EP0828945B1 - Vorgesteuertes servoventil - Google Patents
Vorgesteuertes servoventil Download PDFInfo
- 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
- Authority
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B13/00—Details of servomotor systems ; Valves for servomotor systems
- F15B13/02—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
- F15B13/04—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor
- F15B13/0401—Valve members; Fluid interconnections therefor
- F15B13/0402—Valve members; Fluid interconnections therefor for linearly sliding valves, e.g. spool valves
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- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/86493—Multi-way valve unit
- Y10T137/86574—Supply and exhaust
- Y10T137/86582—Pilot-actuated
- Y10T137/86606—Common to plural valve motor chambers
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/86493—Multi-way valve unit
- Y10T137/86574—Supply and exhaust
- Y10T137/86582—Pilot-actuated
- Y10T137/86614—Electric
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)
- Sliding Valves (AREA)
- Reciprocating Pumps (AREA)
Description
- Figur 1 einen Längsschnitt durch ein erfindungsgemäßes Servoventil;
- Figur 2 einen vergrößerten Ausschnitt der Figur 1.
- 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.
Claims (7)
- Vorgesteuertes Servoventil mit vier Haupstromanschlüssen umfassend:dadurch gekennzeichnet, daß das Ventilgehäuse eine Steuerhülse (12) umfaßt die in eine Bohrung (14) eines Hydraulikblocks (16) axial einsetzbar ist und die derart gestaltet ist, daß sie ringförmige Einmündungen (20', 22', 24') in dieser Bohrung (14) für den ersten, zweiten und dritten Hauptstromanschluss abgrenzt,ein Ventilgehäuse (12, 54) mit:einer Führungsbohrung für einen Hauptsteuerkolben (18),einer ersten hydraulischen Verbindung (28) in der Führungsbohrung zwischen dem vierten Hauptstromanschluß und dem ersten Hauptstromanschluß,einer zweiten hydraulischen Verbindung (30) in der Führungsbohrung zwischen dem ersten Hauptstromanschluß und dem zweiten Hauptstromanschluß,einer dritten hydraulischen Verbindung (32) in der Führungsbohrung zwischen dem zweiten Hauptstromanschluß und dem dritten Hauptstromanschluß,einer vierten hydraulischen Verbindung (34) in der Führungsbohrungzwischen dem dritten Hauptstromanschluß und einer Hilfsanschlusskammer,ein Hauptsteuerkolben (18) der axial verschiebbar in der Führungsbohrung angeordnet ist, mit:wobei der Hauptsteuerkolben (18) innerhalb des Ventilgehäuses eine erste und zweite Steuerkammer (68, 70) abgrenzt und innerhalb der ersten Steuerkammer (68) eine erste Betätigungsfläche (64) und innerhalb der zweiten Steuerkammer (70) eine, der ersten Betätigungsfläche (64) axial entgegenwirkende, zweite Betätigungsfläche (66) ausbildet;einer ersten Steuerkante (28') die der ersten axialen hydraulischen Verbindung (28) zum Regeln des Durchflusses zugeordnet ist,einer zweiten Steuerkante (30') die der zweiten axialen hydraulischen Verbindung (30) zum Regeln des Durchflusses zugeordnet ist,einer dritten Steuerkante (32') die der dritten axialen hydraulischen Verbindung (32) zum Regeln des Durchflusses zugeordnet ist,einer vierten Steuerkante (34') die der vierten axialen hydraulischen Verbindung (34) zum Regeln des Durchflusses zugeordnet ist,eine Rückstellfeder (78) die in einer stirnseitigen Federkammer (52) derart eingespannt und mit dem Hauptsteuerkolben (18) derart in Eingriff steht, daß sie in beide Hubrichtungen des Hauptsteuerkolbens (18) demselben eine Federkraft entgegensetzt und somit eine federzentrierte Mittenstellung des Hauptsteuerkolbens (18) definiert;ein Vorsteuerventil (76) das hydraulisch mit mindestens einer der beiden Steuerkammern (68, 70) verbunden ist;ein Regler (100) für das Vorsteuerventil (76);ein Positionsaufnehmer (96) der mit dem Hauptsteuerkolben (18) verbunden ist und die Position des Hauptsteuerkolbens (18) als Rückführungssignal für den Regler (100) des Vorsteuerventils (76) liefert;
daß eine Einmündung (26') für den vierten Hauptstromanschluß axial am Stirnende der Steuerhülse (18) angeordnet ist, wobei eine erste Kolbenstirnfläche des Haupsteuerkolbens (18) dieser Einmündung (26') axial gegenüberliegt,
daß eine Druckausgleichfläche (60) durch die zweite Kolbenstirnfläche des Hauptsteuerkolbens (18) in der Federkammer (52) ausgebildet wird,
daß ein Druckentlastungskanal (44) durch den Hauptsteuerkolben (18) die Federkammer (52) mit dem vierten Hauptstromanschluß hydraulisch verbindet, so daß die Druckausgleichfläche (60) mit dem Druck im vierten Hauptstromanschluß belastet ist, und
daß eine Querbohrung (46) diesen Druckentlastungskanal mit der Hilfsanschlußkammer (36) hydraulisch verbindet. - Ventil nach Anspruch 1, dadurch gekennzeichnet, daß
der erste Hauptstromanschluß einen ersten Arbeitsanschluß (A) ausbildet, der zweite Hauptstromanschluß einen Tankanschluß (T) ausbildet, der dritte Hauptstromanschluß einen zweiten Arbeitsanschluß (B) ausbildet, und der vierte Hauptstromanschluß einen Pumpenanschluß (P) ausbildet. - Ventil nach Anspruch 1, dadurch gekennzeichnet, daß die Steuerkanten derart angeordnet sind, daß sie bei federzentrierter Mittenstellung des Hauptsteuerkolbens (18) folgende Positionen einnehmen:die erste axiale hydraulische Verbindung (28) ist durch die erste Steuerkante (28') verschlossen,die zweite axiale hydraulische Verbindung (30) ist freigegeben,die dritte axiale hydraulische Verbindung (32) ist freigegeben, unddie vierte axiale hydraulische Verbindung (34) ist durch die vierte Steuerkante (34') verschlossen.
- Ventil nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, daß die erste und zweite Betätigungsfläche (64, 66) Ringflächen sind.
- Ventil nach einem der Ansprüche 1 bis 4, gekennzeichnet durch
einen axialen Verlängerungsschaft (84) des Hauptsteuerkolbens (18) in der Federkammer (52),
einen ersten und zweiten Federteller (80, 82) die axial verschiebbar auf diesem Verlängerungsschaft (84) geführt sind,
eine axiale Anschlagfläche (60) am Hauptsteuerkolben für den ersten Federteller (80),
eine axiale Anschlagfläche (86) am Verlängerungsschaft (84) für den zweiten Federteller (82),
wobei in Ruhestellung des Ventils die Rückstellfeder (78) jeden der beiden Federteller (80, 82) gegen seine Anschlagfläche (60, 86) drückt, und
wobei die Federkammer (52) derart bemessen ist, daß in dieser Ruhestellung beide Federteller (80, 82) in der Federkammer axial anliegen. - Ventil nach Anspruch 5, dadurch gekennzeichnet, daß der Druckentlastungskanal (44) als axiale Bohrung in den Verlängerungsschaft (84) hineingeführt ist und dort über eine erste Querbohrung (50) in die Federkammer (52) mündet.
- Ventil nach Anspruch 6, dadurch gekennzeichnet, daß der Verlängerungsschaft (84) eine zweite Querbohrung (92) in direkter Nachbarschaft der ersten Anschlagfläche (60) für den ersten Federteller (80) aufweist.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| LU88558A LU88558A1 (de) | 1994-11-16 | 1994-11-16 | Vorgesteuertes Servoventil |
| LU88558 | 1994-11-16 | ||
| PCT/EP1995/004454 WO1996015373A1 (de) | 1994-11-16 | 1995-11-13 | Vorgesteuertes servoventil |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0828945A1 EP0828945A1 (de) | 1998-03-18 |
| EP0828945B1 true EP0828945B1 (de) | 2002-09-11 |
Family
ID=19731505
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP95937068A Expired - Lifetime EP0828945B1 (de) | 1994-11-16 | 1995-11-13 | Vorgesteuertes servoventil |
Country Status (11)
| Country | Link |
|---|---|
| US (1) | US5896890A (de) |
| EP (1) | EP0828945B1 (de) |
| JP (1) | JP3638286B2 (de) |
| CN (1) | CN1070584C (de) |
| AT (1) | ATE224012T1 (de) |
| AU (1) | AU3928595A (de) |
| CA (1) | CA2205441C (de) |
| DE (1) | DE59510375D1 (de) |
| LU (1) | LU88558A1 (de) |
| RU (1) | RU2153105C2 (de) |
| WO (1) | WO1996015373A1 (de) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2011154056A1 (de) | 2010-06-11 | 2011-12-15 | Bühler AG | Ventilanordnung |
Families Citing this family (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE19856563A1 (de) * | 1998-12-08 | 2000-06-15 | Mannesmann Rexroth Ag | Wegeventil |
| US6581704B2 (en) | 2001-06-21 | 2003-06-24 | Deere & Company | Steering controls |
| US6725876B2 (en) * | 2001-10-15 | 2004-04-27 | Woodward Governor Company | Control valve with integrated electro-hydraulic actuator |
| US7422033B2 (en) * | 2004-12-16 | 2008-09-09 | Husco International, Inc. | Position feedback pilot valve actuator for a spool control valve |
| CN100348873C (zh) * | 2005-11-03 | 2007-11-14 | 武汉科技大学 | 一种数字输入式电液伺服阀 |
| DE102006006652A1 (de) * | 2006-02-14 | 2007-08-30 | Zf Friedrichshafen Ag | Schaltvorrichtung für Kraftfahrzeug-Wechselgetriebe |
| DE102006034366A1 (de) * | 2006-02-24 | 2007-08-30 | Robert Bosch Gmbh | Wege- oder Stromventil |
| WO2008045074A1 (en) * | 2006-10-12 | 2008-04-17 | United Technologies Corporation | Turbofan engine with variable bypass nozzle exit area and method of operation |
| US20080224353A1 (en) * | 2007-03-14 | 2008-09-18 | Husky Injection Molding Systems Ltd. | Hydraulic Valve of Molding System |
| DE102008058694B4 (de) * | 2007-12-06 | 2019-12-19 | Schaeffler Technologies AG & Co. KG | Verfahren zum Ansteuern eines hydraulischen Folgesystems |
| CN101598151B (zh) * | 2009-06-03 | 2011-10-26 | 北京航空航天大学 | 一种螺旋全桥先导级结构 |
| KR100954867B1 (ko) * | 2009-12-31 | 2010-04-28 | 유영묵 | 공압식 연동 제어 장치 및 시스템 |
| CN101806314B (zh) * | 2010-04-09 | 2012-12-05 | 北京航空航天大学 | 一种液压螺旋半桥先导级结构 |
| CN102032233B (zh) * | 2011-01-08 | 2013-05-15 | 四川省宜宾普什驱动有限责任公司 | 一种多功能比例多路阀 |
| CN102162475B (zh) * | 2011-04-13 | 2015-08-19 | 重庆大学 | 一种具有感知功能的压力控制阀 |
| CN102661299A (zh) * | 2012-05-14 | 2012-09-12 | 三一汽车起重机械有限公司 | 自重落幅恒功率控制阀和起重机 |
| CN102996814B (zh) * | 2012-12-08 | 2015-01-28 | 中国航天科技集团公司第六研究院第十一研究所 | 一种活塞与阀芯分体式设置的控制阀 |
| CN105545856B (zh) * | 2016-02-17 | 2017-07-14 | 武汉市汉诺优电控有限责任公司 | 一种数控旋芯式比例伺服阀 |
| CN108266562B (zh) * | 2016-12-30 | 2019-04-12 | 华中科技大学 | 一种高压气体流量控制装置 |
| EA032854B1 (ru) * | 2017-03-14 | 2019-07-31 | Научно-Исследовательский И Проектный Институт Нефти И Газа (Нипинг) | Устьевое устройство для ударно-волнового воздействия на призабойную зону пласта |
| CN110657267B (zh) * | 2019-11-15 | 2021-02-02 | 临沂市宇顺机械有限公司 | 一种有溢流功能的卸荷阀 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3010438A (en) * | 1957-05-27 | 1961-11-28 | Fife | Pneumatic control valve for hydraulic system |
| US3234968A (en) * | 1962-12-21 | 1966-02-15 | White Sales Corp Graham | Master and slave valve assembly |
| DE4011908C3 (de) * | 1990-02-06 | 1996-08-14 | Festo Kg | Mehrwegeventil |
| SU1735619A1 (ru) * | 1990-04-11 | 1992-05-23 | Всесоюзный научно-исследовательский и проектно-конструкторский институт промышленных гидроприводов и гидроавтоматики | Четырехлинейный гидрораспределитель |
| SU1761983A1 (ru) * | 1990-06-15 | 1992-09-15 | Мелитопольский Завод Тракторных Гидроагрегатов Им.Хху Съезда Кпсс | Гидравлический распределитель |
| LU88278A1 (de) * | 1993-05-27 | 1994-12-01 | Hydrolux Sarl | Vorgesteuertes Servoventil |
| LU88277A1 (de) * | 1993-05-27 | 1994-12-01 | Hydrolux Sarl | Vorgesteuertes Servoventil |
-
1994
- 1994-11-16 LU LU88558A patent/LU88558A1/de unknown
-
1995
- 1995-11-13 AT AT95937068T patent/ATE224012T1/de not_active IP Right Cessation
- 1995-11-13 JP JP51572996A patent/JP3638286B2/ja not_active Expired - Fee Related
- 1995-11-13 RU RU97110059/06A patent/RU2153105C2/ru not_active IP Right Cessation
- 1995-11-13 US US08/817,302 patent/US5896890A/en not_active Expired - Fee Related
- 1995-11-13 WO PCT/EP1995/004454 patent/WO1996015373A1/de not_active Ceased
- 1995-11-13 DE DE59510375T patent/DE59510375D1/de not_active Expired - Lifetime
- 1995-11-13 EP EP95937068A patent/EP0828945B1/de not_active Expired - Lifetime
- 1995-11-13 CN CN95196278A patent/CN1070584C/zh not_active Expired - Fee Related
- 1995-11-13 AU AU39285/95A patent/AU3928595A/en not_active Abandoned
- 1995-11-13 CA CA002205441A patent/CA2205441C/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2011154056A1 (de) | 2010-06-11 | 2011-12-15 | Bühler AG | Ventilanordnung |
Also Published As
| Publication number | Publication date |
|---|---|
| JP3638286B2 (ja) | 2005-04-13 |
| JPH10508679A (ja) | 1998-08-25 |
| CA2205441C (en) | 2005-02-08 |
| EP0828945A1 (de) | 1998-03-18 |
| US5896890A (en) | 1999-04-27 |
| ATE224012T1 (de) | 2002-09-15 |
| CA2205441A1 (en) | 1996-05-23 |
| WO1996015373A1 (de) | 1996-05-23 |
| CN1070584C (zh) | 2001-09-05 |
| AU3928595A (en) | 1996-06-06 |
| DE59510375D1 (de) | 2002-10-17 |
| LU88558A1 (de) | 1996-07-15 |
| CN1163657A (zh) | 1997-10-29 |
| RU2153105C2 (ru) | 2000-07-20 |
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