EP0214164B1 - Machine a deplacement positif, notamment pompe - Google Patents
Machine a deplacement positif, notamment pompe Download PDFInfo
- Publication number
- EP0214164B1 EP0214164B1 EP86901030A EP86901030A EP0214164B1 EP 0214164 B1 EP0214164 B1 EP 0214164B1 EP 86901030 A EP86901030 A EP 86901030A EP 86901030 A EP86901030 A EP 86901030A EP 0214164 B1 EP0214164 B1 EP 0214164B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- displacement
- chambers
- vanes
- displacement chambers
- machine according
- 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
Links
Images
Classifications
-
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C17/00—Arrangements for drive of co-operating members, e.g. for rotary piston and casing
-
- 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
- F04C15/0042—Systems for the equilibration of forces acting on the machines or pump
- F04C15/0046—Internal leakage control
-
- 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
- F04C15/0057—Driving elements, brakes, couplings, transmission specially adapted for machines or pumps
- F04C15/0061—Means for transmitting movement from the prime mover to driven parts of the pump, e.g. clutches, couplings, transmissions
- F04C15/0065—Means for transmitting movement from the prime mover to driven parts of the pump, e.g. clutches, couplings, transmissions for eccentric movement
-
- 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
- F04C2/02—Rotary-piston machines or pumps of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
- F04C2/04—Rotary-piston machines or pumps of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents of internal axis type
Definitions
- the present invention relates to a displacement machine, in particular a displacement pump, with displacement chambers, in each of which a displacement vane engages, the displacement chamber and displacement vane being able to be set in cyclical relative movement, during which the displacement vane with outer and inner sealing surfaces sealingly follow the walls of the displacement chamber with a common central drive , and wherein inlet and outlet channels for the medium flowing through the machine open into the displacement chambers.
- Machines of this type are known, for example, from German Patent 22 30 773.
- the drive takes place by means of rigidly acting eccentrics or cranks.
- the displacement chambers and vanes are shaped in such a way that they only engage sealingly over a section of around 270 ° of the relative movement. It is therefore necessary to connect at least two displacement chambers with overlapping sealing or delivery areas in series in order to achieve even delivery without leaks.
- the aim of the present invention is to provide a machine which allows all the disadvantages mentioned to be avoided.
- a solution is described in the characterizing part of claim 1.
- the radially adjustable member which generates a driving force with a radial and tangential component, acts on the driven carrier in such a way that the displacer vanes and chambers always remain in sealing contact.
- Non-uniformities of the relative movement i.e. Deviations from the circular shape compensates for the radially adjustable link, which acts resilient, wedge-like or otherwise non-positive, but not positive.
- the direction of the driving force can be selected so that the driven carrier is always supported in a certain position in a stable position by the mutual contact points of the displacement vanes and chambers arranged in an outer ring and cannot tilt.
- the flexible drive which allows a not strictly circular relative movement, accordingly allows greater freedom in the design of the shape of the displacement chambers and wings, in particular their design in such a way that each chamber seals for itself over at least 360 ° of the relative movement.
- Each chamber can therefore contribute directly to the funding, without series connection with another.
- the drive preferably consists of a driver fastened on the drive shaft, which acts with a driving surface inclined with respect to the radial direction on a bushing which in turn is mounted on a pin of the carrier to be driven.
- This arrangement has the advantage that the direction of the driving force changes when worn in the sense that the radial component of the force decreases somewhat, which is itself desirable. So that the displacement chambers and vanes expand outwards, there are particularly favorable conditions for stable operation despite the non-positively engaging drive force on one line, and optimal use of the available space.
- Pumps or compressors with a correspondingly constructed, radially adjustable or night-adjustable drive are known, but not in combination with measures for stable operation and optimal use of space with a plurality of displacement chambers (FR-A-825 643, FR-A-1 095 539, GB-A-17,672 / 1909).
- the shaft 5 has a thickened inner end 7 which is milled so that a flat driving surface 7b is formed on a projecting segment 7a.
- the segment 7a engages in a cylindrical recess 8 of a plate-shaped carrier 9, where its driving surface 7b rests on a flattened point of a bush 7c.
- the sleeve 7c is mounted on a pin 9a of the carrier 9.
- This plate-shaped carrier 9 consists of one piece with ribs Migen displacement wings 10, which engage in groove-shaped displacement chambers 11, which are formed in a further plate-shaped carrier 12.
- the displacement chambers 11 are surrounded by raised ribs 121 of the carrier 12.
- a recess 122 is created within the ribs.
- the end faces of both the ribs 121 and the displacer wing 10 are slightly convexly cambered to cover any large area between the parts 9 and 12 and thus to avoid friction.
- the width of the ribs 121 is preferably less than twice the eccentricity of the movement of the carrier 9, which creates favorable conditions for solids that get between the parts 9 and 12 to be worked out effectively and quickly.
- the two supports 9 and 12 can be made of plastic as simple molded parts.
- the rear wall of the pump forms a plate 13, which is designed as a connecting plate by forming connecting channels 14 and 15 on the inside thereof, which inlet and outlet channels 19 and 20 of the displacement chambers 11 are underneath and with an inlet opening 16 and an outlet opening 17 connect.
- FIG. 2 shows the special shape and arrangement of the existing displacement chambers and displacement blades
- FIG. 3 shows the geometric shape of these displacement chambers and displacement blades in more detail.
- Four displacer assemblies 10 are provided on the carrier 9 in a centrally symmetrical arrangement, which engage in four displacer chambers 11 arranged in a correspondingly centrally symmetrical manner in the plate-shaped carrier 12.
- This centrally symmetrical arrangement of four displacement wings or displacement chambers of triangular or heart-shaped shape not only results in a very advantageous use of space on the carriers 9 and 12, but also a high positional stability of the movable carrier 9, when it is driven by the punctiform or linear support of the driving roller 7 in the recess 8.
- a center line of symmetry M shown in FIG. 3 of the displacement wing and the associated displacement chamber is composed of two longer sections M b and M e each with a large radius of curvature R and with centers of curvature B or C and subsequent shorter sections m a , m b and m e with small radii of curvature r and centers of curvature A, B and C.
- the center lines of the end parts above the sections m b and m e either run with a large radius of curvature and center of curvature A or with a small radius of curvature and centers of curvature B or C or according to an intervening curve, as will be explained in more detail.
- the flanks of each displacement wing 10 and each displacement chamber 11 run according to corresponding curves, namely with large or small radii and corresponding centers of curvature A, B and C as can be seen from FIG. 3. It is important here that there are no discontinuities at the transitions between the parts with a small radius of curvature and the parts with a large radius of curvature, that is, the tags at the adjoining curve parts should merge into one another without a jump.
- each of these chamber extensions 18 there is an inlet opening 19 or one penetrating the carrier 12 Outlet opening 20.
- the inlet openings 19 are located radially within the outlet bores 20.
- all inlet openings 19 are connected to one another and to the inlet 16 of the pump through the annular channel 14. Accordingly, all outlet openings 20 are connected to the ring channel 15 and, via the same, to the outlet 17 of the pump.
- the four displacement chambers are therefore connected in parallel and work in parallel, which among other things has a favorable effect on the pulsation of the entire conveyor.
- the carrier 9 is pressed against the carrier 12 by means of helical springs 21, which are supported in recesses in the carrier 9 or the bearing flange 2.
- the carrier 9 is freely movable in an intermediate pressure mer 22.
- this intermediate pressure chamber or compensation chamber 22 occurs during the running of the pump through the gap 23 between the abutting end faces of the carrier 9 and 12 and through a central opening of the carrier 9 under the pressure built up in the displacement chambers 11, a portion of the medium conveyed and collects in the intermediate pressure chamber 22, which fills with this medium. From this intermediate pressure chamber 22, the medium can then pass through the annular gap 24 between the bearing bush 4 and the crankshaft 5 to the outside into the annular space 25 closed by the seal 6.
- the medium can flow back to the pump inlet 16 to the unpressurized suction side through a channel 26, in which an orifice 27 can be installed.
- the channel 26 can be a molded tube. It has been shown that the correct dimensioning of the upstream pressure generated by the springs 21 is an essential prerequisite for the stable operation of the pump.
- the form should, for example, be 1/4 to 1/2 of the total pressure, but should be dimensioned so that the drive motor can start after breaks.
- the carrier 9 is driven by the simple mechanism consisting of the shaft 5, which is set in rotation, its driver segment 7, the bushing 7c and the pin 9a.
- the situation is shown on a larger scale in FIG. 4. Again, it is assumed there that the carrier 9 is in the uppermost symmetrical position, ie the axis of the cylindrical recess 8 or the pin 9a is at point O, which is correspondingly designated in FIG. 2, and during a cyclical movement move this axis along a circle with the radius r e .
- the carrier 9 can therefore perform an eccentric translational movement with the eccentric radius r e with respect to the axis of the shaft 5.
- the driving surface 7b of the segment 7a is inclined relative to the connecting line between the axis 5 and the pin 9a by, for example, 15 to 20 °.
- the acting force F N is perpendicular to the surface 7b, as shown in FIG. 4 . This force can be broken down into a tangential force F T directed in the current direction of movement of the carrier 9 and a radial force F R acting at right angles thereto.
- the predominant tangential force F T in the illustrated conditions causes entrainment of the carrier 9 in the respective tangential direction or circumferential direction and thus brings about the cyclical translational circular movement of the carrier 9 and its displacer vanes 10.
- the radial force F R ensures that the displacer vanes 10 rest securely in the Displacement chambers 11. It can be shown, and tests confirm, that in the arrangement and design of the displacement wings and chambers shown, relatively low resulting hydrostatic pressures act on the carrier 9 in the radial direction.
- the radial component of the driving force F N therefore has an effect, in particular, when the displacer vanes are applied radially outward in the displacer chambers.
- This drive has a quasi-elastic effect or adjusts itself in every direction, so that the above-mentioned optimal conditions are still met even if certain wear and tear has occurred.
- Any wear in the displacement chambers and on the displacement vanes leads to the carrier 9 being displaced somewhat outwards, that is to say that its pin 9a describes a circular movement of somewhat larger diameter.
- the bush moves slightly outwards on the driving surface 7b.
- the drive conditions, in particular the direction of the force F N change only insignificantly. This is due, among other things, to the fact that the flat bearing surfaces of the segment 7a and the bushing 7c are practically not subject to wear.
- the wear in the drive itself can have the effect that the bore of the bushing 7c is somewhat worked off at the location closest to the driving surface 7b, but the location worn in this way also has a radius corresponding to the pin 9a, which may be evenly worn, So that good storage and power transmission is always guaranteed.
- the displacement wing initially moves horizontally to the right in the displacement chamber located at the top in FIG. 2. After a quarter turn, it reaches the position as shown in the chamber on the left in FIG. 2. It can be seen that during this movement the volume between the outer surface of the displacer wing 10 and the outer surface of the displacer chamber 11 has been reduced and the medium has been displaced in the direction of the outlet opening 20. In contrast, the volume between the inner surface of the displacement wing and the opposite the area of the displacement chamber on the inlet side increased significantly, so that 19 medium is sucked in through the inlet opening. After half a turn the position is reached, as shown in Fig. 2 below.
- pulsations in the order of 1% of the delivery rate can be achieved.
- a certain pulsation which is smaller than the leakage current and which mainly affects it is even desirable in order to rinse out any abrasion particles in the capillary gap between the end faces of the supports 9 and 12 and the gap filled with spring medium does not become too small because of the otherwise extremely high shear forces allow.
- the design and arrangement of the displacement chamber and vanes shown allow very good use of space or, in other words, a high specific delivery rate and output of the pump.
- the respective active piston widths are entered in FIG. 2 and designated KB.
- the total active piston width is larger than the diameter of a circle surrounding the delivery chambers.
- a compromise between the need to achieve a good seal and the need to avoid high friction is not only at the contact surface or in the gap 23 between the supports 9 and 12, but also between the end faces of the displacer vanes 10 and the opposite base surfaces of the displacer chambers 11 to find. Tests have shown that perfectly flat surfaces are unfavorable. A final shape according to FIG. 6 is more desirable. This means that the end face of the displacement wing should be slightly cambered so that there is practically only line contact between this end face and the base surface 11 of the displacement chamber 11.
- This shape can be achieved automatically in the above-described fine machining with an abrasive or lapping agent, namely that the displacer blades 10 are slightly deformed during lapping with an alternately opposite direction of rotation and are thus processed somewhat more strongly on the sides.
- the cambered shape can also be specified for the blank.
- the profile of the displacer ribs 10 and displacer chambers 11 can have a slightly trapezoidal shape with rounded corners in order to achieve better demolding from pressing or injection molding tools.
- FIG. 7 shows an embodiment variant in which the radial force component and adjustability are generated by means of an elastic section 5a of the shaft 5 in the form of a lamellar thinned section via a roller 71.
- a compression spring acting radially on a driver could accordingly be provided.
- the relative direction of movement between the two parts must make at least one full rotation through 360 ° with these tangents.
- the piston cross-section that is decisive for the delivery rate is the product of the piston width as a result of the respective distance between these tangents and the invariable immersion depth of the displacer vane in the displacement chamber.
- the respective piston stroke corresponds to the product of the angle of rotation and eccentricity, ie per revolution r e ' 2 n.
- the shape of the displacement chamber depends on the shape of the displacement wing and the radius of the eccentric drive.
- the displacement chambers each have an inlet and an outlet channel and are therefore connected in parallel as described above if a relatively low delivery pressure is desired with a large delivery rate, as is the case, for example, with one Circulation pump is the case. If higher pressures and a lower amount of feed are desired, two out of four chambers can be connected in series crosswise.
- FIG. 8 corresponds to FIG. 3 and shows an embodiment variant of the shape of the displacer wing 10 and the displacer chamber 11. While according to FIG. 3 the end sections m b and m e consistently have the small radius of curvature r, these end sections according to FIG. 8 are each in each case a part mb extending over 60 ° or never with a radius of curvature r, a middle part Mb and Mc with a radius of curvature R and a short end part m'b and m'c with a radius of curvature r. The ends of the displacement chambers 11 are in this case also moved closer together and they open directly into oval inlet and outlet openings 19 'and 20'.
- the displacement chamber 11 is surrounded on the inside by a rib 121, the width of which, according to the rule mentioned above, is less than twice the eccentric stroke right, and within this rib there is a flat recess 122, in the area of which there is an opening 35 which is similar to that with the suction side or pressure side of the pump, i.e. with an opening 19 'or with an annular channel connecting the openings 20' Channels 14 and 15 can be connected.
- Triangular, closed pockets 124 are formed by outer, circumferential ribs 123 together with the delimiting ribs 121 of the displacement chamber. During operation of the pump, a certain intermediate pressure builds up in these pockets between the supports 9 and 12, which can be determined, if necessary, by relief passages with a defined flow resistance. The liquid cushions in the pockets 124 effectively prevent instabilities of the aforementioned type and thus contribute to the smooth running of the machine.
- the drive can also be designed such that a roller corresponding to the roller 71 according to FIG. 7 is mounted on a rigid eccentric of the drive shaft and acts on a cylindrical driving surface of the carrier 9, the eccentricity of the movement of the roller being greater than the radius of the cyclical relative movement of the carrier 9.
- a roller corresponding to the roller 71 according to FIG. 7 is mounted on a rigid eccentric of the drive shaft and acts on a cylindrical driving surface of the carrier 9, the eccentricity of the movement of the roller being greater than the radius of the cyclical relative movement of the carrier 9.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Details And Applications Of Rotary Liquid Pumps (AREA)
- Rotary Pumps (AREA)
Abstract
Claims (9)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH894/85 | 1985-02-27 | ||
CH89485 | 1985-02-27 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0214164A1 EP0214164A1 (fr) | 1987-03-18 |
EP0214164B1 true EP0214164B1 (fr) | 1990-05-23 |
Family
ID=4197655
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP86901030A Expired - Lifetime EP0214164B1 (fr) | 1985-02-27 | 1986-02-21 | Machine a deplacement positif, notamment pompe |
Country Status (6)
Country | Link |
---|---|
US (1) | US4789315A (fr) |
EP (1) | EP0214164B1 (fr) |
JP (1) | JP2771160B2 (fr) |
BR (1) | BR8605494A (fr) |
DE (1) | DE3671503D1 (fr) |
WO (1) | WO1986005241A1 (fr) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5180336A (en) * | 1988-09-20 | 1993-01-19 | Gutag Innovations Ag | Oldham coupling |
DE58901166D1 (de) * | 1988-09-20 | 1992-05-21 | Gutag Innovations Ag | Taumelantrieb fuer ein translatorisch bewegtes bauteil. |
DE58900498D1 (de) * | 1988-09-20 | 1992-01-09 | Gutag Innovations Ag | Verdraengermaschine fuer inkompressible medien. |
CH683552A5 (de) * | 1991-06-22 | 1994-03-31 | Aginfor Ag | Verdrängungspumpe. |
US20040241029A1 (en) * | 2001-09-05 | 2004-12-02 | Rapp Manfred Max | Parallel rotating piston engine with side walls |
EP1423584A1 (fr) * | 2001-09-05 | 2004-06-02 | RAPP, Manfred Max | Machine a piston a rotation parallele pourvue de parois laterales |
GB0600588D0 (en) * | 2006-01-12 | 2006-02-22 | Boc Group Plc | Scroll-type apparatus |
KR101144288B1 (ko) * | 2011-10-11 | 2012-05-11 | 전광석 | 공기 압축기 |
JP5881528B2 (ja) * | 2012-05-21 | 2016-03-09 | 株式会社日本自動車部品総合研究所 | 圧縮機 |
FR3075280B1 (fr) * | 2017-12-14 | 2019-11-22 | Mouvex | Pompe volumetrique a nettoyage ameliore |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2230773A1 (de) * | 1971-12-10 | 1973-06-20 | Aginfor Ag | Verdraengermaschine |
Family Cites Families (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE62264C (de) * | E. H. GOLLINGS in Chicago, V. St. A.: | Kreisel-Kraftmaschine oder Pumpe | ||
FR7156E (fr) * | 1905-03-28 | 1907-05-23 | Pierre Samain | Pompe ou moteur à piston annulaire |
GB190917672A (en) * | 1909-07-30 | 1910-01-06 | Ole Martin Dahl | Improvements in Rotary Pumps. |
FR428218A (fr) * | 1911-04-08 | 1911-08-25 | George F Nelson | Perfectionnements dans les pompes ou moteurs rotatifs |
US1229676A (en) * | 1915-07-28 | 1917-06-12 | Francis D Tice | Pump. |
GB154261A (en) * | 1919-07-10 | 1920-11-10 | Cromwell Hanford Varley | Improvements in rotary engines or pumps |
FR630656A (fr) * | 1927-03-10 | 1927-12-07 | Perfectionnements dans les pompes à tambour à mouvement d'excentrique dans un cylindrique de plus grand diamètre | |
GB290251A (en) * | 1927-05-11 | 1929-04-25 | Vacuum Compressor Ab | Improved process of grinding interfitting surfaces |
US2112890A (en) * | 1936-10-22 | 1938-04-05 | Socony Vacuum Oil Co Inc | Rotary power device |
FR825643A (fr) * | 1936-11-26 | 1938-03-09 | Perfectionnements au capsulisme à excentrique | |
FR1095539A (fr) * | 1953-12-10 | 1955-06-03 | Pompe rotative | |
US2856860A (en) * | 1955-08-03 | 1958-10-21 | Mechanisms Company | Fluid pressure transducer with end clearance control |
FR1197750A (fr) * | 1958-01-06 | 1959-12-02 | Pompe à engrenage exempte de poussée axiale | |
US3097610A (en) * | 1962-01-18 | 1963-07-16 | Procon Pump & Engineering Co | Pump and motor construction |
GB1013263A (en) * | 1962-09-04 | 1965-12-15 | Borg Warner | Pressure loaded rotary hydraulic pump or motor |
DE1962109U (de) | 1964-07-07 | 1967-06-15 | Telefunken Patent | Kondensator veraenderbarer kapazitaet. |
CH476212A (de) * | 1966-06-24 | 1969-07-31 | Schindler Werner | Verdrängungspumpe |
US3627452A (en) * | 1968-12-13 | 1971-12-14 | Worthington Corp | Flexible band fluid device |
US3551079A (en) * | 1969-05-05 | 1970-12-29 | Emerson Electric Co | Pressure sealed hydraulic pump or motor |
GB1379907A (en) * | 1971-05-05 | 1975-01-08 | Stothert & Pitt Ltd | Internally-meshing helical screw pumps |
GB1411749A (en) * | 1971-11-24 | 1975-10-29 | Smiths Industries Ltd | Gear pumps |
DE2509536A1 (de) * | 1975-03-05 | 1976-09-16 | Bosch Gmbh Robert | Kompressor mit einem zu seiner antriebswelle exzentrischen rollkolben |
JPS5523353A (en) * | 1978-08-05 | 1980-02-19 | Mitsubishi Electric Corp | Volume type fluid machine |
DE2911655A1 (de) * | 1979-03-24 | 1980-10-02 | Erich Becker | Rollkolbenpumpe |
JPS5797090A (en) * | 1980-12-06 | 1982-06-16 | Kazuichi Ito | Rotary pump |
DE3106314A1 (de) * | 1981-02-20 | 1982-09-09 | SWF-Spezialfabrik für Autozubehör Gustav Rau GmbH, 7120 Bietigheim-Bissingen | Verdraengermaschine |
DE3112470A1 (de) * | 1981-03-28 | 1982-10-07 | Robert Bosch Gmbh, 7000 Stuttgart | Zahnradmaschine (pumpe oder motor) |
JPS5912188A (ja) * | 1982-07-14 | 1984-01-21 | Hitachi Ltd | スクロ−ル形流体機械 |
JPS59128991A (ja) * | 1983-01-10 | 1984-07-25 | Nippon Soken Inc | リング型ポンプ |
JPS59147893A (ja) * | 1983-02-14 | 1984-08-24 | Nippon Soken Inc | リング型ポンプ |
-
1986
- 1986-02-21 EP EP86901030A patent/EP0214164B1/fr not_active Expired - Lifetime
- 1986-02-21 DE DE8686901030T patent/DE3671503D1/de not_active Expired - Fee Related
- 1986-02-21 JP JP61501021A patent/JP2771160B2/ja not_active Expired - Lifetime
- 1986-02-21 US US06/928,177 patent/US4789315A/en not_active Expired - Lifetime
- 1986-02-21 WO PCT/CH1986/000023 patent/WO1986005241A1/fr active IP Right Grant
- 1986-02-21 BR BR8605494A patent/BR8605494A/pt unknown
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2230773A1 (de) * | 1971-12-10 | 1973-06-20 | Aginfor Ag | Verdraengermaschine |
Also Published As
Publication number | Publication date |
---|---|
DE3671503D1 (de) | 1990-06-28 |
JP2771160B2 (ja) | 1998-07-02 |
WO1986005241A1 (fr) | 1986-09-12 |
JPS62501982A (ja) | 1987-08-06 |
EP0214164A1 (fr) | 1987-03-18 |
US4789315A (en) | 1988-12-06 |
BR8605494A (pt) | 1987-04-22 |
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