EP3420192A1 - Rotary expander - Google Patents

Rotary expander

Info

Publication number
EP3420192A1
EP3420192A1 EP17755674.3A EP17755674A EP3420192A1 EP 3420192 A1 EP3420192 A1 EP 3420192A1 EP 17755674 A EP17755674 A EP 17755674A EP 3420192 A1 EP3420192 A1 EP 3420192A1
Authority
EP
European Patent Office
Prior art keywords
vane
vanes
expander according
rotor
expander
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.)
Withdrawn
Application number
EP17755674.3A
Other languages
German (de)
French (fr)
Other versions
EP3420192A4 (en
Inventor
Tony Sleiman
Buck SLEIMAN
Andre Sarkis Laba
Jessie Joseph Laba
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Vengeance Power Inc
Original Assignee
Vengeance Power Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Vengeance Power Inc filed Critical Vengeance Power Inc
Publication of EP3420192A1 publication Critical patent/EP3420192A1/en
Publication of EP3420192A4 publication Critical patent/EP3420192A4/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/30Rotary-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
    • F01C1/40Rotary-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 having a hinged member
    • F01C1/44Rotary-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 having a hinged member with vanes hinged to the inner member
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/30Rotary-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
    • F01C1/40Rotary-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 having a hinged member
    • F01C1/46Rotary-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 having a hinged member with vanes hinged to the outer member
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C19/00Sealing arrangements in rotary-piston machines or engines
    • F01C19/02Radially-movable sealings for working fluids
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08Rotary pistons
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08Rotary pistons
    • F01C21/0809Construction of vanes or vane holders
    • F01C21/0881Construction of vanes or vane holders the vanes consisting of two or more parts

Definitions

  • the invention relates to the field of rotary expanders.
  • Rotary expanders are well known. Known rotary expanders are either relatively expensive to manufacture, relatively inefficient or relatively expensive to maintain.
  • Forming one aspect of the invention is an improvement to an expander of the type that is used to extract power from a supply of pressurized fluid and that includes: a housing, a rotor and control means.
  • the housing has a rotation axis; defines a hollow interior having an annular surface orientated parallel to the rotation axis and through which the rotation axis extends; and defines one or more ports which extend through the housing to the interior.
  • the rotor is mounted in the housing for rotation about the rotation axis and has a body and vanes.
  • the body has an outer tubular surface, the tubular surface having defined therein a plurality of voids.
  • the vanes are provided one for each of the voids.
  • Each vane has a seal defining a tip of the vane; is mounted in the void for which it is provided for movement between a retracted position and an extended position; and is adapted such that, upon rotation of the rotor in the housing, movement of the vane between the extended and retracted positions causes the tip seal to sweep the annular surface.
  • the control means is for controlling movement of the vanes and access to the ports such that the vanes create chambers which increase in volume when in
  • the improvement comprises: for each vane, a pivot axis orientated parallel to the rotational axis and about which said each vane pivots between the extended and retracted positions.
  • FIG. 1 is a perspective view of an expander according to an exemplary
  • FIG. 2 is a view similar to FIG. 1 with a portion removed for clarity;
  • FIG. 3 is a view of the structure of FIG. 2 from another vantage point
  • FIG. 4 is a view similar to FIG. 3 with a further portion removed and partially exploded, for clarity
  • FIG. 5 is a view of a portion of the structure of FIG. 3;
  • FIG. 6A is a cross sectional, partially schematic view of an expander according to another exemplary embodiment of the invention.
  • FIG. 6B is a view of the structure of FIG. 6A in another position
  • FIG. 6C is view of the structure of FIG. 6A in yet another position
  • FIG. 7 is a view similar to FIG. 6A showing, in partially schematic cross- section, an expander according to yet another embodiment
  • FIG. 8 is a view of another embodiment of the structure of encircled area 8 of
  • FIG. 4
  • FIG. 9 is a view similar to FIG. 6A of another exemplary embodiment.
  • FIG. 1 An expander 20 according to an exemplary embodiment of the invention is illustrated in FIG. 1 and will be understood, upon review of FIG. 1 - FIG. 5, to include a housing 22, a rotor 24, control means 26 and end seals 28.
  • the housing will be understood to: have a rotation axis R-R; define a hollow interior 30 having an annular [generally oval] surface 32 orientated parallel to the rotation axis and through which the rotation axis extends; define one or more ports 34 which extend through the housing to the interior; and be defined by a tubular block 36 disposed between a pair of end plates 37.
  • the rotor will be seen to be disposed in the interior and to include a body 38, a shaft 40 and vanes 42.
  • This body will seen to be a generally cylindrical metal structure suitable for construction with wire EDM and drilling and to have a central bore 43 and an outer tubular surface 44, the tubular surface having defined therein a plurality of voids 46 and, associated with each void, a respective socket 48, each void being defined in part by an arcuate slot 50 and each socket defining a respective pivot axis P-P.
  • the shaft passes through the bore.
  • the vanes are provided one for each of the voids.
  • Each vane has a seal 52 defining a tip of the vane, terminates in a pintle 54 which is mounted in the associated socket for rotational movement, as discussed further below, and includes an arcuate slider 56. Each vane further has vents 57 defined therein.
  • the control means will be seen to include springs 58.
  • the end seals are defined in part by body seals 60 carried by and spring mounted to the body and in part by vane seals 62 carried by and spring mounted to the vanes, all to project to and seal against the end plates.
  • the seals 60,62 in the exemplary embodiment are spring-mounted within slots provided in the vanes and body.
  • the foregoing structure provides the functionality normally associated with an expander, namely, pressurized fluid is introduced into the interior through the ports, thus creating force on the trailing edges of the vanes which causes the rotor to turn.
  • the control means controls movement of the vanes and access to the ports such that the vanes create chambers which increase in volume when in communication with the source of fluid at high pressure.
  • the creation of a chamber that increases in volume when in communication with the source of pressurized fluid is best seen in the schematic views of the alternate expander of FIGS. 6A-6C, wherein a single vane is enumerated, for clarity, a chamber is seen to be created as the vane nears the port, as per the sequence of FIG. 6A, 6B, and the chamber C will be seen to increase in volume in the sequence of FIG. 6B, 6C.
  • annular surface and the tubular surface can both be oval, with the rotor centered in the interior.
  • An embodiment with a modified block 36' to achieve this is shown in FIG. 7.
  • the modified block 36' also shows that the number of ports can be adjusted routinely by persons of ordinary skill in the art.
  • a large range of customized volumetric expansion ratios can be achieved using readily available metered inlet controls without altering the base design.
  • springs are shown to bias the movement of the vanes at low speeds and startup, this is not necessary: there are many viable ways to control the vane movement such as magnets 64 as shown in FIG. 8 which repel vanes 42 from the body 38. Compressed gas and cams/rollers, not shown, can also be used.
  • seals constitute sacrificial wear components
  • numerous lubricants can be employed including wet lubricants (oils) and dry lubricants (graphite, bronze, molybdenum disulfide, etc.) to increase life.
  • wet lubricants oil
  • dry lubricants graphite, bronze, molybdenum disulfide, etc.
  • axle-supported bearings can be provided at the ends of the sockets, not shown. Bearings can also be provided to facilitate movement of the sliders, as indicated by bearings 66 in FIG. 9.
  • FIG. 9 also shows that the annular surface can be cylindrical, which has advantages in terms of machining.
  • the expander can run in constant pressure mode like a hydraulic motor providing maximum torque at lowest speeds. This can be used as a safety fallback, low expansion mode with full torque at low speed should the control means fail.

Abstract

An improvement to an expander is disclosed. The expander is of the type that has vanes that extend and retract from a rotor body during rotation and create chambers that increase and decrease in size. The improvement comprises, for each vane, for each vane, a pivot axis orientated parallel to the rotational axis and about which said each vane pivots between the extended and retracted positions.

Description

ROTARY EXPANDER
FIELD
The invention relates to the field of rotary expanders. BACKGROUND
Rotary expanders are well known. Known rotary expanders are either relatively expensive to manufacture, relatively inefficient or relatively expensive to maintain.
SUMMARY OF THE INVENTION
Forming one aspect of the invention is an improvement to an expander of the type that is used to extract power from a supply of pressurized fluid and that includes: a housing, a rotor and control means. The housing : has a rotation axis; defines a hollow interior having an annular surface orientated parallel to the rotation axis and through which the rotation axis extends; and defines one or more ports which extend through the housing to the interior. The rotor is mounted in the housing for rotation about the rotation axis and has a body and vanes. The body has an outer tubular surface, the tubular surface having defined therein a plurality of voids. The vanes are provided one for each of the voids. Each vane : has a seal defining a tip of the vane; is mounted in the void for which it is provided for movement between a retracted position and an extended position; and is adapted such that, upon rotation of the rotor in the housing, movement of the vane between the extended and retracted positions causes the tip seal to sweep the annular surface.
The control means is for controlling movement of the vanes and access to the ports such that the vanes create chambers which increase in volume when in
communication with the source of pressurized fluid. The improvement comprises: for each vane, a pivot axis orientated parallel to the rotational axis and about which said each vane pivots between the extended and retracted positions.
Advantages, features and characteristics of the present invention will become apparent to persons of ordinary skill upon review of the following detailed description, with reference to the accompanying drawings, the latter being briefly described hereinbelow.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a perspective view of an expander according to an exemplary
embodiment of the invention
FIG. 2 is a view similar to FIG. 1 with a portion removed for clarity;
FIG. 3 is a view of the structure of FIG. 2 from another vantage point;
FIG. 4 is a view similar to FIG. 3 with a further portion removed and partially exploded, for clarity
FIG. 5 is a view of a portion of the structure of FIG. 3;
FIG. 6A is a cross sectional, partially schematic view of an expander according to another exemplary embodiment of the invention;
FIG. 6B is a view of the structure of FIG. 6A in another position;
FIG. 6C is view of the structure of FIG. 6A in yet another position; FIG. 7 is a view similar to FIG. 6A showing, in partially schematic cross- section, an expander according to yet another embodiment;
FIG. 8 is a view of another embodiment of the structure of encircled area 8 of
FIG. 4; and
FIG. 9 is a view similar to FIG. 6A of another exemplary embodiment.
DETAILED DESCRIPTION
An expander 20 according to an exemplary embodiment of the invention is illustrated in FIG. 1 and will be understood, upon review of FIG. 1 - FIG. 5, to include a housing 22, a rotor 24, control means 26 and end seals 28.
The housing will be understood to: have a rotation axis R-R; define a hollow interior 30 having an annular [generally oval] surface 32 orientated parallel to the rotation axis and through which the rotation axis extends; define one or more ports 34 which extend through the housing to the interior; and be defined by a tubular block 36 disposed between a pair of end plates 37.
The rotor will be seen to be disposed in the interior and to include a body 38, a shaft 40 and vanes 42. This body will seen to be a generally cylindrical metal structure suitable for construction with wire EDM and drilling and to have a central bore 43 and an outer tubular surface 44, the tubular surface having defined therein a plurality of voids 46 and, associated with each void, a respective socket 48, each void being defined in part by an arcuate slot 50 and each socket defining a respective pivot axis P-P. The shaft passes through the bore. The vanes are provided one for each of the voids. Each vane has a seal 52 defining a tip of the vane, terminates in a pintle 54 which is mounted in the associated socket for rotational movement, as discussed further below, and includes an arcuate slider 56. Each vane further has vents 57 defined therein. The control means will be seen to include springs 58.
The end seals are defined in part by body seals 60 carried by and spring mounted to the body and in part by vane seals 62 carried by and spring mounted to the vanes, all to project to and seal against the end plates. As best indicated by FIG. 4, the seals 60,62 in the exemplary embodiment are spring-mounted within slots provided in the vanes and body.
In use, it will be understood that the foregoing structure provides the functionality normally associated with an expander, namely, pressurized fluid is introduced into the interior through the ports, thus creating force on the trailing edges of the vanes which causes the rotor to turn. The control means controls movement of the vanes and access to the ports such that the vanes create chambers which increase in volume when in communication with the source of fluid at high pressure. The creation of a chamber that increases in volume when in communication with the source of pressurized fluid is best seen in the schematic views of the alternate expander of FIGS. 6A-6C, wherein a single vane is enumerated, for clarity, a chamber is seen to be created as the vane nears the port, as per the sequence of FIG. 6A, 6B, and the chamber C will be seen to increase in volume in the sequence of FIG. 6B, 6C.
However, tests have been carried out which demonstrate advantages associated with the design. A prototype similar to FIG. 1 was built using small wire EDM and CNC milling machines and produced 60 ft-lbs of stall torque with 90 psig
compressed air. The accumulated run time of the prototype to date is over 100 hours of intermittent testing without any lubrication. Inspection of the vanes showed little wear with no adverse effects on the surrounding housing surfaces. Without intending to be bound by theory, various of the advantages are believed to be attributable as follows:
• the force borne by the vane is transmitted to the hinged socket at the
periphery of the rotor in a mostly perpendicular and highly favorable direction to the center of the shaft
• relatively high working pressures are tolerated by the robust structure of the vanes, which therefore remain true, thereby avoiding undue friction and wear
• the pintle/socket joint allows for relatively low friction movement of the vane between the extended and retracted position
• as the fluid expands and the pressure drops, the exposed surface area of the vane increases and the length of the torque lever increases, boosting efficiency
• pressure-induced force driving the leading faces of adjacent vanes back into the rotor, thus opening up a blow-by window, are negated by vents 57 on the leading face side, equalizing pressure within the rotor chambers and thereby preventing the vanes from being forced away from the block and back into the rotor body prematurely
Variations on the geometry are possible.
For example, the annular surface and the tubular surface can both be oval, with the rotor centered in the interior. An embodiment with a modified block 36' to achieve this is shown in FIG. 7. The modified block 36' also shows that the number of ports can be adjusted routinely by persons of ordinary skill in the art. As well, a large range of customized volumetric expansion ratios can be achieved using readily available metered inlet controls without altering the base design.
Moreover, whereas springs are shown to bias the movement of the vanes at low speeds and startup, this is not necessary: there are many viable ways to control the vane movement such as magnets 64 as shown in FIG. 8 which repel vanes 42 from the body 38. Compressed gas and cams/rollers, not shown, can also be used.
Further, whereas in the exemplary embodiment, no lubrication is provided, such that the seals constitute sacrificial wear components, numerous lubricants can be employed including wet lubricants (oils) and dry lubricants (graphite, bronze, molybdenum disulfide, etc.) to increase life. Similarly, the end seals are not essential and could be removed in some applications.
As well, to reduce friction, wear and mechanical stress, axle-supported bearings can be provided at the ends of the sockets, not shown. Bearings can also be provided to facilitate movement of the sliders, as indicated by bearings 66 in FIG. 9. FIG. 9 also shows that the annular surface can be cylindrical, which has advantages in terms of machining.
Yet further, the expander can run in constant pressure mode like a hydraulic motor providing maximum torque at lowest speeds. This can be used as a safety fallback, low expansion mode with full torque at low speed should the control means fail.
Accordingly, the invention should be understood to be limited only by the
accompanying claims, purposively construed.

Claims

S
An improved expander of the type that is used to extract power from a supply of pressurized fluid and that includes: a housing : having a rotation axis; defining a hollow interior having an annular surface orientated parallel to the rotation axis and through which the rotation axis extends; and defining one or more ports which extend through the housing to the interior; a rotor mounted in the housing for rotation about the rotation axis, the rotor having a body having an outer tubular surface, the tubular surface having defined therein a plurality of voids; for each of the voids of the plurality, a vane, the vane: having a seal defining a tip of the vane; being mounted in the void for which it is provided for movement between a retracted position and an extended position; and being adapted such that, upon rotation of the rotor in the housing, movement of the vane between the extended and retracted positions causes the tip seal to sweep the annular surface; control means for controlling movement of the vanes and access to the ports such that the vanes create chambers which increase in volume when in communication with the source of pressurized fluid, the improvement comprising : for each vane, a pivot axis orientated parallel to the rotational axis and about which said each vane pivots between the extended and retracted positions. The expander according to claim 1, wherein the vane terminates in a pintle and the pivot axis is defined by a socket formed in the body in which the pintle is mounted for rotational movement.
The expander according to claim 1, wherein the void is defined at least in part by an arcuate slot.
The expander according to claim 1, wherein the body is cylindrical and disposed in offset relation to the interior.
The expander according to claim 1, wherein the annular surface and the tubular surface are both oval and the body is centered in the interior.
The expander according to claim 1, wherein the control means comprises springs which bias the vanes for movement towards the extended positions.
The expander according to claim 1, wherein the rotor has a pair of end seals disposed axially apart from one another and defining, in combination with the tubular surface, the annular surface and the tip seal, the chambers.
The expander according to claim 7, wherein the end seals are defined in part by body seals carried by and spring mounted to the body and in part by vane seals carried by and spring mounted to the vanes.
EP17755674.3A 2016-02-24 2017-02-23 Rotary expander Withdrawn EP3420192A4 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201662299046P 2016-02-24 2016-02-24
PCT/CA2017/050223 WO2017143437A1 (en) 2016-02-24 2017-02-23 Rotary expander

Publications (2)

Publication Number Publication Date
EP3420192A1 true EP3420192A1 (en) 2019-01-02
EP3420192A4 EP3420192A4 (en) 2019-10-30

Family

ID=59684648

Family Applications (1)

Application Number Title Priority Date Filing Date
EP17755674.3A Withdrawn EP3420192A4 (en) 2016-02-24 2017-02-23 Rotary expander

Country Status (4)

Country Link
US (1) US20190048720A1 (en)
EP (1) EP3420192A4 (en)
CA (1) CA3015691A1 (en)
WO (1) WO2017143437A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NO343543B1 (en) * 2018-02-27 2019-04-01 Tocircle Ind As A rotary vane machine with a cam track and vane mechanisms
WO2020171891A2 (en) * 2019-01-23 2020-08-27 Jerry Iraj Yadegar Arc turbine

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB190919411A (en) * 1909-08-24 1910-02-10 Thomas Edward Braley Rotary Gasoline Engines.
US1344137A (en) * 1918-10-02 1920-06-22 Sirius E Kochendarfer Rotary engine
US1645069A (en) * 1927-01-15 1927-10-11 Peterson & Nethaway Rotary pump
US1952142A (en) * 1931-06-08 1934-03-27 Francis C Peterson Compressor
DE2314164A1 (en) * 1973-03-22 1974-10-03 Fritz Prescha CIRCULAR LIFT MOTOR WITH CIRCULAR LIFT COMPRESSOR
US3971347A (en) * 1973-10-10 1976-07-27 Michael Vasilantone Rotary internal combustion engine
US3976408A (en) * 1975-01-31 1976-08-24 Empire Oil Tool Company Fluid driven motor having improved blade construction
US4106472A (en) * 1976-11-08 1978-08-15 Glenn Rusk Rotary energy converter with respiring chambers
JPS56113087A (en) * 1980-02-14 1981-09-05 Okimoto Tamada Spring pressure contact deformation type cam ring type radial pump
US4389173A (en) * 1982-04-01 1983-06-21 Earl J. Lee Arcuate piston rotary engine
US5709188A (en) * 1993-12-09 1998-01-20 Al-Qutub; Amro Heat engine
US5494014A (en) * 1994-10-24 1996-02-27 Lobb; David R. Rotary internal combustion engine
US20100143174A1 (en) * 2004-03-09 2010-06-10 Maciej Radziwill Rotary Working Machine Provided with an Assembly of Working Chambers and Periodically Variable Volume, In Particular a Compressor
WO2006042196A2 (en) * 2004-10-07 2006-04-20 Gyroton, Inc. Multilobe rotary motion asymetric compression/expansion engine
EP3323977A1 (en) * 2008-07-08 2018-05-23 RPM Group Limited A rotary expansible chamber device, as a compressor or an expander

Also Published As

Publication number Publication date
EP3420192A4 (en) 2019-10-30
WO2017143437A1 (en) 2017-08-31
CA3015691A1 (en) 2017-08-31
US20190048720A1 (en) 2019-02-14

Similar Documents

Publication Publication Date Title
US4804317A (en) Rotary vane pump with floating rotor side plates
EP2803862B1 (en) Vane-type compressor
JP2010540826A (en) Rotary fluid displacement assembly
RU2010136038A (en) ROTARY COMPRESSOR
CN102162446A (en) Vane rotary type fluid device and compressor
US20190048720A1 (en) Rotary expander
EP2012015A1 (en) Scroll-type fluid machine
US7488166B2 (en) Rotary volumetric machine
JP2856897B2 (en) Wing type positive displacement pump
CN100491734C (en) Single-winged vacuum pump
US4061450A (en) Positive displacement vane type rotary pump
ITTO20121149A1 (en) ADJUSTABLE DISPLACEMENT PUMP PUMP AND METHOD FOR ADJUSTING THE PUMP DISPLACEMENT.
JP2009156231A (en) Lubricant decompressing and supplying structure for vane type compressor
JPWO2012023427A1 (en) Vane type compressor
US7080623B1 (en) Rotor for an axial vane rotary device
BR0113534A (en) Pump vacuum
JP2588911Y2 (en) Rotary compressor
JPH0329995B2 (en)
CN111379699A (en) Compressor with a compressor housing having a plurality of compressor blades
CN106014972A (en) Vane pump
CN216894889U (en) Variable displacement vane pump
WO2016181428A1 (en) Vane pump for compressible fluid
JPS6122151B2 (en)
JPS6329183Y2 (en)
RU2602951C1 (en) Rotary-vane vacuum pump

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

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

Free format text: ORIGINAL CODE: 0009012

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

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20180824

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

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

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
A4 Supplementary search report drawn up and despatched

Effective date: 20190926

RIC1 Information provided on ipc code assigned before grant

Ipc: F01C 21/08 20060101ALI20190920BHEP

Ipc: F01C 1/46 20060101AFI20190920BHEP

Ipc: F01C 19/02 20060101ALI20190920BHEP

Ipc: F01C 1/44 20060101ALI20190920BHEP

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

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20210901