DE1401400A1 - High pressure rotary piston machine - Google Patents
High pressure rotary piston machineInfo
- Publication number
- DE1401400A1 DE1401400A1 DE19601401400 DE1401400A DE1401400A1 DE 1401400 A1 DE1401400 A1 DE 1401400A1 DE 19601401400 DE19601401400 DE 19601401400 DE 1401400 A DE1401400 A DE 1401400A DE 1401400 A1 DE1401400 A1 DE 1401400A1
- Authority
- DE
- Germany
- Prior art keywords
- jacket
- piston
- pressure
- side walls
- working chambers
- 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.)
- Pending
Links
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 239000000725 suspension Substances 0.000 claims description 2
- 238000007789 sealing Methods 0.000 description 3
- 238000005452 bending Methods 0.000 description 1
- 239000002775 capsule Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2/00—Rotary-piston machines or pumps
- F04C2/30—Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F04C2/34—Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members
- F04C2/344—Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
- F04C2/3446—Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along more than one line or surface
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B13/00—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion
- F01B13/04—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder
- F01B13/06—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder in star arrangement
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/34—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
- F01C1/344—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/34—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
- F01C1/344—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
- F01C1/3441—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation
- F01C1/3442—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation the surfaces of the inner and outer member, forming the working space, being surfaces of revolution
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C19/00—Sealing arrangements in rotary-piston machines or engines
- F01C19/08—Axially-movable sealings for working fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C20/00—Control of, monitoring of, or safety arrangements for, machines or engines
- F01C20/18—Control of, monitoring of, or safety arrangements for, machines or engines characterised by varying the volume of the working chamber
- F01C20/22—Control of, monitoring of, or safety arrangements for, machines or engines characterised by varying the volume of the working chamber by changing the eccentricity between cooperating members
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/08—Rotary pistons
- F01C21/0809—Construction of vanes or vane holders
- F01C21/0818—Vane tracking; control therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/08—Rotary pistons
- F01C21/0809—Construction of vanes or vane holders
- F01C21/0818—Vane tracking; control therefor
- F01C21/0827—Vane tracking; control therefor by mechanical means
- F01C21/0836—Vane tracking; control therefor by mechanical means comprising guiding means, e.g. cams, rollers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/08—Rotary pistons
- F01C21/0809—Construction of vanes or vane holders
- F01C21/0818—Vane tracking; control therefor
- F01C21/0854—Vane tracking; control therefor by fluid means
- F01C21/0863—Vane tracking; control therefor by fluid means the fluid being the working fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C15/00—Component parts, details or accessories of machines, pumps or pumping installations, not provided for in groups F04C2/00 - F04C14/00
- F04C15/0003—Sealing arrangements in rotary-piston machines or pumps
- F04C15/0023—Axial sealings for working fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B2730/00—Internal-combustion engines with pistons rotating or oscillating with relation to the housing
- F02B2730/01—Internal-combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber
- F02B2730/012—Internal-combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber with vanes sliding in the piston
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Rotary Pumps (AREA)
- Hydraulic Motors (AREA)
- Medicinal Preparation (AREA)
- Reciprocating Pumps (AREA)
Description
Karl Eiekmann, 2420 Isshiki, Hayama-machi, Kanagawa-Ken/JapanKarl Eiekmann, 2420 Isshiki, Hayama-machi, Kanagawa-Ken / Japan
"Hochdruckfähige Umlaufkolbenmaschine""High pressure rotary piston machine"
Die Erfindung bezieht sich auf eine hochdruckfähige Umlaufkolbenmaschine mit einer Kolbennabe und mit Kolbenschiebern, welche in Schlitzen von mit der Kolbennabe.mitumlaufenden Seitenwänden beweglich gelagert und von einem pendelfähig gelagerten Mantel umgeben sind, der sich zwischen den beiden Seitenwänden der Kolbennabe erstreckt, wobei zwischen der Kolbennabe und dem Mantel, den Seitenwänden und den Kolben- . Schiebern die Arbeitskämmern' der Maschine vorzugsweise in je· zwei diametral einander gegenüberliegenden Saug- und Druekzonen gebildet werden. Der pendelfähig gelagerte Mantel gewährleistet hierbei, daß Rundlauffehler des Umlaufkolbens zwangfrei aufgenommen werden.The invention relates to a high-pressure rotary piston machine with a piston hub and with piston valves, which rotate in slots with the piston hub Sidewalls are movably mounted and surrounded by a pendulum mounted jacket that is between the two Side walls of the piston hub extends, wherein between the piston hub and the skirt, the side walls and the piston. Slide the working chambers of the machine preferably in each two diametrically opposite suction and pressure zones are formed. The pendulum supported jacket ensures here that concentricity errors of the rotary piston were automatically recorded will.
Bei bekannten Maschinen dieser Art besteht die Gefahr, daß bei hohen Drücken, z.B. von mehreren hundert Atmosphären, die Seitenwände durch den in den Arbeitskammern wirkenden Druck auseinandergedrückt werden und dadurch hohe Spaltverluste beider-In known machines of this type there is a risk that at high pressures, for example of several hundred atmospheres, the side walls pushed apart by the pressure acting in the working chambers and thus high gap losses in both
809813/0U1809813 / 0U1
NeU6 Unterlagen (Art. "/ ä ι „.,«. <. ·.ι. ι bau: 3 des Änderungsaea. v. 4. 3 NeU6 documents (Art. "/ Ä ι"., «. <. · .Ι. Ι construction: 3 of the amendment aea. V. 4, 3
seits des Mantels entstehen, die umso höher sind, je höher der Druck in den Arbeitskammern ist. Wenn auch das Auseinanderbiegen der Seitenwände nur geringe Bruchteile eines Millimeters beträgt, können solche Spaltverluste den Wirkungsgrad der Maschine entscheidend herabsetzen. Andererseits würde ein Einpassen des Mantels mit zu geringem Zwischenspiel zwischen den beiden Seitenwänden die Reibung stark erhöhen, was vor allem insbesondere bei niedrigeren Arbeitsdrücken - wiederum zu erheblichen Wirkungsgradverlusten führen kann.arise on the side of the mantle, which are higher, the higher is the pressure in the working chambers. Even if the bending apart the side walls is only a small fraction of a millimeter, such gap losses can reduce the efficiency of the Decrease the machine significantly. On the other hand, fitting the jacket with too little interplay between the both side walls greatly increase the friction, especially at lower working pressures - in turn can lead to considerable losses in efficiency.
Aufgabe de? Erfindung ist es vor allem, solche Spalt- und Wirkungsgradverluste möglichst niedrig zu halten. Die Erfindung besteht demgemäß darin, daßTask de? Invention is, above all, such gap and To keep efficiency losses as low as possible. The invention accordingly consists in that
a) die Schütze zur Lagerung der Kolbenschieber in den Seitenwänden radial auswärts durch die Arbeitskammern gegen den Mantel abdichtende, sich axial erstreckende Ringwandungen geschlossen sind,a) the contactors for storing the piston valve in the Sidewalls that seal radially outward through the working chambers against the jacket, axially extending Ring walls are closed,
b) axial außerhalb der- Seitenwände na-eh außen geschlossene . Ausgleichskammern vorgesehen sind, die mit dem Druckmedium· zur Erzeugung von den Mediumskräften in den Arbeitskammern entgegenwirkenden Druckfeldern belieferbar sind.b) axially outside the sidewalls well closed outside. Compensating chambers are provided, which are connected to the pressure medium can be supplied to generate pressure fields counteracting the medium forces in the working chambers.
Durch die Erfindung läßt sich folgendes erreichen:The invention enables the following to be achieved:
Je nach der Höhe der einander entgegenwirkenden Drücke in den Arbeitskammern einerseits und den Ausgleichskammern andererseits läßt sich das Spiel zwischen den sich axial erstreckendenDepending on the level of the opposing pressures in the working chambers on the one hand and the equalization chambers on the other can be the game between the axially extending
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Ringwandungen der Seitenwinde und dem Mantel derart .wählen;, daß es bei geringem Druck relativ groß land bei höherem Druck relativ gering ist. Dieses ist deshalb von Vorteil, weil unter -der Voraussetzung eines gleichen Laufspieles zwischen den Ringwandungen und dem Mantel-bei geringeren Drucken der schädliche Einfluß der Reibung denjenigen der Spaltverluste überwiegt, während bei höheren Drücken die SpaltVerluste sehr stark ansteigen. Infolge der Entgegenwirkung des in den Ausgleiehskammern wirkenden Druckmediums läßt sich jedoch dieses Läufspiel in Abhängigkeit von dem Arbeitsdruck der Maschine verringern, so daß sowohl bei niedrigen als auch bei hohen Drücken ein optimaler Wirkungsgrad erreichbar ist.Select the ring walls of the cross winds and the jacket in such a way ;, that at low pressure there is relatively large land at higher pressure is relatively low. This is advantageous because, provided that the running game is the same between the Ring walls and the jacket-at lower pressures of the the harmful influence of friction on that of the gap losses predominates, while at higher pressures the gap losses very much solid rising. As a result of the counteraction of the However, pressure medium acting on equalization chambers can be this running game depending on the working pressure of the Reduce the machine so that optimum efficiency can be achieved at both low and high pressures.
Es sind zwar Maschinenbekannt, bei denen die Seitenwände des Kolbens gegen die Endflächen der Kolbennabe gedrückt werden» Das erfindungsgemäße Problem tritt jedoch bei diesen Maschinen nicht auf, da der Mantel einen Bestandteil des Gehäuses bildet bzw. mit den dort vorgesehenen Gehäusedeekeln fest verbunden ist und keine Spaltverluste seitlich am Mantel vorbei entstehen können.There are machines known in which the side walls of the Piston are pressed against the end faces of the piston hub » The problem according to the invention does not arise in these machines, however, since the jacket forms part of the housing or firmly connected to the housing covers provided there and no gap losses occur laterally past the jacket can.
Zur pendelfähigen Lagerung des Mantels kann dieser mit balliger Oberfläche versehen oder mittels einer Kardanringaufhängung in· einem Tragteil aufgehängt sein.For pendulum mounting of the jacket, it can be provided with a spherical surface or by means of a cardan ring suspension be suspended in a supporting part.
Um trotz der pendelfähigen Lagerung des Mantels das Arbeitsmedium, den Arbeitskammern in einfacheriweise von einem feststehenden Gehäuse zuzuführen bzw. zu diesem abzuführen, sind vor-In order to supply the working medium to the working chambers in a simple manner from a stationary housing or to remove it, despite the pendulum bearing of the jacket, it is necessary to
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teilhaft Mittel zwischengeschaltet, welche die Pendelbewegung des Mantels relativ zum feststehenden Gehäuse zulassen. Hierzu können den Mantel bzw. einen Kardanring durchsetzende flexible Zu- oder Abführungen vorgesehen sein, z.B. in Form von den Kardanring durchsetzenden, am Maschinengehäuse bzw. am Mantel sphärisch abgestützten Buchsen oder Leitungsteilen.partly means interposed which allow the pendulum movement of the shell relative to the fixed housing. For this For example, flexible inlets or outlets penetrating the jacket or a cardan ring can be provided, e.g. in the form of the Gimbal penetrating, on the machine housing or on the jacket spherically supported sockets or line parts.
In der Zeichnung sind zwei'Ausführungsbeispiele der Erfindung schematiseh dargestellt. Es zeigenIn the drawing are two embodiments of the invention shown schematically. Show it
Pig. 1 einen Längsschnitt durch das erste Ausführungsbeispiel nach Linie I-I der Fig. 2,Pig. 1 shows a longitudinal section through the first embodiment according to line I-I of FIG. 2,
Fig. 2 einen Querschnitt nach Linie II-II der Fig. 1 und Fig. 3 einen der Fig. 2 entsprechenden Querschnitt durch .das zweite Äusführungsbeispiel.FIG. 2 shows a cross section along line II-II of FIGS. 1 and 3 shows a cross section corresponding to FIG. 2 through the second embodiment.
Im Ausführungsbeispiel nach Fig. 1 und 2 ist auf der Umlaufkolbenwelle 40 die Kolbennabe 4l fest aufgesetzt. Sie wird Tdurch einen exzentrisch zum Umlaufkolben radial verstellbaren Mantel 44 umgeben. Fest mit ihm verbunden sind ferner axial beiderseits angeordnete, zusammen mit ihm mitumlaufende Seitenwände 46f, 46", welche mit radialen Schlitzen 35', 35" zur Aufnahme der axialen Enden der Kolbenschieber 45 versehen sind.In the exemplary embodiment according to FIGS. 1 and 2, the piston hub 4l is firmly placed on the rotating piston shaft 40. It is surrounded by a casing 44 which can be adjusted radially eccentrically to the rotary piston. Furthermore, side walls 46 f , 46 ″ which are axially arranged on both sides and rotate with it and which are provided with radial slots 35 ′, 35 ″ for receiving the axial ends of the piston slides 45 are firmly connected to it.
Auf der axial äußeren Seite stützen sich die Seitenwände 46 %, 46" gegen Verschlußhauben 39 bzw. 38 ab, von denen die VerschluS-haube 39 einen mit der Welle 40 fest verbundenen Flanschteil bildet, während die Verschlußhaube 38 verschiebbar auf der Welle 40 gelagert ist. Die Teile 38 j 46", 41, 46' und 39 werden durchOn the axially outer side, the side walls 46 % , 46 ″ are supported against closure hoods 39 and 38, of which the closure hood 39 forms a flange part firmly connected to the shaft 40, while the closure hood 38 is slidably mounted on the shaft 40 The parts 38 j 46 ", 41, 46 'and 39 are through
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Spannbolzen J>6 axial zusammengehalten und zugleich, gegen Drehen mit Bezug auf die Welle 40 gesichert.Clamping pin J> 6 held together axially and at the same time secured against turning with respect to the shaft 40.
Wie aus Fig. 2 ersichtlich, weist zum Zwecke des Ausgleichs der radialen Druckbelastung die Umlaufkolbenmaschine diametral gegenüberliegend je zwei Saugzonen und Druckzonen auf. Diese werden durch die Innenfläche des Mantels 44 bestimmt, welche zwei etwa halbmondförmige Räume bilden, die durch die Kolbenschieber 45 je In eine als Saugraum wirkende Arbeitskammer 42 und in eine als Druckraum wirkende Arbeitskammer 43 unterteilt werden. Die Zu- und Abführung des Mediums zu und von den Arbeitskammern erfolgt durch die Kanäle 4?1 bzw. 47", die durch den Mantel 44, einen geteilten Lagerring 48 und ein als Tragteil dienendes Maschinengehäuse 49 durchgeführt sind. Dichtungen 48' und 49f können an den Übergangsstellen vorgesehen sein.As can be seen from FIG. 2, for the purpose of compensating for the radial pressure load, the rotary piston machine has two suction zones and two pressure zones diametrically opposite each other. These are determined by the inner surface of the jacket 44, which form two approximately crescent-shaped spaces, which are each divided by the piston slide 45 into a working chamber 42 acting as a suction chamber and a working chamber 43 acting as a pressure chamber. The supply and removal of the medium to and from the working chambers takes place through channels 4? 1 and 47 ″, which are passed through the jacket 44, a split bearing ring 48 and a machine housing 49 serving as a support part. Seals 48 ′ and 49 f can be provided at the transition points.
Um einen optimalen Spalt zwischen dem Mantel 44 und den Kolbenschiebern 45 zu erhalten, sind die radial äußeren Enden der Schlitze 35f bzw. 35" auf gleichem oder etwas kleinerem Radius als der die Arbeitskammern 42, 4j5 begrenzende Innenradius des Mantels angeordnet. Bei entsprechender Bemessung der Seitenwände 46 % 9 46" bzw. der von Ihnen gegebenenfalls gesondert hergestellten, die Schlitze 35 V, 35" radial außen begrenzenden Ringwandungen dieser Seitenwände dehnen sich diese bei Innendruck, so daß sich das Spiel zwischen dem Mantel 44 und den Kolben-Schiebern 45 verringert.In order to obtain an optimal gap between the jacket 44 and the piston valves 45, the radially outer ends of the slots 35 f or 35 "are arranged on the same or slightly smaller radius than the inner radius of the jacket delimiting the working chambers 42, 4j5. With appropriate dimensioning of the side walls 46 % 9 46 "or the ring walls of these side walls which you may have produced separately and which delimit the slots 35 V, 35" radially on the outside, they expand under internal pressure, so that the play between the jacket 44 and the piston slides 45 decreased.
809813/0141809813/0141
In der axial äußeren Verschlußhaube 38 ist des weiteren eine ' ringförmige Ausgleichskammer 34 vorgesehen, welche durch einen Ringkolben 33 abgeschlossen wird, der sich über das benachbarte Lager des Gehäuses 49 am Sprengring 37 und damit an der Welle abstützt. Die Ausgleichskammer kann mit Druckmittel beliefert werden, und zwar derart, daß sie bei niedrigem Druck in den Arbeitskammern ebenfalls niedrigen Druck und bei hohem Druck in den Arbeitskammern ebenfalls hohen Druck erhalten, fiierdurch kann erreicht werden, daß das Spiel 32', 32", das in der Zeichnung übertrieben groß dargestellt ist und höchstens nur 0,1, meist aber 0,01 oder 0,001 mm beträgt, eine bestimmte Größe nicht übersteigt. Dadurch kann erreicht werden, daß bei niedrigem Druck in den Arbeitskammern zur Erzielung einer geringen Reibung das Spiel relativ groß, bei hohem Druck in den Arbeitskanmern zur Vermeidung von Druckmittelverlusten dagegen relativ klein ist.In the axially outer closure hood 38 is also a ' annular compensation chamber 34 is provided, which by a Ring piston 33 is closed, which is located on the adjacent bearing of the housing 49 on the snap ring 37 and thus on the shaft supports. The compensation chamber can be supplied with pressure medium, in such a way that it is at low pressure in the Working chambers also receive low pressure and at high pressure in the working chambers also high pressure, fiier durch can be achieved that the game 32 ', 32 "shown in the drawing is shown exaggeratedly large and at most only 0.1, but mostly 0.01 or 0.001 mm, a certain size does not exceed. In this way it can be achieved that at low pressure in the working chambers to achieve a low pressure Friction the game relatively large, with high pressure in the working chambers to avoid pressure medium losses, however, is relatively small.
In Fig. 3 ist beispielsweise" gezeigt, wie einflekibler Druckmitteldurchtritt bei Beaufschlagung des ümlaufkolbens von außen vom Gehäuse her in die Arbeitskammern möglich ist, um die Bewegungsfähigkeit des Mantels zur Befolgung von Umlauffehlern nicht durch starre Leitungen einzuschränken. Am Gewinde 88 ist der Gehäuseanschluß mit dem Kanal 87 vorgesehen. Auf der planen Backfläche 94 des Anschlusses am Gehäuse 50 liegt ein Ring 86 mit planer Fläche auf, der auf der anderen Seite eine sphärische Fläche hat, in die die Hülse 85 mit ihrer sphärischen Rückwand eingreift." Entsprechend hat der Mantel 54 ein Kanalfenster 8l mit einer planen Auflagefläche 82. Darauf liegt wiederum einIn Fig. 3, for example, "shows how a flexible pressure medium passage when the overflow piston is acted upon from the outside of the housing into the working chambers, it is possible to increase the mobility of the jacket must not be restricted by rigid lines in order to comply with orbital errors. At the thread 88 is the Housing connection with channel 87 is provided. A ring 86 lies on the flat baking surface 94 of the connection on the housing 50 with a flat surface, which on the other hand has a spherical surface into which the sleeve 85 with its spherical rear wall engages. "Correspondingly, the jacket 54 has a channel window 8l with a planar support surface 82. This is in turn a
8098 13/0 UI8098 13/0 UI
Ring 80 mit einer planen Fläche und einer sphärischen Endfläche am anderen Ende., in dem wiederum eine Hülse 8j5 mit sphärischer Rückwand liegt» Die Ringe 80 und 86 können gleich sein. Die Hülsen 8.5 und 85 werden praktischerweise teleskopartig ineinandergesteckt, so daß sie gegenseitig dicht sind. Eine oder mehrere Federn 84 können die Hülsen 83 und 85 in ihre rückwärtigen sphärischen Sitze drücken. Der Durchmesser der ineinandergesteckten Abschnitte der Buchsen 83 und 85 ist größer als der Innendurchmesser der planen und der sphärischen Dichtungsflachen,-so daß ein Druck vom Medium her auf die Buchsen in Richtung ihrer rückwärtigen Dichtflächen verbleibt. Wenn die Reaktionsdruckfläche aus der Arbeitskammer gleich groß, aber entgegengesetzt gerichtet ist wie der Druckmitteldruck'aus den Buchsen 8j5 und 85, dann sind die Druckmittelkräfte aus der flexiblen Leitung auf den Mantel 54 aufgehoben.Ring 80 with a flat surface and a spherical end surface at the other end., in which again a sleeve 8j5 with spherical The rear wall is »The rings 80 and 86 can be the same. The pods 8.5 and 85 are conveniently nested telescopically so that they are mutually sealed. One or more Springs 84 can the sleeves 83 and 85 in their rear press spherical seats. The diameter of the nested portions of the sockets 83 and 85 is greater than that Inner diameter of the flat and spherical sealing surfaces, -so that a pressure from the medium remains on the bushes in the direction of their rear sealing surfaces. If the Reaction pressure area from the working chamber is the same, but is directed in the opposite direction as the pressure medium pressure from the Bushings 8j5 and 85, then the pressure medium forces are from the flexible line on the jacket 54 lifted.
Man kann auch umgekehrterweise eine Verbindungsbuchse mit sphärischen Flächen vorsehen., und die Buchsen in den Ansenlußbohrungen gleiten lassen, und ,dazwischen Ringe, wie sie bei und 86 gezeigt sind, einlegen. Schließlich kann man durch eine Ringkombination flexibel abdichten, oder auch andere bekannte flexible Dichtungen zwischen Gehäuse 50 und Mantel 54 anordnen. Die flexiblen Dichtungen können durch Ausnehmungen 79 im Kardanring 55 geführt werden. Die durch die flexiblen Dichtungen auf den Kapselring ausgeübten verbleibenden Kräfte, in Rotationsrichtung oder entgegengesetzt dazu, können durch Druekmittelbalancefeider 89 und 90 im Kardanring, im Mantel, im Gehäuse, oder an den Kardanringbolzen ganz oder teilweise ausgeglichenYou can also use a connection socket in reverse Provide spherical surfaces., and the sockets in the Ansenlußbohrungen Let it slide and insert rings between them as shown at and 86. After all, you can go through a Seal the ring combination flexibly, or arrange other known flexible seals between the housing 50 and the jacket 54. The flexible seals can through recesses 79 in the cardan ring 55 are performed. The remaining forces exerted on the capsule ring by the flexible seals, in the direction of rotation or in the opposite direction, can be controlled by means of pressure balance springs 89 and 90 in the cardan ring, in the jacket, in the housing, or fully or partially balanced on the gimbal ring bolts
werden.will.
BADBATH
8098 13/0 Ui8098 13/0 Ui
Es ist selbstverständlich auch möglich, Einzelteile derIt is of course also possible to use individual parts of the
Kolbens chieber
Maschine wie die FKJgSQ? od.dgl. in einer abgeänderten Ausführungsform
vorzusehen* So können die Kolbenschieber z.B. statt in den Schlitzen der Kolbennabe dicht geführt zu werden
auch mit Spiel in diesen Schlitzen gleiten, derart, daß sie durch den Druck des Arbeitsmediums in den Arbeitskammern
einseitig gegen die Schlitzwände gedrückt werden und dadurch eine wirksame Abdichtung der Kammern gegeneinander bewirken.
Auch können die Kolbenschieber mit gelenkig oder fest mit ihnen verbundenen Gleitschuhen am Innenumfang des Mantels
gleiten.Piston valve
Machine like the FKJgSQ? or the like. to be provided in a modified embodiment cause effective sealing of the chambers against each other. The piston slides can also slide on the inner circumference of the casing with sliding shoes connected to them in an articulated or fixed manner.
Die Erfindung wird nur in der Gesamtheit aller Merkmale des Patentanspruchs 1 gesehen. Für die Merkmale der Unteransprüche wird kein selbständiger Schutz beansprucht.The invention is only in the entirety of all features of the Claim 1 seen. No independent protection is claimed for the features of the subclaims.
809813/0-U1809813/0-U1
Claims (4)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2923859 | 1959-09-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE1401400A1 true DE1401400A1 (en) | 1968-12-19 |
Family
ID=12270640
Family Applications (5)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19601401396 Pending DE1401396A1 (en) | 1959-09-11 | 1960-04-02 | High-pressure rotary vane machines, in particular hydraulic pumps and hydraulic motors, gas or steam engines and internal combustion engines of the vane cell type |
DE19601551103 Pending DE1551103A1 (en) | 1959-09-11 | 1960-04-02 | Rotary piston machine with piston valves guided in slots in the piston hub |
DE19601401400 Pending DE1401400A1 (en) | 1959-09-11 | 1960-04-02 | High pressure rotary piston machine |
DE19601551102 Pending DE1551102A1 (en) | 1959-09-11 | 1960-04-02 | Rotary piston machine |
DE19611401399 Pending DE1401399A1 (en) | 1959-09-11 | 1961-08-02 | High pressure rotary wing machine with a pressure compensation device |
Family Applications Before (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19601401396 Pending DE1401396A1 (en) | 1959-09-11 | 1960-04-02 | High-pressure rotary vane machines, in particular hydraulic pumps and hydraulic motors, gas or steam engines and internal combustion engines of the vane cell type |
DE19601551103 Pending DE1551103A1 (en) | 1959-09-11 | 1960-04-02 | Rotary piston machine with piston valves guided in slots in the piston hub |
Family Applications After (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19601551102 Pending DE1551102A1 (en) | 1959-09-11 | 1960-04-02 | Rotary piston machine |
DE19611401399 Pending DE1401399A1 (en) | 1959-09-11 | 1961-08-02 | High pressure rotary wing machine with a pressure compensation device |
Country Status (2)
Country | Link |
---|---|
US (2) | US3256831A (en) |
DE (5) | DE1401396A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USD957643S1 (en) | 2009-02-03 | 2022-07-12 | Abbott Diabetes Care Inc. | Analyte sensor device |
USD980986S1 (en) | 2015-05-14 | 2023-03-14 | Abbott Diabetes Care Inc. | Analyte sensor inserter |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3417706A (en) * | 1963-12-05 | 1968-12-24 | Eickmann Karl | Slots-containing bodies in fluid handling devices |
US3516769A (en) * | 1967-02-10 | 1970-06-23 | Martti Korhonen | Rotary vane hydraulic motor |
US3426735A (en) * | 1967-07-26 | 1969-02-11 | Donald A Kelly | Compound rotary engines |
US3455245A (en) * | 1967-11-16 | 1969-07-15 | Sperry Rand Corp | Power transmission |
AT329341B (en) * | 1970-07-15 | 1976-05-10 | Eickmann Karl | HYDRAULIC OR PNEUMATICALLY OPERATED VENTILATION MACHINE |
US3723033A (en) * | 1971-07-14 | 1973-03-27 | Impact Inc | Rotary power device |
US4028022A (en) * | 1972-09-20 | 1977-06-07 | Nissan Motor Co., Ltd. | Oil seal assembly |
NL8100705A (en) * | 1981-02-13 | 1982-09-01 | Abraham De Kok | ROTARY SHOT PUMP OR MOTOR. |
US4619594A (en) * | 1985-05-13 | 1986-10-28 | Lear Siegler, Inc. | Stackable rotary vane pump with improved volumetric efficiency |
DE3624532A1 (en) * | 1986-07-19 | 1988-02-04 | Pierburg Gmbh | FLUEGELZELLEN- OR INNER AND OUTDOOR PUMP |
US5033265A (en) * | 1989-03-08 | 1991-07-23 | Sundstrand Corporation | Coaxial hydraulic actuator system |
EP0399387B1 (en) * | 1989-05-24 | 1992-09-30 | Vickers Incorporated | Rotary vane machine |
US5217357A (en) * | 1992-09-10 | 1993-06-08 | Welch Robert E | Rotary vane pump with removable particulate collection chamber |
CN104271960A (en) * | 2012-03-01 | 2015-01-07 | 托拉德机械有限公司 | Rotor assembly for rotary compressor |
US9617994B2 (en) | 2014-04-18 | 2017-04-11 | Delaware Capital Formation, Inc. | Pump with mechanical seal assembly |
EP3109473B1 (en) * | 2015-06-26 | 2021-03-10 | Danfoss A/S | Vane cell machine |
EP3109468B1 (en) | 2015-06-26 | 2022-06-29 | Danfoss A/S | Hydraulic machine |
EP3109470B1 (en) | 2015-06-26 | 2019-03-27 | Danfoss A/S | Hydraulic machine arrangement |
WO2017048571A1 (en) | 2015-09-14 | 2017-03-23 | Torad Engineering Llc | Multi-vane impeller device |
CN107120274B (en) * | 2017-06-28 | 2019-07-30 | 广西大学 | Rotary blade type compressor |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US810062A (en) * | 1905-06-13 | 1906-01-16 | Gustaf A L Lind | Rotary engine. |
US1001162A (en) * | 1910-06-13 | 1911-08-22 | Fred A Parsons | Combined rotary engine and pump. |
US2098652A (en) * | 1935-08-13 | 1937-11-09 | Buckbee John Calvin | Rotary pump |
US2371081A (en) * | 1941-02-06 | 1945-03-06 | Hydraulic Dev Corp Inc | Vane pump |
US2386873A (en) * | 1943-08-16 | 1945-10-16 | Mercier Jean | Duplex elastic seal |
US2654325A (en) * | 1950-08-11 | 1953-10-06 | Borg Warner | Gear type pump with pressure loaded bushing and wear insert element |
US2778598A (en) * | 1953-07-20 | 1957-01-22 | Exxon Research Engineering Co | Valve with pressure sealing device |
US3011803A (en) * | 1958-01-31 | 1961-12-05 | Dumont Aviat Associates | Swivel conduit joint |
US2962314A (en) * | 1958-07-09 | 1960-11-29 | Mcdowell Mfg Co | Gasket |
-
1960
- 1960-04-02 DE DE19601401396 patent/DE1401396A1/en active Pending
- 1960-04-02 DE DE19601551103 patent/DE1551103A1/en active Pending
- 1960-04-02 DE DE19601401400 patent/DE1401400A1/en active Pending
- 1960-04-02 DE DE19601551102 patent/DE1551102A1/en active Pending
-
1961
- 1961-08-02 DE DE19611401399 patent/DE1401399A1/en active Pending
-
1962
- 1962-09-06 US US221909A patent/US3256831A/en not_active Expired - Lifetime
-
1965
- 1965-02-11 US US436709A patent/US3246574A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USD957643S1 (en) | 2009-02-03 | 2022-07-12 | Abbott Diabetes Care Inc. | Analyte sensor device |
USD980986S1 (en) | 2015-05-14 | 2023-03-14 | Abbott Diabetes Care Inc. | Analyte sensor inserter |
Also Published As
Publication number | Publication date |
---|---|
DE1551103A1 (en) | 1970-02-12 |
US3256831A (en) | 1966-06-21 |
DE1401399A1 (en) | 1968-10-17 |
DE1401396A1 (en) | 1969-03-20 |
DE1551102A1 (en) | 1970-02-12 |
US3246574A (en) | 1966-04-19 |
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