers.
  • the well-known pilot operated 4-way servo valves all have one spring-centered rest position. In most cases this is done Centering of the main spool over two opposite Return springs which are arranged in the front control chambers and work against each other. However, centering is also known to accomplish by a single spring. This single spring is then in a spring chamber on the front clamped between two spring plates.
  • a pilot operated 4-way proportional valve with one one-sided spring centering is described in the book "Der Hydraulik Trainer Band 2", Publisher and publisher: Mannesmann Rexroth GmbH, DE-8770 Lohr am Main, 3rd edition 1989, page 31, picture 33 shown.
  • the tax chambers of this Valves are arranged in end caps on both sides of the valve housing are flanged.
  • DE-A-4011908 describes a multi-way valve (five ways) known with one-sided spring centering and opposite actuating piston. Both valves have a valve housing for mounting on a connection surface of a hydraulic block.
  • Pilot operated 4-way servo valves with valve body for mounting on a pad of a hydraulic block are very space consuming and require complicated drilling in the hydraulic block for the four Main power connections.
  • the invention is therefore based on the object of a piloted To create servo valve, which saves space in a hydraulic block can be integrated and has a clearly defined center position, without sacrificing good dynamic behavior of the servo valve to have to. According to the invention, this object is achieved by pilot control Servo valve according to claim 1 solved.
  • the pilot operated 4-way servo valve according to the invention has one Control sleeve on the directly in a stepped bore of a hydraulic block is mountable.
  • This control sleeve includes openings for a first, second and third side working connection in the hydraulic block.
  • the It opens into the control sleeve for the fourth main power connection on the other hand, arranged at the front end of the control sleeve that this fourth Main power connector opens axially into the control sleeve.
  • the hydraulic block, in which the control sleeve is used then has three lateral block holes for the first, second and third main power connection. Regarding the Arrangement of the block hole for the fourth main power connection exists however maximum freedom.
  • This block hole for the fourth Main power connection can, for example, directly in the axial extension of the Stepped bore for the control sleeve to be carried out, which is conventional pilot operated servo valves with more than two main ports so far not possible. Bridge formation in the hydraulic block between individual Main power connections are also no longer required.
  • the servo valve according to the invention thus becomes a much more compact design of the control blocks than is the case with conventional servo valves is.
  • This can also be done in more complex hydraulic controls servo valve according to the invention together with various additional valves, for example 2-way cartridge valves, space-saving in a hydraulic block to get integrated.
  • a direct installation in the cylinder cover of larger ones Cylinders are also possible.
  • the main control piston of the valve according to the invention is axial slidably arranged in the control sleeve.
  • One of the two Piston face of the main control piston lies the fourth axial Working connection axially opposite.
  • the second piston face of the The main control piston forms in an extension of the spring chamber Control sleeve one, the first piston face hydrostatic counteracting, pressure compensation surface of the piston.
  • the spring chamber is through a pressure relief duct in the main spool with the fourth Main power connection hydraulically connected. This pressure relief channel also connects an auxiliary connection chamber to the fourth Main power supply.
  • a return spring is in the spring chamber clamped and engaged with the main spool via spring plates that them in both stroke directions of the piston of the hydraulic actuating force in the Control chambers opposed a spring force proportional to the piston stroke and one for the main control piston in unpressurized control chambers pressure-centered position defined.
  • a pilot valve with regulator is hydraulically connected to the two control chambers. On Position sensor of the main control piston delivers a feedback signal for the regulator of the pilot valve.
  • This hydrostatic compensation are the required actuation forces for the main control piston is reduced, whereby the actuating surfaces in the Control chambers can be designed smaller. It follows smaller control oil volumes, that is, with the same large pilot valve shorter positioning times can be achieved.
  • This hydrostatic compensation for the Main control piston also enables the easy use of a one - sided return spring for the spring centering of the main control piston in both stroke directions. As a result, with the same signal for each stroke direction ensures an equal deflection. Furthermore, the mechanical Return spring acting directly on the main control piston Center position of the main spool reliably determined.
  • the pump connection (P) can axially into the Control sleeve are introduced; the tank connection (T) is between the first and second work connection.
  • Other assignments of the Main power connections are also possible, however, without the to dispense with the main advantages of the servo valve according to the invention.
  • hydraulic is generally under pump Pressure source, under the tank a vessel or a line without essential Back pressure and under consumer a hydraulic consumer with two Displacement chambers (for example a rotary or linear drive) is understood.
  • the working connections (A) and (B) are thus spring-centered Center position of the main control spool connected to the tank connection (T). in other words, the two displacement chambers of one connected Consumers are in the spring-centered center position of the main control spool both relieved of pressure.
  • the four control edges of the Main control piston preferably has a zero overlap. This will For example, excellent positioning accuracy when using the Valve in a position control loop of a hydraulic cylinder, and a excellent dynamic behavior when using the valve Pressure control achieved. However, other arrangements of the control edges are also possible. For example, in a spring-centered center position of the main control piston all connections through the control edges to be introverted.
  • the spring centering is preferably designed as follows.
  • the The main control piston has an axial one in the spring chamber Extension shaft on.
  • a first and a second spring plate are axial slidably guided on this extension shaft.
  • the return spring presses the first spring plate against a valve Stop surface on the main control piston and the second spring plate against one Stop surface at the free end of the extension piston.
  • the spring chamber is then dimensioned such that in this rest position both spring plates in the Apply spring chamber axially.
  • the servo valve according to the invention is as such with the Reference number 10 denotes.
  • a control sleeve 12 is in a stepped bore 14 one (only indicated) hydraulic block 16 used.
  • the control sleeve 12 forms an axial guide bore into which a main control piston 18 axially is slidably fitted.
  • the servo valve 10 shown in the figures is a 4-way servo valve and has a pump connection (P), a tank connection (T), and a first working connection (A) and a second working connection (B).
  • the Pump connection (P) is hydraulically connected to a pressure line (Not shown).
  • the tank connection (T) is in hydraulic connection with an unpressurized line (not shown).
  • the working connections (A) and (B) are in hydraulic connection with a first or second Displacement chamber of a hydraulic linear or rotary drive (not shown).
  • Three block bores 22, 20, 24 in the hydraulic block 16 for the Tank connection (T) 22, the first working connection (A) 20 and the second Working connection (B) 24, are arranged transversely to the stepped bore 14 and open laterally into the stepped bore 14.
  • the Control sleeve 12 each have an annular junction 22 ', 20', 24 'in the area the corresponding block bores 22, 20, 24. Any of these Mouths 22 ', 20', 24 'has several transverse bores 25 through the wall the control sleeve 12, which each have a hydraulic connection with the Make the guide bore of the main control piston 18.
  • a fourth Block bore 26 for the pump connection (P) is in a coaxial extension the stepped bore 14 arranged.
  • the control sleeve 12 has this fourth Block bore 26 an end opening 26 '.
  • a first axial hydraulic Connection 28 the end opening 26 'for the pump connection (P) with the lateral mouth 20 'for the work connection (A); a second axial hydraulic connection 30 the mouth 22 'for the tank connection (T) with the mouth 20 'for the working connection (A); a third axial hydraulic connection 32 with the mouth 22 'for the tank connection (T) the mouth 24 'for the work connection (B); and a fourth axial hydraulic connection 34 the mouth 24 'for the working connection (B) with one inside the control sleeve 12 by the main control piston 18th delimited auxiliary connection chamber 36.
  • the main control piston 18 has a first coaxial piston collar 38 on which is assigned to the working connection (A) and axially in the first and second axial hydraulic connection 28 and 30 is slidable. He also has a second coaxial piston collar 40, which the Working connection (B) is assigned and axially in the third and fourth axial hydraulic connection 32 and 34 is displaceable.
  • the first piston collar 38 forms a first, assigned to the first hydraulic connection 28 Control edge 28 'and one of the second hydraulic connection 30 assigned second control edge 30 '. Both control edges 28 ', 30' point a zero coverage.
  • the second piston collar 40 forms one, the third hydraulic connection 32 assigned, third control edge 32 ', and a fourth control edge assigned to the fourth hydraulic connection 34 34 '.
  • the auxiliary connection chamber 36 is annular in the control sleeve around the Main control piston 18 is formed. It is on one side through the Piston collar 40 and on the other side by a piston collar 42 axially sealed.
  • auxiliary connection chamber 36 Via an axial piston bore 44 and a piston transverse bore 46 through the main control piston 18 is the auxiliary connection chamber 36 with the Pump connection (P) connected.
  • the main spool can therefore over its coaxial piston collar 38 the first working port (A) and over its coaxial piston collar 40 optionally the second working port (B) connect to the pump connection (P) or the tank connection (T), whereby the respective flow of the hydraulic fluid over the four control edges 28 ', 30 ', 32', 34 'is regulated.
  • the spring chamber 52 is in the axial extension of the control sleeve 12 in a valve cover 54 is arranged.
  • This valve cover 54 is on the Hydraulic block 16 fastens and fixes the control sleeve 12 in the stepped bore 14.
  • the second end of the main spool 18 is axially sealed by a sealing insert 56 is inserted into the spring chamber 52 and forms one therein Pressure equalization approach 58.
  • This points in the pressure compensation chamber 52 one hydrostatically counteracting the first piston face 48 Pressure compensation surface 60.
  • the pressure compensation area 60 is equal to that Piston face 48 so that there is a complete hydrostatic Pressure equalization of the pump pressure results.
  • the main control piston 18 is actuated via a processed coaxial actuating piston collar 62, by appropriate Pressurizing its ring-shaped first, respectively second Actuating surface 64, 66. Between the piston collar 42 and the Actuating surface 64 becomes a first annular in the control sleeve Control chamber 68 and between sealing insert 56 and the actuating surface 66 a second annular control chamber 68 is formed.
  • the first tax chamber 68 is via a pilot port 72 in the valve cover 54 with the Working port (A ') and the second control chamber 70 is via a pilot port 74 in the valve cover 54 with the working connection (B ') one Flanged 4-way pilot servo valve 76 connected.
  • the Actuating surfaces 64, 66 are designed so large that the Overflow of the control edges 28 ', 32' or 30 ', 34' Flow forces are surely overcome. That’s why Control oil volumes are very small and very short positioning times can be achieved to reach.
  • the main control piston 18 by pressurizing the first Control chamber 68 from its central position in the direction of spring chamber 52 is moved, the return spring 78 by the, on the end face 60 of Main control piston 18 adjacent, first spring plate 80 in the spring chamber 52 compressed.
  • she exercises one on the main control piston 18 Spring force that opposes this movement and its module is proportional to the stroke of the main control piston 18.
  • Will the Main control piston 18 by pressurizing the second control chamber 70 moves from its central position in the direction of the pump connection 26, exercises the extension shaft 84 on the second spring plate a tensile force, so that the return spring 78 now through the second spring plate 82 in the Spring chamber 52 is compressed.
  • This spring force arises here against the movement of the main control piston 18 and its module proportional to the stroke of the main spool 18.
  • Extension shaft 84 is screwed into the main control piston and through a pin 90 is secured.
  • the axial piston bore 44 is in the Extension shaft 84 continued to the transverse bore 46.
  • Another Cross bore 92 is located directly above the end face 60 of the Main control piston 18. This second transverse bore 92 has one for the purpose To ensure pressure equalization above and below the spring plate 80. In the second spring plate 82, this pressure equalization through holes 94 in Spring plate 82 reached.
  • the main control piston is over a Position sensor 96 in a closed position control loop involved.
  • a shaft 98 of the position sensor 96 is mechanical connected to the extension shaft 84 of the main control piston.
  • the Output signal of the position sensor 96 (that of the position of the Main control piston 18) is included in a control amplifier 100 compared to a target value (S), and the pilot servo valve 76 is in the Ratio to the determined target / actual value difference.
  • the Pilot control valve 76 then regulates the control oil pressure in the two Control chambers 68 and 70 of the main stage and places, against the action of Return spring 78, the piston stroke firmly, so that a closed, electro-hydraulic Control loop is formed.
  • the work connections are thus in this spring-centered center position (A) and (B) depressurized to the tank.
  • the main spool 18 is off this center position in the direction of the pump connection (P) remains the work connection (A) to the tank is relieved.
  • the work connection (B) will however via the auxiliary connection chamber 36 and the axial piston bore 44 the pump connection (P) hydraulically connected.
  • the Main control piston 18 from this central position in the direction of the spring chamber 52 driven, the work connection (B) to the tank remains unloaded.
  • the working connection (A) becomes the tank through the second control edge 30 ' blocked, and via the first control edge 32 'with the pump connection (P) hydraulically connected.
  • the main spool takes off 18 in its spring-centered center position, in which both working connections (A) and (B) are relieved to the tank as described above.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Servomotors (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Reciprocating Pumps (AREA)

Abstract

PCT No. PCT/EP95/04454 Sec. 371 Date Sep. 16, 1997 Sec. 102(e) Date Sep. 16, 1997 PCT Filed Nov. 13, 1995 PCT Pub. No. WO96/15373 PCT Pub. Date May 23, 1996A pilot controlled servo-valve has four main flow connections, an axially sliding main control piston with four control edges and a front restoring spring that defines a spring-centered middle position of the main control piston. A control sleeve has ring shaped openings for the first, second and third main flow connections and a front opening for the fourth main flow connection. A first front face of the main control piston is axially opposed to the front opening. A pressure compensation surface is formed by the second front face of the main control piston in a spring chamber. The main control piston applies the pressure in the fourth main flow connection on said pressure compensating surface through a pressure relief channel. A traverse bore connects said pressure relief channel to an auxiliary connection chamber connected to the third main flow connection by the forth control edge. This valve may be space-savingly integrated in a hydraulic block and has a clearly defined middle position, as well as a remarkable dynamic performance.

Description

Die Erfindung betrifft ein vorgesteuertes Servoventil mit vier Hauptstromanschlüssen.The invention relates to a pilot operated servo valve with four Power terminals.

Vorgesteuerte elektrohydraulische Servoventile in zwei- und mehrstufiger Ausführung mit vier Hauptstromanschlüssen werden, als 4-Wege-Ventile, zur Steuerung von Position, Geschwindigkeit und Kraft bei Zylindern für Linearbewegungen, respektiv Position, Drehzahl und Drehmoment bei Hydromotoren für Drehbewegungen, eingesetzt. Sie sind in der bekannten Bauform als Plattenaufbauventile ausgeführt, das heißt sie weisen ein prismatisches Ventilgehäuse zum Aufbau auf eine Anschlußfläche eines Hydraulikblocks auf. Die vier Hauptstromanschlüsse des Ventils liegen in einer planaren Anschlußfläche des Ventilgehäuses und ihre Einmündungen in die Führungsbohrung eines Hauptsteuerkolbens sind symmetrisch ausgebildet. Steuerkammern sind in Endkappen angeordnet, die beidseitig am Ventilgehäuse angeflanscht sind. Diese Steuerkammern sind über Steuerbohrungen mit einem Vorsteuer-Servoventil verbunden. Die hydraulische Betätigung des symmetrischen Hauptsteuerkolbens erfolgt durch Druckbeaufschlagung seiner beiden Stirnflächen in den stirnseitigen Steuerkammern.Pilot operated electrohydraulic servo valves in two or more stages Version with four main power connections are used as 4-way valves Control of position, speed and force in cylinders for Linear movements, respectively position, speed and torque at Hydraulic motors for rotary movements. They are known in the Design as a panel-mounted valve, which means that they have one prismatic valve housing for mounting on a connection surface of a Hydraulic blocks on. The four main power connections of the valve are in one planar connection surface of the valve housing and its openings in the The guide bore of a main control piston is symmetrical. Control chambers are arranged in end caps on both sides of the Valve housing are flanged. These tax chambers are over Control holes connected to a pilot servo valve. The hydraulic The symmetrical main spool is actuated by Pressurization of its two end faces in the front Control chambers.

Die bekannten vorgesteuerten 4-Wege-Servoventile haben alle eine federzentrierte Ruhestellung. In den meisten Fällen erfolgt hierbei eine Mittenzentrierung des Hauptsteuerkolbens über zwei sich gegenüberliegende Rückstellfedern, die in den stirnseitigen Steuerkammern angeordnet sind und gegeneinander wirken. Es ist jedoch ebenfalls bekannt eine Mittenzentrierung durch eine einzelne Feder zu bewerkstelligen. Diese einzelne Feder ist dann in einer stirnseitigen Federkammer zwischen zwei Federtellern eingespannt.The well-known pilot operated 4-way servo valves all have one spring-centered rest position. In most cases this is done Centering of the main spool over two opposite Return springs which are arranged in the front control chambers and work against each other. However, centering is also known to accomplish by a single spring. This single spring is then in a spring chamber on the front clamped between two spring plates.

Ein vorgesteuerstes 4-Wege-Proportionalventil mit einer solchen einseitigen Federzentrierung wird in dem Buch "Der Hydraulik Trainer Band 2", Herausgeber und Verleger: Mannesmann Rexroth GmbH, DE-8770 Lohr am Main, 3. Auflage 1989, Seite 31, Bild 33 gezeigt. Die Steuerkammern dieses Ventils sind in Endkappen angeordnet, die beidseitig am Ventilgehäuse angeflanscht sind. Aus der DE-A-4011908 ist ein Mehrwegeventil (fünf Wege) mit einseitiger Federzentrierung und gegenüberliegendem Stellkolben bekannt. Beide Ventile weisen ein Ventilgehäuse zum Aufbau auf eine Anschlußfläche eines Hydraulikblocks auf.A pilot operated 4-way proportional valve with one one-sided spring centering is described in the book "Der Hydraulik Trainer Band 2", Publisher and publisher: Mannesmann Rexroth GmbH, DE-8770 Lohr am Main, 3rd edition 1989, page 31, picture 33 shown. The tax chambers of this Valves are arranged in end caps on both sides of the valve housing are flanged. DE-A-4011908 describes a multi-way valve (five ways) known with one-sided spring centering and opposite actuating piston. Both valves have a valve housing for mounting on a connection surface of a hydraulic block.

Vorgesteuerte 4-Wege-Servoventile mit Ventilgehäuse zum Aufbau auf eine Anschlußfläche eines Hydraulikblocks sind sehr platzaufwendig und erfordern komplizierte Bohrungen im Hydraulikblock für die vier Hauptstromanschlüsse.Pilot operated 4-way servo valves with valve body for mounting on a pad of a hydraulic block are very space consuming and require complicated drilling in the hydraulic block for the four Main power connections.

Der Erfindung liegt daher die Aufgabe zugrunde, ein vorgesteuertes Servoventil zu schaffen, welches raumsparend in einen Hydraulikblock integriert werden kann und eine eindeutig festgelegte Mittenstellung aufweist, ohne dabei auf ein gutes dynamisches Verhalten des Servoventils verzichten zu müssen. Diese Aufgabe wird erfindungsgemäß durch vorgesteuertes Servoventil nach Anspruch 1 gelöst.The invention is therefore based on the object of a piloted To create servo valve, which saves space in a hydraulic block can be integrated and has a clearly defined center position, without sacrificing good dynamic behavior of the servo valve to have to. According to the invention, this object is achieved by pilot control Servo valve according to claim 1 solved.

Das erfindungsgemäße vorgesteuerte 4-Wege-Servoventil weist eine Steuerhülse auf die direkt in eine Stufenbohrung eines Hydraulikblocks montierbar ist. Diese Steuerhülse umfaßt Einmündungen für einen ersten, zweiten und dritten seitlichen Arbeitsanschluß im Hydraulikblock. Die Einmündung in die Steuerhülse für den vierten Hauptstromanschluß ist dagegen derart am Stirnende der Steuerhülse angeordnet, daß dieser vierte Hauptstromanschluß axial in die Steuerhülse einmündet. Der Hydraulikblock, in den die Steuerhülse eingesetzt wird, weist dann drei seitliche Blockbohrungen für den ersten, zweiten und dritten Hauptstromanschluß auf. Betreffend die Anordnung der Blockbohrung für den vierten Hauptstromanschluß besteht jedoch größtmögliche Freiheit. Diese Blockbohrung für den vierten Hauptstromanschluß kann zum Beispiel unmittelbar in axialer Verlängerung der Stufenbohrung für die Steuerhülse ausgeführt sein, was bei herkömmlichen vorgesteuerten Servoventilen mit mehr als zwei Hauptanschlüssen bis jetzt nicht möglich ist. Brückenbildungen im Hydraulikblock zwischen einzelnen Hauptstromanschlüssen sind ebenfalls nicht mehr erfordert. Mit dem erfindungsgemäßen Servoventil wird somit eine weitaus kompaktere Bauweise der Steuerblöcke erreicht, als dies bei herkömmlichen Servoventilen der Fall ist. Auch in komplexeren hydraulischen Steuerungen kann das erfindungsgemäße Servoventil zusammen mit diversen zusätzlichen Ventilen, zum Beispiel 2-Wege-Einbauventilen, in einen Hydraulikblock raumsparend integriert werden. Ein direkter Einbau in den Zylinderdeckel von größeren Zylindern ist ebenfalls möglich.The pilot operated 4-way servo valve according to the invention has one Control sleeve on the directly in a stepped bore of a hydraulic block is mountable. This control sleeve includes openings for a first, second and third side working connection in the hydraulic block. The It opens into the control sleeve for the fourth main power connection on the other hand, arranged at the front end of the control sleeve that this fourth Main power connector opens axially into the control sleeve. The hydraulic block, in which the control sleeve is used, then has three lateral block holes for the first, second and third main power connection. Regarding the Arrangement of the block hole for the fourth main power connection exists however maximum freedom. This block hole for the fourth Main power connection can, for example, directly in the axial extension of the Stepped bore for the control sleeve to be carried out, which is conventional pilot operated servo valves with more than two main ports so far not possible. Bridge formation in the hydraulic block between individual Main power connections are also no longer required. With the servo valve according to the invention thus becomes a much more compact design of the control blocks than is the case with conventional servo valves is. This can also be done in more complex hydraulic controls servo valve according to the invention together with various additional valves, for example 2-way cartridge valves, space-saving in a hydraulic block to get integrated. A direct installation in the cylinder cover of larger ones Cylinders are also possible.

Der Hauptsteuerkolben des erfindungsgemäßen Ventils ist axial verschiebbar in der Steuerhülse angeordnet. Eine der beiden Kolbenstimflächen des Hauptsteuerkolbens liegt dem vierten axialen Arbeitsanschluß axial gegenüber. Die zweite Kolbenstirnfläche des Hauptsteuerkolbens bildet in einer Federkammer in Verlängerung der Steuerhülse eine, der ersten Kolbenstirnfläche hydrostatisch entgegenwirkende, Druckausgleichfläche des Kolbens aus. Die Federkammer ist durch einen Druckentlastungskanal im Hauptsteuerkolben mit dem vierten Hauptstromanschluß hydraulisch verbunden. Dieser Druckentlastungskanal verbindet ebenfalls eine Hilfsanschlußkammer mit dem vierten Hauptstromanschluß. Eine Rückstellfeder ist in der Federkammer derart eingespannt und mit dem Hauptsteuerkolben über Federteller in Eingriff, daß sie in beiden Hubrichtungen des Kolbens der hydraulischen Stellkraft in den Steuerkammern eine zum Kolbenhub proportionale Federkraft entgegensetzt und für den Hauptsteuerkolben bei drucklosen Steuerkammern eine druckzentrierte Mittenstellung definiert. Ein Vorsteuerventil mit Regler ist hydraulisch mit den beiden Steuerkammern verbunden. Ein Positionsaufnehmer des Hauptsteuerkolbens liefert ein Rückführungssignal für den Regler des Vorsteuerventils.The main control piston of the valve according to the invention is axial slidably arranged in the control sleeve. One of the two Piston face of the main control piston lies the fourth axial Working connection axially opposite. The second piston face of the The main control piston forms in an extension of the spring chamber Control sleeve one, the first piston face hydrostatic counteracting, pressure compensation surface of the piston. The spring chamber is through a pressure relief duct in the main spool with the fourth Main power connection hydraulically connected. This pressure relief channel also connects an auxiliary connection chamber to the fourth Main power supply. A return spring is in the spring chamber clamped and engaged with the main spool via spring plates that them in both stroke directions of the piston of the hydraulic actuating force in the Control chambers opposed a spring force proportional to the piston stroke and one for the main control piston in unpressurized control chambers pressure-centered position defined. A pilot valve with regulator is hydraulically connected to the two control chambers. On Position sensor of the main control piston delivers a feedback signal for the regulator of the pilot valve.

Beim erfindungsgemäßen Ventil wird die unsymmetrische hydrostatische Belastung des Hauptsteuerkolben durch entsprechende Dimensionierung der Druckausgleichsfläche des Hauptsteuerkolbens kompensiert. Durch diese hydrostatische Kompensation werden die erforderlichen Betätigungskräfte für den Hauptsteuerkolben verringert, wodurch die Betätigungsflächen in den Steuerkammern kleiner ausgelegt werden können. Es ergeben sich somit kleinere Steuerölvolumina, das heißt, daß bei gleich großem Vorsteuerventil kürzere Stellzeiten erzielt werden. Diese hydrostatische Kompensation für den Hauptsteuerkolben ermöglicht ebenfalls den problemlosen Einsatz einer einseitigen Rückstellfeder für die Federzentrierung des Hauptsteuerkolbens in beide Hubrichtungen. Hierdurch wird bei gleichem Signal für jede Hubrichtung eine gleiche Auslenkung gewährleistet. Weiterhin ist durch die mechanisch unmittelbar auf den Hauptsteuerkolben wirkende Rückstellfeder, die Mittenstellung des Hauptsteuerkolbens zuverlässig festgelegt.In the valve according to the invention, the asymmetrical hydrostatic Load the main control piston through appropriate dimensioning of the Pressure compensation area of the main control piston compensated. Through this hydrostatic compensation are the required actuation forces for the main control piston is reduced, whereby the actuating surfaces in the Control chambers can be designed smaller. It follows smaller control oil volumes, that is, with the same large pilot valve shorter positioning times can be achieved. This hydrostatic compensation for the Main control piston also enables the easy use of a one - sided return spring for the spring centering of the main control piston in both stroke directions. As a result, with the same signal for each stroke direction ensures an equal deflection. Furthermore, the mechanical Return spring acting directly on the main control piston Center position of the main spool reliably determined.

Die Anschlüsse des Servoventils werden vorzugsweise wie folgt belegt:

  • der erste Hauptstromanschluß wird hydraulisch mit einer ersten Verdrängerkammer eines Verbrauchers verbunden und bildet somit einen ersten Arbeitsanschluß (A),
  • der zweite Hauptstromanschluß wird hydraulisch mit einem Tank verbunden und bildet somit einen Tankanschluß (T),
  • der dritte Hauptstromanschluß wird hydraulisch mit einer zweiten Verdrängerkammer eines Verbrauchers verbunden und bildet somit einen zweiten Arbeitsanschluß (B),
  • der vierte Hauptstromanschluß wird hydraulisch mit einer Pumpe verbunden und bildet somit einen Pumpenanschluß (P).
  • The connections of the servo valve are preferably assigned as follows:
  • the first main flow connection is hydraulically connected to a first displacement chamber of a consumer and thus forms a first working connection (A),
  • the second main flow connection is hydraulically connected to a tank and thus forms a tank connection (T),
  • the third main flow connection is hydraulically connected to a second displacement chamber of a consumer and thus forms a second work connection (B),
  • the fourth main flow connection is hydraulically connected to a pump and thus forms a pump connection (P).
  • Bei dieser Ausführung kann der Pumpenanschluß (P) axial in die Steuerhülse eingeführt werden; der Tankanschluß (T) befindet sich zwischen dem ersten und zweiten Arbeitsanschluß. Andere Belegungen der Hauptstromanschlüsse sind jedoch ebenfalls möglich, ohne auf die wesentlichsten Vorteile des erfindungsgemäßen Servoventils zu verzichten.In this version, the pump connection (P) can axially into the Control sleeve are introduced; the tank connection (T) is between the first and second work connection. Other assignments of the Main power connections are also possible, however, without the to dispense with the main advantages of the servo valve according to the invention.

    Es bleibt anzumerken, daß allgemein unter Pumpe eine hydraulische Druckquelle, unter Tank ein Gefäß oder eine Leitung ohne wesentlichen Gegendruck und unter Verbraucher ein hydraulischer Verbraucher mit zwei Verdrängerkammern (zum Beispiel ein Rotations- oder Linearantrieb) verstanden wird.It should be noted that hydraulic is generally under pump Pressure source, under the tank a vessel or a line without essential Back pressure and under consumer a hydraulic consumer with two Displacement chambers (for example a rotary or linear drive) is understood.

    In einer bevorzugten Ausführungsform des Servoventils nehmen bei federzentrierter Mittenstellung des Hauptsteuerkolbens die Steuerkanten folgende Position ein:

  • die erste axiale hydraulische Verbindung ist durch die erste Steuerkante verschlossen,
  • die zweite axiale hydraulische Verbindung ist freigegeben,
  • die dritte axiale hydraulische Verbindung ist freigegeben,
  • die vierte axiale hydraulische Verbindung ist durch die vierte Steuerkante verschlossen.
  • In a preferred embodiment of the servo valve, with the spring-centered central position of the main control piston, the control edges assume the following position:
  • the first axial hydraulic connection is closed by the first control edge,
  • the second axial hydraulic connection is released,
  • the third axial hydraulic connection is released,
  • the fourth axial hydraulic connection is closed by the fourth control edge.
  • Die Arbeitsanschlüsse (A) und (B) sind somit in der federzentrierten Mittenstellung des Hauptsteuerkolbens mit dem Tankanschluß (T) verbunden. in anderen Worten, die beiden Verdrängerkammern eines angeschlossenen Verbrauchers sind bei federzentrierter Mittenstellung des Hauptsteuerkolbens beide druckentlastet. In dieser Ausführung weisen die vier Steuerkanten des Hauptsteuerkolbens vorzugsweise eine Nullüberdeckung auf. Dadurch werden zum Beispiel eine ausgezeichnete Positioniergenauigkeit, bei Einsatz des Ventils in einem Lageregelkreis eines Hydraulikzylinders, und ein ausgezeichnetes dynamisches Verhalten, bei Einsatz des Ventils zur Druckregelung, erzielt. Andere Anordnungen der Steuerkannten sind jedoch ebenfalls möglich. So könnten zum Beispiel in federzentrierter Mittenstellung des Hauptsteuerkolbens sämtliche Anschlüsse durch die Steuerkannten verschlossen sein.The working connections (A) and (B) are thus spring-centered Center position of the main control spool connected to the tank connection (T). in other words, the two displacement chambers of one connected Consumers are in the spring-centered center position of the main control spool both relieved of pressure. In this version, the four control edges of the Main control piston preferably has a zero overlap. This will For example, excellent positioning accuracy when using the Valve in a position control loop of a hydraulic cylinder, and a excellent dynamic behavior when using the valve Pressure control achieved. However, other arrangements of the control edges are also possible. For example, in a spring-centered center position of the main control piston all connections through the control edges to be introverted.

    Die Federzentrierung ist vorzugsweise wie folgt gestaltet. Der Hauptsteuerkolben weist in der Federkammer einen axialen Verlängerungsschaft auf. Ein erster und zweiter Federteller sind axial verschiebbar auf diesem Verlängerungsschaft geführt. In Ruhestellung des Ventils drückt die Rückstellfeder den ersten Federteller gegen eine Anschlagfläche am Hauptsteuerkolben und den zweiten Federteller gegen eine Anschlagfläche am freien Ende des Verlängerungskolbens. Die Federkammer ist dann derart bemessen, daß in dieser Ruhestellung beide Federteller in der Federkammer axial anliegen.The spring centering is preferably designed as follows. The The main control piston has an axial one in the spring chamber Extension shaft on. A first and a second spring plate are axial slidably guided on this extension shaft. At rest of the The return spring presses the first spring plate against a valve Stop surface on the main control piston and the second spring plate against one Stop surface at the free end of the extension piston. The spring chamber is then dimensioned such that in this rest position both spring plates in the Apply spring chamber axially.

    Ein Ausführungsbeispiel der Erfindung ist in den beigefügten Zeichnungen dargestellt und wird im folgenden näher beschrieben. Es zeigen:

    • Figur 1 einen Längsschnitt durch ein erfindungsgemäßes Servoventil;
    • Figur 2 einen vergrößerten Ausschnitt der Figur 1.
    An embodiment of the invention is illustrated in the accompanying drawings and will be described in more detail below. Show it:
    • 1 shows a longitudinal section through an inventive servo valve;
    • FIG. 2 shows an enlarged section of FIG. 1.

    In Figur 1 ist das erfindungsgemäße Servoventil als solches mit der Referenzzahl 10 bezeichnet. Eine Steuerhülse 12 ist in eine Stufenbohrung 14 eines (nur angedeuteten) Hydraulikblockes 16 eingesetzt. Die Steuerhülse 12 bildet eine axiale Führungsbohrung aus, in die ein Hauptsteuerkolben 18 axial verschiebbar eingepaßt ist.In Figure 1, the servo valve according to the invention is as such with the Reference number 10 denotes. A control sleeve 12 is in a stepped bore 14 one (only indicated) hydraulic block 16 used. The control sleeve 12 forms an axial guide bore into which a main control piston 18 axially is slidably fitted.

    Das in den Figuren gezeigte Servoventil 10 ist ein 4-Wege-Servoventil und weist einen Pumpenanschluß (P), einen Tankanschluß (T), sowie einen ersten Arbeitsanschluß (A) und einen zweiten Arbeitsanschluß (B) auf. Der Pumpenanschluß (P) steht in hydraulischer Verbindung mit einer Druckleitung (nicht gezeigt). Der Tankanschluß (T) steht in hydraulischer Verbindung mit einer drucklosen Leitung (nicht gezeigt). Die Arbeitsanschlüsse (A) und (B) stehen in hydraulischer Verbindung mit einer ersten, respektiv zweiten Verdrängerkammer eines hydraulischen Linear- oder Rotationsantrieb (nicht gezeigt).The servo valve 10 shown in the figures is a 4-way servo valve and has a pump connection (P), a tank connection (T), and a first working connection (A) and a second working connection (B). The Pump connection (P) is hydraulically connected to a pressure line (Not shown). The tank connection (T) is in hydraulic connection with an unpressurized line (not shown). The working connections (A) and (B) are in hydraulic connection with a first or second Displacement chamber of a hydraulic linear or rotary drive (not shown).

    Drei Blockbohrungen 22, 20, 24 im Hydraulikblock 16 für den Tankanschluß (T) 22, den ersten Arbeitsanschluß (A) 20 und den zweiten Arbeitsanschluß (B) 24, sind quer zur Stufenbohrung 14 angeordnet und münden seitlich in die Stufenbohrung 14 ein. In der Stufenbohrung 14 bildet die Steuerhülse 12 jeweils eine ringförmige Einmündung 22', 20', 24' im Bereich der entsprechenden Blockbohrungen 22, 20, 24 aus. Jede dieser Einmündungen 22', 20', 24' weist mehrere Querbohrungen 25 durch die Wand der Steuerhülse 12 auf, welche jeweils eine hydraulische Verbindung mit der Führungsbohrung des Haupsteuerkolbens 18 herstellen. Eine vierte Blockbohrung 26 für den Pumpenanschluß (P) ist in koaxialer Verlängerung der Stufenbohrung 14 angeordnet. Die Steuerhülse 12 weist für diese vierte Blockbohrung 26 eine stirnseitige Einmündung 26' auf.Three block bores 22, 20, 24 in the hydraulic block 16 for the Tank connection (T) 22, the first working connection (A) 20 and the second Working connection (B) 24, are arranged transversely to the stepped bore 14 and open laterally into the stepped bore 14. In the stepped bore 14 forms the Control sleeve 12 each have an annular junction 22 ', 20', 24 'in the area the corresponding block bores 22, 20, 24. Any of these Mouths 22 ', 20', 24 'has several transverse bores 25 through the wall the control sleeve 12, which each have a hydraulic connection with the Make the guide bore of the main control piston 18. A fourth Block bore 26 for the pump connection (P) is in a coaxial extension the stepped bore 14 arranged. The control sleeve 12 has this fourth Block bore 26 an end opening 26 '.

    Innerhalb der Steuerhülse 12 verbindet eine erste axiale hydraulische Verbindung 28 die stirnseitige Einmündung 26' für den Pumpenanschluß (P) mit der seitlichen Einmündung 20' für den Arbeitsanschluß (A); eine zweite axiale hydraulische Verbindung 30 die Einmündung 22' für den Tankanschluß (T) mit der Einmündung 20' für den Arbeitsanschluß (A); eine dritte axiale hydraulische Verbindung 32 die Einmündung 22' für den Tankanschluß (T) mit der Einmündung 24' für den Arbeitsanschluß (B); und eine vierte axiale hydraulische Verbindung 34 die Einmündung 24' für den Arbeitsanschluß (B) mit einer innerhalb der Steuerhülse 12 durch den Hauptsteuerkolben 18 abgegrenzten Hilfsanschlußkammer 36. Bedingt durch die Anordnung der ringförmigen Einmündungen 22', 20', 24' ist der axiale Abstand zwischen der zweiten und dritten ( 30 und 32) axialen hydraulischen Verbindung weitaus größer, als der axiale Abstand zwischen der ersten und zweiten (28 und 30), respektiv der dritten und vierten 32 und 34) axialen hydraulischen Verbindung.Within the control sleeve 12 connects a first axial hydraulic Connection 28 the end opening 26 'for the pump connection (P) with the lateral mouth 20 'for the work connection (A); a second axial hydraulic connection 30 the mouth 22 'for the tank connection (T) with the mouth 20 'for the working connection (A); a third axial hydraulic connection 32 with the mouth 22 'for the tank connection (T) the mouth 24 'for the work connection (B); and a fourth axial hydraulic connection 34 the mouth 24 'for the working connection (B) with one inside the control sleeve 12 by the main control piston 18th delimited auxiliary connection chamber 36. Due to the arrangement of the annular outlets 22 ', 20', 24 'is the axial distance between the second and third (30 and 32) axial hydraulic connection by far larger than the axial distance between the first and second (28 and 30), respectively the third and fourth 32 and 34) axial hydraulic connection.

    Der Hauptsteuerkolben 18 weist einen ersten koaxialen Kolbenbund 38 auf, welcher dem Arbeitsanschluß (A) zugeordnet ist und axial in der ersten und zweiten axialen hydraulischen Verbindung 28 und 30 verschiebbar ist. Er weist ebenfalls einen zweiten koaxialen Kolbenbund 40 auf, welcher dem Arbeitsanschluß (B) zugeordnet ist und axial in der dritten und vierten axialen hydraulischen Verbindung 32 und 34 verschiebbar ist. Der erste Kolbenbund 38 bildet eine, der ersten hydraulischen Verbindung 28 zugeordnete, erste Steuerkante 28' aus, sowie eine, der zweiten hydraulischen Verbindung 30 zugeordnete, zweite Steuerkante 30' aus. Beide Steuerkanten 28', 30' weisen eine Nullüberdeckung auf. Der zweite Kolbenbund 40 bildet eine, der dritten hydraulischen Verbindung 32 zugeordnete, dritte Steuerkante 32' aus, sowie eine, der vierten hydraulischen Verbindung 34 zugeordnete, vierte Steuerkante 34' aus. Beide Steuerkanten 32', 34' weisen ebenfalls eine Nullüberdeckung auf. Die Hilfsanschlußkammer 36 ist in der Steuerhülse ringförmig um den Hauptsteuerkolben 18 ausgebildet. Sie ist auf der einen Seite durch den Kolbenbund 40 und auf der anderen Seite durch einen Kolbenbund 42 axial abgedichtet.The main control piston 18 has a first coaxial piston collar 38 on which is assigned to the working connection (A) and axially in the first and second axial hydraulic connection 28 and 30 is slidable. He also has a second coaxial piston collar 40, which the Working connection (B) is assigned and axially in the third and fourth axial hydraulic connection 32 and 34 is displaceable. The first piston collar 38 forms a first, assigned to the first hydraulic connection 28 Control edge 28 'and one of the second hydraulic connection 30 assigned second control edge 30 '. Both control edges 28 ', 30' point a zero coverage. The second piston collar 40 forms one, the third hydraulic connection 32 assigned, third control edge 32 ', and a fourth control edge assigned to the fourth hydraulic connection 34 34 '. Both control edges 32 ', 34' also have a zero overlap on. The auxiliary connection chamber 36 is annular in the control sleeve around the Main control piston 18 is formed. It is on one side through the Piston collar 40 and on the other side by a piston collar 42 axially sealed.

    Über eine axiale Kolbenbohrung 44 und eine Kolbenquerbohrung 46 durch den Hauptsteuerkolben 18 ist die Hilfsanschlußkammer 36 mit dem Pumpenanschluß (P) verbunden. Der Hauptsteuerkolben kann demnach über seinen koaxialen Kolbenbund 38 den ersten Arbeitsanschluß (A) und über seinen koaxialen Kolbenbund 40 den zweiten Arbeitsanschluß (B) wahlweise mit dem Pumpenanschluß (P) oder dem Tankanschluß (T) verbinden, wobei der jeweilige Durchfluß der Hydraulikflüssigkeit über die vier Steuerkanten 28', 30', 32', 34' geregelt wird.Via an axial piston bore 44 and a piston transverse bore 46 through the main control piston 18 is the auxiliary connection chamber 36 with the Pump connection (P) connected. The main spool can therefore over its coaxial piston collar 38 the first working port (A) and over its coaxial piston collar 40 optionally the second working port (B) connect to the pump connection (P) or the tank connection (T), whereby the respective flow of the hydraulic fluid over the four control edges 28 ', 30 ', 32', 34 'is regulated.

    Über seine druckbeaufschlagte Kolbenstirnfläche 48, ist der Hauptsteuerkolben 18 hydrostatisch unsymmetrisch belastet. Ein hydrostatischer Druckausgleich des Hauptsteuerkolbens erfolgt durch Weiterführung der koaxialen Kolbenbohrung 44 zum zweiten Ende des Hauptsteuerkolbens 18, wo sie über eine Kolbenquerbohrung 50 in eine Druckausgleichs- oder Federkammer 52 einmündet. Dieser obere Teil des Ventils wird anhand des vergrößerten Ausschnitts der Figur 2 näher beschrieben. About its pressurized piston face 48, the Main control piston 18 loaded hydrostatically asymmetrically. On hydrostatic pressure equalization of the main control piston is carried out by Continuation of the coaxial piston bore 44 to the second end of the Main control piston 18, where it via a piston cross bore 50 in a Pressure compensation or spring chamber 52 opens out. This upper part of the Valve is closer with reference to the enlarged section of Figure 2 described.

    Die Federkammer 52 ist in axialer Verlängerung der Steuerhülse 12 in einem Ventildeckel 54 angeordnet. Dieser Ventildeckel 54 wird auf dem Hydraulikblock 16 befestigt und fixiert die Steuerhülse 12 in der Stufenbohrung 14. Das zweite Ende des Hauptsteuerkolbens 18 ist, axial abgedichtet durch einen Dichteinsatz 56, in die Federkammer 52 eingeführt und bildet darin einen Druckausgleichsansatz 58 aus. Dieser weist in der Druckausgleichskammer 52 eine, der ersten Kolbenstirnfläche 48 hydrostatisch entgegenwirkende, Druckausgleichsfläche 60 auf. Die Druckausgleichsfläche 60 ist gleich der Kolbenstirnfläche 48, so daß sich ein vollständiger hydrostatischer Druckausgleich des Pumpendrucks ergibt.The spring chamber 52 is in the axial extension of the control sleeve 12 in a valve cover 54 is arranged. This valve cover 54 is on the Hydraulic block 16 fastens and fixes the control sleeve 12 in the stepped bore 14. The second end of the main spool 18 is axially sealed by a sealing insert 56 is inserted into the spring chamber 52 and forms one therein Pressure equalization approach 58. This points in the pressure compensation chamber 52 one hydrostatically counteracting the first piston face 48 Pressure compensation surface 60. The pressure compensation area 60 is equal to that Piston face 48 so that there is a complete hydrostatic Pressure equalization of the pump pressure results.

    Die Betätigung des Hauptsteuerkolbens 18 erfolgt über einen angearbeiteten koaxialen Betätigungskolbenbund 62, durch entsprechende Druckbeaufschlagung seiner ringförmigen ersten, respektiv zweiten Betätigungsfläche 64, 66. Zwischen dem Kolbenbund 42 und der Betätigungsfläche 64 wird in der Steuerhülse eine erste ringförmige Steuerkammer 68 und zwischen Dichteinsatz 56 und der Betätigungsfläche 66 eine zweite ringförmige Steuerkammer 68 ausgebildet. Die erste Steuerkammer 68 ist über einen Vorsteuer-Anschluß 72 im Ventildeckel 54 mit dem Arbeitsanschluß (A') und die zweite Steuerkammer 70 ist über einen Vorsteuer-Anschluß 74 im Ventildeckel 54 mit dem Arbeitsanschluß (B') eines angeflanschten 4-Wege-Vorsteuer-Servoventils 76 verbunden. Die Betätigungsflächen 64, 66 sind gerade so groß ausgelegt, daß die beim Überströmen der Steuerkanten 28', 32', bzw. 30', 34' entstehenden Strömungskräfte sicher überwunden werden. Dadurch sind die Steuerölvolumina sehr klein und es lassen sich sehr kurze Stellzeiten erreichen.The main control piston 18 is actuated via a processed coaxial actuating piston collar 62, by appropriate Pressurizing its ring-shaped first, respectively second Actuating surface 64, 66. Between the piston collar 42 and the Actuating surface 64 becomes a first annular in the control sleeve Control chamber 68 and between sealing insert 56 and the actuating surface 66 a second annular control chamber 68 is formed. The first tax chamber 68 is via a pilot port 72 in the valve cover 54 with the Working port (A ') and the second control chamber 70 is via a pilot port 74 in the valve cover 54 with the working connection (B ') one Flanged 4-way pilot servo valve 76 connected. The Actuating surfaces 64, 66 are designed so large that the Overflow of the control edges 28 ', 32' or 30 ', 34' Flow forces are surely overcome. That’s why Control oil volumes are very small and very short positioning times can be achieved to reach.

    In der Federkammer 52 ist eine Rückstellfeder 78 zwischen einem ersten und zweiten Federteller 80 und 82 axial eingespannt. Ein Verlängerungsschaft 84 ist starr mit dem zweiten Ende des Haupsteurkolbens 18 verbunden. Auf diesem Schaft 84 sind die Federteller 80 und 82 axial verschiebbar geführt. Der Schaft 84 weist an seinem freien Ende eine axiale Anschlagfläche 86 für den zweiten Federteller 82 auf. Die zweite Kolbenstirnfläche 60 bildet eine axiale Anschlagfläche für den ersten Federteller 80. In Figur 2 drückt die Rückstellfeder 78 den ersten Federteller 80 gegen die Anschlagfläche 60 und den zweiten Federteller 82 gegen die Anschlagfläche 86. In dieser Position befindet sich der erste Federteller 80 ebenfalls in Gehäuseanschlag am Dichteinsatz 56 und der zweite Federteller 82 in Gehäuseanschlag an einer axial gegenüberliegenden Anschlagfläche 88 des Ventildeckels 54. Beide Federteller 80 und 82 liegen demnach in Gehäuseanschlag an, und der Hauptsteuerkolben 18 ist über den Verlängerungsschaft 84 zwischen den beiden Federtellern 80 und 82 eingespannt, die durch die Rückstellfeder 78 in entgegengesetzten Richtungen federbelastet sind. In anderen Worten, der Haupsteurkolbens 18 befindet sich in einer federzentrierten Ruhestellung, die auch als Mittenstellung bezeichnet wird.In the spring chamber 52 there is a return spring 78 between a first one and second spring plate 80 and 82 axially clamped. An extension shaft 84 is rigidly connected to the second end of the main control piston 18. On the spring plates 80 and 82 are guided axially displaceably in this shaft 84. The Shaft 84 has at its free end an axial stop surface 86 for the second spring plate 82. The second piston end face 60 forms an axial one Stop surface for the first spring plate 80. In Figure 2, the Return spring 78 the first spring plate 80 against the stop surface 60 and the second spring plate 82 against the stop surface 86. In this position is the first spring plate 80 also in the housing stop on Sealing insert 56 and the second spring plate 82 in the housing stop on one axially opposite stop surface 88 of the valve cover 54. Both Spring plates 80 and 82 are therefore in the housing stop, and the Main control piston 18 is over the extension shaft 84 between the two spring plates 80 and 82 clamped by the return spring 78 in opposite directions are spring loaded. In other words, the The main control piston 18 is in a spring-centered rest position is also referred to as the center position.

    Wird der Haupsteurkolbens 18 durch Druckbeaufschlagung der ersten Steuerkammer 68 aus seiner Mittenstellung in Richtung der Federkammer 52 bewegt, wird die Rückstellfeder 78 durch den, an der Stirnseite 60 des Hauptsteuerkolben 18 anliegenden, ersten Federteller 80 in der Federkammer 52 zusammengedrückt. Sie übt dadurch auf den Hauptsteuerkolben 18 eine Federkraft aus, die sich dieser Bewegung entgegenstellt und deren Modul proportional zum Hub des Haupsteuerkolbens 18 ist. Wird der Haupsteurkolbens 18 durch Druckbeaufschlagung der zweiten Steuerkammer 70 aus seiner Mittenstellung in Richtung der Pumpenanschluß 26 bewegt, übt der Verlängerungsschaft 84 auf den zweiten Federteller eine Zugkraft aus, so daß die Rückstellfeder 78 jetzt durch den zweiten Federteller 82 in der Federkammer 52 zusammengedrückt wird. Diese Federkraft stellt sich hierbei der Bewegung des Hauptsteuerkolbens 18 entgegen und ihr Modul ist proportional zum Hub des Haupsteuerkolbens 18. Durch den Einsatz einer einzigen Rückstellfeder 78, die als Druckfeder für beide Hubrichtungen arbeitet, ist gewährleistet, daß der Hauptsteuerkolben 18 in beiden Richtungen genau der gleichen Rückstellkraft ausgesetzt ist.The main control piston 18 by pressurizing the first Control chamber 68 from its central position in the direction of spring chamber 52 is moved, the return spring 78 by the, on the end face 60 of Main control piston 18 adjacent, first spring plate 80 in the spring chamber 52 compressed. As a result, she exercises one on the main control piston 18 Spring force that opposes this movement and its module is proportional to the stroke of the main control piston 18. Will the Main control piston 18 by pressurizing the second control chamber 70 moves from its central position in the direction of the pump connection 26, exercises the extension shaft 84 on the second spring plate a tensile force, so that the return spring 78 now through the second spring plate 82 in the Spring chamber 52 is compressed. This spring force arises here against the movement of the main control piston 18 and its module proportional to the stroke of the main spool 18. By using a single return spring 78, which acts as a compression spring for both stroke directions works, it is ensured that the main control piston 18 in both directions is subjected to exactly the same restoring force.

    Aus dem Teilschnitt der Figur 2 ist ersichtlich, daß der Verlängerungsschaft 84 in den Hauptsteuerkolben eingeschraubt ist und durch einen Stift 90 gesichert ist. Die axiale Kolbenbohrung 44 ist im Verlängerungsschaft 84 bis zur Querbohrung 46 weitergeführt. Eine weitere Querbohrung 92 befindet sich direkt oberhalb der Stirnfläche 60 des Hauptsteuerkolbens 18. Diese zweite Querbohrung 92 hat zum Zweck einen Druckausgleich ober- und unterhalb des Federtellers 80 zu gewährleisten. Beim zweiten Federteller 82 wird dieser Druckausgleich durch Löcher 94 im Federteller 82 erreicht. From the partial section of Figure 2 it can be seen that the Extension shaft 84 is screwed into the main control piston and through a pin 90 is secured. The axial piston bore 44 is in the Extension shaft 84 continued to the transverse bore 46. Another Cross bore 92 is located directly above the end face 60 of the Main control piston 18. This second transverse bore 92 has one for the purpose To ensure pressure equalization above and below the spring plate 80. In the second spring plate 82, this pressure equalization through holes 94 in Spring plate 82 reached.

    Wie aus Figur 1 ersichtlich, ist der Hauptsteuerkolben über einen Positionsaufnehmer 96 in einen geschossenen Positionsregelkreis eingebunden. Ein Schaft 98 des Positionsaufnehmers 96 ist dabei mechanisch mit dem Verlängerungsschaft 84 des Hauptsteurkolbens verbunden. Das Ausgangssignal des Positionsaufnehmers 96 (das der Position des Hauptsteuerkolbens 18 entspricht) wird in einem Regelverstärker 100 mit einem Sollwert (S) verglichen, und das Vorsteuerservoventil 76 wird im Verhältnis zur ermittelten Soll-lstwert-Differenz ansteuert. Das Vorsteuerservoventil 76 regelt daraufhin den Steueröldruck in den beiden Steuerkammern 68 und 70 der Haupstufe und legt, gegen die Wirkung der Rückstellfeder 78, den Kolbenhub fest, so daß ein geschlossener, elektrohydraulischer Regelkreis gebildet wird.As can be seen from Figure 1, the main control piston is over a Position sensor 96 in a closed position control loop involved. A shaft 98 of the position sensor 96 is mechanical connected to the extension shaft 84 of the main control piston. The Output signal of the position sensor 96 (that of the position of the Main control piston 18) is included in a control amplifier 100 compared to a target value (S), and the pilot servo valve 76 is in the Ratio to the determined target / actual value difference. The Pilot control valve 76 then regulates the control oil pressure in the two Control chambers 68 and 70 of the main stage and places, against the action of Return spring 78, the piston stroke firmly, so that a closed, electro-hydraulic Control loop is formed.

    Auch in Figur 1 ist der Hauptsteuerkolben 18 in federzentrierter Ruheoder Mittenstellung gezeigt. Die Steuerkannten 28', 30', 32', 34' sind derart am Hauptsteuerkolben 18 angeordnet, daß in dieser Mittenstellung:

    • die erste Steuerkante 28' die erste hydraulische Verbindung 28 zwischen Pumpenanschluß (P) und Arbeitsanschluß (A) verschließt;
    • die zweite Steuerkante 30' die zweite hydraulische Verbindung 30 zwischen Tankanschluß (T) und Arbeitsanschluß (A) freigibt;
    • die dritte Steuerkante 32' die dritte hydraulische Verbindung 30 zwischen Tankanschluß (T) und Arbeitsanschluß (B) freigibt;
    • die vierte Steuerkante 34' die vierte hydraulische Verbindung zwischen Arbeitsanschluß (B) und Hilfsanschlußkammer 36 verschließt, und dadurch die hydraulische Verbindung über die axiale Kolbenbohrung 44 zwischen Arbeitsanschluß (B) und Pumpenanschluß (P) unterbindet.
    The main control piston 18 is also shown in FIG. 1 in the spring-centered rest or center position. The control edges 28 ', 30', 32 ', 34' are arranged on the main control piston 18 such that in this central position:
    • the first control edge 28 'closes the first hydraulic connection 28 between the pump connection (P) and the working connection (A);
    • the second control edge 30 'enables the second hydraulic connection 30 between the tank connection (T) and the working connection (A);
    • the third control edge 32 'enables the third hydraulic connection 30 between the tank connection (T) and the working connection (B);
    • the fourth control edge 34 'closes the fourth hydraulic connection between the working connection (B) and the auxiliary connection chamber 36, and thereby prevents the hydraulic connection via the axial piston bore 44 between the working connection (B) and the pump connection (P).

    In dieser federzentrierten Mittenstellung sind somit die Arbeitsanschlüsse (A) und (B) drucklos zum Tank entlastet. Wird der Hauptsteuerkolben 18 aus dieser Mittenstellung in Richtung des Pumpenanschluß (P) gefahren, verbleibt der Arbeitsanschluß (A) zum Tank entlastet. Der Arbeitsanschluß (B) wird jedoch über die Hilfsanschlußkammer 36 und die axiale Kolbenbohrung 44 mit dem Pumpenanschluß (P) hydraulisch verbunden. Wird dagegen der Hauptsteuerkolben 18 aus dieser Mittenstellung in Richtung der Federkammer 52 gefahren, verbleibt der Arbeitsanschluß (B) zum Tank entlastet. Der Arbeitsanschluß (A) wird jedoch durch die zweite Steuerkante 30' zum Tank gesperrt, und über die erste Steuerkante 32' mit dem Pumpenanschluß (P) hydraulisch verbunden. Bei Steuerdruckausfall nimmt der Hauptsteuerkolben 18 seine federzentrierte Mittenstellung ein, in der beide Arbeitsanschlüsse (A) und (B) wie vorbeschrieben zum Tank entlastet sind.The work connections are thus in this spring-centered center position (A) and (B) depressurized to the tank. The main spool 18 is off this center position in the direction of the pump connection (P) remains the work connection (A) to the tank is relieved. The work connection (B) will however via the auxiliary connection chamber 36 and the axial piston bore 44 the pump connection (P) hydraulically connected. However, if the Main control piston 18 from this central position in the direction of the spring chamber 52 driven, the work connection (B) to the tank remains unloaded. The However, the working connection (A) becomes the tank through the second control edge 30 ' blocked, and via the first control edge 32 'with the pump connection (P) hydraulically connected. In the event of a control pressure failure, the main spool takes off 18 in its spring-centered center position, in which both working connections (A) and (B) are relieved to the tank as described above.

    Claims (7)

    1. A pilot-operated servo valve with four main-stream ports comprising:
      a valve housing (12, 54) having:
      a guide bore for a main control piston (18),
      a first hydraulic connection (28) in the guide bore between the fourth and first main-stream ports,
      a second hydraulic connection (30) in the guide bore between the first and second main-stream ports,
      a third hydraulic connection (32) in the guide bore between the second and third main-stream ports,
      a fourth hydraulic connection (34) in the guide bore between the third main-stream port and an auxiliary port chamber;
      a main control piston (18), which is axially displaceable in the guide bore, having:
      a first control edge (28'), which is assigned to the first axial hydraulic connection (28) for control of the throughflow,
      a second control edge (30'), which is assigned to the second axial hydraulic connection (30) for control of the throughflow,
      a third control edge (32'), which is assigned to the third axial hydraulic connection (32) for control of the throughflow,
      a fourth control edge (34'), which is assigned to the fourth axial hydraulic connection (34) for control of the throughflow,
      the main control piston (18) delimiting a first and second control chamber (68, 70) within the valve housing and forming within the first control chamber (68) a first actuating surface (64) and within the second control chamber (70) a second actuating surface (66) axially opposing the first actuating surface (64);
      a return spring (78), which is clamped in an end spring chamber (52) in such a way and engages with the main control piston (18) in such a way that in both lifting directions of the main control piston (18) it opposes the latter with a spring force and thus defines a spring-centered centre position of the main control piston (18);
      a pilot valve (76), which is connected hydraulically to at least one of the two control chambers (68, 70);
      a controller (100) for the pilot valve (76);
      a position transducer (96), which is connected to the main control piston (18) and supplies the position of the main control piston (18) as a feedback signal for the controller (100) of the pilot valve (76);
      characterised in that
      the valve housing comprises a control sleeve (12), which can be inserted axially in a bore (14) of a hydraulic block (16) and is designed in such a way that it delimits annular openings (20', 22', 24') in this bore (14) for the first, second and third main-stream port,
      an opening (26') for the fourth main-stream port is arranged axially at the end of the control sleeve (18), a first piston end surface of the main control piston (18) being positioned axially opposite this opening (26'),
      a pressure-equalising surface (60) is formed by the second piston end surface of the main control piston (18) in the spring chamber (52),
      a pressure-relief duct (44) hydraulically connects the spring chamber (52) to the fourth main-stream port through the main control piston (18), so that the pressure equalising surface (60) is loaded with the pressure in the fourth main-stream port, and
      a cross-bore (46) hydraulically connects this pressure-relief duct to the auxiliary port chamber (36).
    2. Valve according to claim 1, characterised in that
      the first main-stream port forms a first working port (A),
      the second main-stream port forms a tank port (T),
      the third main-stream port forms a second working port (B), and
      the fourth main-stream port forms a pump port (P).
    3. Valve according to claim 1, characterised in that the control edges are arranged in such a way that they assume the following positions when the main control piston (18) is in the spring-centered centre position:
      the first axial hydraulic connection (28) is closed by the first control edge (28'),
      the second axial hydraulic connection (30) is opened,
      the third axial hydraulic connection (32) is opened, and
      the fourth axial hydraulic connection (34) is closed by the fourth control edge (34').
    4. Valve according to one of claims 1 to 3, characterised in that the first and second actuating surfaces (64, 66) are annular surfaces.
    5. Valve according to one of claims 1 to 4, characterised by
      an axial extension shaft (84) of the main control piston (18) in the spring chamber (52),
      a first and second spring plate (80, 82), which are axially displaceable on this extension shaft (84),
      an axial stop surface (60) on the main control piston for the first spring plate (80),
      an axial stop surface (86) on the displacement shaft (84) for the second spring plate (82),
      the return spring (78) forcing each of the two spring plates (80, 82) against its stop surface (60, 86) when the valve is in the rest position, and
      the spring chamber (52) being dimensioned in such a way that in this rest position both spring plates (80, 82) abut axially in the spring chamber.
    6. Valve according to claim 5, characterised in that the pressure-relief duct (44) is introduced as an axial bore into the extension shaft (84) and there terminates in the spring chamber (52) via a first cross bore (50).
    7. Valve according to claim 6, characterised in that the extension shaft (84) has a second cross-bore (92) in the immediate vicinity of the first stop surface (60) for the first spring plate (80).
    EP95937068A 1994-11-16 1995-11-13 Pilot controlled servo-valve Expired - Lifetime EP0828945B1 (en)

    Applications Claiming Priority (3)

    Application Number Priority Date Filing Date Title
    LU88558 1994-11-16
    LU88558A LU88558A1 (en) 1994-11-16 1994-11-16 Pilot operated servo valve
    PCT/EP1995/004454 WO1996015373A1 (en) 1994-11-16 1995-11-13 Pilot controlled servo-valve

    Publications (2)

    Publication Number Publication Date
    EP0828945A1 EP0828945A1 (en) 1998-03-18
    EP0828945B1 true EP0828945B1 (en) 2002-09-11

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    ID=19731505

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    Application Number Title Priority Date Filing Date
    EP95937068A Expired - Lifetime EP0828945B1 (en) 1994-11-16 1995-11-13 Pilot controlled servo-valve

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    US (1) US5896890A (en)
    EP (1) EP0828945B1 (en)
    JP (1) JP3638286B2 (en)
    CN (1) CN1070584C (en)
    AT (1) ATE224012T1 (en)
    AU (1) AU3928595A (en)
    CA (1) CA2205441C (en)
    DE (1) DE59510375D1 (en)
    LU (1) LU88558A1 (en)
    RU (1) RU2153105C2 (en)
    WO (1) WO1996015373A1 (en)

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    Also Published As

    Publication number Publication date
    CA2205441A1 (en) 1996-05-23
    RU2153105C2 (en) 2000-07-20
    AU3928595A (en) 1996-06-06
    CA2205441C (en) 2005-02-08
    CN1070584C (en) 2001-09-05
    DE59510375D1 (en) 2002-10-17
    JPH10508679A (en) 1998-08-25
    LU88558A1 (en) 1996-07-15
    JP3638286B2 (en) 2005-04-13
    US5896890A (en) 1999-04-27
    ATE224012T1 (en) 2002-09-15
    WO1996015373A1 (en) 1996-05-23
    EP0828945A1 (en) 1998-03-18
    CN1163657A (en) 1997-10-29

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