EP0845602B1 - Electrohydraulic control device - Google Patents

Electrohydraulic control device Download PDF

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Publication number
EP0845602B1
EP0845602B1 EP97118001A EP97118001A EP0845602B1 EP 0845602 B1 EP0845602 B1 EP 0845602B1 EP 97118001 A EP97118001 A EP 97118001A EP 97118001 A EP97118001 A EP 97118001A EP 0845602 B1 EP0845602 B1 EP 0845602B1
Authority
EP
European Patent Office
Prior art keywords
valve
cone
main control
slide
control device
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
EP97118001A
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German (de)
French (fr)
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EP0845602A3 (en
EP0845602A2 (en
Inventor
Hartmut Sandau
Werner Schumacher
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Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
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Filing date
Publication date
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Publication of EP0845602A2 publication Critical patent/EP0845602A2/en
Publication of EP0845602A3 publication Critical patent/EP0845602A3/en
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Publication of EP0845602B1 publication Critical patent/EP0845602B1/en
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Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00Details of servomotor systems ; Valves for servomotor systems
    • F15B13/01Locking-valves or other detent i.e. load-holding devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00Details of servomotor systems ; Valves for servomotor systems
    • F15B13/01Locking-valves or other detent i.e. load-holding devices
    • F15B13/015Locking-valves or other detent i.e. load-holding devices using an enclosed pilot flow valve
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • 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
    • 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
    • F15B13/0405Valve members; Fluid interconnections therefor for seat valves, i.e. poppet valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00Details of servomotor systems ; Valves for servomotor systems
    • 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
    • F15B13/044Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by electrically-controlled means, e.g. solenoids, torque-motors
    • 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
    • F15B19/00Testing; Calibrating; Fault detection or monitoring; Simulation or modelling of fluid-pressure systems or apparatus not otherwise provided for

Definitions

  • the invention is based on an electro-hydraulic control device for controlling the volume flows for a hydraulic Actuator depending on the electrical input signals on the proportional magnet according to that in the preamble of claim 1 specified genus.
  • Such an electrohydraulic control device has already been developed proposed after the older, unpublished patent application 195 22 746.8, with two such control devices to one double-acting control valve are connected.
  • a single one Control device works with a solenoid operated Slider with which a 4/2 function is displayed. At the deflection of the slide is a volume flow from the Pump passed to the servomotor, this feed flow over a slide valve is guided; at the same time that of Actuator coming volume flow led to the return, whereby this drain flow is controlled by an unlockable seat valve becomes.
  • the one-piece, as the main control element working slide is here for both valve functions provided at the same time.
  • the power of the proportional magnet is done with the help of a hydraulic sequence control increasingly transferred to the slider.
  • the slider can either be on the inflow stream or dependent on the discharge current coming from the servomotor be adjusted by the electric current.
  • the other volume flow arises according to the tolerances of the control edges of the slide and the housing. It can now be in may be a disadvantage in some cases, especially automatic ongoing control processes, so that not all Volume flows depending on the electrical current are known are.
  • DE 44 46 143 A1 is an electrohydraulic one Proportional valve known, the one operated by a magnet Control spool via a preloaded control spring on an adjusting screw, which is supported by a worm gear is fine adjustable.
  • this proportional valve can the control spring in a simple and precise way with different strength be biased.
  • this proportional valve points no 4/2 function.
  • the electrohydraulic control device has with the characterizing features of claim 1 in contrast the advantage that they are for precise control processes suitable because the overlaps of the control edges for both volume flows are adjustable.
  • the control device for a 4/2 function and the combination of Seat valve and slide valve can be adjusted here two characteristic curves occur; the disturbing influence of Tolerances in control processes can thus be largely avoided turn off.
  • the adjustment devices can with this Control device also the control sequence for the two control edges to get voted.
  • the control device builds relatively simple and compact and suitable for precise control operation.
  • valve carrier assigned to the poppet valve directly in the longitudinal bore can be arranged. It is advantageous further an embodiment according to claims 23 to 24, whereby also the pilot operated seat valve via a sequence control can be operated.
  • FIG. 1 shows a longitudinal section through a first electrohydraulic Control device 10, which acts as a 4/2 solenoid valve is executed.
  • the control device 10 consists of a Seat valve 11 and a slide valve 12, the control members coaxially in a longitudinal bore 13 of a housing 14 are arranged one behind the other and by a proportional magnet 15 are operated.
  • the control device 10 is thus executed in direct actuated design and has none pushing force-increasing sequence control so that it is suitable for low switching capacities.
  • a first motor chamber 16 with the motor connection B Connection has a return chamber 17 with the return port R is connected to a second motor chamber 18
  • Motor connection A has connection, while an inlet chamber 19th is connected to the inlet port P.
  • These working chambers 16 to 19 are arranged in the longitudinal bore 13 so that the return chamber 17 between the two engine chambers 16, 18 and the inlet chamber 19 between the second Motor chamber 18 and proportional magnet 15 is arranged.
  • the longitudinal bore 13 is multiple in the area of the seat valve 11 expanded and receives a valve carrier 21, in the inside of which a valve cone 22 of the seat valve 11 is arranged is.
  • the valve cone slidingly guided in the valve carrier 21 22 has a control edge 23 with subsequent fine control recesses 24, which with associated control openings 25 work together in valve carrier 21. This allows a volume flow proportional to the deflection of the valve plug 22 control that coming from a consumer from the motor connection B led to the return port R and as a drain stream referred to as.
  • the cone 26 and on the other hand a large overlap on the valve plug stem 27.
  • the valve plug 22 is opposite the pressures in the first engine chamber 16 and pressure-balanced in the return chamber 17, for which he serves to equalize the pressure inside Bores 28, 29 has.
  • the valve cone 22 is from a control spring 31 with its cone 26 on a valve seat 32 pressed, which is arranged inside the valve carrier 21 is and between the first motor chamber 16 and the return chamber 17 lies.
  • the control spring 31 is supported on an adjusting screw 33, which in turn is arranged in a screw cap 34.
  • the Screw cover 34 is screwed into the face of the valve carrier 21 and limits one that receives the control spring 31 Spring chamber 35 inside the valve carrier 21.
  • the adjusting screw 33 is secured by the lock nut 36.
  • the valve support 21 has at its front end External thread 37 with which it fits into an internal thread 38 in Housing 14 is screwed. Furthermore, the valve support 21 at a distance from the external thread 37 a collar with external teeth 39, in which a transverse to the longitudinal axis of the valve carrier 21 in the housing 14 screw 41 engages and forms a worm gear 42. By turning the Screw 41 allows valve carrier 21 to move about its longitudinal axis rotate, the pitch of the external thread 37 the axial adjustment determined. Arranged in the longitudinal bore 13 Sealing rings 43 provide a seal for the first motor chamber 16 to both sides.
  • a bolt-like actuator 44 is arranged, that penetrates the return chamber 17 and into the longitudinal bore 13 protrudes coaxially and the adjustment path of a longitudinal slide 45 transfers to the valve plug 22.
  • the longitudinal bore 13 is in the region of the slide valve 12 executed with the same diameter and takes a piston-like Longitudinal slide 45 on.
  • the longitudinal slide 45 has one first control edge 46 with adjacent fine control notches 47 to a volume flow from the inlet port P to the second To control motor connection A proportionally. With a second Control edge 48 affects the connection from the second Motor chamber 18 to the return chamber 17.
  • the longitudinal slide 45 is opposite the pressures in the inlet chamber 19, the second Motor chamber 18 and the return chamber 17 pressure balanced executed what he did one of his two faces connecting compensating bore 49.
  • the longitudinal slide 45 is coaxial to the valve plug 22 in the longitudinal bore 13 arranged and lies with its left end face on the actuator 44 while he was on his right, opposite lying end face acted upon by the armature axis 51 becomes.
  • the slide valve 12 always controls the Actuator flowing volume flow from the inlet connection P flows to the second motor chamber A and as an inlet flow referred to as.
  • the operation of the control device 10 is as follows, a 4/2 function with the solenoid-operated valve axis is pictured.
  • the seat valve 11 In the drawn zero position at not excited proportional solenoid 15, the seat valve 11 is like also the slide valve 12 blocked for the two volume flows; only the second motor connection A is over the second control edge 48 in the slide valve 12 to the return connection R relieved.
  • the proportional magnet 15 is excited and the longitudinal slide 45 and the one resting against it Valve plug 22 deflected to the left, so the connection closed from A to R via the second control edge 48 and the connection for the feed flow from P to A over the first control edge 46 on the longitudinal slide 45 and the connection for the drain flow from B to R via the Control edge 23 on the valve plug 22 opened, the plug 26 stands out from its valve seat 32.
  • volume flows can be controlled Size proportional to the electrical input signal on the magnet 15 is.
  • the discharge flow controlled from B via seat valve 11 to R. can be adjusted in size by a first adjusting device 52 can be set to which the set screw 33 and the control spring 31 count. So you can Change the size of this volume flow by using the Set screw 33 adjusts the bias of the control spring 31 against which the proportional magnet 15 works.
  • the from P via the slide valve 12 to A feed flow can be adjusted with the aid of a second adjusting device 53, why the worm gear 42, the valve carrier 21 and the valve cone 22 count. By turning the worm 42 the valve carrier 21 experiences a rotary movement about its Longitudinal axis that leads to an axial via the external thread 37 Adjustment leads.
  • the longitudinal slide 45 in it Axially adjusted position and thus the coverage of the Control edge 46 changed.
  • the overlap at the control edge 46 of the longitudinal slide 45 can thus be independent of the Coverage of the control edge 23 on the valve cone 22 is adjusted and the associated volume flow can be set.
  • the characteristic curves can thus be adjusted 52, 53 set for both volume flows of the 4/2 solenoid valve, see above that the disruptive influence of tolerances of the control edges can be balanced and thus also the tax sequence of the Control edges are easier to handle.
  • FIG. 2 shows a longitudinal section through a second control device 60, which is different from the first control device 10 mainly differs according to Figure 1 in that the seat valve 61 and the slide valve 62 as piloted Valves are formed, the first adjusting device 63 and the second adjusting device 64 are designed differently and are arranged; otherwise the same components as provided with the same reference numerals in FIG.
  • the housing-fixed valve seat 67 works with one in the Longitudinal bore 67 sliding main control cone 68 together, inside which a valve carrier 69 is concentrically supported, which in turn has a main control cone inside 68 piloting cone 71 takes.
  • a valve carrier 69 is concentrically supported, which in turn has a main control cone inside 68 piloting cone 71 takes.
  • To the outer edge of the main control cone 68 is again the control edge 23 and the fine control recesses 24 arranged with which controls the volume flow referred to as the discharge flow becomes; with its cone 26 it is supported on the housing side Valve seat 67 from.
  • On its opposite face the main control cone 68 limits in the longitudinal bore 65 a pressure chamber 72 which receives a compression spring 73.
  • This compression spring 73 is supported on the one hand on a housing-fixed Cover 74 off while using its other end over a locking ring 75 loads the main control cone 68 and presses on its valve seat 67. Between the fine control recesses 24 and the diameter of the cone 26 an annular space 76 is formed in the longitudinal bore 65, which likewise as the pressure chamber 72 with the same pressure as in the first Engine chamber 16 is loaded because the main control cone 68th is guided with sufficient play in the longitudinal bore 65.
  • valve carrier arranged coaxially in the main control cone 68 69 has an external thread 77 with which it fits into an internal thread is screwed into the main control cone 68 so that it can be adjusted axially by rotating it about its longitudinal axis.
  • One formed between valve carrier 69 and main control cone 68 Annulus 78 is axially extending Slot 79 in connection with the pressure chamber 72.
  • the essentially sleeve-shaped valve carrier 69 has in Connection to the external thread 77 an axially formed External hexagon 81, which protrudes into the pressure chamber 72 and penetrates the locking ring 75.
  • valve carrier 69 For backup of valve carrier 69 against adjustment in main control cone 68 serves this locking ring 75; it faces the front Teeth and engages in a toothing 82 of the main control cone 68.
  • the inner contour of the locking ring 75 engages form-fitting around the external hexagon 81 of the valve carrier 69, and also has breakthroughs 83 that the oil exchange between allow the pressure space 72 and the annular space 78.
  • the valve carrier 69 is the one used for pilot control Pilot cone 71 arranged by a spring 84 its seat in the valve carrier 69 is pressed. With this Pilot cone 71 is the seat diameter and the shaft diameter the same size, and there is an equalization hole inside provided so that the pilot cone 71 as pressure balanced valve can work.
  • the spring 84 receiving space is through a floor 85 which is in the valve support 69 is closely arranged, separated from the pressure chamber 72. in the closed state of the pilot cone 71 seals it due to its seat and its long shaft, which only has a small game, the annulus 78 well opposite the return chamber 17.
  • the valve carrier 69 forms here a part of the second adjustment device 64.
  • a main control slide 86 in the longitudinal bore 65 performed which is a part of the pilot operated slide valve 62nd forms. It has the first control edge on its outer circumference 46 and the fine control notches 47, which the from P after A controlled volume flow, the inlet flow. Further the main control slide 86 has the second control edge 48 to control the connection from A to R.
  • Main spool 86 is coaxially a pilot spool 87 slidably guided by the main spool 86 after Kind of a hydraulic sequencer works together.
  • the pilot spool 87 has a control edge 88 with which he has a cross bore 89 in the main spool 86 controls.
  • the spool can 87 influence a control oil flow, which of the Inlet chamber 19 branches off via the transverse bore 89 and Control edge 88 in a longitudinal bore 91 of the pilot spool 87 arrives, from there via a throttle point 92 in one Unlocking piston 93 flows and continues through openings in a screw cap 94 reaches the return chamber 17.
  • the screw cover 94 fastened in the main control slide 86 protrudes with a plunger 95 into the return chamber 17 and lies with its end having a slot 96 on the valve carrier 69 in the seat valve. Inside the plunger is 95 coaxially guided an unlock pin 97, the one hand on the unlocking piston 93 and on the other hand on the pilot cone 71 is present.
  • the unlocking piston 93 has a larger diameter than the pilot spool 87 and is coaxial to the latter in one Recess of the main control slide 86 slidably longitudinally guided.
  • the recess is through the screw cap 94 shut off, which the unlocking piston 93 additionally as a stop serves.
  • the unlocking piston 93 limits in this way in the recess a space 98 in which the longitudinal bore 91 of the pilot valve 87 opens.
  • the control spring 103 is now arranged, the one hand on a free end of the adjusting screw 101 and on the other hand on a bolt-shaped End of the pilot spool 87 supports that in the adjusting screw 101 protrudes.
  • this is bolt-shaped End of the armature axis 51 of the proportional magnet 15 on.
  • the adjusting screw 101 with the worm gear 42 forms here the first adjustment device 63, which in this way between the pilot operated slide valve 62 and the Proportional magnets 15 arranged in the longitudinal bore 65 is.
  • the operation of the second control device 60 which here is designed as a pilot operated 4/2 solenoid valve, is how follows explained, the slide axis being controlled by the pilot Construction can be used for larger performances.
  • the second control device 60 part of a double acting control valve is, as in the or part of the application mentioned in the introduction of a similar valve. In this case it is at zero the second control device 60 at the inlet connection P always the control pressure of a pressure compensator or the Standby pressure of a control pump on.
  • the control edge 88 of the Pilot spool 87 blocks a control oil flow, so that the pressure chamber 99 over the hollow spool 87 and the throttle point 92 in the unlocking piston 93 Return chamber 17 is relieved.
  • there is in the first motor chamber 16 of the line B coming up Load pressure which affects the radial play of the main control cone 68 also form in the annular space 76 and in the pressure space 72 can.
  • the pilot operated seat valve 61 ensures this for a secure seal of the motor connection B.
  • This pent up Pressure passes through the longitudinal bore 91 in the pilot valve 87 also in the pressure chamber 99, where he the main slide 86 acted on its right face.
  • the pressure in room 98 acts on the unlocking piston 93 and presses the unlocking pin 97 the pilot cone 71 in an open position, when the force on the unlocking piston 93 the force of the spring 84, which acts on the pilot cone 71, exceeds. If the pilot cone 71 opens, the pressure chamber becomes 72 through the openings 83, the slot 79 and the Annulus 78 to the return chamber 17 is relieved. With that the sinks Pressure in the pressure chamber 72 and the main control cone 68 can in the manner of an unlockable check valve by the Tappet 95 on the main control slide 86 can be moved to the left.
  • the pressure in the pressure chamber 99 is from the throttle point 92 in the unlocking piston 93 and on the other hand from the opening cross section determined on the transverse bore 89, and pushes first the unlocking piston 93 to the left until it stops on screw cap 94. After fitting the unlocking piston 93 this pressure will also change in the pressure chamber 99 fully build up and cover the entire face of the main spool Act on 86.
  • the power that thereby acting on the main spool 86 larger than that restoring force of the compression spring 73, the moves Main control spool 86 with the main control cone 68 as one one-piece, related control element with all its Split left.
  • control spring 103 Since the control spring 103 is supported on the adjusting screw 101, can by turning the screw 41 and the associated axial adjustment of the adjusting screw 101 the bias the control spring 103 can be changed so that the location the flow characteristic flow rate Q as a function of Current I in the magnet 60 is adjustable. This will also the position of the control edge 46 changed, so that a total of of the first adjusting device 63, the inlet flow can be adjusted is.
  • valve carrier 69 of the pilot cone 71 through its external thread 77 axially adjustable relative to the main control cone 68.
  • the valve carrier 69 is rotated with a special tool, the axially inserted for adjustment in the pressure chamber 72 and reaches over the external hex 81.
  • the plunger 95 is supported on the screw cap 94.
  • the rotation of the valve support 69 thus has a change in distance of the two fine control recesses 24 on the main control cone 68 and 47 on the main control slide 86 relative to each other result. In this way the overlaps are on two control edges 23 and 46 adjustable for both volume flows, so that the drain flow can be adjusted from B to R. is.
  • FIG. 4 shows a longitudinal section through a third control device 110, which is different from the second control device 60 according to Figure 2 differs as follows, wherein for same components same reference numerals are used.
  • the third control device 110 uses a different seat valve 111 in connection with another second adjustment device 112, the pilot operated slide valve 62 remains unchanged with the first adjusting device 63.
  • the pilot operated poppet valve 111 is the pilot pilot cone 113 slidingly arranged directly in the main control cone 114, while the main control cone 114 in turn in the Valve carrier 115 is slidably disposed.
  • the valve carrier 115 is in an expanded section of the longitudinal bore 65 rotatably and axially movable, for which he with a External thread 116 in a corresponding internal thread Longitudinal bore 65 is screwed. Furthermore, is on the valve support 115 a similar worm drive 117 is formed, as it already has the adjusting screw 101.
  • the valve carrier 115 has one at its end facing the return chamber 17 Valve seat 119 for the associated main control cone 114 while its other end is closed by a lid 120 which is the pressure chamber accommodating the compression spring 73 72 cordoned off.
  • the pilot cone 113 is the same Way as carried out according to Figure 2 in a pressure-balanced manner and serves in a corresponding manner for pilot control of the Main control cone 114.
  • the inlet flow from P to A in the same way via the first adjustment device 63 set while setting the drain current from B to R the second adjustment device 112 is used.
  • the valve carrier can be 115 adjust axially in the longitudinal bore 65, whereby its effective control edge in the control opening 121 relative to the control edge fixed to the housing in the slide valve in its position is changed. This can be done in a corresponding manner in the second control device 60 according to FIG. 2 also the Drain current from B to R can be adjusted or set.
  • FIG. 5 shows a longitudinal section through a fourth control device 130, which is different from the third control device 110 as shown in Figure 4, where for same components same reference numerals are used.
  • the fourth control device 130 uses a different seat valve 131 and a little modified slide valve 132, the control members themselves in the manner of a hydraulic Sequence control work together so that the Main control cone 133 in the seat valve no longer mechanically from Main spool 134 is operated, but hydraulically.
  • the structure of the housing 66 with the four working chambers 16 to 19, the basic structure of the main control spool 134 with its control edge 46 and the fine control notches 47, the Pilot valve 87 and the adjusting screw 101 with the first adjustment device 63 are essentially the same as in the third control device 110 according to FIG. 4.
  • the Main spool 134 is instead of the screw cap 94 now a plunger 135 with a plate-shaped extension 136 held.
  • the plate-shaped projection 136 is thereby by a return spring 140 which is supported fixed to the housing loaded and thus against the left face of the main spool 134 pressed, the lug 136 on its Outer circumference is centered in the main control slide 134.
  • the throttle point 92 provided for the control oil flow is now arranged in the plate-shaped neck 92, since a separate Unlocking piston 93 in the main control slide 134 is omitted.
  • the pilot operated seat valve 131 is like the third Control device 110 according to Figure 4 inside a valve carrier 137 arranged, which in turn in the remote Section of the longitudinal bore 65 is mounted.
  • the valve carrier 137 has the external thread 116 on its outer surface with which it fits into a suitable internal thread of the longitudinal bore 65 is screwed in and is therefore axially adjustable.
  • On a worm gear 117, the valve carrier 137 dispenses with the position of a lock nut 138 is secured.
  • the main control cone 133 arranged in the valve carrier 137 is here designed as a differential area valve, in which a ring surface formed by seat edge and valve stem 139 of the one prevailing in the first motor chamber 16 Pressure is applied in the opening direction.
  • the main tax cone 133 compression spring 73 loading in the closing direction lies in the pressure chamber 72, which is arranged in the valve stem Throttle 141 in connection with the first motor chamber 16 stands.
  • the main control cone 133 has as before Main control edge 23 and the fine control grooves 24 for control of the drain stream, whereby it is the actual one in the drain stream Cones are connected downstream.
  • the pilot cone arranged in the main control cone 133 is here designed as a ball 142, which sits between two valve seats is arranged in the main control cone 133 and with a tapered extension 143 of the plunger 135 in operative connection stands as it is required for the hydraulic sequence control is.
  • the valve carrier 137 is rotatable about its longitudinal axis and undergoes an axial adjustment as a result of the external thread 116, so that it is part of the second adjustment device 144 represents.
  • the operation of the fourth control device 130 is the same to that extent that of the third control device 110 Figure 4, as the main spool 134 with the spool 87 works in the manner of a hydraulic follow-up control, to control the feed flow from P to A.
  • the main spool 134 Tappet 135 for additional hydraulic sequence control of the seat valve 131.
  • Main control cone 133 the opening force by the pressure of the Load in the first motor chamber 16 on the ring surface 139 exerted while the closing force on the main control cone 133 from the pressure in the pressure chamber 72 to the whole effective area of the main control cone 133 becomes.
  • Ball 142 in main control cone 133 is part of its pilot valve. Raise the plunger 135 over his Extension 143 the ball 142 from its seat, so that opens Pilot valve and relieves pressure chamber 72 to the return chamber 17.
  • the one hand via the throttle 141 in the pressure chamber 72 inflowing oil and the other through the ball valve flowing out of the pressure chamber 72 to the return chamber 17 Oil determine the pressure in the pressure chamber 72 that on the left Front of the main control cone 133 acts and thus its direction of movement.
  • the main control cone 133 is thus hydraulically adjusted against the force of the spring 73, wherein it follows the position of the plunger 135 with its position, so that the seat valve 131 also has a sequence control here, which derive their energy from the load pressure of the first motor connection 16 relates.
  • the fourth controller 130 is therefore suitable for great performances.
  • FIG. 6 shows a longitudinal section through a fifth control device 150, which is different from the second control device 60 according to Figure 2 differs as follows, wherein for same components same reference numerals are used.
  • the fifth controller 150 uses another one Main control slide 151, in which the plunger 95 with the actual Main control slide is made in one piece.
  • the main control slide 151 has one Adjustment screw 101 open blind hole 152, in which of the pilot spool 87 and the unlocking piston 93 are slid in a row.
  • the blind hole 152 is of the same diameter throughout, so that the unlocking piston 93 and the spool 87 have the same outside diameter.
  • the slide valve 62 in the fifth control device 150 therefore comes along fewer components and is easier and cheaper produce.
  • the adjustment devices 63 and 64 can remain unchanged. Otherwise, the Operation of the fifth controller 115 like that the second control device 60.

Description

Stand der TechnikState of the art

Die Erfindung geht aus von einer elektrohydraulischen Steuervorrichtung zur Steuerung der Volumenströme für einen hydraulischen Stellmotor abhängig von den elektrischen Eingangssignalen am Proportionalmagnet nach der im Oberbegriff des Anspruchs 1 näher angegeben Gattung.The invention is based on an electro-hydraulic control device for controlling the volume flows for a hydraulic Actuator depending on the electrical input signals on the proportional magnet according to that in the preamble of claim 1 specified genus.

Es wurde bereits eine solche elektrohydraulische Steuervorrichtung nach der älteren nicht-vorveröffentlichten Patentanmeldung 195 22 746.8 vorgeschlagen, wobei zwei derartige Steuervorrichtungen zu einem doppeltwirkenden Regelventil verschaltet sind. Eine einzelne Steuervorrichtung arbeitet mit einem magnetbetätigten Schieber, mit dem eine 4/2-Funktion dargestellt wird. Bei der Auslenkung des Schiebers wird ein Volumenstrom von der Pumpe zum Stellmotor geleitet, wobei dieser Zulaufstrom über ein Schieberventil geführt ist; gleichzeitig wird der vom Stellmotor kommende Volumenstrom zum Rücklauf geführt, wobei dieser Ablaufstrom von einem entsperrbaren Sitzventil gesteuert wird. Der einstückig ausgebildete, als Hauptsteuerglied arbeitende Schieber ist hier für beide Ventilfunktionen gleichzeitig vorgesehen. Die Kraft des Proportionalmagneten wird dabei mit Hilfe einer hydraulischen Folgesteuerung verstärkt auf den Schieber übertragen. Bei dieser Bauweise kann der Schieber entweder auf den Zuflußstrom oder auf den vom Stellmotor kommenden Abflußstrom in Abhängigkeit vom elektrischen Strom eingestellt werden. Der andere Volumenstrom stellt sich entsprechend den Toleranzen der Steuerkanten des Schiebers und des Gehäuses ein. Es kann nun in manchen Fällen von Nachteil sein, insbesondere bei automatisch ablaufenden Regelvorgängen, daß hierdurch nicht alle Volumenströme in Abhängigkeit vom elektrischen Strom bekannt sind.Such an electrohydraulic control device has already been developed proposed after the older, unpublished patent application 195 22 746.8, with two such control devices to one double-acting control valve are connected. A single one Control device works with a solenoid operated Slider with which a 4/2 function is displayed. At the deflection of the slide is a volume flow from the Pump passed to the servomotor, this feed flow over a slide valve is guided; at the same time that of Actuator coming volume flow led to the return, whereby this drain flow is controlled by an unlockable seat valve becomes. The one-piece, as the main control element working slide is here for both valve functions provided at the same time. The power of the proportional magnet is done with the help of a hydraulic sequence control increasingly transferred to the slider. With this design the slider can either be on the inflow stream or dependent on the discharge current coming from the servomotor be adjusted by the electric current. The other volume flow arises according to the tolerances of the control edges of the slide and the housing. It can now be in may be a disadvantage in some cases, especially automatic ongoing control processes, so that not all Volume flows depending on the electrical current are known are.

Ferner ist aus der DE 44 46 143 A1 ein elektrohydraulisches Proportionalventil bekannt, dessen von einem Magneten betätigter Steuerschieber sich über eine vorgespannte Regelfeder auf einer Einstellschraube abstützt, die über einen Schnekkentrieb feineinstellbar ist. Für die Einstellung der Durchflußkennlinie dieses Proportionalventils kann die Regelfeder in einfacher und genauer Weise mit unterschiedlicher Kraft vorgespannt werden. Dieses Proportionalventil weist jedoch keine 4/2-Funktion auf.Furthermore, DE 44 46 143 A1 is an electrohydraulic one Proportional valve known, the one operated by a magnet Control spool via a preloaded control spring on an adjusting screw, which is supported by a worm gear is fine adjustable. For setting the flow characteristic this proportional valve can the control spring in a simple and precise way with different strength be biased. However, this proportional valve points no 4/2 function.

Vorteile der ErfindungAdvantages of the invention

Die erfindungsgemäße elektrohydraulische Steuervorrichtung mit den kennzeichnenden Merkmalen des Anspruchs 1 hat demgegenüber den Vorteil, daß sie sich für genaue Regelvorgänge eignet, da die Überdeckungen der Steuerkanten für beide Volumenströme justierbar sind. Trotz der Ausbildung der Steuervorrichtung für eine 4/2-Funktion und der Kombination von Sitzventil und Schieberventil kann hier die Einstellung zweier Kennlinien erfolgen; der bisher störende Einfluß von Toleranzen bei Regelvorgängen läßt sich damit weitgehend ausschalten. Mit den Justiereinrichtungen kann bei dieser Steuervorrichtung auch die Steuerfolge für die beiden Steuerkanten gewählt werden. Die Steuervorrichtung baut relativ einfach und kompakt und eignet sich für einen genauen Regelbetrieb.The electrohydraulic control device according to the invention has with the characterizing features of claim 1 in contrast the advantage that they are for precise control processes suitable because the overlaps of the control edges for both volume flows are adjustable. Despite the design of the control device for a 4/2 function and the combination of Seat valve and slide valve can be adjusted here two characteristic curves occur; the disturbing influence of Tolerances in control processes can thus be largely avoided turn off. With the adjustment devices can with this Control device also the control sequence for the two control edges to get voted. The control device builds relatively simple and compact and suitable for precise control operation.

Durch die in den Unteransprüchen aufgeführten Maßnahmen sind vorteilhafte Weiterbildungen und Verbesserungen der im Anspruch 1 angegebenen elektrohydraulischen Steuervorrichtung möglich. Eine besonders vorteilhafte Ausgestaltung ergibt sich gemäß Anspruch 2, da diese Zuordnung eine schnelle und genaue Justierung erlaubt. Ferner ist es günstig, die Steuervorrichtung nach den Ansprüchen 3 bis 9 auszubilden, wodurch eine direktgesteuerte Ventilbauweise ermöglicht wird, die zu einer kompakten Steuervorrichtung mit gut zugänglichen Einstellmöglichkeiten führt. Zweckmäßig sind ferner Ausbildungen nach den Ansprüchen 10 bis 26, wodurch vorgesteuerte Ventilbauweisen möglich sind, die unterschiedlich aufgebaute Schieberachsen zulassen. Dabei führen die Ausführungen nach den Ansprüchen 10 bis 12 zu relativ einfach und kompakt bauenden Steuervorrichtungen, die kostengünstig herstellbar sind und leicht verstellbar sind. Vorteilhaft sind ferner Ausführungen nach den Ansprüchen 13 bis 15, was eine Steuervorrichtung mit geringem Raumbedarf ergibt, da die Steuerglieder von Sitzventil und Schieberventil unmittelbar in der Längsbohrung gleitend geführt sind. Bei den Ausführungen nach den Ansprüchen 16 bis 22 ist es zweckmäßig, wenn der dem Sitzventil zugeordnete Ventilträger unmittelbar in der Längsbohrung angeordnet werden kann. Vorteilhaft ist ferner eine Ausführung nach den Ansprüchen 23 bis 24, wodurch auch das vorgesteuerte Sitzventil über eine Folgesteuerung betrieben werden kann. Eine äußerst kostengünstige und einfache Bauweise ergibt sich gemäß Anspruch 27, die mit wenig Bauteilen auskommt und relativ einfach herstellbar ist. Weitere Vorteile ergeben sich aus den übrigen Ansprüchen, der Beschreibung sowie der Zeichnung. By the measures listed in the subclaims advantageous developments and improvements in the claim 1 specified electro-hydraulic control device possible. A particularly advantageous embodiment results itself according to claim 2, since this assignment is a fast and exact adjustment allowed. It is also favorable to the control device to train according to claims 3 to 9, whereby a directly controlled valve design is made possible to a compact control device with easily accessible Setting options leads. Are also useful Training according to claims 10 to 26, whereby pilot-controlled Valve designs are possible that vary Allow mounted slide axes. The statements lead according to claims 10 to 12 to relatively simple and compact control devices that can be manufactured inexpensively are and are easily adjustable. Are advantageous further embodiments according to claims 13 to 15, which a Control device with a small footprint results because the Control elements of seat valve and slide valve directly are slidably guided in the longitudinal bore. In the executions according to claims 16 to 22, it is advantageous if the valve carrier assigned to the poppet valve directly in the longitudinal bore can be arranged. It is advantageous further an embodiment according to claims 23 to 24, whereby also the pilot operated seat valve via a sequence control can be operated. An extremely inexpensive and simple construction results according to claim 27, which with few components are needed and relatively easy to manufacture is. Further advantages result from the remaining claims, the description and the drawing.

Zeichnungdrawing

Fünf Ausführungsbeispiele der Erfindung sind in der Zeichnung dargestellt und in der nachfolgenden Beschreibung näher erläutert.
Es zeigen:

Figur 1
einen Längsschnitt durch ein erstes Ausführungsbeispiel einer elektrohydraulischen Steuervorrichtung in direktgesteuerter Bauweise in vereinfachter Darstellung,
Figur 2
als zweites Ausführungsbeispiel der Erfindung einen Längsschnitt durch eine elektrohydraulische Steuervorrichtung in vorgesteuerter Bauweise in vereinfachter Darstellung,
Figur 3
einen Teilschnitt nach III-III in Figur 2, und die
Figuren 4 bis 6
jeweils Längsschnitte durch eine dritte, vierte bzw. fünfte Ausführungsform der Steuervorrichtung.
Five embodiments of the invention are shown in the drawing and explained in more detail in the following description.
Show it:
Figure 1
2 shows a longitudinal section through a first exemplary embodiment of an electrohydraulic control device in a directly controlled construction in a simplified representation,
Figure 2
as a second exemplary embodiment of the invention, a longitudinal section through an electrohydraulic control device in a pilot-controlled design in a simplified representation,
Figure 3
a partial section according to III-III in Figure 2, and the
Figures 4 to 6
longitudinal sections through a third, fourth and fifth embodiment of the control device.

Beschreibung der AusführungsbeispieleDescription of the embodiments

Die Figur 1 zeigt einen Längsschnitt durch eine erste elektrohydraulische Steuervorrichtung 10, die als 4/2-Magnetventil ausgeführt ist. Die Steuervorrichtung 10 besteht aus einem Sitzventil 11 und einem Schieberventil 12, deren Steuerglieder koaxial in einer Längsbohrung 13 eines Gehäuses 14 hintereinander angeordnet sind und von einem Proportionalmagneten 15 betätigt werden. Die Steuervorrichtung 10 ist somit in direktbetätigter Bauweise ausgeführt und weist keine schieberkraftverstärkende Folgesteuerung auf, so daß sie sich für geringe Schaltleistungen eignet. 1 shows a longitudinal section through a first electrohydraulic Control device 10, which acts as a 4/2 solenoid valve is executed. The control device 10 consists of a Seat valve 11 and a slide valve 12, the control members coaxially in a longitudinal bore 13 of a housing 14 are arranged one behind the other and by a proportional magnet 15 are operated. The control device 10 is thus executed in direct actuated design and has none pushing force-increasing sequence control so that it is suitable for low switching capacities.

In der das Gehäuse 14 durchdringenden Längsbohrung 13 sind durch ringförmige Erweiterungen vier Kammern ausgebildet, von denen eine erste Motorkammer 16 mit dem Motoranschluß B Verbindung hat, eine Rücklaufkammer 17 mit dem Rücklaufanschluß R verbunden ist, eine zweite Motorkammer 18 mit dem Motoranschluß A Verbindung hat, während eine Zulaufkammer 19 mit dem Zulaufanschluß P verbunden ist. Diese Arbeitskammern 16 bis 19 sind in der Längsbohrung 13 so angeordnet, daß die Rücklaufkammer 17 zwischen den beiden Motorkammern 16, 18 liegt und die Zulaufkammer 19 zwischen zweiter Motorkammer 18 und Proportionalmagnet 15 angeordnet ist.In the longitudinal bore 13 penetrating the housing 14 four chambers formed by annular extensions, of which a first motor chamber 16 with the motor connection B Connection has a return chamber 17 with the return port R is connected to a second motor chamber 18 Motor connection A has connection, while an inlet chamber 19th is connected to the inlet port P. These working chambers 16 to 19 are arranged in the longitudinal bore 13 so that the return chamber 17 between the two engine chambers 16, 18 and the inlet chamber 19 between the second Motor chamber 18 and proportional magnet 15 is arranged.

Die Längsbohrung 13 ist im Bereich des Sitzventils 11 mehrfach aufgeweitet und nimmt einen Ventilträger 21 auf, in dessen Innern ein Ventilkegel 22 des Sitzventils 11 angeordnet ist. Der im Ventilträger 21 gleitend geführte Ventilkegel 22 hat eine Steuerkante 23 mit anschließenden Feinsteuerausnehmungen 24, welche mit zugehörigen Steueröffnungen 25 im Ventilträger 21 zusammenarbeiten. Damit läßt sich ein Volumenstrom proportional zur Auslenkung des Ventilkegels 22 steuern, der von einem Verbraucher kommend vom Motoranschluß B zum Rücklaufanschluß R geführt und als Ablaufstrom bezeichnet wird. Für eine sichere Abdichtung der ersten Motorkammer 16 sorgt einerseits der Kegel 26 und andererseits eine große Überdeckung am Ventilkegelschaft 27. Der Ventilkegel 22 ist gegenüber den Drücken in der ersten Motorkammer 16 sowie in der Rücklaufkammer 17 druckausgeglichen ausgebildet, wozu er in seinem Inneren dem Druckausgleich dienende Bohrungen 28, 29 aufweist. Der Ventilkegel 22 wird von einer Regelfeder 31 mit seinem Kegel 26 auf einen Ventilsitz 32 gedrückt, welcher innen am Ventilträger 21 angeordnet ist und zwischen der ersten Motorkammer 16 und der Rücklaufkammer 17 liegt. The longitudinal bore 13 is multiple in the area of the seat valve 11 expanded and receives a valve carrier 21, in the inside of which a valve cone 22 of the seat valve 11 is arranged is. The valve cone slidingly guided in the valve carrier 21 22 has a control edge 23 with subsequent fine control recesses 24, which with associated control openings 25 work together in valve carrier 21. This allows a volume flow proportional to the deflection of the valve plug 22 control that coming from a consumer from the motor connection B led to the return port R and as a drain stream referred to as. For a secure seal of the first engine chamber 16 on the one hand the cone 26 and on the other hand a large overlap on the valve plug stem 27. The valve plug 22 is opposite the pressures in the first engine chamber 16 and pressure-balanced in the return chamber 17, for which he serves to equalize the pressure inside Bores 28, 29 has. The valve cone 22 is from a control spring 31 with its cone 26 on a valve seat 32 pressed, which is arranged inside the valve carrier 21 is and between the first motor chamber 16 and the return chamber 17 lies.

Die Regelfeder 31 stützt sich auf einer Stellschraube 33 ab, die ihrerseits in einem Schraubdeckel 34 angeordnet ist. Der Schraubdeckel 34 ist stirnseitig in den Ventilträger 21 eingeschraubt und begrenzt einen die Regelfeder 31 aufnehmenden Federraum 35 innerhalb des Ventilträgers 21. Die Stellschraube 33 ist durch die Kontermutter 36 gesichert.The control spring 31 is supported on an adjusting screw 33, which in turn is arranged in a screw cap 34. The Screw cover 34 is screwed into the face of the valve carrier 21 and limits one that receives the control spring 31 Spring chamber 35 inside the valve carrier 21. The adjusting screw 33 is secured by the lock nut 36.

Der Ventilträger 21 weist an seinem stirnseitigen Ende ein Außengewinde 37 auf, mit dem er in ein Innengewinde 38 im Gehäuse 14 eingeschraubt ist. Ferner weist der Ventilträger 21 im Abstand vom Außengewinde 37 einen Bund mit Außenverzahnung 39 auf, in die eine quer zur Längsachse des Ventilträgers 21 im Gehäuse 14 gelagerte Schnecke 41 greift und dabei einen Schneckentrieb 42 bildet. Durch Drehen der Schnecke 41 läßt sich der Ventilträger 21 um seine Längsachse drehen, wobei die Steigung des Außengewindes 37 dabei die axiale Verstellung bestimmt. In der Längsbohrung 13 angeordnete Dichtringe 43 sorgen für eine Abdichtung der ersten Motorkammer 16 nach beiden Seiten hin. An dem im Ventilträger 21 geführten Ventilkegel 22 ist auf der Seite des Kegels 26 ein bolzenartiges Betätigungsglied 44 angeordnet, das die Rücklaufkammer 17 durchdringt und in die Längsbohrung 13 koaxial hineinragt und den Verstellweg eines Längsschiebers 45 auf den Ventilkegel 22 überträgt.The valve support 21 has at its front end External thread 37 with which it fits into an internal thread 38 in Housing 14 is screwed. Furthermore, the valve support 21 at a distance from the external thread 37 a collar with external teeth 39, in which a transverse to the longitudinal axis of the valve carrier 21 in the housing 14 screw 41 engages and forms a worm gear 42. By turning the Screw 41 allows valve carrier 21 to move about its longitudinal axis rotate, the pitch of the external thread 37 the axial adjustment determined. Arranged in the longitudinal bore 13 Sealing rings 43 provide a seal for the first motor chamber 16 to both sides. On the one in the valve carrier 21 guided valve plug 22 is on the side of the plug 26 a bolt-like actuator 44 is arranged, that penetrates the return chamber 17 and into the longitudinal bore 13 protrudes coaxially and the adjustment path of a longitudinal slide 45 transfers to the valve plug 22.

Im Bereich des Schieberventils 12 ist die Längsbohrung 13 mit gleichem Durchmesser ausgeführt und nimmt einen kolbenartigen Längsschieber 45 auf. Der Längsschieber 45 weist eine erste Steuerkante 46 mit angrenzenden Feinsteuerkerben 47 auf, um einen Volumenstrom vom Zulaufanschluß P zum zweiten Motoranschluß A proportional zu steuern. Mit einer zweiten Steuerkante 48 beeinflußt er die Verbindung von der zweiten Motorkammer 18 zur Rücklaufkammer 17. Der Längsschieber 45 ist gegenüber den Drücken in der Zulaufkammer 19, der zweiten Motorkammer 18 sowie der Rücklaufkammer 17 druckausgeglichen ausgeführt, wozu er eine seine beiden Stirnseiten verbindende Ausgleichsbohrung 49 aufweist. Der Längsschieber 45 ist in der Längsbohrung 13 koaxial zum Ventilkegel 22 angeordnet und liegt mit seiner linken Stirnseite an dem Betätigungsglied 44 an, während er an seiner rechten, entgegengesetzt liegenden Stirnseite von der Ankerachse 51 beaufschlagt wird. Das Schieberventil 12 steuert stets den zum Stellmotor hinfließenden Volumenstrom, der vom Zulaufanschluß P zur zweiten Motorkammer A fließt und als Zulaufstrom bezeichnet wird.The longitudinal bore 13 is in the region of the slide valve 12 executed with the same diameter and takes a piston-like Longitudinal slide 45 on. The longitudinal slide 45 has one first control edge 46 with adjacent fine control notches 47 to a volume flow from the inlet port P to the second To control motor connection A proportionally. With a second Control edge 48 affects the connection from the second Motor chamber 18 to the return chamber 17. The longitudinal slide 45 is opposite the pressures in the inlet chamber 19, the second Motor chamber 18 and the return chamber 17 pressure balanced executed what he did one of his two faces connecting compensating bore 49. The longitudinal slide 45 is coaxial to the valve plug 22 in the longitudinal bore 13 arranged and lies with its left end face on the actuator 44 while he was on his right, opposite lying end face acted upon by the armature axis 51 becomes. The slide valve 12 always controls the Actuator flowing volume flow from the inlet connection P flows to the second motor chamber A and as an inlet flow referred to as.

Die Wirkungsweise der Steuervorrichtung 10 ist wie folgt, wobei mit der magnetbetätigten Ventilachse eine 4/2-Funktion dargestellt wird. In der gezeichneten Nullstellung bei nicht erregtem Proportionalmagnet 15 ist das Sitzventil 11 wie auch das Schieberventil 12 für die beiden Volumenströme gesperrt; lediglich der zweite Motoranschluß A wird dabei über die zweite Steuerkante 48 im Schieberventil 12 zum Rücklaufanschluß R entlastet. Wird der Proportionalmagnet 15 erregt und dabei der Längsschieber 45 sowie der an ihm anliegende Ventilkegel 22 nach links ausgelenkt, so wird die Verbindung von A nach R über die zweite Steuerkante 48 geschlossen und die Verbindung für den Zulaufstrom von P nach A über die erste Steuerkante 46 am Längsschieber 45 sowie die Verbindung für den Ablaufstrom von B nach R über die Steuerkante 23 am Ventilkegel 22 geöffnet, wobei der Kegel 26 von seinem Ventilsitz 32 abhebt. Mit dem Proportionalmagnet 15 lassen sich dabei Volumenströme steuern, deren Größe proportional zum elektrischen Eingangssignal am Magneten 15 ist.The operation of the control device 10 is as follows, a 4/2 function with the solenoid-operated valve axis is pictured. In the drawn zero position at not excited proportional solenoid 15, the seat valve 11 is like also the slide valve 12 blocked for the two volume flows; only the second motor connection A is over the second control edge 48 in the slide valve 12 to the return connection R relieved. The proportional magnet 15 is excited and the longitudinal slide 45 and the one resting against it Valve plug 22 deflected to the left, so the connection closed from A to R via the second control edge 48 and the connection for the feed flow from P to A over the first control edge 46 on the longitudinal slide 45 and the connection for the drain flow from B to R via the Control edge 23 on the valve plug 22 opened, the plug 26 stands out from its valve seat 32. With the proportional magnet 15, volume flows can be controlled Size proportional to the electrical input signal on the magnet 15 is.

Der von B über das Sitzventil 11 nach R gesteuerte Ablaufstrom kann dabei in seiner Größe durch eine erste Justiereinrichtung 52 eingestellt werden, zu der die Stellschraube 33 und die Regelfeder 31 zählen. So läßt sich die Größe dieses Volumenstromes ändern, indem mit Hilfe der Stellschraube 33 die Vorspannung der Regelfeder 31 verstellt wird, gegen welche der Proportionalmagnet 15 arbeitet. Der von P über das Schieberventil 12 nach A geführte Zulaufstrom läßt sich mit Hilfe einer zweiten Justiereinrichtung 53 einstellen, wozu der Schneckentrieb 42, der Ventilträger 21 sowie der Ventilkegel 22 zählen. Durch Drehen der Schnecke 42 erfährt der Ventilträger 21 eine Drehbewegung um seine Längsachse, die über das Außengewinde 37 zu einer axialen Verstellung führt. Über den Ventilkegel 22 mit seinem Entsperrglied 44 wird dadurch der Längsschieber 45 in seiner Lage axial verstellt und damit auch die Überdeckung der Steuerkante 46 geändert. Die Überdeckung an der Steuerkante 46 des Längsschiebers 45 kann somit unabhängig von der Überdeckung der Steuerkante 23 am Ventilkegel 22 justiert und der zugehörige Volumenstrom eingestellt werden. Mit den Justiereinrichtungen 52, 53 lassen sich somit die Kennlinien für beide Volumenströme des 4/2-Magnetventils einstellen, so daß der störende Einfluß von Toleranzen der Steuerkanten ausgeglichen werden kann und damit auch die Steuerfolge der Steuerkanten leichter beherschbar ist.The discharge flow controlled from B via seat valve 11 to R. can be adjusted in size by a first adjusting device 52 can be set to which the set screw 33 and the control spring 31 count. So you can Change the size of this volume flow by using the Set screw 33 adjusts the bias of the control spring 31 against which the proportional magnet 15 works. The from P via the slide valve 12 to A feed flow can be adjusted with the aid of a second adjusting device 53, why the worm gear 42, the valve carrier 21 and the valve cone 22 count. By turning the worm 42 the valve carrier 21 experiences a rotary movement about its Longitudinal axis that leads to an axial via the external thread 37 Adjustment leads. About the valve plug 22 with his Unlocking member 44 is the longitudinal slide 45 in it Axially adjusted position and thus the coverage of the Control edge 46 changed. The overlap at the control edge 46 of the longitudinal slide 45 can thus be independent of the Coverage of the control edge 23 on the valve cone 22 is adjusted and the associated volume flow can be set. With the The characteristic curves can thus be adjusted 52, 53 set for both volume flows of the 4/2 solenoid valve, see above that the disruptive influence of tolerances of the control edges can be balanced and thus also the tax sequence of the Control edges are easier to handle.

Die Figur 2 zeigt einen Längsschnitt durch eine zweite Steuereinrichtung 60, die sich von der ersten Steuereinrichtung 10 nach Figur 1 vor allem dadurch unterscheidet, daß das Sitzventil 61 und das Schieberventil 62 als vorgesteuerte Ventile ausgebildet sind, die erste Justiereinrichtung 63 und die zweite Justiereinrichtung 64 anders ausgebildet und angeordnet sind; im übrigen werden gleiche Bauelemente wie in Figur 1 mit gleichen Bezugszeichen versehen.FIG. 2 shows a longitudinal section through a second control device 60, which is different from the first control device 10 mainly differs according to Figure 1 in that the seat valve 61 and the slide valve 62 as piloted Valves are formed, the first adjusting device 63 and the second adjusting device 64 are designed differently and are arranged; otherwise the same components as provided with the same reference numerals in FIG.

In der das Gehäuse 66 durchdringenden Längsbohrung 65 sind in gleicher Weise die beiden Motorkammern 16, 18 sowie die Rücklaufkammer 17 und die Zulaufkammer 19 angeordnet, wobei im Bereich zwischen der ersten Motorkammer 16 und der Rücklaufkammer 17 in der Längsbohrung 65 ein dem Sitzventil 61 zugeordneter Ventilsitz 67 ausgebildet ist.In the longitudinal bore 65 penetrating the housing 66 in the same way, the two motor chambers 16, 18 and Return chamber 17 and the inlet chamber 19 arranged, wherein in the area between the first motor chamber 16 and the return chamber 17 in the longitudinal bore 65 and the seat valve 61 associated valve seat 67 is formed.

Der gehäusefeste Ventilsitz 67 arbeitet mit einem in der Längsbohrung 67 gleitend geführten Hauptsteuerkegel 68 zusamen, in dessen Innern konzentrisch ein Ventilträger 69 lagert, der seinerseits in seinem Innern einen den Hauptsteuerkegel 68 vorsteuernden Vorsteuerkegel 71 aufnimmt. An dem Außenumfang des Hauptsteuerkegels 68 sind wiederum die Steuerkante 23 und die Feinsteuerausnehmungen 24 angeordnet, mit welchen der als Ablaufstrom bezeichnete Volumenstrom gesteuert wird; mit seinem Kegel 26 stützt er sich am gehäuseseitigen Ventilsitz 67 ab. Auf seiner entgegengesetzten Stirnseite begrenzt der Hauptsteuerkegel 68 in der Längsbohrung 65 einen Druckraum 72, der eine Druckfeder 73 aufnimmt. Diese Druckfeder 73 stützt sich einerseits an einem gehäusefesten Deckel 74 ab, während sie mit ihrem anderen Ende über einen Sicherungsring 75 den Hauptsteuerkegel 68 belastet und auf seinen Ventilsitz 67 drückt. Zwischen den Feinsteuerausnehmungen 24 und dem im Durchmesser abgesetzten Kegel 26 ist in der Längsbohrung 65 ein Ringraum 76 gebildet, der ebenso wie der Druckraum 72 mit dem gleichen Druck wie in der ersten Motorkammer 16 belastet ist, da der Hauptsteuerkegel 68 mit ausreichend Spiel in der Längsbohrung 65 geführt ist.The housing-fixed valve seat 67 works with one in the Longitudinal bore 67 sliding main control cone 68 together, inside which a valve carrier 69 is concentrically supported, which in turn has a main control cone inside 68 piloting cone 71 takes. To the The outer edge of the main control cone 68 is again the control edge 23 and the fine control recesses 24 arranged with which controls the volume flow referred to as the discharge flow becomes; with its cone 26 it is supported on the housing side Valve seat 67 from. On its opposite face the main control cone 68 limits in the longitudinal bore 65 a pressure chamber 72 which receives a compression spring 73. This compression spring 73 is supported on the one hand on a housing-fixed Cover 74 off while using its other end over a locking ring 75 loads the main control cone 68 and presses on its valve seat 67. Between the fine control recesses 24 and the diameter of the cone 26 an annular space 76 is formed in the longitudinal bore 65, which likewise as the pressure chamber 72 with the same pressure as in the first Engine chamber 16 is loaded because the main control cone 68th is guided with sufficient play in the longitudinal bore 65.

Der koaxial im Hauptsteuerkegel 68 angeordnete Ventilträger 69 weist ein Außengewinde 77 auf, mit dem er in ein Innengewinde im Hauptsteuerkegel 68 eingeschraubt ist, so daß er durch Drehen um seine Längsachse axial verstellbar ist. Ein zwischen Ventilträger 69 und Hauptsteuerkegel 68 ausgebildeter Ringraum 78 steht über einen axial verlaufenden Schlitz 79 mit dem Druckraum 72 in Verbindung. Der im wesentlichen hülsenförmig aufgebaute Ventilträger 69 weist im Anschluß an das Außengewinde 77 einen axial ausgebildeten Außensechskant 81 auf, welcher in den Druckraum 72 ragt und dabei den Sicherungsring 75 durchdringt. Für die Sicherung des Ventilträgers 69 gegen Verstellen im Hauptsteuerkegel 68 dient dabei dieser Sicherungsring 75; er weist stirnseitig Zähne auf und greift in eine Verzahnung 82 des Hauptsteuerkegels 68. Die Innenkontur des Sicherungsrings 75 greift formschlüssig um den Außensechskant 81 des Ventilträgers 69, und weist zudem Durchbrüche 83 auf, die den Ölaustausch zwischen dem Druckraum 72 und dem Ringraum 78 gestatten.The valve carrier arranged coaxially in the main control cone 68 69 has an external thread 77 with which it fits into an internal thread is screwed into the main control cone 68 so that it can be adjusted axially by rotating it about its longitudinal axis. One formed between valve carrier 69 and main control cone 68 Annulus 78 is axially extending Slot 79 in connection with the pressure chamber 72. The essentially sleeve-shaped valve carrier 69 has in Connection to the external thread 77 an axially formed External hexagon 81, which protrudes into the pressure chamber 72 and penetrates the locking ring 75. For backup of valve carrier 69 against adjustment in main control cone 68 serves this locking ring 75; it faces the front Teeth and engages in a toothing 82 of the main control cone 68. The inner contour of the locking ring 75 engages form-fitting around the external hexagon 81 of the valve carrier 69, and also has breakthroughs 83 that the oil exchange between allow the pressure space 72 and the annular space 78.

In dem Ventilträger 69 ist der zur Vorsteuerung dienende Vorsteuerkegel 71 angeordnet, der von einer Feder 84 auf seinen Sitz im Ventilträger 69 gedrückt wird. Bei diesem Vorsteuerkegel 71 ist der Sitzdurchmesser und der Schaftdurchmesser gleich groß, und in seinem Innern ist eine Ausgleichsbohrung vorgesehen, so daß der Vorsteuerkegel 71 als druckausgeglichenes Ventil arbeiten kann. Der die Feder 84 aufnehmende Raum ist durch einen Boden 85, der im Ventilträger 69 dicht angeordnet ist, vom Druckraum 72 getrennt. Im geschlossenen Zustand des Vorsteuerkegels 71 dichtet dieser aufgrund seines Sitzes und seines langen Schaftes, der nur ein kleines Spiel aufweist, den Ringraum 78 gut gegenüber der Rücklaufkammer 17 ab. Der Ventilträger 69 bildet hier ein Teil der zweiten Justiereinrichtung 64.The valve carrier 69 is the one used for pilot control Pilot cone 71 arranged by a spring 84 its seat in the valve carrier 69 is pressed. With this Pilot cone 71 is the seat diameter and the shaft diameter the same size, and there is an equalization hole inside provided so that the pilot cone 71 as pressure balanced valve can work. The spring 84 receiving space is through a floor 85 which is in the valve support 69 is closely arranged, separated from the pressure chamber 72. in the closed state of the pilot cone 71 seals it due to its seat and its long shaft, which only has a small game, the annulus 78 well opposite the return chamber 17. The valve carrier 69 forms here a part of the second adjustment device 64.

Im Bereich der Zulaufkammer 19 und der zweiten Motorkammer 18 ist in der Längsbohrung 65 ein Hauptsteuerschieber 86 geführt, der ein Teil des vorgesteuerten Schieberventils 62 bildet. An seinem Außenumfang weist er die erste Steuerkante 46 und die Feinsteuerkerben 47 auf, welche den von P nach A geführten Volumenstrom, den Zulaufstrom, steuern. Ferner weist der Hauptsteuerschieber 86 die zweite Steuerkante 48 auf, um die Verbindung von A nach R zu steuern. In dem Hauptsteuerschieber 86 ist koaxial ein Vorsteuerschieber 87 gleitend geführt, der mit dem Hauptsteuerschieber 86 nach Art einer hydraulischen Folgesteuerung zusammenarbeitet. Zu diesem Zweck weist der Vorsteuerschieber 87 eine Steuerkante 88 auf, mit welcher er eine Querbohrung 89 im Hauptsteuerschieber 86 steuert. Auf diese Weise kann der Vorsteuerschieber 87 einen Steuerölstrom beeinflussen, der von der Zulaufkammer 19 abzweigt, über die Querbohrung 89 und die Steuerkante 88 in eine Längsbohrung 91 des Vorsteuerschiebers 87 gelangt, von dort über eine Drosselstelle 92 in einem Entsperrkolben 93 fließt und weiter über Öffnungen in einem Schraubdeckel 94 in die Rücklaufkammer 17 gelangt. Der im Hauptsteuerschieber 86 befestigte Schraubdeckel 94 ragt mit einem Stößel 95 in die Rücklaufkammer 17 hinein und liegt mit seinem einen Schlitz 96 aufweisenden Ende am Ventilträger 69 im Sitzventil an. Im Innern des Stößels 95 ist koaxial ein Entsperrstift 97 gleitend geführt, der einerseits am Entsperrkolben 93 und andererseits am Vorsteuerkegel 71 anliegt. Durch den Stößel 95 und den Entsperrstift 97 ist zwischen dem Schieberventil 62 und dem Sitzventil 61 eine mechanische Wirkverbindung hergestellt. Der Entsperrkolben 93 weist hier einen größeren Durchmesser als der Vorsteuerschieber 87 auf und ist koaxial zu letzterem in einer Ausnehmung des Hauptsteuerschiebers 86 längsbeweglich gleitend geführt. Die Ausnehmung ist durch den Schraubdeckel 94 abgesperrt, welche dem Entsperrkolben 93 zusätzlich als Anschlag dient. Der Entsperrkolben 93 begrenzt auf diese Weise in der Ausnehmung einen Raum 98, in welchen die Längsbohrung 91 des Vorsteuerschiebers 87 mündet.In the area of the inlet chamber 19 and the second motor chamber 18 is a main control slide 86 in the longitudinal bore 65 performed, which is a part of the pilot operated slide valve 62nd forms. It has the first control edge on its outer circumference 46 and the fine control notches 47, which the from P after A controlled volume flow, the inlet flow. Further the main control slide 86 has the second control edge 48 to control the connection from A to R. By doing Main spool 86 is coaxially a pilot spool 87 slidably guided by the main spool 86 after Kind of a hydraulic sequencer works together. To for this purpose the pilot spool 87 has a control edge 88 with which he has a cross bore 89 in the main spool 86 controls. In this way, the spool can 87 influence a control oil flow, which of the Inlet chamber 19 branches off via the transverse bore 89 and Control edge 88 in a longitudinal bore 91 of the pilot spool 87 arrives, from there via a throttle point 92 in one Unlocking piston 93 flows and continues through openings in a screw cap 94 reaches the return chamber 17. The screw cover 94 fastened in the main control slide 86 protrudes with a plunger 95 into the return chamber 17 and lies with its end having a slot 96 on the valve carrier 69 in the seat valve. Inside the plunger is 95 coaxially guided an unlock pin 97, the one hand on the unlocking piston 93 and on the other hand on the pilot cone 71 is present. Through the plunger 95 and the unlocking pin 97 is between the slide valve 62 and the seat valve 61 mechanical operative connection established. The unlocking piston 93 has a larger diameter than the pilot spool 87 and is coaxial to the latter in one Recess of the main control slide 86 slidably longitudinally guided. The recess is through the screw cap 94 shut off, which the unlocking piston 93 additionally as a stop serves. The unlocking piston 93 limits in this way in the recess a space 98 in which the longitudinal bore 91 of the pilot valve 87 opens.

Der von der Drosselstelle 92 in dem Entsperrkolben 93 angestaute Druck wirkt über den hohlen Vorsteuerschieber 87 auch in einer Druckkammer 99, die in der Längsbohrung 65 von der rechten Stirnseite des Hauptsteuerschiebers 68 begrenzt wird. In dieser Druckkammer 99 liegt eine Einstellschraube 101, die mit ihrem Außengewinde 102 in ein entsprechendes Innengewinde der Längsbohrung 65 eingeschraubt ist. Diese Einstellschraube 101 weist an ihrem Außenumfang die Außenverzahnung 39 auf, in welche die Schnecke 41 eingreift und somit den Schneckentrieb 42 bildet. Ein Längsschnitt durch diesen Schneckentrieb 42 ist in Figur 3 dargestellt, die einen Teilschnitt nach III-III in Figur 2 zeigt. Im Innern dieser Einstellschraube 101 ist nun die Regelfeder 103 angeordnet, die sich einerseits an einem freien Ende der Einstellschraube 101 und andererseits an einem bolzenförmigen Ende des Vorsteuerschiebers 87 abstützt, das in die Einstellschraube 101 hineinragt. Zudem liegt an diesem bolzenförmigen Ende die Ankerachse 51 des Proportionalmagneten 15 an. Die Einstellschraube 101 mit dem Schneckentrieb 42 bildet hier die erste Justiereinrichtung 63, die auf diese Weise zwischen dem vorgesteuerten Schieberventil 62 und dem Proportionalmagneten 15 in der Längsbohrung 65 angeordnet ist.The accumulated by the throttle point 92 in the unlocking piston 93 Pressure also acts through the hollow spool 87 in a pressure chamber 99 which in the longitudinal bore 65 of the right end of the main spool 68 limited becomes. An adjusting screw lies in this pressure chamber 99 101, which with its external thread 102 in a corresponding Internal thread of the longitudinal bore 65 is screwed. This Adjusting screw 101 has the external toothing on its outer circumference 39, in which the screw 41 engages and thus forms the worm gear 42. A longitudinal section through this worm drive 42 is shown in Figure 3, the one Partial section according to III-III in Figure 2 shows. At the inside this adjusting screw 101, the control spring 103 is now arranged, the one hand on a free end of the adjusting screw 101 and on the other hand on a bolt-shaped End of the pilot spool 87 supports that in the adjusting screw 101 protrudes. In addition, this is bolt-shaped End of the armature axis 51 of the proportional magnet 15 on. The adjusting screw 101 with the worm gear 42 forms here the first adjustment device 63, which in this way between the pilot operated slide valve 62 and the Proportional magnets 15 arranged in the longitudinal bore 65 is.

Die Wirkungsweise der zweiten Steuereinrichtung 60, die hier als vorgesteuertes 4/2-Magnetventil ausgeführt ist, wird wie folgt erläutert, wobei die Schieberachse durch die vorgesteuerte Bauweise für größere Leistungen verwendbar ist.The operation of the second control device 60, which here is designed as a pilot operated 4/2 solenoid valve, is how follows explained, the slide axis being controlled by the pilot Construction can be used for larger performances.

Es sei angenommen, daß die zweite Steuereinrichtung 60 Teil eines doppelt wirkenden Regelventils ist, wie dies in der eingangs genannten Anmeldung vorgeschlagen wurde oder Teil eines ähnlichen Ventils ist. In diesem Fall liegt bei Nullstellung der zweiten Steuereinrichtung 60 am Zulaufanschluß P immer der Regeldruck einer Druckwaage oder der Standby-Druck einer Regelpumpe an. Die Steuerkante 88 des Vorsteuerschiebers 87 blockiert dabei einen Steuerölstrom, so daß die Druckkammer 99 über den hohlen Vorsteuerschieber 87 und die Drosselstelle 92 im Entsperrkolben 93 zur Rücklaufkammer 17 entlastet ist. Andererseits herrscht in der ersten Motorkammer 16 der im Anschluß B anstehende Lastdruck, der sich über das radiale Spiel des Hauptsteuerkegels 68 auch in dem Ringraum 76 sowie im Druckraum 72 ausbilden kann. Infolge der größeren wirksamen Fläche im Druckraum 72 wird dabei der Hauptsteuerkegel 68 auf seinen Ventilsitz 67 gedrückt, wobei die Druckfeder 73 in die gleiche Richtung wirkt. Das vorgesteuerte Sitzventil 61 sorgt dabei für eine sichere Abdichtung des Motoranschlusses B.It is assumed that the second control device 60 part of a double acting control valve is, as in the or part of the application mentioned in the introduction of a similar valve. In this case it is at zero the second control device 60 at the inlet connection P always the control pressure of a pressure compensator or the Standby pressure of a control pump on. The control edge 88 of the Pilot spool 87 blocks a control oil flow, so that the pressure chamber 99 over the hollow spool 87 and the throttle point 92 in the unlocking piston 93 Return chamber 17 is relieved. On the other hand, there is in the first motor chamber 16 of the line B coming up Load pressure, which affects the radial play of the main control cone 68 also form in the annular space 76 and in the pressure space 72 can. As a result of the larger effective area in the pressure chamber The main control cone 68 becomes 72 on its valve seat 67 pressed, the compression spring 73 in the same Direction works. The pilot operated seat valve 61 ensures this for a secure seal of the motor connection B.

Wird nun der Proportionalmagnet 15 erregt, so übt dessen Ankerachse 51 eine Kraft auf den Vorsteuerschieber 87 aus, wobei die vorgespannte Regelfeder 103 der magnetischen Kraft das Gleichgewicht hält. Der Vorsteuerschieber 87 wird dabei nach links ausgelenkt, wobei seine Steuerkante 88 die Querbohrung 89 aufsteuert, so daß sich ein Steuerölstrom von dem Zulaufanschluß P über den Vorsteuerschieber 87 und die Drosselstelle 92 im Entsperrkolben 93 zum Rücklaufanschluß R aufbauen kann. Die Stauung des Steuerölstroms durch die Drosselstelle 92 erhöht je nach Öffnung der Querbohrung 89 durch den Vorsteuerschieber 87 den Druck stromaufwärts von der Drosselstelle 92 und damit im Raum 98. Dieser aufgestaute Druck gelangt über die Längsbohrung 91 im Vorsteuerschieber 87 auch in die Druckkammer 99, wo er den Hauptschieber 86 auf seiner rechten Stirnseite beaufschlagt. Der Druck im Raum 98 wirkt auf den Entsperrkolben 93 und drückt über den Entsperrstift 97 den Vorsteuerkegel 71 in eine Öffnungsstellung, wenn die Kraft auf den Entsperrkolben 93 die Kraft der Feder 84, die auf den Vorsteuerkegel 71 einwirkt, übersteigt. Öffnet der Vorsteuerkegel 71, so wird der Druckraum 72 über die Durchbrüche 83, den Schlitz 79 und den Ringraum 78 zur Rücklaufkammer 17 entlastet. Damit sinkt der Druck in der Druckkammer 72 und der Hauptsteuerkegel 68 kann nach Art eines entsperrbaren Rückschlagventils durch den Stößel 95 am Hauptsteuerschieber 86 nach links bewegt werden.If the proportional magnet 15 is now excited, its armature axis exercises 51 exerts a force on the pilot spool 87, whereby the prestressed control spring 103 of the magnetic force keeps the balance. The pilot spool 87 is thereby deflected to the left, its control edge 88 the transverse bore 89 controls, so that a control oil flow from the Inlet connection P via the pilot valve 87 and the throttle point 92 in the unlocking piston 93 to the return port R can build up. The stagnation of the control oil flow through the Throttle point 92 increases depending on the opening of the transverse bore 89 through the spool 87 the pressure upstream of the throttle point 92 and thus in the room 98. This pent up Pressure passes through the longitudinal bore 91 in the pilot valve 87 also in the pressure chamber 99, where he the main slide 86 acted on its right face. The pressure in room 98 acts on the unlocking piston 93 and presses the unlocking pin 97 the pilot cone 71 in an open position, when the force on the unlocking piston 93 the force of the spring 84, which acts on the pilot cone 71, exceeds. If the pilot cone 71 opens, the pressure chamber becomes 72 through the openings 83, the slot 79 and the Annulus 78 to the return chamber 17 is relieved. With that the sinks Pressure in the pressure chamber 72 and the main control cone 68 can in the manner of an unlockable check valve by the Tappet 95 on the main control slide 86 can be moved to the left.

Der Druck in der Druckkammer 99 wird von der Drosselstelle 92 im Entsperrkolben 93 und andererseits von dem Öffnungsquerschnitt an der Querbohrung 89 bestimmt, und schiebt zuerst den Entsperrkolben 93 nach links bis zu seinem Anschlag am Schraubdeckel 94. Nach dem Anlegen des Entsperrkolbens 93 wird sich dieser Druck auch in der Druckkammer 99 voll aufbauen und dabei die gesamte Stirnfläche des Hauptsteuerschiebers 86 beaufschlagen. Ist dabei die Kraft, die dadurch auf den Hauptsteuerschieber 86 wirkt, größer als die rückstellende Kraft der Druckfeder 73, so bewegt sich der Hauptsteuerschieber 86 mit dem Hauptsteuerkegel 68 wie ein einstückiges, zusammengehöriges Steuerglied mit all seinen Teilen nach links. Dabei wird durch Aufsteuern oder Zusteuern der Querbohrung 89 die gesamte Ventilachse nach links oder rechts verschoben, d. h. der Hauptsteuerschieber 86 mit dem an seinem Stößel 95 anliegenden Hauptsteuerkegel 68 folgt den Bewegungen des Vorsteuerschiebers 87 nach Art einer hydraulischen Folgesteuerung. Dabei wird nun einerseits der Senkenstrom von B nach R über die Steuerkante 23 mit den Feinsteuerphasen 24 am Hauptsteuerkegel 68 beeinflußt, während der Volumenstrom von P nach A hin zum Stellmotor von den Steuerkanten 46 mit den Feinsteuerkerben 47 in seiner Größe beeinflußt wird. Die Auslenkung des Vorsteuerschiebers 87 wird dabei durch die Kraft des Proportionalmagneten 15 und die Kraft der vorgespannten Regelfeder 103 bestimmt.The pressure in the pressure chamber 99 is from the throttle point 92 in the unlocking piston 93 and on the other hand from the opening cross section determined on the transverse bore 89, and pushes first the unlocking piston 93 to the left until it stops on screw cap 94. After fitting the unlocking piston 93 this pressure will also change in the pressure chamber 99 fully build up and cover the entire face of the main spool Act on 86. Here is the power that thereby acting on the main spool 86, larger than that restoring force of the compression spring 73, the moves Main control spool 86 with the main control cone 68 as one one-piece, related control element with all its Split left. This is done by stepping up or stepping on the transverse bore 89 the entire valve axis to the left or shifted to the right, d. H. the main control slide 86 with the main control cone 68 resting on its tappet 95 follows the movements of the pilot spool 87 in the manner of a hydraulic sequence control. Now, on the one hand the sink current from B to R via the control edge 23 with the Fine control phases 24 on the main control cone 68 are affected while the volume flow from P to A to the servomotor from the control edges 46 with the fine control notches 47 in it Size is affected. The deflection of the spool 87 is thereby by the force of the proportional magnet 15 and the force of the prestressed control spring 103 is determined.

Da sich die Regelfeder 103 an der Einstellschraube 101 abstützt, kann durch Drehen der Schnecke 41 und die damit verbundene axiale Verstellung der Einstellschraube 101 die Vorspannung der Regelfeder 103 verändert werden, so daß die Lage der Durchflußkennlinie Durchfluß Q in Abhängigkeit vom Strom I im Magneten 60 einstellbar ist. Dadurch wird auch die Lage der Steuerkante 46 verändert, so daß insgesamt mit der ersten Justiereinrichtung 63 der Zulaufstrom einstellbar ist. Since the control spring 103 is supported on the adjusting screw 101, can by turning the screw 41 and the associated axial adjustment of the adjusting screw 101 the bias the control spring 103 can be changed so that the location the flow characteristic flow rate Q as a function of Current I in the magnet 60 is adjustable. This will also the position of the control edge 46 changed, so that a total of of the first adjusting device 63, the inlet flow can be adjusted is.

Nach dem Einstellen des Zulaufstroms über das vorgesteuerte Schieberventil 62 kann zusätzlich der Ablaufstrom über das vorgesteuerte Sitzventil 61 mit Hilfe der zweiten Justiereinrichtung 64 eingestellt werden. Zu diesem Zweck ist der Ventilträger 69 des Vorsteuerkegels 71 durch sein Außengewinde 77 axial gegenüber dem Hauptsteuerkegel 68 verstellbar. Gedreht wird der Ventilträger 69 mit einem Spezialwerkzeug, das zum Justieren in den Druckraum 72 axial eingeführt wird und über den Außensechskant 81 greift. An dem Ventilträger 69 stützt sich der Stößel 95 vom Schraubdeckel 94 ab. Das Verdrehen des Ventilträgers 69 hat somit eine Abstandsänderung der beiden Feinsteuerausnehmungen 24 am Hauptsteuerkegel 68 bzw. 47 am Hauptsteuerschieber 86 relativ zueinander zur Folge. Auf diese Weise sind die Überdeckungen an beiden Steuerkanten 23 und 46 für beide Volumenströme justierbar, so daß auch der Ablaufstrom von B nach R einstellbar ist.After setting the feed flow via the pilot operated Slider valve 62 can also drain the current through the pilot operated seat valve 61 with the aid of the second adjusting device 64 can be set. For this purpose the valve carrier 69 of the pilot cone 71 through its external thread 77 axially adjustable relative to the main control cone 68. The valve carrier 69 is rotated with a special tool, the axially inserted for adjustment in the pressure chamber 72 and reaches over the external hex 81. On the valve carrier 69, the plunger 95 is supported on the screw cap 94. The rotation of the valve support 69 thus has a change in distance of the two fine control recesses 24 on the main control cone 68 and 47 on the main control slide 86 relative to each other result. In this way the overlaps are on two control edges 23 and 46 adjustable for both volume flows, so that the drain flow can be adjusted from B to R. is.

Die Figur 4 zeigt einen Längsschnitt durch eine dritte Steuereinrichtung 110, die sich von der zweiten Steuereinrichtung 60 nach Figur 2 wie folgt unterscheidet, wobei für gleiche Bauelemente gleiche Bezugszeichen verwendet werden.FIG. 4 shows a longitudinal section through a third control device 110, which is different from the second control device 60 according to Figure 2 differs as follows, wherein for same components same reference numerals are used.

Die dritte Steuereinrichtung 110 verwendet ein anderes Sitzventil 111 in Verbindung mit einer anderen zweiten Justiereinrichtung 112, wobei das vorgesteuerte Schieberventil 62 mit erster Justiereinrichtung 63 unverändert bleibt. Bei dem vorgesteuerten Sitzventil 111 ist der Vorsteuerkegel 113 unmittelbar im Hauptsteuerkegel 114 gleitend angeordnet, während der Hauptsteuerkegel 114 seinerseits in dem Ventilträger 115 gleitend angeordnet ist. Der Ventilträger 115 ist in einem aufgeweiteten Abschnitt der Längsbohrung 65 drehbar und axial beweglich geführt, wozu er mit einem Außengewinde 116 in ein entsprechendes Innengewinde der Längsbohrung 65 eingeschraubt ist. Ferner ist an dem Ventilträger 115 ein gleichartiger Schneckentrieb 117 ausgebildet, wie ihn bereits die Einstellschraube 101 aufweist. In vergleichbarer Weise wie in der ersten Steuervorrichtung 10 nach Figur 1 ist die erste Motorkammer 16 durch Dichtungen 118 nach beiden Seiten abgesichert. Der Ventilträger 115 weist an seinem der Rücklaufkammer 17 zugewandten Ende einen Ventilsitz 119 für den zugeordneten Hauptsteuerkegel 114 auf, während sein anderes Ende durch einen Deckel 120 verschlossen ist, der den die Druckfeder 73 aufnehmenden Druckraum 72 absperrt. Der Vorsteuerkegel 113 ist in gleicher Weise wie nach Figur 2 in druckausgeglichener Weise ausgeführt und dient in entsprechender Weise zur Vorsteuerung des Hauptsteuerkegels 114.The third control device 110 uses a different seat valve 111 in connection with another second adjustment device 112, the pilot operated slide valve 62 remains unchanged with the first adjusting device 63. In the pilot operated poppet valve 111 is the pilot pilot cone 113 slidingly arranged directly in the main control cone 114, while the main control cone 114 in turn in the Valve carrier 115 is slidably disposed. The valve carrier 115 is in an expanded section of the longitudinal bore 65 rotatably and axially movable, for which he with a External thread 116 in a corresponding internal thread Longitudinal bore 65 is screwed. Furthermore, is on the valve support 115 a similar worm drive 117 is formed, as it already has the adjusting screw 101. Comparable Way as in the first control device 10 according to Figure 1, the first motor chamber 16 by seals 118 secured on both sides. The valve carrier 115 has one at its end facing the return chamber 17 Valve seat 119 for the associated main control cone 114 while its other end is closed by a lid 120 which is the pressure chamber accommodating the compression spring 73 72 cordoned off. The pilot cone 113 is the same Way as carried out according to Figure 2 in a pressure-balanced manner and serves in a corresponding manner for pilot control of the Main control cone 114.

Bei der dritten Steuereinrichtung 110 wird der Zulaufstrom von P nach A in gleicher Weise über die erste Justiereinrichtung 63 eingestellt, während zum Einstellen des Ablaufstroms von B nach R die zweite Justiereinrichtung 112 dient. Mit Hilfe des Schneckentriebs 117 läßt sich der Ventilträger 115 in der Längsbohrung 65 axial verstellen, wodurch seine wirksame Steuerkante in der Steueröffnung 121 relativ zur gehäusefesten Steuerkante im Schieberventil in ihrer Lage verändert wird. Dadurch kann in entsprechender Weise wie bei der zweiten Steuereinrichtung 60 nach Figur 2 auch der Ablaufstrom von B nach R justiert bzw. eingestellt werden.In the third control device 110, the inlet flow from P to A in the same way via the first adjustment device 63 set while setting the drain current from B to R the second adjustment device 112 is used. With the help of the worm gear 117, the valve carrier can be 115 adjust axially in the longitudinal bore 65, whereby its effective control edge in the control opening 121 relative to the control edge fixed to the housing in the slide valve in its position is changed. This can be done in a corresponding manner in the second control device 60 according to FIG. 2 also the Drain current from B to R can be adjusted or set.

Die Figur 5 zeigt einen Längsschnitt durch eine vierte Steuereinrichtung 130, die sich von der dritten Steuereinrichtung 110 nach Figur 4 wie folgt unterscheidet, wobei für gleiche Bauelemente gleiche Bezugszeichen verwendet werden. Die vierte Steuereinrichtung 130 verwendet ein anderes Sitzventil 131 sowie ein nur wenig geändertes Schieberventil 132, wobei deren Steuerglieder selbst nach Art einer hydraulischen Folgesteuerung zusammenarbeiten, so daß der Hauptsteuerkegel 133 im Sitzventil nicht mehr mechanisch vom Hauptsteuerschieber 134 betätigt wird, sondern hydraulisch.FIG. 5 shows a longitudinal section through a fourth control device 130, which is different from the third control device 110 as shown in Figure 4, where for same components same reference numerals are used. The fourth control device 130 uses a different seat valve 131 and a little modified slide valve 132, the control members themselves in the manner of a hydraulic Sequence control work together so that the Main control cone 133 in the seat valve no longer mechanically from Main spool 134 is operated, but hydraulically.

Der Aufbau des Gehäuses 66 mit den vier Arbeitskammern 16 bis 19, der prinzipielle Aufbau des Hauptsteuerschiebers 134 mit seiner Steuerkante 46 und den Feinsteuerkerben 47, der Vorsteuerschieber 87 sowie die Einstellschraube 101 mit der ersten Justiereinrichtung 63 sind im wesentlichen gleich wie bei der dritten Steuereinrichtung 110 nach Figur 4. Im Hauptsteuerschieber 134 ist jedoch anstelle des Schraubdekkels 94 nun ein Stößel 135 mit einem tellerförmigen Ansatz 136 gehalten. Der tellerförmige Ansatz 136 wird dabei von einer sich gehäusefest abstützenden Rückstellfeder 140 belastet und dadurch gegen die linke Stirnseite des Hauptsteuerschiebers 134 gedrückt, wobei der Ansatz 136 an seinem Außenumfang im Hauptsteuerschieber 134 zentriert ist. Die für den Steuerölstrom vorgesehene Drosselstelle 92 ist nun im tellerförmigen Ansatz 92 angeordnet, da ein gesonderter Entsperrkolben 93 im Hauptsteuerschieber 134 entfällt.The structure of the housing 66 with the four working chambers 16 to 19, the basic structure of the main control spool 134 with its control edge 46 and the fine control notches 47, the Pilot valve 87 and the adjusting screw 101 with the first adjustment device 63 are essentially the same as in the third control device 110 according to FIG. 4. In the Main spool 134 is instead of the screw cap 94 now a plunger 135 with a plate-shaped extension 136 held. The plate-shaped projection 136 is thereby by a return spring 140 which is supported fixed to the housing loaded and thus against the left face of the main spool 134 pressed, the lug 136 on its Outer circumference is centered in the main control slide 134. The throttle point 92 provided for the control oil flow is now arranged in the plate-shaped neck 92, since a separate Unlocking piston 93 in the main control slide 134 is omitted.

Das vorgesteuerte Sitzventil 131 ist wie bei der dritten Steuereinrichtung 110 nach Figur 4 im Innern eines Ventilträgers 137 angeordnet, der seinerseits in dem abgesetzten Abschnitt der Längsbohrung 65 gelagert ist. Der Ventilträger 137 weist an seiner Mantelfläche das Außengewinde 116 auf, mit dem er in ein passendes Innengewinde der Längsbohrung 65 eingeschraubt ist und somit axial verstellbar ist. Auf einen Schneckentrieb 117 wird bei dem Ventilträger 137 verzichtet, der in seiner Lage durch eine Kontermutter 138 gesichert ist.The pilot operated seat valve 131 is like the third Control device 110 according to Figure 4 inside a valve carrier 137 arranged, which in turn in the remote Section of the longitudinal bore 65 is mounted. The valve carrier 137 has the external thread 116 on its outer surface with which it fits into a suitable internal thread of the longitudinal bore 65 is screwed in and is therefore axially adjustable. On a worm gear 117, the valve carrier 137 dispenses with the position of a lock nut 138 is secured.

Der im Ventilträger 137 angeordnete Hauptsteuerkegel 133 ist hier als Differenzflächenventil ausgebildet, bei dem eine durch Sitzkante und durch Ventilschaft gebildetet Ringfläche 139 von dem in der ersten Motorkammer 16 herrschenden Druck in Öffnungsrichtung beaufschlagt wird. Die den Hauptsteuerkegel 133 in Schließrichtung belastende Druckfeder 73 liegt in dem Druckraum 72, der über eine im Ventilschaft angeordnete Drossel 141 mit der ersten Motorkammer 16 in Verbindung steht. Der Hauptsteuerkegel 133 weist wie bisher die Hauptsteuerkante 23 und die Feinsteuernuten 24 zur Steuerung des Ablaufstromes auf, wobei sie nun im Ablaufstrom dem eigentlichen Kegel nachgeschaltet sind. Der im Hauptsteuerkegel 133 angeordnete Vorsteuerkegel ist hier als Kugel 142 ausgebildet, die zwischen zwei Ventilsitzen im Hauptsteuerkegel 133 angeordnet ist und mit einem verjüngten Fortsatz 143 des Stößels 135 in Wirkverbindung steht, wie er für die hydraulische Folgesteuerung erforderlich ist.The main control cone 133 arranged in the valve carrier 137 is here designed as a differential area valve, in which a ring surface formed by seat edge and valve stem 139 of the one prevailing in the first motor chamber 16 Pressure is applied in the opening direction. The main tax cone 133 compression spring 73 loading in the closing direction lies in the pressure chamber 72, which is arranged in the valve stem Throttle 141 in connection with the first motor chamber 16 stands. The main control cone 133 has as before Main control edge 23 and the fine control grooves 24 for control of the drain stream, whereby it is the actual one in the drain stream Cones are connected downstream. The pilot cone arranged in the main control cone 133 is here designed as a ball 142, which sits between two valve seats is arranged in the main control cone 133 and with a tapered extension 143 of the plunger 135 in operative connection stands as it is required for the hydraulic sequence control is.

Der Ventilträger 137 ist um seine Längsachse verdrehbar und erfährt dabei infolge des Außengewindes 116 eine axiale Verstellung, so daß er ein Teil der zweiten Justiereinrichtung 144 darstellt.The valve carrier 137 is rotatable about its longitudinal axis and undergoes an axial adjustment as a result of the external thread 116, so that it is part of the second adjustment device 144 represents.

Die Wirkungsweise der vierten Steuereinrichtung 130 gleicht insofern derjenigen der dritten Steuereinrichtung 110 nach Figur 4, als der Hauptsteuerschieber 134 mit dem Vorsteuerschieber 87 nach Art einer hydraulischen Folgeregelung zusammenarbeitet, um den Zulaufstrom von P nach A zu steuern. Der von der Drosselstelle 92 im Steuerölstrom mit beeinflußte Staudruck, der auch in der Steuerkammer 99 auf die rechte Stirnseite des Hauptsteuerschiebers 134 wirkt, verschiebt nun diesen - im Unterschied zur dritten Steuereinrichtung 110 - im wesentlichen gegen die Rückstellfeder 140, die sich über den Ventilträger 137 gehäusefest abstützt. Darüberhinaus dient der mit dem Hauptsteuerschieber 134 gekoppelte Stößel 135 für eine zusätzliche hydraulische Folgesteuerung des Sitzventils 131. Zu diesem Zweck wird am The operation of the fourth control device 130 is the same to that extent that of the third control device 110 Figure 4, as the main spool 134 with the spool 87 works in the manner of a hydraulic follow-up control, to control the feed flow from P to A. The influenced by the throttle point 92 in the control oil flow Back pressure, which is also in the control chamber 99 on the right Front of the main control spool 134 acts, shifts now this - in contrast to the third control device 110 - essentially against the return spring 140, the is supported on the valve carrier 137 fixed to the housing. Furthermore serves the coupled with the main spool 134 Tappet 135 for additional hydraulic sequence control of the seat valve 131. For this purpose, on

Hauptsteuerkegel 133 die öffnende Kraft durch den Druck der Last in der ersten Motorkammer 16 auf die Ringfläche 139 ausgeübt, während die schließende Kraft auf den Hauptsteuerkegel 133 von dem Druck in dem Druckraum 72 auf die gesamte wirksame Fläche des Hauptsteuerkegels 133 hervorgerufen wird. Die Kugel 142 im Hauptsteuerkegel 133 ist ein Teil von dessen Vorsteuerventil. Hebt der Stößel 135 über seinen Fortsatz 143 die Kugel 142 von ihrem Sitz ab, so öffnet das Vorsteuerventil und entlastet den Druckraum 72 zur Rücklaufkammer 17. Das einerseits über die Drossel 141 in den Druckraum 72 zufließende Öl und das andererseits über das Kugelventil aus dem Druckraum 72 zur Rücklaufkammer 17 abströmende Öl bestimmen den Druck im Druckraum 72, der auf die linke Stirnseite des Hauptsteuerkegels 133 wirkt und damit auch dessen Bewegungsrichtung. Der Hauptsteuerkegel 133 wird somit hydraulisch gegen die Kraft der Feder 73 verstellt, wobei er mit seiner Lage der Stellung des Stößels 135 folgt, so daß auch das Sitzventil 131 hier eine Folgesteuerung aufweist, die ihre Energie aus dem Lastdruck des ersten Motoranschlusses 16 bezieht. Die vierte Steuereinrichtung 130 eignet sich daher für große Leistungen.Main control cone 133 the opening force by the pressure of the Load in the first motor chamber 16 on the ring surface 139 exerted while the closing force on the main control cone 133 from the pressure in the pressure chamber 72 to the whole effective area of the main control cone 133 becomes. Ball 142 in main control cone 133 is part of its pilot valve. Raise the plunger 135 over his Extension 143 the ball 142 from its seat, so that opens Pilot valve and relieves pressure chamber 72 to the return chamber 17. The one hand via the throttle 141 in the pressure chamber 72 inflowing oil and the other through the ball valve flowing out of the pressure chamber 72 to the return chamber 17 Oil determine the pressure in the pressure chamber 72 that on the left Front of the main control cone 133 acts and thus its direction of movement. The main control cone 133 is thus hydraulically adjusted against the force of the spring 73, wherein it follows the position of the plunger 135 with its position, so that the seat valve 131 also has a sequence control here, which derive their energy from the load pressure of the first motor connection 16 relates. The fourth controller 130 is therefore suitable for great performances.

Während der Zulaufstrom von P nach A wie bisher über die erste Justiereinrichtung 63 einstellbar ist, läßt sich der Ablaufstrom von B nach R über die zweite Justiereinrichtung 144 einstellen. Eine Drehbewegung des Ventilträgers 137 wird über das Außengewinde 116 in eine axiale Verstellung umgewandelt, wodurch die Lage der Steuerkante 23 relativ zur Lage des Hauptsteuerschiebers 134 verändert wird, so daß auch der Ablaufstrom justiert werden kann.While the feed flow from P to A continues as before via the first Adjustment device 63 is adjustable, the drain current from B to R via the second adjustment device Set 144. A rotational movement of the valve carrier 137 is in an axial adjustment via the external thread 116 converted, whereby the position of the control edge 23 relative to Position of the main control spool 134 is changed so that the drain current can also be adjusted.

Die Figur 6 zeigt einen Längsschnitt durch eine fünfte Steuervorrichtung 150, die sich von der zweiten Steuereinrichtung 60 nach Figur 2 wie folgt unterscheidet, wobei für gleiche Bauelemente gleiche Bezugszeichen verwendet werden. FIG. 6 shows a longitudinal section through a fifth control device 150, which is different from the second control device 60 according to Figure 2 differs as follows, wherein for same components same reference numerals are used.

Die fünfte Steuereinrichtung 150 verwendet einen anderen Hauptsteuerschieber 151, bei dem der Stößel 95 mit dem eigentlichen Hauptsteuerschieber einstückig ausgeführt ist. In seinem Innern weist der Hauptsteuerschieber 151 eine zur Einstellschraube 101 hin offene Sacklochbohrung 152 auf, in welcher der Vorsteuerschieber 87 sowie der Entsperrkolben 93 hintereinander gleitend geführt sind. Die Sacklochbohrung 152 ist durchgehend mit gleichem Durchmesser ausgeführt, so daß der Entsperrkolben 93 und der Vorsteuerschieber 87 gleiche Außendurchmesser aufweisen. Das Schieberventil 62 in der fünften Steuervorrichtung 150 kommt daher mit weniger Bauteilen aus und läßt sich einfacher und kostengünstiger herstellen. Die Justiereinrichtungen 63 und 64 können dabei unverändert beibehalten werden. Im übrigen ist die Wirkungsweise der fünften Steuervorrichtung 115 wie diejenige der zweiten Steuervorrichtung 60.The fifth controller 150 uses another one Main control slide 151, in which the plunger 95 with the actual Main control slide is made in one piece. In the inside of the main control slide 151 has one Adjustment screw 101 open blind hole 152, in which of the pilot spool 87 and the unlocking piston 93 are slid in a row. The blind hole 152 is of the same diameter throughout, so that the unlocking piston 93 and the spool 87 have the same outside diameter. The slide valve 62 in the fifth control device 150 therefore comes along fewer components and is easier and cheaper produce. The adjustment devices 63 and 64 can remain unchanged. Otherwise, the Operation of the fifth controller 115 like that the second control device 60.

Selbstverständlich sind an den gezeigten Ausführungsformen Änderungen möglich, ohne Von den Merkmalen der Erfindung, wie im Anspruch 1 definiert, abzuweichen. Dabei wird davon ausgegangen, daß auch bei einer hydraulischen Folgesteuerung eine mechanische Wirkverbindung zwischen vorsteuerndem und gesteuertem Ventilglied vorliegt.Of course, the embodiments shown are Changes possible without any of the features of the invention, as defined in claim 1. It is assumed that even with a hydraulic Sequence control a mechanical operative connection between pilot and controlled valve member.

Claims (27)

  1. Electrohydraulic control device for controlling the volume flows for a hydraulic servomotor as a function of electrical input signals at the proportional magnet, with valve means which perform a 4/2-way function and which have a releasable seat valve (11; 61; 111; 131) for controlling the volume flow flowing out from the servomotor and a slide valve (12; 62; 132) for controlling the inflowing volume flow, the control members of the seat valve and slide valve being arranged one behind the other in a longitudinal bore of a housing, so that the slide valve (12; 62; 132) is located between the seat valve (11; 61; 111; 131) and the proportional magnet (15), and in which, in the housing (14), a first motor chamber (16) and a return chamber (17) are assigned to the outflow, whilst a second motor chamber (18) and an inflow chamber (19) are assigned to the inflow, the return chamber (17) being located between the two motor chambers (16, 18) and the inflow chamber (19) being located outside the two motor chambers (16, 18), and with a first adjusting arrangement (33; 42; 101), in which one of the volume flows can be set by a change in the prestress of a regulating spring (31, 103), characterized in that the seat valve (11; 61; 111; 131) and the slide valve (12, 62; 132) have control members (22, 45; 68, 71; 86, 87; 114, 113; 133, 142, 134; 151) which are separate from one another and are operatively connected to one another mechanically, and in that a second adjusting arrangement (53; 64; 112; 144) is provided, by means of which the other volume flow can be set.
  2. Electrohydraulic control device according to Claim 1, characterized in that, by means of the first adjusting arrangement (52; 63), the position of the throughflow characteristic of volume flow as a function of the electrical input signal at the proportional magnet (15) can be set at one of the control edges (23, 46), whilst, by means of the second adjusting arrangement (53; 64; 112; 144), the position of the effective control edges (23, 46) on the seat valve (11; 61; 111; 131) and on the slide valve (12; 62; 132) relative to one another can be adjusted.
  3. Electrohydraulic control device according to Claim 1 or 2, characterized in that the seat valve (11) and the slide valve (12) which provide the 4/2-way function are designed as directly controlled valves, and the seat valve (11) has a sleeve-shaped valve carrier (21) which receives inside it a valve cone (22) and on which the two adjusting arrangements (52, 53) are arranged.
  4. Electrohydraulic control device according to Claim 3, characterized in that the first adjusting arrangement (52) has a setscrew (33) which is arranged coaxially in the valve carrier (21) and on which the regulating spring (31) acting on the valve cone (22) is supported.
  5. Electrohydraulic control device according to Claim 3 or 4, characterized in that the second adjusting arrangement (53) has a worm drive (42), in which an external toothing (39) on the valve carrier (21) has engaging into it a worm (41) mounted transversely thereto in the housing (14), and in that the valve carrier (21) is screwed via a thread (37) into the longitudinal bore (13).
  6. Electrohydraulic control device according to one of Claims 3 to 5, characterized in that the valve carrier (21) has, at its end located opposite the first adjusting arrangement (52), a valve seat (32) which is assigned to the valve cone (22).
  7. Electrohydraulic control device according to one of Claims 3 to 6, characterized in that the valve cone (22) is coupled mechanically to a longitudinal slide (45) of the slide valve (12) via an actuating member (44) fastened, in particular, to the valve cone.
  8. Electrohydraulic control device according to one of Claims 3 to 7, characterized in that the valve cone (22) is designed to be pressure-compensated with respect to the pressures in the first motor chamber (16) and in the return chamber (17), and the longitudinal slide (45) is pressure-compensated with respect to the pressures in the second motor chamber (18) and in the inflow chamber (19).
  9. Electrohydraulic control device according to one or more of Claims 3 to 8, characterized in that the valve cone (22) and the longitudinal slide (45) each have a control edge (23, 46) inserted into the outflow (B-R) and the inflow (P-A) respectively and with fine control recesses (24, 47).
  10. Electrohydraulic control device according to Claim 1 or 2, characterized in that the seat valve (61; 111; 131) and the slide valve (62; 132) which form the 4/2-way function are in each case designed as pilot-controlled valves which are operatively connected to one another.
  11. Electrohydraulic control device according to Claim 10, characterized in that the first adjusting arrangement (63) is arranged between the slide valve (62, 132) and the proportional magnet (15) in the longitudinal bore (65), whilst the second adjusting arrangement (64; 112; 144) is assigned to the seat valve (61; 111; 131).
  12. Electrohydraulic control device according to Claim 11, characterized in that the first adjusting arrangement (63) has a setting screw (101) which is screwed with its external thread (102) into an internal thread of the longitudinal bore (65), so that said setting screw is arranged axially adjustably between a main control slide (86; 134; 151) of the slide valve (62, 132) and the proportional magnet (15), in that the setting screw (101) has an external toothing (39), into which a worm (41) mounted transversely thereto in the housing (66) engages in the manner of a worm drive (42), and in that the regulating spring (103) is supported between the setting screw (101) and a pilot-control slide (87) which co-operates with the main control slide (86; 134; 151) in the manner of a hydraulic follow-up control.
  13. Electrohydraulic control device according to one of Claims 10 to 12, characterized in that the second adjusting arrangement (64) has a sleeve-shaped valve carrier (69) which receives inside it a pilot-control cone (71) which pilot-controls a main control cone (68) and which is arranged axially adjustably in the main control cone and is operatively connected to a tappet (95) of the main control slide (86) in the slide valve (62).
  14. Electrohydraulic control device according to Claim 13, characterized in that the valve carrier (69) is screwed in the axial direction with an external thread (77) into an internal thread of the hollow main control cone (68) and has an outer key surface (61), by means of which said valve carrier is secured fixedly in terms of rotation in the main control cone (68) via an axially installable retaining ring (75).
  15. Electrohydraulic control device according to Claim 14, characterized in that a compression spring (73) loading the main control cone (68) is supported on the main control cone (68) via the retaining ring (75).
  16. Electrohydraulic control device according to one of Claims 10 to 12, characterized in that the second adjusting arrangement (112; 144) has a sleeve-shaped valve carrier (115; 137) which receives the valve seat (119) and which is arranged axially adjustably in a stepped part of the longitudinal bore (65) and which receives inside it the main control cone (114; 133) together with the pilot-control cone (113; 142) arranged in the latter.
  17. Electrohydraulic control device according to Claim 16, characterized in that the valve carrier (115) is screwed with an external thread (116) into an internal thread of the longitudinal bore (65) and has an external toothing, into which a worm mounted transversely thereto in the housing (66) engages in the manner of a worn drive (117), and in that the main control cone (114) is operatively connected to a tappet (95) of the main control slide (86).
  18. Electrohydraulic control device according to Claim 16 or 17, characterized in that the valve carrier (115; 137) receives the compression spring (73) loading the main control cone (114; 133), in a pressure space (72) which is closed relatively outside, in particular, by means of a cover (120) arranged in the valve carrier.
  19. Electrohydraulic control device according to one of Claims 13 to 18, characterized in that the pilot-control cone (71; 113) pilot-controlling the main control cone (68; 114) is designed to be pressure-compensated on all sides, and in that said pilot-control cone is inserted into the hydraulic connection from a pressure space (72) assigned to the main control cone (68, 114) to the return chamber (17) and is operatively connected to a release pin (97) which is mounted slideably in a tappet (95) of the main control slide (86).
  20. Electrohydraulic control device according to one of Claims 13 to 19, characterized in that the main control slide (86) has arranged in it coaxially to the pilot-control slide (87) a hydraulically actuable release piston (93), the associated throttle point (92) of which is inserted into a control-oil flow serving for the follow-up control and carried by the inflow chamber (18) to the return chamber (17), said release piston (93) being operatively connected to the release pin (97).
  21. Electrohydraulic control device according to one of Claims 13 to 20, characterized in that the main control slide (86; 134; 151) and the main control cone (68; 114; 133) each have a control edge (23, 46) inserted into the inflow and the outflow respectively and with fine control recesses (24, 47).
  22. Electrohydraulic control device according to one of Claims 10 to 12, characterized in that the second adjusting arrangement (144) has a sleeve-shaped valve carrier (137) without external toothing, which is screwed axially adjustably in a stepped part of the longitudinal bore (65) by means of an external thread (116) and which receives inside it the main control cone (133) and the pilot-control member (142) arranged in the latter, the main control cone (133) delimiting in the valve carrier (137) a pressure space (72) receiving the compression spring (73), and in that the valve carrier (137) is capable of being locked in its rotary position on the housing (66) by means of a retaining element (138).
  23. Electrohydraulic control device according to Claim 22, characterized in that the main control cone (133) is designed as a differential-area valve and the pilot-control cone as a spherical closing member (42), which, together with the tappet (135) operatively connected to the main control slide (134), form a follow-up control, and in that the main control slide (134) is supported at its non-pressure-loaded end fixedly relatively to the housing via a restoring spring (140).
  24. Electrohydraulic control device according to Claim 23, characterized in that the tappet (135) is guided in the main control slide (134) via a dish-shaped extension (136) and is held in bearing contact on the latter by the restoring spring (140), and in that a throttle point (92) is arranged, in particular, in the extension (136).
  25. Electrohydraulic control device according to one of Claims 10 to 12 and 16 to 21, characterized in that the valve carrier (21; 115; 137) passes through the first motor chamber (16) and is sealed off on the outside in the longitudinal bore (13, 65) on the first motor chamber (16) on both sides by means of sealing rings (43; 118).
  26. Electrohydraulic control device according to one of Claims 13 to 15, characterized in that the main control cone (68) and the main control slide (86) are slideably guided directly in the longitudinal bore (65), in which a valve seat (67) for the main control cone (68) is arranged between the first motor chamber (16) and the return chamber (17).
  27. Electrohydraulic control device according to one or more of Claims 10 to 26, characterized in that the main control slide (151) is designed in one piece with the tappet (95), and in that the pilot-control slide (87) and blocking piston (93), which are guided slideably in said main control slide and are arranged one behind the other, have the same outside diameter and are guided in the same bore (152).
EP97118001A 1996-12-02 1997-10-17 Electrohydraulic control device Expired - Lifetime EP0845602B1 (en)

Applications Claiming Priority (2)

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DE19649833 1996-12-02
DE19649833A DE19649833A1 (en) 1996-12-02 1996-12-02 Electro-hydraulic control device

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EP0845602A2 EP0845602A2 (en) 1998-06-03
EP0845602A3 EP0845602A3 (en) 1998-07-15
EP0845602B1 true EP0845602B1 (en) 2001-12-19

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EP1492951A1 (en) 2002-04-11 2005-01-05 Siemens Aktiengesellschaft Injection device for internal combustion engines comprising a control valve and a valve for controlling the supply of fuel to an injection device
DE102005013611B4 (en) * 2005-03-24 2008-09-25 Bosch Rexroth Ag Peumatic valve with means for actuating at least one central valve seat
US20200326012A1 (en) * 2016-05-30 2020-10-15 Hema Endustri Anomin Sirketi An electrohydraulic valve with adjustable performance
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CN102213242A (en) * 2011-07-19 2011-10-12 宁波克泰液压有限公司 Thread plug-in type electronic control hydraulic lock
CN102213242B (en) * 2011-07-19 2013-12-11 宁波克泰液压有限公司 Thread plug-in type electronic control hydraulic lock

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DE19649833A1 (en) 1998-06-04
EP0845602A3 (en) 1998-07-15
EP0845602A2 (en) 1998-06-03
DE59705881D1 (en) 2002-01-31

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