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EP0654584B1 - Hydrostatic radial piston machine with axial thrust compensation - Google Patents

Hydrostatic radial piston machine with axial thrust compensation Download PDF

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Publication number
EP0654584B1
EP0654584B1 EP94114848A EP94114848A EP0654584B1 EP 0654584 B1 EP0654584 B1 EP 0654584B1 EP 94114848 A EP94114848 A EP 94114848A EP 94114848 A EP94114848 A EP 94114848A EP 0654584 B1 EP0654584 B1 EP 0654584B1
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EP
European Patent Office
Prior art keywords
rotors
hydrostatic
machine according
hydrostatic machine
control
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP94114848A
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German (de)
French (fr)
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EP0654584A1 (en
Inventor
Gerhard Fähnle
Günther Nagel
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JM Voith GmbH
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JM Voith GmbH
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Publication of EP0654584A1 publication Critical patent/EP0654584A1/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B13/00Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion
    • F01B13/04Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder
    • F01B13/06Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder in star arrangement
    • F01B13/061Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder in star arrangement the connection of the pistons with the actuated or actuating element being at the outer ends of the cylinders
    • F01B13/063Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder in star arrangement the connection of the pistons with the actuated or actuating element being at the outer ends of the cylinders with two or more series radial piston-cylinder units
    • 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 Radial piston machine.
  • Double flow according to the system of axial thrust compensation radial piston machines constructed for two rotors known; the rotors on these machines are non-rotatable on a wave. Basically are building on this Arrangement of both a hydrostatic pump and a hydrostatic motor can be displayed.
  • the object underlying the present invention is a hydrostatic radial piston machine specify the axial forces on the axis can be compensated.
  • the system should equally a hydrostatic pump with one or two Flow, a corresponding hydrostatic motor and a hydrostatic transmission can be represented.
  • Embodiments of hydrostatic Radial piston machines have a housing that has two, 5 interiors separated by an intermediate floor Has. These interiors are over on both sides a housing cover completed. In the respective two A stroke ring is stored in each of the subspaces (interior) both connected to each other via at least one bearing shaft are.
  • a hydrostatic radial piston machine with the features described above are from the after Priority date of the present application published EP-A-0 585 609 has become known.
  • hydrostatic radial piston machines can the conjugate cam rings 109, 208 using Adjusting pistons 131, 132, 231, 232 independently of one another be adjusted (see reference numbers 111, 211).
  • the drive or output of the machine is over Input and output shafts 2, 20 (Fig. 1, Fig. 7, Fig. 10) or 102, 202 (see Fig. 4) and via driver 41, 42 to a so-called Rotor 18, 19 forming cylindrical star.
  • the rotors 18, 19 have lateral control slots 21, 22, which with machined in axially arranged control disks 25, 26 kidney-shaped channels 23, 24 correspond.
  • the axial Sealing of these channels 23, 24 in the control disks 25, 26 takes place via elastic sealing elements 38, 39.
  • the known radial piston machines have an axis 43 on that fastened in the respective intermediate floor 5, 205, 305, 405 and at the ends of the rotors 18, 19 on the one hand between thrust washers 37, 44 and on the other hand the control discs 25, 26 are stored.
  • cam ring 8 9 (FIG. 1) or 109, 208 (FIGS. 4, 7, 10) are provided, both of which have a respective bearing shaft 10 Intermediate floor 5, 205, 305, 405 are stored.
  • the rotors 18, 19 are specific in terms of their Function as a pump or motor element as follows coordinated:
  • Control slots 21, 22 are provided through which the bores 16, 17 to the respective intermediate floor 5, 205, 305, 405 are open.
  • the control slots 21, 22 correspond in turn with those in the control discs (axial discs) 25, 26 incorporated kidney-shaped (compare Fig. 3, Fig. 6, Fig. 9, Fig. 11) channels 23, 24.
  • the control discs 25, 26 are in corresponding recesses on both Sides of the intermediate floor 5, 205, 305, 405 inserted.
  • the Intermediate floor 5, 205, 305, 405 itself are corresponding to said control slots 21, 22 and kidney-shaped Channels 23, 24 connecting channels 27, 28 (Fig.
  • the by the pressurization of the (displacement) pistons 15 and the control slots 21, 22 resulting axial thrust is due to the clamping of the axis 43 in the mezzanine 5, 205, 305, 405 between those supported on it Control disc 26 and a thrust washer 44 respectively which are supported on the intermediate floor 5, 205, 305, 405 Control disc 25 and a thrust washer 37 added and thus not on the housing cover 3, 4; 103, 204; 203, 304 transfer.
  • the two thrust washers 37, 44 are each biased against a collar 33, 34 on axis 43, that the distance between the thrust washers and the intermediate floor or the control disks 25, 26 is slightly larger than the width of the rotor 18, 19 corresponds.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Reciprocating Pumps (AREA)
  • Details Of Reciprocating Pumps (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
  • Hydraulic Motors (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)

Abstract

The invention relates to a hydrostatic radial piston machine with two rotors (17, 18) which are mounted to allow easy rotation on a spindle and which have a plurality of radially extending holes with displacer elements (piston plus sliding block 15, 14) sliding on the inside of a cam ring (8, 9). For control of the delivery of the pressure medium, the holes are connected via control slots (21, 22) to delivery passages (high-/low-pressure 27, 28) opening at the sides of the rotors. The invention is characterised in that the two rotors (17, 18) are mounted in an easily rotatable manner on a spindle (43) installed rigidly in an intermediate plate (5), in that the intermediate plate (5) is situated between the rotors (17, 18), in that thrust washers (37, 44) which accept the axial forces caused by the pressure medium in the control slots (21, 22) of the rotors (17, 18) are mounted on the ends of the spindle (43), and in that the cam rings (8, 9) are mounted in the intermediate plate by way of a common connecting shaft (10). <IMAGE>

Description

Die vorliegende Erfindung betrifft eine hydrostatische Radialkolbenmaschine.The present invention relates to a hydrostatic Radial piston machine.

Zweiflutige, nach dem System der axialen Schubkompensation für zwei Rotoren aufgebaute Radialkolbenmaschinen sind bekannt; bei diesen Maschinen sitzen die Rotoren drehfest auf einer Welle. Grundsätzlich sind aufbauend auf dieser Anordnung sowohl eine hydrostatische Pumpe, als auch ein hydrostatischer Motor darstellbar.Double flow, according to the system of axial thrust compensation radial piston machines constructed for two rotors known; the rotors on these machines are non-rotatable on a wave. Basically are building on this Arrangement of both a hydrostatic pump and a hydrostatic motor can be displayed.

Die der vorliegenden Erfindung zugrunde liegende Aufgabe besteht darin, eine hydrostatische Radialkolbenmaschine anzugeben, bei der die axialen Kräfte auf der Achse kompensiert werden können. Vom System her soll dabei gleichermaßen eine hydrostatische Pumpe mit ein oder zwei Strömen, ein entsprechender hydrostatischer Motor und ein hydrostatisches Getriebe dargestellt werden können.The object underlying the present invention is a hydrostatic radial piston machine specify the axial forces on the axis can be compensated. The system should equally a hydrostatic pump with one or two Flow, a corresponding hydrostatic motor and a hydrostatic transmission can be represented.

Diese Aufgabe wird durch die im Patentanspruch 1 angegebenen Merkmale gelöst. This object is achieved by the in claim 1 specified features solved.

Die besonderen Vorteile dieser Konfigurationen bestehen darin, daß sowohl die axialen, als auch die radialen Kräfte im Inneren der Radialkolbenmaschine aufgenommen werden, so daß über die jeweiligen Außenflächen keine Geräusche nach außen abgegeben beziehungsweise abgestrahlt werden.The particular advantages of these configurations exist in that both the axial and the radial forces be recorded inside the radial piston machine, so that no noise after the respective outer surfaces emitted or emitted outside.

Besondere Weiterbildungen und Ausgestaltungen der Erfindung sind Gegenstand der Unteransprüche.Special developments and refinements of the invention are the subject of the subclaims.

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

Fig. 1
einen Längsschnitt durch eine hydrostatische Pumpe beziehungsweise einen hydrostatischen Motor;
Fig. 2
einen Querschnitt durch die hydrostatische Maschine gemäß Fig. 1 längs der Schnittlinie II-II;
Fig. 3
einen Querschnitt durch die hydrostatische Maschine gemäß Fig. 1 längs der Schnittlinie III-III;
Fig. 4
einen Längsschnitt durch ein hydrostatisches Getriebe;
Fig. 5
einen Querschnitt durch die hydrostatische Maschine gemäß Fig. 4 längs der Schnittlinie V-V;
Fig. 6
einen Querschnitt durch die hydrostatische Maschine gemäß Fig. 4 längs der Schnittlinie IV-IV;
Fig. 7
einen Längsschnitt durch eine hydrostatische Zweistrom-Pumpe beziehungsweise einen hydrostatischen Zwei strom-Motor;
Fig. 8
einen Querschnitt durch die hydrostatische Maschine gemäß Fig. 7 längs der Schnittlinie VII-VII;
Fig. 9
einen Querschnitt durch die hydrostatische Maschine gemäß Fig. 7 längs der Schnittlinie VI-VI;
Fig. 10
einen Längsschnitt durch eine hydrostatische Zweistrom-Pumpe beziehungsweise einen hydrostatischen Zweistrom-Motor für unterschiedliche Drücke;
Fig. 11
einen Querschnitt durch die hydrostatische Maschine gemäß Fig. 10 längs der Schnittlinie VIII VIII.
The details of the hydrostatic radial piston 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 pump or a hydrostatic motor;
Fig. 2
a cross section through the hydrostatic machine according to Figure 1 along the section line II-II.
Fig. 3
a cross section through the hydrostatic machine of Figure 1 along the section line III-III.
Fig. 4
a longitudinal section through a hydrostatic transmission;
Fig. 5
a cross section through the hydrostatic machine according to FIG 4 along the section line VV.
Fig. 6
a cross section through the hydrostatic machine according to FIG 4 along the section line IV-IV.
Fig. 7
a longitudinal section through a hydrostatic two-stream pump or a hydrostatic two-stream motor;
Fig. 8
a cross section through the hydrostatic machine according to FIG 7 along the section line VII-VII.
Fig. 9
a cross section through the hydrostatic machine according to FIG 7 along the section line VI-VI.
Fig. 10
a longitudinal section through a hydrostatic two-stream pump or a hydrostatic two-stream motor for different pressures;
Fig. 11
a cross section through the hydrostatic machine according to FIG. 10 along the section line VIII VIII.

Sämtliche in den Fig. 1 bis Fig. 11 dargestellten Ausführungsbeispiele von hydrostatischen Radialkolbenmaschinen weisen ein Gehäuse auf, das zwei, durch jeweils einen Zwischenboden 5 getrennte Innenräume hat. Diese Innenräume sind von beiden Seiten her über je ein Gehäusedeckel abgeschlossen. In den jeweiligen beiden Teilräumen (Innenraum) ist je ein Hubring gelagert, welche beide über mindestens eine Lagerwelle miteinander verbunden sind. Eine hydrostatische Radialkolbenmaschine mit den zuvor beschriebenen Merkmalen sind aus der nach dem Prioritätstag der vorliegenden Anmeldung veröffentlichten EP-A-0 585 609 bekanntgeworden.All shown in FIGS. 1 to 11 Embodiments of hydrostatic Radial piston machines have a housing that has two, 5 interiors separated by an intermediate floor Has. These interiors are over on both sides a housing cover completed. In the respective two A stroke ring is stored in each of the subspaces (interior) both connected to each other via at least one bearing shaft are. A hydrostatic radial piston machine with the features described above are from the after Priority date of the present application published EP-A-0 585 609 has become known.

Die beiden Teilräume lassen dabei genügend Platz, um die Hubringe 8, 9 der hydrostatischen Pumpe nach Fig. 1 - wie in Fig. 3 dargestellt - mittels zweier Verstellkolben 32, das Hubvolumen pro Umdrehung der hydrostatischen Radialkolbenmaschine auf eine gewünschte spezifische Größe einzustellen. Bei den in Fig. 4, Fig. 7 und Fig. 10 dargestellten hydrostatischen Radialkolbenmaschinen können die konjugierten Hubringe 109, 208 mit Hilfe von Verstellkolben 131, 132, 231, 232 unabhängig voneinander verstellt werden (vergleiche Bezugszeichen 111, 211).The two subspaces leave enough space to hold the Lifting rings 8, 9 of the hydrostatic pump according to Fig. 1 - like 3 - by means of two adjusting pistons 32, the stroke volume per revolution of the hydrostatic Radial piston machine to a desired specific size adjust. In the case of FIGS. 4, 7 and 10 shown hydrostatic radial piston machines can the conjugate cam rings 109, 208 using Adjusting pistons 131, 132, 231, 232 independently of one another be adjusted (see reference numbers 111, 211).

Der Antrieb beziehungsweise Abtrieb der Maschine wird über An- beziehungsweise Abtriebswellen 2, 20 (Fig. 1, Fig. 7, Fig. 10) beziehungsweise 102, 202 (vergleiche Fig. 4)und über Mitnehmer 41, 42 auf je einen einen sogenannten Zylinderstern bildenden Rotor 18, 19 geleitet. Die Rotoren 18, 19 weisen seitliche Steuerschlitze 21, 22 auf, die mit in axial angeordneten Steuerscheiben 25, 26 eingearbeiteten nierenförmigen Kanälen 23, 24 korrespondieren. Die axiale Abdichtung dieser Kanäle 23, 24 in den Steuerscheiben 25, 26 erfolgt über elastische Dichtelemente 38, 39.The drive or output of the machine is over Input and output shafts 2, 20 (Fig. 1, Fig. 7, Fig. 10) or 102, 202 (see Fig. 4) and via driver 41, 42 to a so-called Rotor 18, 19 forming cylindrical star. The rotors 18, 19 have lateral control slots 21, 22, which with machined in axially arranged control disks 25, 26 kidney-shaped channels 23, 24 correspond. The axial Sealing of these channels 23, 24 in the control disks 25, 26 takes place via elastic sealing elements 38, 39.

Die bekannten Radialkolbenmaschinen weisen eine Achse 43 auf, die im jeweiligen Zwischenboden 5, 205, 305, 405 befestigt ist und an deren Enden die Rotoren 18, 19 einerseits zwischen Anlaufscheiben 37, 44 und andererseits den Steuerscheiben 25, 26 gelagert sind.The known radial piston machines have an axis 43 on that fastened in the respective intermediate floor 5, 205, 305, 405 and at the ends of the rotors 18, 19 on the one hand between thrust washers 37, 44 and on the other hand the control discs 25, 26 are stored.

Für jeden Rotor 18, 19 ist je ein Hubring 8, 9 (Fig. 1) beziehungsweise 109, 208 (Fig. 4, Fig. 7, Fig. 10) vorgesehen, welche beide über eine Lagerwelle 10 im jeweiligen Zwischenboden 5, 205, 305, 405 gelagert sind.For each rotor 18, 19 there is one cam ring 8, 9 (FIG. 1) or 109, 208 (FIGS. 4, 7, 10) are provided, both of which have a respective bearing shaft 10 Intermediate floor 5, 205, 305, 405 are stored.

An der Innenseite 12, 13 der Hubringe 8, 9 beziehungsweise 109, 208 gleiten - in an sich bekannter Weise - die der Funktion beziehungsweise Verwendung als hydrostatische Radialkolbenmaschine dienenden Verdrängerelemente, die jeweils aus der funktionalen Verbindung eines Gleitschuhs oder eines Gleitsteins 14 und eines gelenkig damit verbundenen (Verdränger-) Kolbens 15 bestehen. Diese Kolben 15 sind in radialen Bohrungen 16, 17 je eines der Rotoren 18, 19 angeordnet, die ihrerseits leicht verdrehbar gelagert, aber axial fixiert - wie bereits erwähnt - über die Mitnehmer 41, 42 angetrieben werden beziehungsweise abtreiben.On the inside 12, 13 of the cam rings 8, 9 and respectively 109, 208 slide - in a manner known per se - that of Function or use as a hydrostatic Radial piston machine displacement elements that each from the functional connection of a slide shoe or a sliding block 14 and one articulated thereto (Displacement) piston 15 exist. These pistons 15 are in radial bores 16, 17 each of the rotors 18, 19 arranged, which in turn is easily rotatable, but axially fixed - as already mentioned - via the driver 41, 42 are driven or driven off.

Die im Vorstehenden beschriebene Konfiguration entspricht abgesehen davon, daß noch keine Angaben über den Förderstrom beziehungsweise die Pumpfunktion gemacht wurden, dem Stand der Technik insoweit, als die Rotoren 18, 19 an sich bekannt sind. Die besondere Konfiguration besteht nun darin, daß die hydrostatische Radialkolbenmaschine nicht von zwei Rotoren 18, 19 auf einer Welle als Lager ausgeht, sondern von einer Achse 43, auf der die beiden Rotoren leicht drehbar gelagert sind, so daß ein asynchrones Arbeiten der Rotoren 18, 19 möglich ist und die axialen Kräfte auf diese Achse 43 kompensiert werden.The configuration described above corresponds apart from the fact that no information about the flow rate or the pump function was made, the State of the art insofar as the rotors 18, 19 per se are known. The special configuration now exists in that the hydrostatic radial piston machine is not starts from two rotors 18, 19 on a shaft as a bearing, but from an axis 43 on which the two rotors are easily rotatably mounted, so that asynchronous work the rotors 18, 19 is possible and the axial forces be compensated for on this axis 43.

Die Rotoren 18, 19 sind im Hinblick auf ihre spezifische Funktion als Pumpen- beziehungsweise Motorelement wie folgt aufeinander abgestimmt:The rotors 18, 19 are specific in terms of their Function as a pump or motor element as follows coordinated:

In den radialen Bohrungen 16, 17 der Rotoren 18, 19 sind - wie bereits erwähnt - einander zugewandte axiale seitliche Steuerschlitze 21, 22 vorgesehen, über die die Bohrungen 16, 17 zum jeweiligen Zwischenboden 5, 205, 305, 405 hin offen sind. Die Steuerschlitze 21, 22 korrespondieren ihrerseits mit den in den Steuerscheiben (Axialscheiben) 25, 26 eingearbeiteten nierenförmigen (vergleiche Fig. 3, Fig. 6, Fig. 9, Fig. 11) Kanälen 23, 24. Die Steuerscheiben 25, 26 sind in entsprechenden Ausnehmungen auf beiden Seiten des Zwischenbodens 5, 205, 305, 405 eingelegt. Im Zwischenboden 5, 205, 305, 405 selbst sind korrespondierend zu den genannten Steuerschlitzen 21, 22 und den nierenförmigen Kanälen 23, 24 Verbindungskanäle 27, 28 (Fig. 1), 127, 128, 228 (Fig. 4); 127, 128, 228 (Fig. 7); 128, 228, 328, 428 (Fig. 10) eingearbeitet, so daß beide Rotoren 18, 19 über ihre Verdrängerelemente jeweils gemeinsam als Pumpe beziehungsweise als hydrostatische Maschine zu arbeiten vermögen.In the radial bores 16, 17 of the rotors 18, 19 are - As already mentioned - facing axial lateral Control slots 21, 22 are provided through which the bores 16, 17 to the respective intermediate floor 5, 205, 305, 405 are open. The control slots 21, 22 correspond in turn with those in the control discs (axial discs) 25, 26 incorporated kidney-shaped (compare Fig. 3, Fig. 6, Fig. 9, Fig. 11) channels 23, 24. The control discs 25, 26 are in corresponding recesses on both Sides of the intermediate floor 5, 205, 305, 405 inserted. in the Intermediate floor 5, 205, 305, 405 itself are corresponding to said control slots 21, 22 and kidney-shaped Channels 23, 24 connecting channels 27, 28 (Fig. 1), 127, 128, 228 (Fig. 4); 127, 128, 228 (Fig. 7); 128, 228, 328, 428 (Fig. 10) incorporated so that both rotors 18, 19 via their displacement elements together as a pump or to work as a hydrostatic machine capital.

Der durch die Druckbeaufschlagung der (Verdränger-) Kolben 15 und der Steuerschlitze 21, 22 entstehende axiale Schub wird aufgrund der Einspannung der Achse 43 im Zwischenboden 5, 205, 305, 405 zwischen der sich an diesem abstützenden Steuerscheibe 26 und einer Anlaufscheibe 44 beziehungsweise der sich am Zwischenboden 5, 205, 305, 405 abstützenden Steuerscheibe 25 und einer Anlaufscheibe 37 aufgenommen und somit nicht auf die Gehäusedeckel 3, 4; 103, 204; 203, 304 übertragen. Die beiden Anlaufscheiben 37, 44 sind dabei jeweils gegenüber einem Bund 33, 34 auf der Achse 43 so vorgespannt, daß der Abstand zwischen den Anlaufscheiben und dem Zwischenboden beziehungsweise den Steuerscheiben 25, 26 etwas größer ist, als es der Breite des Rotors 18, 19 entspricht.The by the pressurization of the (displacement) pistons 15 and the control slots 21, 22 resulting axial thrust is due to the clamping of the axis 43 in the mezzanine 5, 205, 305, 405 between those supported on it Control disc 26 and a thrust washer 44 respectively which are supported on the intermediate floor 5, 205, 305, 405 Control disc 25 and a thrust washer 37 added and thus not on the housing cover 3, 4; 103, 204; 203, 304 transfer. The two thrust washers 37, 44 are each biased against a collar 33, 34 on axis 43, that the distance between the thrust washers and the intermediate floor or the control disks 25, 26 is slightly larger than the width of the rotor 18, 19 corresponds.

Die im Vorstehenden erläuterte Konfiguration und die in Verbindung damit beschriebenen Zusammenhänge beziehen sich in erster Linie auf eine hydrostatische Radialkolbenmaschine mit zwei auf einer Achse leicht verdrehbar gelagerten Rotoren, die eine Mehrzahl von radial verlaufenden Bohrungen mit an der Innenseite gleitende Verdrängerelemente aufweist, wobei die Bohrungen zur Steuerung der Förderung des Druckmediums über Steuerschlitze mit seitlich an den Rotoren mündenden Förderkanälen verbunden sind.The configuration explained above and the in Connections with it described relate primarily on a hydrostatic radial piston machine with two easily rotatable on one axis Rotors that have a plurality of radial bores with displacement elements sliding on the inside has, the holes for controlling the promotion of the pressure medium via control slots on the side Rotor discharge channels are connected.

Je nach spezifischer Ausführung als Pumpe, als Motor oder als Getriebe werden das Gehäuse 1, 201, 301, 401 und die Gehäusedeckel (3, 4); (103, 204); (203, 304), sowie die An- / Abtriebswelle 2, 20; 102, 202 modifiziert.Depending on the specific version as a pump, as a motor or the housing 1, 201, 301, 401 and the Housing cover (3, 4); (103, 204); (203, 304), as well as the Input / output shaft 2, 20; 102, 202 modified.

Es entsteht so je nach Anordnung entsprechend

  • nach Fig. 1 eine hydrostatische Pumpe beziehungsweise ein hydrostatischer Motor,
  • nach Fig. 4 ein hydrostatisches Getriebe,
  • nach Fig. 7 eine hydrostatische Zweistrom-Pumpe beziehungsweise ein hydrostatischer Zweistrom-Motor für
  • vergleiche Fig. 10 mögliche unterschiedliche Drücke in den Kanälen 128, 228, 328, 428.
It arises accordingly depending on the arrangement
  • 1 shows a hydrostatic pump or a hydrostatic motor,
  • 4 shows a hydrostatic transmission,
  • 7 a hydrostatic two-flow pump or a hydrostatic two-flow motor for
  • compare FIG. 10 possible different pressures in the channels 128, 228, 328, 428.

Claims (7)

  1. Hydrostatic radial piston machine with two rotors (18, 19) mounted on a shaft member (43) to be easily rotatable, said rotors having a plurality of radially extending holes (16, 17) with displacer elements sliding on the inside of a lifting ring (8, 9, 109, 208),
    whereby the holes (16, 17) are connected to delivery channels opening laterally on the rotors for control of the delivery of the pressure medium via control slots (21, 22);
    the two rotors (18, 19) are mounted on a shaft member (43) firmly installed in an intermediate base (5, 205, 305, 405) so as to be easily rotatable;
    the intermediate base (5, 205, 305, 405) lies between the rotors (18, 19);
    thrust washers (37, 44), which absorb the axial forces caused by the pressure medium in the control slots (21, 22) of the rotors (18, 19), are attached to the ends of the shaft member (43);
    the lifting rings (8, 9, 109, 208) are mounted in the intermediate base (5, 205, 305, 405) via a joint connecting shaft (10).
  2. Hydrostatic machine according to Claim 1, characterised in that a collar (33, 34), against which the thrust washers (37, 44) are clamped, is provided on the shaft member (43) for each rotor (18, 19), so that the distance between the thrust washers (37, 44) and the intermediate base (5, 205, 305, 405) or the control discs (25, 26) is slightly greater than that corresponding to the width of the rotor (18, 19).
  3. Hydrostatic machine according to Claim 1 or 2, characterised in that both displacer volumes may be varied via a joint control system.
  4. Hydrostatic machine according to Claim 1 or 2 for set up of a compact gear in secondary regulated construction, characterised in that the pressure sides of both rotors are connected to one another and the low-pressure sides of both rotors are separated.
  5. Hydrostatic machine according to Claim 1 or 2, characterised in that for the set up of pumps or motors with different operating pressures and, in the case of motors, different rotational speeds, characterised in that the two low-pressure sides are connected to one another and the high-pressure sides are separated.
  6. Hydrostatic machine according to Claim 1 or 2, characterised in that each rotor (18, 19) has its own high- and low-pressure connection.
  7. Hydrostatic machine according to Claim 1 or 2, characterised in that the two rotors (18, 19) have different displacer volumes.
EP94114848A 1993-10-19 1994-09-21 Hydrostatic radial piston machine with axial thrust compensation Expired - Lifetime EP0654584B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4335513 1993-10-19
DE4335513 1993-10-19

Publications (2)

Publication Number Publication Date
EP0654584A1 EP0654584A1 (en) 1995-05-24
EP0654584B1 true EP0654584B1 (en) 1998-04-15

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EP94114848A Expired - Lifetime EP0654584B1 (en) 1993-10-19 1994-09-21 Hydrostatic radial piston machine with axial thrust compensation

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US (1) US5622052A (en)
EP (1) EP0654584B1 (en)
JP (1) JPH084548A (en)
AT (1) ATE165139T1 (en)
DE (1) DE59405708D1 (en)
DK (1) DK0654584T3 (en)
ES (1) ES2117180T3 (en)

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US6021635A (en) * 1996-12-23 2000-02-08 Parker-Hannifin Corporation Dual orifice liquid fuel and aqueous flow atomizing nozzle having an internal mixing chamber
SE517873C2 (en) * 1997-04-10 2002-07-30 Haegglunds Drives Ab Piston for a hydraulic radial piston motor and hydraulic radial motor with such piston
US6151990A (en) * 1998-05-06 2000-11-28 Tecumseh Products Company Hydrostatic transaxle having a casing split along one or more vertical planes
US6212994B1 (en) * 1999-06-07 2001-04-10 David A. Estrabrooks Positive displacement rotary machine
JP4040355B2 (en) 2002-04-26 2008-01-30 スガツネ工業株式会社 Hinge
CN102720630B (en) * 2012-06-08 2014-09-24 燕山大学 Multispeed roller motor with double rotors in casing and rotating cam-link
EP3513029B1 (en) * 2016-09-16 2020-06-03 Robert Bosch GmbH Rotary electrohydraulic actuator
WO2018205015A1 (en) * 2017-05-06 2018-11-15 Kinetics Drive Solutions Inc. Hydrostatic variator based on radial piston machines

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EP0585609A1 (en) * 1992-09-04 1994-03-09 J.M. Voith GmbH Hydrostatic machine with axial thrust balancing

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DE2301448C3 (en) * 1973-01-12 1980-01-24 Robert Bosch Gmbh, 7000 Stuttgart Hydrostatic radial piston pump
AT345103B (en) * 1973-05-04 1978-08-25 Eickmann Karl FOUR STREAM OR MORE THAN FOUR STREAM RADIAL PISTON MACHINE
AT338104B (en) * 1973-05-04 1977-07-25 Eickmann Karl HYDROSTATIC RADIAL PISTON MOTOR FOR DRIVING THE ROTATING WINGS OR. THE PROPELLER OF AIRCRAFT OR MARINE VEHICLES
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Also Published As

Publication number Publication date
DE59405708D1 (en) 1998-05-20
ATE165139T1 (en) 1998-05-15
JPH084548A (en) 1996-01-09
EP0654584A1 (en) 1995-05-24
DK0654584T3 (en) 1999-03-08
US5622052A (en) 1997-04-22
ES2117180T3 (en) 1998-08-01

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