Nothing Special   »   [go: up one dir, main page]

EP0585609B1 - Hydrostatic machine with axial thrust balancing - Google Patents

Hydrostatic machine with axial thrust balancing Download PDF

Info

Publication number
EP0585609B1
EP0585609B1 EP93112131A EP93112131A EP0585609B1 EP 0585609 B1 EP0585609 B1 EP 0585609B1 EP 93112131 A EP93112131 A EP 93112131A EP 93112131 A EP93112131 A EP 93112131A EP 0585609 B1 EP0585609 B1 EP 0585609B1
Authority
EP
European Patent Office
Prior art keywords
rotors
shaft
bores
channels
hydrostatic machine
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
EP93112131A
Other languages
German (de)
French (fr)
Other versions
EP0585609A1 (en
Inventor
Gerhard Fähnle
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JM Voith GmbH
Original Assignee
JM Voith GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by JM Voith GmbH filed Critical JM Voith GmbH
Publication of EP0585609A1 publication Critical patent/EP0585609A1/en
Application granted granted Critical
Publication of EP0585609B1 publication Critical patent/EP0585609B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B33/00Engines characterised by provision of pumps for charging or scavenging
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B1/00Multi-cylinder machines or pumps characterised by number or arrangement of cylinders
    • F04B1/04Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
    • F04B1/10Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement the cylinders being movable, e.g. rotary
    • F04B1/107Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement the cylinders being movable, e.g. rotary with actuating or actuated elements at the outer ends of the cylinders
    • F04B1/1071Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement the cylinders being movable, e.g. rotary with actuating or actuated elements at the outer ends of the cylinders with rotary cylinder blocks
    • F04B1/1074Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement the cylinders being movable, e.g. rotary with actuating or actuated elements at the outer ends of the cylinders with rotary cylinder blocks with two or more serially arranged radial piston-cylinder units

Definitions

  • the present invention relates to a hydrostatic machine according to the preamble of claim 1.
  • a single-flow so-called side-loaded hydrostatic machine is known from DE-OS 39 05 936. Measures and means are provided to absorb or compensate for the axial thrust forces acting on the cylinder star (rotor) via the (drive) shaft.
  • the axial forces are disadvantageously large and that the pulsating radial forces flow back over the outer surface of the machine to the bearing points, with undesirable loud noises being produced.
  • Another problem is that the bearing points of the central shaft of the previously mentioned machine have to be aligned very precisely, which necessitates an increased production outlay.
  • the object on which the present invention is based is to provide a hydrostatic machine of the generic type in which no pulsating forces arising from the hydrostatic load have to be conducted over the outer surfaces of the machine and in which the alignment of the housing cover, which is technically complex to produce, is superfluous .
  • the radial piston machine representing the hydrostatic machine has a housing 1 with two interior spaces 6, 7 separated by an intermediate floor 5.
  • the interiors 6, 7 are closed from both sides via a housing cover 3.
  • a cam ring 8, 9 is mounted, which both are connected to one another via at least one connecting shaft 11 and via a bearing shaft 10 and to the intermediate floor 5 via bearings 36.
  • the displacement elements serving the function or use as a hydrostatic machine or as a radial piston machine, which consist of the functional connection of a sliding block or sliding block 14 and an articulated (displacement) block Piston 15 exist.
  • These pistons 15 are each arranged in radial bores 16, 17 of one of the rotors 18, 19 forming the cylindrical star, which in turn are coupled in a rotationally fixed and axially fixed manner to a shaft 20 driven by a drive connector 26 mounted in a bearing 4.
  • the configuration described above corresponds - apart from the fact that nothing has been said about the flow rate or the pumping function - to the state of the art insofar as the rotors 18, 19 are known per se.
  • the special configuration consists in the fact that the hydrostatic machine does not start from one rotor 18, 19, but from two, which act synchronously with one another as a motor or pump unit (which ultimately achieves twice the delivery capacity with radially identical dimensions) and that Drive shaft is mounted between the rotors 18, 19 in connection with the cam ring bearing located in the intermediate floor 5 between the cam rings 8, 9.
  • the two rotors 18, 19 are coupled or functionally connected to one another in a coordinated manner as follows:
  • axial lateral control slots face one another 21, 22 are provided, through which the bores 16, 17 are open to the intermediate floor 5.
  • These control slots 21, 22 in turn correspond to kidney-shaped channels 23, 24 incorporated in control disks (axial disks) 25, 26 (cf. FIG. 4).
  • the control disks 25, 26 are inserted in corresponding recesses on both sides of the intermediate base 5.
  • transverse connecting channels 27, 28 are incorporated so that both rotors 18, 19 are connected to one another via their displacement elements - and together as a pump or hydrostatic machine able to work; this creates a double-flow hydrostatic machine or radial piston machine, the connecting channels 27, 28 forming the inlet and outlet channels and accordingly being open to the outside.
  • the two cam rings 8, 9 are positioned together via an adjusting device consisting of an adjusting piston 31 and a counter-piston 32.
  • This adjustment device is mounted or attached to the intermediate floor 5 and is effective.
  • the connecting channels 27, 28, i.e. the inlet-side low-pressure duct and the outlet-side high-pressure duct are incorporated.
  • the rotors 18, 19 are fixed in a rotationally fixed and axially fixed manner on the shaft 20. As shown, both rotors can be removed from the shaft 20 (see clamping nut 37); the shaft 20 is driven via a coupling sleeve 40 from the drive socket 2.
  • a collar 33, 34 is provided on the shaft 20 for each rotor 18, 19.
  • the rotors 18, 19 are pressed against these collars 33 and 34 by means of clamping elements 37.
  • the distance between the bundles 33, 34 is slightly larger than the sum of the thickness of the intermediate floor 5 and the thickness of the control discs 25, 26.
  • the rotors 18, 19 can also be fixed on the shaft 20 in such a way that one rotor is formed in one piece with the shaft 20, while the second rotor is fixed via a clamping nut.
  • the axial fixation of the two rotors 18, 19 on the shaft 20 ensures that the axial forces do not have to be supported on the housing covers 3.
  • the mounting of the drive shaft 20 via bearings 35 in the intermediate floor 5, as well as the mounting of the lifting rings 8, 9 in the same intermediate floor 5 enable the frictional connections A, B and C, all of which have an effect inside the machine.
  • the gap required for the rotors 18, 19 to run reliably relative to the control disks (axial disks) 25, 26 should be kept as small as possible because of the tightness which depends on them.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Reciprocating Pumps (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
  • Hydraulic Motors (AREA)
  • Control Of Non-Positive-Displacement Pumps (AREA)
  • Hydraulic Turbines (AREA)
  • Gripping On Spindles (AREA)

Abstract

The invention relates to a hydrostatic machine with a cylinder assembly which is arranged on the shaft and has radial bores with displacer elements (piston and sliding block) sliding on the inside of a cam ring, the bores being connected to delivery passages. The invention is characterised in that the radial cylinder assembly comprises two rotors mounted a distance apart, the bores of which have intercommunicating timing ports, in that an intermediate casing wall is provided between the two rotors, this wall having control discs with passages and connecting passages for the respectively associated passages, and in that the cam rings of the two rotors are rigidly connected to one another by a bearing shaft and the shaft and the bearing shaft are each supported by a bearing in the intermediate wall. <IMAGE>

Description

Die vorliegende Erfindung betrifft eine hydrostatische Maschine nach dem Oberbegriff des Patentanspruchs 1.The present invention relates to a hydrostatic machine according to the preamble of claim 1.

Eine derartige Maschine ist aus US-A-3 044 412 bekanntgeworden. Die beiden Rotoren jener Maschine sind als Doppelrotoren ausgebildet. Auf der Rotorwelle befindet sich zwischen den beiden Rotoren ein mit der Welle drehfester Flansch.Such a machine has become known from US-A-3 044 412. The two rotors of that machine are designed as double rotors. On the rotor shaft there is a flange that is fixed to the shaft between the two rotors.

Bei dieser Maschine besteht die Gefahr, daß aus der hydrostatischen Belastung pulsierende Kräfte entstehen, die über die Außenflächen der Maschine geführt werden müssen.With this machine there is a risk that pulsating forces arise from the hydrostatic load which have to be guided over the outer surfaces of the machine.

Eine einflutige sogenannte seitenbeaufschlagte hydrostatische Maschine ist aus der DE-OS 39 05 936 bekannt. Dabei sind Maßnahmen und Mittel vorgesehen, um die auf den Zylinderstern (Rotor) einwirkenden axialen Schubkräfte über die (Antriebs-) Welle aufzunehmen beziehungsweise zu kompensieren. Es hat sich jedoch gezeigt, daß die axialen Kräfte dabei ungünstig groß sind und daß die pulsierenden radialen Kräfte über die Außenfläche der Maschine zu den Lagerstellen zurückfließen, wobei unerwünschte laute Geräusche entstehen. Ein weiterer Problempunkt ist, daß die Lagerstellen der Zentralwelle der zuvor erwähnten Maschine sehr genau fluchten müssen, was einen erhöhten Fertigungsaufwand erforderlich macht.A single-flow so-called side-loaded hydrostatic machine is known from DE-OS 39 05 936. Measures and means are provided to absorb or compensate for the axial thrust forces acting on the cylinder star (rotor) via the (drive) shaft. However, it has been shown that the axial forces are disadvantageously large and that the pulsating radial forces flow back over the outer surface of the machine to the bearing points, with undesirable loud noises being produced. Another problem is that the bearing points of the central shaft of the previously mentioned machine have to be aligned very precisely, which necessitates an increased production outlay.

Die der vorliegenden Erfindung zugrunde liegende Aufgabe besteht darin, eine hydrostatische Maschine der gattungsgemäßen Art anzugeben, bei der keine pulsierenden, aus der hydrostatischen Belastung entstehenden Kräfte über die Außenflächen der Maschine geführt werden müssen und bei der außerdem die technisch aufwendig herzustellende Fluchtung der Gehäusedeckel überflüssig wird.The object on which the present invention is based is to provide a hydrostatic machine of the generic type in which no pulsating forces arising from the hydrostatic load have to be conducted over the outer surfaces of the machine and in which the alignment of the housing cover, which is technically complex to produce, is superfluous .

Diese Aufgabe wird durch die im kennzeichnenden Teil des Patentanspruchs 1 angegebenen Merkmale gelöst.This object is achieved by the features specified in the characterizing part of patent claim 1.

Die besonderen Vorteile dieser Konfiguration beziehungsweise Konstruktion liegen darin, daß sowohl die axialen Kräfte wie auch die radialen Kräfte im Inneren der Pumpe aufgenommen werden und somit über die Außenfläche keine Geräuschanregung bewirken können.The particular advantages of this configuration or construction lie in the fact that both the axial forces and the radial forces are absorbed inside the pump and therefore cannot cause noise excitation via the outer surface.

Außerdem ist die einfache Lagerung des Zylindersterns und des Hubrings für die Fertigung sehr vorteilhaft.In addition, the simple mounting of the cylinder star and the cam ring is very advantageous for production.

Besondere Ausgestaltungen und Weiterbildungen der im Patentanspruch 1 spezifizierten hydrostatischen Maschine sind Gegenstand der Unteransprüche.Special refinements and developments of the hydrostatic machine specified in claim 1 are the subject of the dependent claims.

Die Einzelheiten der erfindungsgemäßen hydrostatischen Maschine werden im folgenden anhand der Zeichnung näher erläutert. Diese zeigt in

Fig. 1
einen Längsschnitt durch eine hydrostatische Maschine;
Fig. 2
einen Querschnitt durch die hydrostatische Maschine gemäß Fig. 1 längs der Schnittlinie II-II;
Fig. 3
den Längsschnitt durch die hydrostatische Maschine gemäß Fig. 1 mit Angabe der axialen und radialen Kraftflüsse innerhalb der hydrostatischen Maschine;
Fig. 4
einen Querschnitt durch die hydrostatische Maschine gemäß Fig. 1 längs der Schnittlinie III-III.
The details of the hydrostatic machine according to the invention are explained in more detail below with reference to the drawing. This shows in
Fig. 1
a longitudinal section through a hydrostatic machine;
Fig. 2
a cross section through the hydrostatic machine according to Figure 1 along the section line II-II.
Fig. 3
the longitudinal section through the hydrostatic machine according to FIG 1 with indication of the axial and radial force flows within the hydrostatic machine.
Fig. 4
a cross section through the hydrostatic machine according to FIG. 1 along the section line III-III.

Die die hydrostatische Maschine repräsentierende Radialkolbenmaschine weist ein Gehäuse 1 mit zwei durch einen Zwischenboden 5 getrennten Innenräumen 6, 7 auf. Die Innenräume 6, 7 sind von beiden Seiten her über je einen Gehäusedeckel 3 abgeschlossen. In den beiden Teilräumen (Innenräumen) 6, 7 ist je ein Hubring 8, 9 gelagert, welche beide über mindestens eine Verbindungswelle 11 und über eine Lagerwelle 10 miteinander und - über Lager 36 - mit dem Zwischenboden 5 verbunden sind.The radial piston machine representing the hydrostatic machine has a housing 1 with two interior spaces 6, 7 separated by an intermediate floor 5. The interiors 6, 7 are closed from both sides via a housing cover 3. In each of the two subspaces (interior spaces) 6, 7, a cam ring 8, 9 is mounted, which both are connected to one another via at least one connecting shaft 11 and via a bearing shaft 10 and to the intermediate floor 5 via bearings 36.

An der Innenseite 12, 13 der Hubringe 8, 9 gleiten in an sich bekannter Weise die der Funktion beziehungsweise Verwendung als hydrostatische Maschine beziehungsweise als Radialkolbenmaschine dienenden Verdrängerelemente, die aus der funktionalen Verbindung eines Gleitschuhs oder Gleitsteins 14 und eines gelenkig damit verbundenen (Verdränger-) Kolbens 15 bestehen. Diese Kolben 15 sind in radialen Bohrungen 16, 17 je eines der den Zylinderstern bildenden Rotoren 18, 19 angeordnet, die ihrerseits verdrehfest und axial fixiert mit einer über einen in einem Lager 4 gelagerten Antriebsstutzen 26 angetriebenen Welle 20 gekoppelt sind.On the inside 12, 13 of the lifting rings 8, 9, in a manner known per se, the displacement elements serving the function or use as a hydrostatic machine or as a radial piston machine, which consist of the functional connection of a sliding block or sliding block 14 and an articulated (displacement) block Piston 15 exist. These pistons 15 are each arranged in radial bores 16, 17 of one of the rotors 18, 19 forming the cylindrical star, which in turn are coupled in a rotationally fixed and axially fixed manner to a shaft 20 driven by a drive connector 26 mounted in a bearing 4.

Die im vorstehenden beschriebene Konfiguration entspricht - abgesehen davon, daß über den Förderstrom beziehungsweise die Pumpfunktion noch nichts ausgesagt wurde - dem stand der Technik insoweit, als die Rotoren 18, 19 an sich bekannt sind. Die besondere Konfiguration bestehet jedoch darin, daß die hydrostatische Maschine nicht von einem Rotor 18, 19 ausgeht, sondern von zweien, die synchron miteinander als Motor- beziehungsweise Pumpeinheit wirken (wodurch letztlich bei radial gleichen Abmessungen die doppelte Förderleistung erreicht wird), und daß die Antriebswelle zwischen den Rotoren 18, 19 gelagert wird und zwar in Verbindung mit der zwischen den Hubringen 8, 9 liegenden Hubringlagerung im Zwischenboden 5.The configuration described above corresponds - apart from the fact that nothing has been said about the flow rate or the pumping function - to the state of the art insofar as the rotors 18, 19 are known per se. The special configuration, however, consists in the fact that the hydrostatic machine does not start from one rotor 18, 19, but from two, which act synchronously with one another as a motor or pump unit (which ultimately achieves twice the delivery capacity with radially identical dimensions) and that Drive shaft is mounted between the rotors 18, 19 in connection with the cam ring bearing located in the intermediate floor 5 between the cam rings 8, 9.

Die beiden Rotoren 18, 19 sind im Hinblick auf ihre Funktion als Pumpelement wie folgt in aufeinander abgestimmter Weise miteinander gekoppelt beziehungsweise funktionell verbunden: In den radialen Bohrungen 16, 17 der Rotoren 18, 19 sind einander zugewandt axiale seitliche Steuerschlitze 21, 22 vorgesehen, über die die Bohrungen 16, 17 zum Zwischenboden 5 hin offen sind. Diese Steuerschlitze 21, 22 korrespondierenden ihrerseits mit in Steuerscheiben (Axialscheiben) 25, 26 eingearbeiteten nierenförmigen (vergleiche Fig. 4) Kanälen 23, 24. Die Steuerscheiben 25, 26 sind in entsprechenden Ausnehmungen auf beiden Seiten des Zwischenbodens 5 eingelegt. Im Zwischenboden 5 selbst sind korrespondierend zu den genannten Steuerschlitzen 21, 22 und den nierenförmigen Kanälen 23, 24 quer durchgehend Verbindungskanäle 27, 28 eingearbeitet, so daß beide Rotoren 18, 19 über ihre Verdrängerelemente miteinander verbunden sind - und gemeinsam als Pumpe beziehungsweise hydrostatische Maschine zu arbeiten vermögen; es entsteht so eine zweiflutige hydrostatische Maschine beziehungsweise Radialkolbenmaschine, wobei die Verbindungskanäle 27, 28 den Ein- beziehungsweise Auslaßkanal bilden und dementsprechend nach außen hin offen sind.With regard to their function as a pump element, the two rotors 18, 19 are coupled or functionally connected to one another in a coordinated manner as follows: In the radial bores 16, 17 of the rotors 18, 19, axial lateral control slots face one another 21, 22 are provided, through which the bores 16, 17 are open to the intermediate floor 5. These control slots 21, 22 in turn correspond to kidney-shaped channels 23, 24 incorporated in control disks (axial disks) 25, 26 (cf. FIG. 4). The control disks 25, 26 are inserted in corresponding recesses on both sides of the intermediate base 5. In the intermediate floor 5 itself, corresponding to the control slots 21, 22 and the kidney-shaped channels 23, 24, transverse connecting channels 27, 28 are incorporated so that both rotors 18, 19 are connected to one another via their displacement elements - and together as a pump or hydrostatic machine able to work; this creates a double-flow hydrostatic machine or radial piston machine, the connecting channels 27, 28 forming the inlet and outlet channels and accordingly being open to the outside.

Der durch die (seitliche) Druckbeaufschlagung der Kolben 15 und der Steuerschlitze 21, 22 entstehende axiale Schub wird aufgrund der gleich groß ausgebildeten axialen Kanäle 23, 24 in den Steuerscheiben 25, 26 und der diese Kanäle 23, 24 in den Spalten zwischen den Rotoren 18, 19 und den Steuerscheiben 25, 26 umgebenden Druckfelder 29, 30 somit durch eine entgegengesetzt gerichtete Wirkung der hydrostatischen Kräfte ausgeglichen. Der Kraftschluß B zwischen den Rotoren 18, 19 über die Welle 20 vermeidet so jegliche axiale Kraftbeaufschlagung des Gehäuses 1.The axial thrust resulting from the (lateral) pressurization of the pistons 15 and the control slots 21, 22 becomes due to the equally large axial channels 23, 24 in the control disks 25, 26 and these channels 23, 24 in the gaps between the rotors 18 , 19 and the control discs 25, 26 surrounding pressure fields 29, 30 thus compensated for by an oppositely directed effect of the hydrostatic forces. The frictional connection B between the rotors 18, 19 via the shaft 20 thus avoids any axial application of force to the housing 1.

Bei entsprechend der Zeichnung geeigneter Lagerung beziehungsweise Abstützung der Welle 20 relativ zum Zwischenboden 5 und der Abstützung der Hubringe 8, 9 über die Lagerwelle (Schwenkwelle) 10 am Zwischenboden 5 läßt sich darüberhinaus eine einfache Lagerung darstellen, die wie in Fig. 3 gezeigt, die radialen Kraftschlüsse A und C im Inneren der Pumpe führt.With appropriate storage or support of the shaft 20 relative to the intermediate floor 5 and the support of the cam rings 8, 9 via the bearing shaft (pivot shaft) 10 on the intermediate floor 5, a simple mounting can also be represented, as shown in FIG. 3, the radial frictional connections A and C inside the pump leads.

Bezüglich der konstruktiven Gesamtkonfiguration ist noch anzumerken - vergleiche Fig. 4 - die beiden Hubringe 8, 9 gemeinsam über eine aus einem Verstellkolben 31 und einem Gegenkolben 32 bestehende Verstelleinrichtung positioniert werden. Diese Verstelleinrichtung ist am Zwischenboden 5 montiert beziehungsweise angebaut und wirksam. Im Zwischenboden 5 sind darüberhinaus - wie erwähnt - die Verbindungskanäle 27, 28, d.h. der einlaßseitige Niederdruckkanal und der auslaßseitige Hochdruckkanal eingearbeitet.With regard to the overall structural configuration, it should also be noted - compare FIG. 4 - the two cam rings 8, 9 are positioned together via an adjusting device consisting of an adjusting piston 31 and a counter-piston 32. This adjustment device is mounted or attached to the intermediate floor 5 and is effective. In the intermediate floor 5 there are - as mentioned - the connecting channels 27, 28, i.e. the inlet-side low-pressure duct and the outlet-side high-pressure duct are incorporated.

Die Rotoren 18, 19 sind - wie bereits erwähnt - verdrehfest und axial fixiert auf der Welle 20 befestigt. Dabei können - wie dargestellt - beide Rotoren demontierbar (vergleiche Spannmutter 37) auf der Welle 20 sitzen; die Welle 20 wird über eine Kupplungshülse 40 vom Antriebsstutzen 2 her angetrieben.As already mentioned, the rotors 18, 19 are fixed in a rotationally fixed and axially fixed manner on the shaft 20. As shown, both rotors can be removed from the shaft 20 (see clamping nut 37); the shaft 20 is driven via a coupling sleeve 40 from the drive socket 2.

Bei der vorstehend beschriebenen und in der Zeichnung dargestellten Konstruktion ist in der Zeichnung für jeden Rotor 18, 19 auf der Welle 20 je ein Bund 33, 34 vorgesehen. Bei der Montage werden die Rotoren 18, 19 mittels Spannelementen 37 gegen diese Bunde 33 beziehungsweise 34 gedrückt. Der Abstand der Bunde 33, 34 ist dabei geringfügig größer, als es der Summe aus der Dicke des Zwischenbodens 5 und der Dicke der Steuerscheiben 25, 26 entspricht.In the construction described above and shown in the drawing, a collar 33, 34 is provided on the shaft 20 for each rotor 18, 19. During assembly, the rotors 18, 19 are pressed against these collars 33 and 34 by means of clamping elements 37. The distance between the bundles 33, 34 is slightly larger than the sum of the thickness of the intermediate floor 5 and the thickness of the control discs 25, 26.

Grundsätzlich können die Rotoren 18, 19 auch derart auf der Welle 20 fixiert werden, daß der eine Rotor einstückig mit der Welle 20 ausgebildet ist, während der zweite Rotor über eine Spannmutter fixiert wird.In principle, the rotors 18, 19 can also be fixed on the shaft 20 in such a way that one rotor is formed in one piece with the shaft 20, while the second rotor is fixed via a clamping nut.

In besonderer Ausgestaltung ist es auch möglich, die beiden Rotoren 18, 19 relativ zueinander beispielsweise um eine halbe Teilung der radial angeordneten Verdrängerelemente zu fixieren.In a special embodiment, it is also possible to rotate the two rotors 18, 19 relative to one another, for example by one to fix half division of the radially arranged displacement elements.

Zusammenfassend soll nochmals folgendes angemerkt werden:
Durch die axiale Fixierung der beiden Rotoren 18, 19 auf der Welle 20 wird erreicht, daß die axialen Kräfte nicht an den Gehäusedeckeln 3 abgestützt werden müssen. Die Lagerung der Antriebswelle 20 über Lager 35 im Zwischenboden 5, sowie die Lagerung der Hubringe 8, 9 im selben Zwischenboden 5 ermöglichen die Kraftschlüsse A, B und C, welche sämtlich sich im Inneren der Maschine auswirken. Der für einen sicheren Lauf der Rotoren 18, 19 notwendige Spalt relativ zu den Steuerscheiben (Axialscheiben) 25, 26 soll wegen der davon abhängenden Dichtigkeit möglichst gering gehalten werden. Dies wird schließlich dadurch erreicht, daß in den Steuerscheiben 25, 26 auf den dem Zwischenboden 5 zugewandten Seiten elastische Dichtung 38, 39, zum Beispiel O-Ringe, eingelegt werden, welche durch die Begrenzung der Druckfelder 29, 30 gegen den jeweils anliegenden Rotor 18, 19 eine Kraft erzeugen, die durch Auslegung geringfügig größer bestimmt wird, als die vom über der metallischen Dichtung auf der Rotorseite der Steuerscheiben 25, 26 verteilten Druckfeld erzeugte. Dadurch wird der Spalt zwischen den Rotoren 18, 19 und den Steuerscheiben 25, 26 sehr klein gehalten.
In summary, the following should be noted again:
The axial fixation of the two rotors 18, 19 on the shaft 20 ensures that the axial forces do not have to be supported on the housing covers 3. The mounting of the drive shaft 20 via bearings 35 in the intermediate floor 5, as well as the mounting of the lifting rings 8, 9 in the same intermediate floor 5 enable the frictional connections A, B and C, all of which have an effect inside the machine. The gap required for the rotors 18, 19 to run reliably relative to the control disks (axial disks) 25, 26 should be kept as small as possible because of the tightness which depends on them. This is finally achieved by inserting elastic seals 38, 39, for example O-rings, in the control disks 25, 26 on the sides facing the intermediate base 5, which seals by limiting the pressure fields 29, 30 against the respective adjacent rotor 18 , 19 generate a force that is determined by design slightly larger than that generated by the pressure field distributed over the metallic seal on the rotor side of the control disks 25, 26. As a result, the gap between the rotors 18, 19 and the control disks 25, 26 is kept very small.

Claims (2)

  1. Hydrostatic machine with a cylinder star disposed on the shaft (20) fixed non-rotatably and axially which has a plurality of radial bores (16, 17) with displacer elements (15, 14) sliding on the inside of a lift ring (8, 9), whereby the bores (16, 17) are connected to transporting channels issuing from the sides of the cylinder star to control the amount of pressure medium conveyed by means of control slots (21, 22), whereby the cylindrical star comprises two rotors (18, 19) mounted at a distance from one another, the bores (16, 17) of which have control slots (21, 22) communicating with one another, in particular opposite one another,
    whereby a casing false-floor (5) is provided between the two rotors (18, 19) which has control discs (25, 26) opposite the rotors (18, 19) with channels (23, 24) corresponding with the control slots (21, 22) and connecting channels serving as transporting channels (27, 28) for the channels (23, 24) connected together,
    characterised in that
    the lift rings (8, 9) of both rotors (18, 19) are rigidly connected to each other by a bearing shaft (10) and the shaft (20) and the bearing shaft (10) are both mounted on a bearing (35, 36) in the false floor (5).
  2. Hydrostatic machine according to claim 1
    characterised in that
    for each rotor (18, 19) a flange (33, 34) is provided on the shaft (20) against which the rotors (18, 19) are pressed by means of clamping elements (37) and the distance of which is somewhat greater than the sum of the thickness of the false floor (5) and the control discs (25, 26).
EP93112131A 1992-09-04 1993-07-29 Hydrostatic machine with axial thrust balancing Expired - Lifetime EP0585609B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4229656 1992-09-04
DE4229656 1992-09-04

Publications (2)

Publication Number Publication Date
EP0585609A1 EP0585609A1 (en) 1994-03-09
EP0585609B1 true EP0585609B1 (en) 1995-10-25

Family

ID=6467288

Family Applications (1)

Application Number Title Priority Date Filing Date
EP93112131A Expired - Lifetime EP0585609B1 (en) 1992-09-04 1993-07-29 Hydrostatic machine with axial thrust balancing

Country Status (8)

Country Link
US (1) US5374165A (en)
EP (1) EP0585609B1 (en)
JP (1) JPH06193558A (en)
KR (1) KR940007345A (en)
AT (1) ATE129546T1 (en)
DE (1) DE59300817D1 (en)
DK (1) DK0585609T3 (en)
ES (1) ES2079927T3 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2706539B1 (en) * 1993-06-14 1995-09-01 Poclain Hydraulics Sa Set of two pressurized fluid motors.
DE59405708D1 (en) * 1993-10-19 1998-05-20 Voith Gmbh J M Hydrostatic radial piston machine with axial thrust compensation
US7484939B2 (en) * 2004-12-17 2009-02-03 Eaton Corporation Variable displacement radial piston pump
WO2018205015A1 (en) * 2017-05-06 2018-11-15 Kinetics Drive Solutions Inc. Hydrostatic variator based on radial piston machines
SK288973B6 (en) * 2020-08-13 2022-06-30 Up-Steel, S.R.O. Radial piston rotary machine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3044412A (en) * 1958-05-13 1962-07-17 New York Air Brake Co High pressure hydraulic pump or motor
GB1003122A (en) * 1961-01-27 1965-09-02 Nat Res Dev Improvements in hydraulic ball piston pumps and motors
DE2301448C3 (en) * 1973-01-12 1980-01-24 Robert Bosch Gmbh, 7000 Stuttgart Hydrostatic radial piston pump
DE7605633U1 (en) * 1976-02-25 1977-08-18 Robert Bosch Gmbh, 7000 Stuttgart RADIAL PISTON MULTIPLE PUMP

Also Published As

Publication number Publication date
US5374165A (en) 1994-12-20
DE59300817D1 (en) 1995-11-30
KR940007345A (en) 1994-04-27
DK0585609T3 (en) 1996-02-26
JPH06193558A (en) 1994-07-12
ATE129546T1 (en) 1995-11-15
ES2079927T3 (en) 1996-01-16
EP0585609A1 (en) 1994-03-09

Similar Documents

Publication Publication Date Title
DE4138313C2 (en) Radial piston pump
DE19706114C2 (en) Device for reducing pulsation on a hydrostatic displacement unit
DE3590198C2 (en) Valve plate for a hydrostatic axial piston unit
DE2306064C2 (en) Vane pump
DE2954135C2 (en) Positive displacement pumps, in particular for servo devices in motor vehicles
EP2235374A2 (en) Variable-volume internal gear pump
EP0585609B1 (en) Hydrostatic machine with axial thrust balancing
DE3233579C2 (en) Axial piston machine
EP0602231B1 (en) Hydrostatic machine with axial thrust compensation
DE10353027A1 (en) Adjustable pump, in particular vane pump
DE19900142A1 (en) Fuel pump used in motor vehicle
DE69506530T2 (en) TRANSLATION CONTROL FOR CONTINUOUSLY HYDROSTATIC GEARBOX
EP0654584B1 (en) Hydrostatic radial piston machine with axial thrust compensation
DE3242983A1 (en) ADJUSTABLE WING CELL PUMP
DE4110392C2 (en) Vane type rotary pump (vane pump)
EP0383167B1 (en) Axial piston engine
AT504984B1 (en) INJECTION AND OUTLET CONTROL FOR AN AXIAL PISTON MACHINE
WO1995029324A1 (en) Engine brake for a multi-cylinder internal combustion engine
DE3225790A1 (en) PUMP OR MOTOR
DE69207224T2 (en) Swashplate piston hydraulic system
DE2248316C2 (en) Radial piston machine
DE3930248C2 (en) Radial piston pump
DE9208850U1 (en) Hydrostatic machine with axial thrust compensation
DE4039926C2 (en) Axial piston pump, especially for water high-pressure cleaners
DE2163442B2 (en) DEVICE TO PREVENT THE ROTATING CYLINDER DRUM FROM LIFTING UP FROM THE CONTROL MIRROR OF AN AXIAL PISTON MACHINE

Legal Events

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

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19930729

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH DE DK ES FR GB IT LI NL SE

17Q First examination report despatched

Effective date: 19940919

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE CH DE DK ES FR GB IT LI NL SE

REF Corresponds to:

Ref document number: 129546

Country of ref document: AT

Date of ref document: 19951115

Kind code of ref document: T

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 19951024

REF Corresponds to:

Ref document number: 59300817

Country of ref document: DE

Date of ref document: 19951130

ET Fr: translation filed
REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2079927

Country of ref document: ES

Kind code of ref document: T3

ITF It: translation for a ep patent filed
REG Reference to a national code

Ref country code: DK

Ref legal event code: T3

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

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

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

26N No opposition filed
REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

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

Ref country code: GB

Payment date: 20030707

Year of fee payment: 11

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

Ref country code: ES

Payment date: 20030711

Year of fee payment: 11

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

Ref country code: SE

Payment date: 20030716

Year of fee payment: 11

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

Ref country code: DK

Payment date: 20030717

Year of fee payment: 11

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

Ref country code: NL

Payment date: 20030718

Year of fee payment: 11

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

Ref country code: FR

Payment date: 20030723

Year of fee payment: 11

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

Ref country code: BE

Payment date: 20030724

Year of fee payment: 11

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

Ref country code: AT

Payment date: 20030729

Year of fee payment: 11

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

Ref country code: CH

Payment date: 20030731

Year of fee payment: 11

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

Ref country code: DE

Payment date: 20030804

Year of fee payment: 11

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

Ref country code: GB

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

Effective date: 20040729

Ref country code: AT

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

Effective date: 20040729

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

Ref country code: SE

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

Effective date: 20040730

Ref country code: ES

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

Effective date: 20040730

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

Ref country code: LI

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

Effective date: 20040731

Ref country code: CH

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

Effective date: 20040731

Ref country code: BE

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

Effective date: 20040731

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

Ref country code: DK

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

Effective date: 20040802

BERE Be: lapsed

Owner name: J.M. *VOITH G.M.B.H.

Effective date: 20040731

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

Ref country code: NL

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

Effective date: 20050201

Ref country code: DE

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

Effective date: 20050201

REG Reference to a national code

Ref country code: DK

Ref legal event code: EBP

EUG Se: european patent has lapsed
REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20040729

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

Ref country code: FR

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

Effective date: 20050331

NLV4 Nl: lapsed or anulled due to non-payment of the annual fee

Effective date: 20050201

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

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

Ref country code: IT

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

Effective date: 20050729

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20040730

BERE Be: lapsed

Owner name: J.M. *VOITH G.M.B.H.

Effective date: 20040731