EP3824186A1 - Compresseur à spirales - Google Patents

Compresseur à spirales

Info

Publication number
EP3824186A1
EP3824186A1 EP19864598.8A EP19864598A EP3824186A1 EP 3824186 A1 EP3824186 A1 EP 3824186A1 EP 19864598 A EP19864598 A EP 19864598A EP 3824186 A1 EP3824186 A1 EP 3824186A1
Authority
EP
European Patent Office
Prior art keywords
scroll
frame
body portion
sub
orbiting scroll
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.)
Granted
Application number
EP19864598.8A
Other languages
German (de)
English (en)
Other versions
EP3824186B1 (fr
EP3824186A4 (fr
Inventor
Takashi Uekawa
Yang Hee Cho
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.)
Samsung Electronics Co Ltd
Original Assignee
Samsung Electronics Co Ltd
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 Samsung Electronics Co Ltd filed Critical Samsung Electronics Co Ltd
Priority claimed from PCT/KR2019/012532 external-priority patent/WO2020067739A1/fr
Publication of EP3824186A1 publication Critical patent/EP3824186A1/fr
Publication of EP3824186A4 publication Critical patent/EP3824186A4/fr
Application granted granted Critical
Publication of EP3824186B1 publication Critical patent/EP3824186B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/02Rotary-piston pumps specially adapted for elastic fluids 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
    • F04C18/0207Rotary-piston pumps specially adapted for elastic fluids 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 both members having co-operating elements in spiral form
    • F04C18/0215Rotary-piston pumps specially adapted for elastic fluids 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 both members having co-operating elements in spiral form where only one member is moving
    • 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
    • F01C21/007General arrangements of parts; Frames and supporting elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C23/00Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids
    • F04C23/008Hermetic pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C27/00Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
    • F04C27/005Axial sealings for working fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/0042Driving elements, brakes, couplings, transmissions specially adapted for pumps
    • F04C29/005Means for transmitting movement from the prime mover to driven parts of the pump, e.g. clutches, couplings, transmissions
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/12Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2210/00Fluid
    • F04C2210/26Refrigerants with particular properties, e.g. HFC-134a
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2240/00Components
    • F04C2240/20Rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2240/00Components
    • F04C2240/50Bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2240/00Components
    • F04C2240/50Bearings
    • F04C2240/56Bearing bushings or details thereof
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2240/00Components
    • F04C2240/60Shafts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2240/00Components
    • F04C2240/80Other components
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2210/00Working fluid
    • F05B2210/10Kind or type
    • F05B2210/14Refrigerants with particular properties, e.g. HFC-134a
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/50Bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/57Seals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/60Shafts

Definitions

  • the disclosure relates to a scroll compressor.
  • a scroll compressor is configured as follows.
  • a sealed container is maintained at high pressure.
  • a fixed scroll and an orbiting scroll configured in such a way that spiral shaped wraps thereof are engaged with each other to form a compression chamber on a support plate, a main shaft configured to drive the orbiting scroll by inserting an eccentric shaft potion into a boss portion provided on a side opposite to the spiral shaped wrap of the orbiting scroll, a compliant frame configured to support the orbiting scroll in an axial direction while radially supporting the main shaft, which drives the orbiting scroll, on a main shaft portion provided in the main shaft, and a guide frame configured to support the compliant frame in a radial direction so as to be fixed to the sealed container are provided. Therefore, the orbiting scroll is moveable in the axial direction by the sliding movement of the compliant frame about the guide frame in the axial direction (refer to Patent document).
  • a scroll compressor in accordance with an aspect of the disclosure, includes a fixed scroll fixed to a body, an orbiting scroll configured to orbit in engagement with the fixed scroll, a rotary shaft configured to allow the orbiting scroll to orbit, a holding member configured to hold the fixed scroll from a side opposite to the orbiting scroll, and a support member arranged between the rotary shaft and the holding member to support the orbiting scroll by a load applied to a position away from the center of the orbiting scroll.
  • the support member may be movable in one direction about the holding member.
  • the support member may be movable in a direction along the rotary shaft and further movable in a rotational direction about a virtual axis approximately perpendicular to the rotary shaft.
  • the support member may be movable in a direction opposite to a moment generated in the orbiting scroll among rotational directions about the virtual axis.
  • the support member may be movable in a rotational direction opposite to a moment generated in the orbiting scroll by receiving a reaction force, which is in the holding member against a load that the orbiting scroll receives, from a certain position in the orbiting scroll side rather than a position receiving a load in the rotary shaft.
  • the certain position may be between an end face of a rotary shaft bearing of the support member in the orbiting scroll side and a surface on which a plate of the orbiting scroll is engaged with the fixed scroll.
  • the support member may be movable in a rotational direction opposite to a moment generated in the orbiting scroll because as for a position receiving a load about the rotary shaft, the smallest gap with the holding member in the same side as the orbiting scroll is less than the smallest gap with the holding member in the opposite side to the orbiting scroll.
  • the certain position may be between an end face of a rotary shaft bearing of the support member in the orbiting scroll side and a surface on which a plate of the orbiting scroll is engaged with the fixed scroll.
  • the support member may be movable in a rotational direction opposite to a moment generated in the orbiting scroll by being in contact with a protrusion provided on the holding member.
  • a portion of the support member may have a shape that is elastically deformable upon being in contact with a surface on which a plate of the orbiting scroll is engaged with the fixed scroll due to the inclination of the support member.
  • the scroll compressor may further include an Oldham ring configured to prevent a pivot of the orbiting scroll, and the Oldham ring may be coupled to the orbiting scroll and the support member, the orbiting scroll and the holding member, or the orbiting scroll and the fixed scroll.
  • the scroll compressor may further include a seal mechanism configured to form an internal space between at least the holding member and the support member by sealing at least a portion of the gap between the holding member and the support member.
  • the holding member may be provided with a holding member internal passage configured to introduce a refrigerant, which is introduced from a compression chamber, which is formed in such a way that the orbiting scroll orbits by being engaged with the fixed scroll, into an inner space.
  • the fixed scroll may be provided with a fixed scroll internal passage configured to move a refrigerant from the compression chamber and introduce the refrigerant into the holding member internal passage.
  • the fixed scroll may be provided with a fixed scroll internal passage configured to move a refrigerant from the compression chamber and introduce the refrigerant into the holding member internal passage
  • the orbiting scroll may be provided with an orbiting scroll internal passage configured to move a refrigerant from the compression chamber and introduce the refrigerant into the fixed scroll internal passage.
  • the fixed scroll internal passage may be in communication with the orbiting scroll internal passage for at least a part of a period in which the orbiting scroll orbits.
  • the fixed scroll internal passage may include an inlet on a track of an outlet of orbiting scroll internal passage at the orbit of the orbiting scroll, and an inlet connected to a groove portion covering the entire of the track of an outlet of orbiting scroll internal passage at the orbit of the orbiting scroll.
  • FIG. 1 illustrates an axial cross-sectional view of a scroll compressor according to an embodiment of the disclosure
  • FIG. 2 illustrates an axial cross-sectional view of a compression portion and a rotary shaft of a modification of the scroll compressor according to an embodiment of the disclosure
  • FIG. 3 illustrates an axial cross-sectional view of a compression portion and a rotary shaft of a modification of the scroll compressor according to an embodiment of the disclosure
  • FIG. 4 illustrates an axial cross-sectional view of a compression portion and a rotary shaft of a modification of the scroll compressor according to an embodiment of the disclosure
  • FIG. 5 illustrates an axial cross-sectional view of a compression portion and a rotary shaft of a modification of the scroll compressor according to an embodiment of the disclosure
  • FIG. 6 illustrates an axial cross-sectional view of a scroll compressor according to an embodiment of the disclosure
  • FIG. 7A is a perspective view illustrating a moment that an orbiting scroll receives
  • FIG. 7B is a view illustrating a shape in which the orbiting scroll is about to incline
  • FIG. 8 illustrates an axial cross-sectional view of a compression portion and a rotary shaft when a moment applied to a sub frame is in the same direction as a moment applied to the orbiting scroll;
  • FIG. 9 illustrates an axial cross-sectional view of the compression portion and the rotary shaft when a moment applied to a sub frame is in an opposite direction to a moment applied to the orbiting scroll;
  • FIG. 10 illustrates an axial cross-sectional view of a compression portion and a rotary shaft according to an implementation of the scroll compressor
  • FIG. 11 illustrates an axial cross-sectional view of a compression portion and a rotary shaft according to an implementation of the scroll compressor
  • FIG. 12 illustrates an axial cross-sectional view of a compression portion and a rotary shaft according to an implementation example of the scroll compressor
  • FIG. 13 illustrates an axial cross-sectional view of a compression portion and a rotary shaft of a modification of the scroll compressor according to an embodiment of the disclosure
  • FIG. 14 is a top view illustrating an end portion of a plate of the orbiting scroll in the compression portion when viewed from the top, according to a modification of the scroll compressor according to an embodiment of the disclosure;
  • FIG. 15 is a bottom view illustrating a body portion of the fixed scroll in the compression portion when viewed from the bottom, according to a modification of the scroll compressor according to an embodiment of the disclosure
  • FIG. 16 illustrates an axial cross-sectional view of a compression portion and a rotary shaft of a modification of the scroll compressor according to an embodiment of the disclosure.
  • FIG. 17 is a bottom view illustrating a body portion of a fixed scroll in the compression portion when viewed from the bottom, according to a modification of the scroll compressor according to an embodiment of the disclosure.
  • a scroll compressor is provided with a fixed scroll, an orbiting scroll configured to orbit in engagement with the fixed scroll, a rotary shaft configured to allow the orbiting scroll to orbit, a holding member configured to hold the fixed scroll on the opposite side of the orbiting scroll, and a support member arranged between the rotary shaft and the holding member.
  • the support member supports the orbiting scroll by a load applied to a position away from the center of the orbiting scroll. That is, the support member may be provided to support the orbiting scroll at a position away from the center of the orbiting scroll.
  • some configurations may be considered. Hereinafter the configurations will be described as embodiments.
  • FIG. 1 illustrates an axial cross-sectional view of a scroll compressor 1 according to an embodiment of the disclosure.
  • the scroll compressor 1 is a compressor widely used for an air conditioner, a freezer, and a pump.
  • FIG. 1 is a longitudinal sectional view of a hermetic scroll compressor used in a refrigerant circuit of an air conditioner.
  • the scroll compressor 1 includes a compression portion 10 configured to compress a refrigerant, a drive motor 20 configured to drive the compression portion 10, and a casing 30 corresponding to a body configured to receive the compression portion 10 and the drive motor 20.
  • the scroll compressor 1 is a vertical scroll compressor in which an axial direction of a rotary shaft 23, which will be described later, of the drive motor 20 is coincident with the gravity direction.
  • the axial direction of the rotary shaft 23 will be referred to as "vertical direction”, and based on FIG. 1, the up side may be referred to as “upper side” and the down side may be referred to as "lower side".
  • the vertical scroll compressor is described as an example, but an embodiment of the disclosure will be applicable to a horizontal scroll compressor.
  • the compression portion 10 includes a fixed scroll 11 fixed to the casing 30, an orbiting scroll 12 orbiting by being engaged with the fixed scroll 11, a main frame 13 fixed to the casing 30 and configured to support the fixed scroll 11, a sub frame 14 arranged in a space surrounded by the orbiting scroll and the main frame 13 and configured to support the orbiting scroll 12, and an Oldham ring 15 configured to allow the orbiting scroll 12 to orbit without pivoting the orbiting scroll 12.
  • the fixed scroll 11 may include a fixed scroll body and a fixed wrap 114 protruding from the fixed scroll body.
  • the fixed wrap 114 may protrude downward from the fixed scroll body.
  • the fixed scroll body may include a cylindrical body portion 111, a plate 112 configured to cover an opening in an upper side of the body portion 111, and a protrusion 113 extending from a lower end of the body portion 111 in radially outward direction.
  • the fixed wrap 114 may protrude downward from a lower portion of the plate 112 and have a spiral shape when viewed from the bottom.
  • the fixed scroll 11 may be formed of cast iron such as gray cast iron FC 250.
  • the body portion 111 may be provided with a through hole 111a in the radial direction.
  • the though hole 111a may serve as a suction port configured to suction the refrigerant into a space surrounded by the body portion 111, the plate 112 and the orbiting scroll 12.
  • a through hole 112a in the vertical direction is formed at the center of the plate 112.
  • the through hole 112a may serve as a discharge port configured to discharge the refrigerant from the space surrounded by the plate 112, the fixed wrap 114 and the orbiting scroll 12.
  • the fixed scroll 11 constructed as described above is fixed to the main frame 13 by a positioning means such as a bolt or a positioning pin passed through the through hole in the vertical direction formed in the protrusion 113.
  • the orbiting scroll 12 may include an orbiting scroll body and an orbiting wrap 122 protruding from the orbiting scroll body to form a compression chamber 16 by being engaged with the fixed wrap 114 of the fixed scroll 11.
  • the orbiting wrap 122 may protrude upward from the orbiting scroll body.
  • the orbiting scroll 12 may perform an orbital movement by being coupled the rotary shaft 23.
  • the orbiting scroll body may include a plate 121 having a disk shape, and a cylindrical body portion 123 protruding downward from a lower end of the plate 121.
  • the orbiting wrap 122 may protrude upward from an upper end of the plate 121 and have a spiral shape when viewed from the top.
  • the orbiting scroll 12 may be formed of FC material or FCD material.
  • the orbiting wrap 122 of the orbiting scroll 12 may be engaged with the fixed wrap 114 of the fixed scroll 11. Further, the orbiting wrap 122 of the orbiting scroll 12 and the fixed wrap 114 of the fixed scroll 11 may be placed in a space formed by the body portion 111 and the plate 112 of the fixed scroll 11, and of the plate 121 so as to form the compression chamber 16. Because the orbiting wrap 122 is circularly moved about the fixed wrap 114 that is fixed, a volume of the compression chamber 16 is reduced and the refrigerant of the compression chamber 16 is compressed. In other words, as an internal space between the fixed wrap 114 and the orbiting wrap 122 is reduced toward a center of rotation, the refrigerant is compressed.
  • An eccentric shaft 232 of the rotary shaft 23, which is described later, is inserted into the body portion 123 through a sliding bearing. As described above, the body portion 123 functions as a bearing of the eccentric shaft 232.
  • the main frame 13 is an example of a holding member configured to hold the fixed scroll 11.
  • the main frame 13 may include a cylindrical first body portion 131, a cylindrical second body portion 132 protruding downward from the radially inner side of the lower end of the first body portion 131, a cylindrical third body portion 133 protruding radially inwardly from the lower end of the second body portion 132, and a cylindrical fourth body portion 134 protruding upward and downward from the inner end of the third body portion 133.
  • An outer circumferential surface of the first body portion 131 of the main frame 13 is fixed to a central casing 31 of the casing 30, which is described later.
  • the main frame 13 also functions as a bearing for rotatably supporting the rotary shaft 23.
  • a protrusion 131a protruding upward from the upper end surface is installed on an outer circumferential portion of the first body portion 131.
  • a female screw is formed in the protrusion 131a, and a bolt, which passed through the through hole formed in the protrusion 113 of the fixed scroll 11, is engaged with the female screw. Therefore, the fixed scroll 11 is fixed to the main frame 13.
  • a groove 131b elongating in the vertical direction may be provided on the outer circumferential portion of the first body portion 131. That is, in the first body portion 131, the groove 131b extending in the vertical direction from the center to the lower portion of the outer circumferential portion may be formed. In the first body portion 131, a portion where the groove 131b is formed may be spaced apart from the central casing 31.
  • the rotary shaft 23 is fitted in the inner circumference of the fourth body portion 134 with the journal bearing interposed therebetween and thus the fourth body portion 134 functions as a bearing for rotatably supporting the rotary shaft 23.
  • the main frame 13 may further include a fixed scroll support surface 11a configured to support the fixed scroll 11.
  • the fixed scroll support surface 11a may be formed on the protrusion 131a.
  • the sub-frame 14 is an example of a support member for supporting the orbiting scroll 12.
  • a gap may be formed between the main frame 13 and the sub frame 14 such that the sub -frame 14 is movable with respect to the main frame 13.
  • the sub-frame 14 may be arranged inside the main frame 13 to be spaced apart from the main frame 13.
  • the sub-frame 14 may include a cylindrical first body portion 141 and a cylindrical second body portion 142 protruding downward from a lower end surface of the first body portion 141. Between an outer circumferential surface of the first body portion 141 of the sub-frame 14 and an inner circumferential surface of the first body portion 131 of the main frame 13, and between an inner circumferential surface of the second body portion 142 of the sub-frame 14 and an outer circumferential surface of the fourth body portion 134 of the main frame 13, the sub-frame 14 may be arranged in a space surrounded by the orbiting scroll 12 and the main frame 13 with a gap in which the sub-frame 14 is movable about the main frame 13 only in the axial direction of the rotary shaft 23.
  • a first groove 141a and a second groove 141b recessed downward from an upper end surface are formed.
  • the first groove 141a is formed in the center portion
  • the second groove 141b is formed between the first groove 141a and the protrusion 131a.
  • the body portion 123 of the orbiting scroll 12 is inserted into the first groove 141a.
  • the Oldham ring 15 preventing a pivot of the orbiting scroll 12 is arranged between the main frame 13 and the orbiting scroll 12.
  • a discharge passage discharging refrigerant compressed in the compression chamber 16 is formed.
  • the discharge passage is configured to discharge the high-pressure refrigerant, one end thereof is connected to the through hole 112a of the plate 112, which is configured to discharge the high-pressure refrigerant from the space surrounded by the fixed scroll 11 and the orbiting scroll 12, and the other end thereof is connected to a space lower than the main frame 13 in the casing 30 and further connected to a chamber 121a.
  • a discharge passage configured to discharge an intermediate pressure refrigerant
  • one end thereof is connected to a discharge port, which is configured to discharge the intermediate-pressure refrigerant from a space surrounded by the fixed scroll 11 and the orbiting scroll 12, and the other end thereof is connected to chambers 121b and 142a.
  • the drive motor 20 is fixed to the casing 30 under the compression portion 10.
  • the drive motor 20 may include a stator 21 constituting a stator, a rotor 22 constituting a rotor, the rotary shaft 23 supporting the rotor 22 and rotating with respect to the casing 30, and a support member 24 rotatably supporting the rotary shaft 23.
  • the stator 21 may include a stator body 211 and a coil 212 wound around the stator body 211.
  • the stator body 211 is a laminated body in which a plurality of electrical steel sheets is laminated, and has an approximately cylindrical shape. A diameter of an outer circumferential surface of the stator body 211 is formed greater than a diameter of an inner circumferential surface of the central casing 31 of the casing 30 which is described later.
  • the stator body 211 (stator 21) is forcedly inserted to the central casing 31.
  • a method for inserting the stator body 211 to the central casing 31 may employ shrink fitting or press fitting method
  • the stator body 211 has a plurality of teeth in the circumferential direction on the inner side portion facing the outer circumference of the rotor 22.
  • the coil 212 is arranged in a slot formed between adjacent tooth.
  • a concentrated winding in which the coil 212 is inserted into a slot placed between a plurality of adjacent tooth, is described as an example of the coil 212.
  • the rotor 22 is a laminated body in which a plurality of electrical steel sheets having a ring shape is laminated, and has an approximately cylindrical shape. A diameter of an inner circumferential surface of the rotor 22 is formed less than the diameter of an outer circumferential surface of the rotary shaft 23. The rotor 22 is forcedly inserted to the rotary shaft 23. A method for inserting the rotor 22 to the rotary shaft 23 may employ the press fitting method. The rotor 22 is fixed to the rotary shaft 23 and rotates together with the rotary shaft 23. Further, a rotor in which one permanent magnet is embedded therein is described as an example of the rotor 22.
  • the diameter of the outer circumferential surface of the rotor 22 is less than the diameter of the inner circumferential surface of the stator body 211 of the stator 21 and a gap is formed between the rotor 22 and the stator 21.
  • the rotary shaft 23 may include a main shaft 231 to which the rotor 22 is fitted and coupled, and the eccentric shaft 232 provided on the upper portion of the main shaft 231 and having an axis eccentric from the axis of the main shaft 231.
  • the lower portion of the main shaft 231 is rotatably supported by the support member 24 and the upper portion of the main shaft 231 is rotatably supported by the main frame 13 of the compression portion 10.
  • the eccentric shaft 232 is rotatably supported by the body portion 123 of the orbiting scroll 12.
  • the rotary shaft 23 is provided with a through hole 233 passing through the rotary shaft 23 in the axial direction.
  • a first communication hole 234 allowing the through hole 233 to communicate with the bearing of the support member 24, a second communication hole 235 allowing the through hole 233 to communicate with the bearing of the main frame 13, and a third communication hole 236 allowing the through hole 233 to communicate with the bearing of the body portion 123 are formed in the radial direction.
  • the support member 24 includes a cylindrical first body portion 241 and a cylindrical second body portion 242 protruding downward from the lower end of the first body portion 241.
  • the support member 24 is fixed to the central casing 31 in such a way that an outer circumferential surface of the first body portion 241 faces an inner circumferential surface of the central casing 31 of the casing 30 which is described later.
  • the rotary shaft 23 is inserted into the inside of the first body portion 241 and the second body portion 242 with a journal bearing interposed therebetween.
  • the support member 24 functions as a bearing for rotatably supporting the rotary shaft 23.
  • a hole and a groove allowing an upper space than the first body portion 241 to communicate with a lower space than the first body portion 241 is formed.
  • a pump 243 pumping lubricant is mounted to the lower end of the second body portion 242 of the support member 24.
  • the casing 30 may include the central casing 31 arranged in the center in the vertical direction and having a cylindrical shape, an upper casing 32 covering an upper opening of the central casing 31, and a lower casing 33 covering a lower opening of the central casing 31. Further, the casing 30 may include a discharge portion 34 discharging the high pressure refrigerant compressed by the compression portion 10 to the outside of the casing 30, and a suction portion 35 suctioning the refrigerant from the outside of the casing 30.
  • the main frame 13 of the compression portion 10 and the stator 21 and the support member 24 of the drive motor 20 are fixed to the central casing 31 as described above.
  • the discharge portion 34 and the suction portion 35 are provided by inserting a pipe into a through hole formed in the central casing 31.
  • the suction portion 35 is installed at a position corresponding to the through the hole 111a formed in the body portion 111 of the fixed scroll 11.
  • the suction portion 35 suctions the refrigerant from the outside of the casing 30 into the space surrounded by the fixed scroll 11 and the orbiting scroll 12.
  • the lower casing 33 is formed in a bowl shape and thus lubricant can be collected.
  • the rotary shaft 23 rotates and the orbiting scroll 12 fitted in the eccentric shaft 232 of the rotary shaft 23 orbits about the fixed scroll 11.
  • the low pressure refrigerant is suctioned from the outside of the casing 30 into the space surrounded by the fixed scroll 11 and the orbiting scroll 12 through the suction portion 35.
  • the refrigerant is compressed in accordance with the volume change of the compression chamber 16.
  • the high-pressure refrigerant in the compression chamber 16 is discharged to the lower side of the compression portion 10.
  • the high-pressure refrigerant discharged to the lower side of the compression portion 10 is discharged to the outside of the casing 30 through the discharge portion 34 provided in the casing 30.
  • the high-pressure refrigerant is distributed to the gap between the rotor 22 and the stator 21 and the gap between the stator 21 and the central casing 31.
  • the high-pressure refrigerant discharged to the outside of the casing 30 is suctioned into the suction portion 35 again after each operation of condensation, expansion and evaporation in the refrigerant circuit.
  • the lubricant stored in the lower casing 33 of the casing 30 is pumped up by the pump 243 and raised through the through hole 233 formed in the rotary shaft 23.
  • the raised lubricant is supplied to each bearing of the rotary shaft 23 through the first communication hole 234, the second communication hole 235 and the third communication hole 236 formed in the rotary shaft 23, or is supplied to a sliding member of the compression portion 10.
  • the lubricant which is supplied to the sliding member of the compression portion 10 or the lubricant supplied to the bearing of the rotary shaft 23 through the second communication hole 235 and the third communication hole 236, is returned to the lower casing 33 through the communication hole 131e and the groove 131b formed in the main frame 13, the gap between the rotor 22 and the stator 21, and the axial direction hole formed in the support member 24, and then stored in the lower portion of the casing 30.
  • the lubricant and the refrigerant flow into the low pressure side while cooling the drive motor 20.
  • the lubricant which has been distributed together with the high pressure refrigerant, is separated from the refrigerant and then stored in the lower portion of the casing 30.
  • the sub-frame 14 supporting the orbiting scroll 12 is arranged in the space surrounded by the orbiting scroll 12 and the main frame 13.
  • a moment load applied to the orbiting scroll 12 from the refrigerant sucked by the suction portion 35 is offset by an upper thrust load in the fixed scroll 11 and a back pressure load of the orbiting scroll 12.
  • a moment load F M applied to the orbiting scroll 12 from the refrigerant sucked by the suction portion 35 is offset by an upper thrust reaction force F U in the fixed scroll 11 and a lower surface thrust reaction force F L in the sub-frame 14.
  • the scroll compressor 1 improves the efficiency by reducing the friction loss between the fixed scroll 11 and the orbiting scroll 12, and improves the reliability by reducing the load on the upper surface and lower surface sliding portion of the plate 121 of the orbiting scroll 12.
  • FIG. 2 is an axial cross-sectional view of a compression portion and a rotary shaft of a modification of the scroll compressor according to an embodiment of the disclosure.
  • a compression portion 10 may include a fixed scroll 11, an orbiting scroll 12, a main frame 13, a sub-frame 14, and an Oldham ring as illustrated in FIG. 1. Further, sealing members 123c and 123d configured to seal a gap between a fourth body portion 134 of the main frame 13 and a body portion 123 and the orbiting scroll 12 is provided in the body portion 123 of the orbiting scroll 12. That is, the sealing members 123c and 123d may be provided between the body portion 123 of the orbiting scroll 12 and the fourth body portion 134 of the main frame 13. According to the a modification, because the sealing members 123c and 123d are provided, it is possible to maintain the inside of a chamber 121a at a high pressure.
  • sealing members 141c and 141d as an example of a first sealing member is provided in a first body portion 141 of the sub-frame 14 to seal a gap between the first body portion 141 of the sub-frame 14 and the first body portion 131 of the main frame 13 (a first gap between the sub-frame 14 and the main frame 13), and at the same time, sealing members 142c and 142d as an example of a second sealing member is provided in a second body portion 142 of the sub-frame 14 to seal a gap between the second body portion 142 of the sub-frame 14 and the fourth body portion 134 of the main frame 13 (a second gap between the sub-frame 14 and the main frame 13). Therefore, according to a modification, by providing sealing members 141c, 141d, 142c, and 142d, it is possible to maintain the pressure of a chamber 142a at a certain intermediate pressure.
  • the sealing members 141c, 141d, 142c, and 142d configured to seal the gap between the sub-frame 14 and the main frame 13 are provided.
  • a sealing member configured to seal a gap between the sub-frame 14 and at least one member facing the sub-frame 14 is provided.
  • FIG. 3 illustrates an axial cross-sectional view of a compression portion and a rotary shaft of a modification of the scroll compressor according to an embodiment of the disclosure.
  • an outer diameter of a sub-frame 14 is increased in comparison with the compression portion 10 of the scroll compressor 1 according to a modification as illustrated in FIG. 2. Because an Oldham ring 15 is moved radially inward, a position where a first body portion 141 of the sub-frame 14 supports an orbiting scroll 12 is moved to radially outward. According to a modification, because a distance from an operating point of an upper thrust reaction force to an operating point of a lower thrust reaction force becomes increased, it is possible to decrease the upper thrust reaction force and the lower thrust reaction force.
  • FIG. 4 illustrates an axial cross-sectional view of a compression portion and a rotary shaft of a modification of the scroll compressor according to an embodiment of the disclosure.
  • guide members 134g and 134h are provided in a fourth body portion 134 of a main frame 13 in comparison with the compression portion 10 of the scroll compressor 1 according to a modification as illustrated in FIG. 3.
  • a rail may be described as an example of the guide member.
  • a wheel rolling on a rail may be used and provided in a sub-frame 14.
  • the sub-frame 14 may not be inclined and movable only in the axial direction of a rotary shaft 23.
  • FIG. 5 illustrates an axial cross-sectional view of a compression portion and a rotary shaft of a modification of the scroll compressor according to an embodiment of the disclosure.
  • sealing members 141e and 141f configured to seal a gap between a first body portion 141 of a sub-frame 14 and a plate 121 of the orbiting scroll 12 is provided in the first body portion 141 of the sub-frame 14, instead of the sealing members 142c and 142d configured to seal the gap between the second body portion 142 of the sub-frame 14 and the fourth body portion 134 of the main frame 13 in the compression portion 10 of the scroll compressor 1 according to a modification as illustrated in FIG. 2.
  • the sealing members 141c, 141d, 141e, and 141f are provided, it is possible to maintain the pressure of the inside of a chamber 121b at a certain intermediate pressure identical to the pressure of the inside of a chamber 142a, by moving the refrigerant of the chamber 142a to the chamber 121b.
  • the sealing members 141c and 141d configured to seal the gap between the sub-frame 14 and the main frame 13 and the sealing members 141e and 141f configured to seal the gap between the sub-frame 14 and the orbiting scroll 12 are provided.
  • a sealing member configured to seal a gap between the sub-frame 14 and at least one member facing the sub-frame 14 is provided.
  • the sub-frame 14 configured to support the orbiting scroll 12 is provided in a space surrounded by the orbiting scroll 12, the rotary shaft 23 and the main frame 13 to be movable only in the axial direction of the rotary shaft 23 about the main frame 13. Accordingly, the pressure applied to the orbiting scroll 12 from the sub-frame 14 may be equalized regardless of the place, and the thrust load for stabilizing the orbiting scroll 12 may be reduced, thereby improving the efficiency and reliability of the scroll compressor 1.
  • the sub-frame 14 is configured to be movable only in the direction along the rotary shaft 23 about the main frame 13. However, it does not mean that the sub-frame 14 does not move at all except the movement in the direction along the rotation axis 23 about the main frame 13. In addition to movement in the direction of the rotary shaft 23, when a rotation about the axis perpendicular to the rotary shaft 23 is not allowed among a rotation about the rotary shaft 23, a movement in a direction along an axis perpendicular to the rotary shaft 23, and a rotation about the axis perpendicular to the rotary shaft 23 other movements or rotations may be allowed. Further, it should be understood that the sub-frame 14 may be movable in a direction along the rotary shaft 23 about the main frame 13. Further, the sub-frame 14 may be movable in one direction about the main frame 13
  • FIG. 6 illustrates an axial cross-sectional view of a scroll compressor according to an embodiment of the disclosure.
  • a scroll compressor 2 is a compressor widely used for an air conditioner, a freezer, and a heat pump.
  • FIG. 6 illustrates a longitudinal sectional view of a hermetic scroll compressor used in a refrigerant circuit of an air conditioner.
  • the scroll compressor 2 includes a compression portion 10 configured to compress a refrigerant, a drive motor 20 configured to drive the compression portion 10, and a casing 30 corresponding to a body configured to receive the compression portion 10 and the drive motor 20.
  • the scroll compressor 2 is a vertical scroll compressor in which an axial direction of a rotary shaft 23, which will be described later, of the drive motor 20 is coincident with the gravity direction.
  • the axial direction of the rotary shaft 23 will be referred to as "vertical direction”, and based on FIG. 6, the up side may be referred to as “upper side” and the down side may be referred to as "lower side".
  • the vertical scroll compressor is described as an example, an embodiment of the disclosure will be applicable to a horizontal scroll compressor.
  • the compression portion 10 may include a fixed scroll 11 fixed to the casing 30, an orbiting scroll 12 orbiting by being engaged with the fixed scroll 11, a main frame 13 fixed to the casing 30 and configured to support the fixed scroll 11, a sub frame 14 arranged between a rotary shaft 23 and the main frame 13 and configured to support the orbiting scroll 12, and an Oldham ring 15 configured to allow the orbiting scroll 12 to orbit without pivoting the orbiting scroll 12.
  • the fixed scroll 11 may include a fixed scroll body and a fixed wrap 114 protruding from the fixed scroll body.
  • the fixed wrap 114 may protrude downward from the fixed scroll body.
  • the fixed scroll body may include a cylindrical body portion 111, a plate 112 configured to cover an opening in an upper side of the body portion 111, and a protrusion 113 extending from a lower end of the body portion 111 in radially outward direction.
  • the fixed wrap 114 may protrude downward from a lower end of the plate 112 and have a spiral shape when viewed from the bottom.
  • the fixed scroll 11 may be formed of cast iron such as gray cast iron FC 250.
  • the body portion 111 may be provided with a through hole 111a in the radial direction.
  • the though hole 111a may serve as a suction port configured to suction the refrigerant into a space surrounded by the body portion 111, the plate 112 and the orbiting scroll 12.
  • a through hole 112a in the vertical direction is formed at the center of the plate 112.
  • the through hole 112a may serve as a discharge port configured to discharge the refrigerant from the space surrounded by the plate 112, the fixed wrap 114 and the orbiting scroll 12.
  • the fixed scroll 11 constructed as described above is fixed to the main frame 13 by a positioning means such as a bolt or a positioning pin passed through the through hole in the vertical direction formed in the protrusion 113.
  • the orbiting scroll 12 may include an orbiting scroll body and an orbiting wrap 122 protruding from the orbiting scroll body to form a compression chamber 16 by being engaged with the fixed wrap 114 of the fixed scroll 11.
  • the orbiting wrap 122 may protrude upward from the orbiting scroll body.
  • the orbiting scroll body may include a plate 121 having a disk shape, and a cylindrical body portion 123 protruding downward from a lower end of the plate 121.
  • the orbiting wrap 122 may protrude upward from an upper end of the plate 121 and have a spiral shape when viewed from the top.
  • the orbiting scroll 12 may be formed of FC material or FCD material.
  • the orbiting wrap 122 of the orbiting scroll 12 may be engaged with the fixed wrap 114 of the fixed scroll 11. Further, the orbiting wrap 122 of the orbiting scroll 12 and the fixed wrap 114 of the fixed scroll 11 may be placed in a space formed by the body portion 111 and the plate 112 of the fixed scroll 11 and the plate 121 so as to form the compression chamber 16. Because the orbiting wrap 122 is circularly moved about the fixed wrap 114 that is fixed, a volume of the compression chamber 16 is reduced and the refrigerant of the compression chamber 16 is compressed. In other words, as an internal space between the fixed wrap 114 and the orbiting wrap 122 is reduced toward a center of rotation, the refrigerant is compressed.
  • An eccentric shaft 232 of the rotary shaft 23, which is described later, is inserted into the body portion 123 through a sliding bearing. Therefore, the body portion 123 functions as a bearing of the eccentric shaft 232.
  • the main frame 13 is an example of a holding member configured to hold the fixed scroll 11.
  • the main frame 13 may include a cylindrical first body portion 131, a cylindrical second body portion 132 protruding downward from the radially inner side of the lower end of the first body portion 131, and a cylindrical third body portion 133 protruding radially inwardly from the lower end of the second body portion 132.
  • a through hole 133a to which the rotary shaft 23 is inserted may be provided in the third body portion 133.
  • An outer circumferential surface of the first body portion 131 of the main frame 13 is fixed to a central casing 31 of the casing 30, which is described later.
  • the main frame 13 does not support the rotary shaft 23 of a drive motor 20, which is described later, according to an embodiment.
  • a protrusion 131a protruding upward from the upper end surface is installed on an outer circumferential portion of the first body portion 131.
  • a female screw is formed in the protrusion 131a, and a bolt, which passed through the through hole formed in the protrusion 113 of the fixed scroll 11, is engaged with the female screw. Therefore, the fixed scroll 11 is installed to the main frame 13.
  • a groove 131b elongating in the vertical direction may be provided on the outer circumferential portion of the first body portion 131. That is, in the first body portion 131, the groove 131b extending in the vertical direction from the center to the lower portion of the outer circumferential portion may be formed. In the first body portion 131, a portion where the groove 131b is formed may be spaced apart from a central casing 31.
  • the main frame 13 may further include a fixed scroll support surface 11a configured to support the fixed scroll 11.
  • the fixed scroll support surface 11a may be formed on the protrusion 131a.
  • the sub-frame 14 is an example of a support member for supporting the orbiting scroll 12.
  • a gap may be formed between the main frame 13 and the sub frame 14 to allow the sub frame 14 to be movable about the main frame 13.
  • the sub-frame 14 may be arranged inside the main frame 13 to be spaced apart from the main frame 13.
  • the sub-frame 14 may include a cylindrical first body portion 141, a cylindrical second body portion 142 protruding downward from a lower end surface of the first body portion 141, and a cylindrical third body portion 143 protruding downward from an inner end surface of the second body portion 142.
  • the third body portion 143 may have a smaller width than the first body portion 141 and the second body portion 142. Particularly, a width of the inner circumferential surface of the third body portion 143 may be smaller than a width of an inner circumferential surface of the first body portion 141 and a width of an inner circumferential surface of the second body portion 142.
  • the third body portion 143 may be inserted into the shaft through hole 133a to be positioned between the rotary shaft 23 and the third body portion 133 of the main frame 13.
  • the sub-frame 14 functions as a bearing for rotatably supporting the rotary shaft 23.
  • the sub-frame 14 may be configured to be movable about the main frame 13 along at least one of the axial direction of the rotary shaft 23 and the direction perpendicular to the axial direction of the rotary shaft 23.
  • the sub-frame 14 may be arranged between the rotary shaft 23 and the main frame 13 with a gap allowing the sub-frame 14 to be movable in the axial direction of the rotary shaft 23 about the main frame 13 and to be movable in a rotational direction about a virtual axis approximately perpendicular to the rotary shaft 23.
  • a first groove 141a and a second groove 141b recessed downward from an upper end surface are formed.
  • the first groove 141a is formed in the center portion
  • the second groove 141b is formed between the first groove 141a and the protrusion 131a.
  • the body portion 123 of the orbiting scroll 12 is inserted into the first groove 141a.
  • the Oldham ring 15 preventing a pivot of the orbiting scroll 12 is arranged between the main frame 13 and the orbiting scroll 12.
  • a discharge passage discharging refrigerant compressed in the compression chamber 16 is formed.
  • the discharge passage configured to discharge the high-pressure refrigerant one end thereof is connected to the through hole 112a of the plate 112, which is configured to discharge the high-pressure refrigerant from the space surrounded by the fixed scroll 11 and the orbiting scroll 12, and the other end thereof is connected to a space lower than the main frame 13 in the casing 30 and further connected to the chamber 121a.
  • a discharge passage configured to discharge an intermediate pressure refrigerant
  • one end thereof is connected to a discharge port, which is configured to discharge a refrigerant from a space which has the intermediate-pressure refrigerant and is surrounded by the fixed scroll 11 and the orbiting scroll 12, and the other end thereof is connected to the chamber 121b and 142a.
  • the orbiting scroll 12 is about to incline due to a compressive load of the gas.
  • FIG. 7A is a perspective view illustrating a moment that an orbiting scroll receives.
  • the orbiting scroll 12 receives a compressive load F t from a direction orthogonal to an eccentric direction of the eccentric shaft 232 on a plane, from the main shaft 231 of the rotary shaft 23. Therefore, in the orbiting scroll 12, a clockwise moment M S as viewed from a viewpoint A is generated.
  • FIG. 7B is a view illustrating a shape in which the orbiting scroll is about to incline.
  • FIG. 7B is a view illustrating a case in which the orbiting scroll 12 is about to incline when viewed from the viewpoint A of FIG. 7A.
  • the orbiting scroll 12 receives a compressive load F t and generates a clockwise moment load and thus the orbiting scroll is about to incline.
  • the sub-frame 14 receives a lateral load from the shaft, and thus tries to move in the load direction.
  • FIG. 8 illustrates an axial cross-sectional view of a compression portion and a rotary shaft when a moment applied to a sub frame is in the same direction as a moment applied to the orbiting scroll.
  • a position supporting a lateral load F MJ in the axis is opposite to the orbiting scroll 12 in relation to the lateral load F MJ , as illustrated in FIG. 8.
  • a reaction force R MJ applied to the sub-frame 14 is generated in a position as illustrated in FIG. 8 as a protrusion 135 of the main frame 13 comes in contact with the sub-frame 14. Therefore, it is hard to effectively suppress an inclination of the orbiting scroll 12 because the moment M F applied to the sub-frame 14 and the moment M S applied to the orbiting scroll 12 are generated in the clockwise direction.
  • the sub-frame 14 it is possible to suppress the inclination of the orbiting scroll 12 by generating a moment in the direction opposite to the orbiting scroll 12, in the sub-frame 14 by using the lateral load.
  • This is an example of allowing the sub-frame 14 to be movable in a direction opposite to the moment generated in the orbiting scroll 12 among rotational directions about a virtual axis approximately orthogonal to the rotary shaft 23.
  • FIG. 9 illustrates an axial cross-sectional view of the compression portion and the rotary shaft when a moment applied to a sub frame is in an opposite direction to a moment applied to the orbiting scroll.
  • a position supporting a lateral load F MJ in the axis is in the same side as the orbiting scroll 12 in relation to the lateral load F MJ , as illustrated in FIG. 9.
  • a reaction force R MJ applied to the sub-frame 14 is generated in a position as illustrated in FIG. 9 as a protrusion 136 formed in an inner circumferential surface of the main frame 13 comes in contact with the sub-frame 14. Therefore, it is possible to effectively suppress the inclination of the orbiting scroll 12 because the moment M F applied to the sub-frame 14 is generated in the counterclockwise direction.
  • L1 is a position of an end surface the third body portion 143 of the sub-frame 14 in the orbiting scroll 12 side. When the end surface is inclined, it may be the lowest position of the end surface.
  • L1 is an example of a position of an end surface of a rotary shaft bearing of the support member in the orbiting scroll side.
  • L2 is a position of a surface on which the orbiting wrap 122 of the plate 121 of the orbiting scroll 12 is formed.
  • the plate 121 of the orbiting scroll 12 may include an orbiting warp forming surface 121aa on which the orbiting wrap 122 is formed, and L2 is a position of the orbiting wrap forming surface 121aa. When this surface is inclined, it may be the uppermost position of the surface.
  • L2 is an example of a position of a surface on which the plate of the orbiting scroll is engaged with the fixed scroll.
  • the first body portion 131 of the main frame 13 and the first body portion 141 of the sub-frame 14 may be in contact before the third body portion 133 of the main frame 13 and the third body portion 143 of the sub-frame 14 are in contact. That is, when the sub-frame 14 is inclined upon the movement, the protrusion 136 of the main frame 13 and the first body portion 141 of the sub-frame 14 may be in contact before the third body portion 133 of the main frame 13 and the third body portion 143 of the sub-frame 14 are in contact.
  • the first body portion 131 of the main frame 13 and the first body portion 141 of the sub-frame 14 may be in contact before the third body portion 133 of the main frame 13 and the third body portion 143 of the sub-frame 14 are in contact.
  • a gap between the first body portion 131 of the main frame 13 and the first body portion 141 of the sub-frame 14 is less than a gap between the third body portion 133 of the main frame 13 and the third body portion 143 of the sub-frame 14. It is an example in which as for a position receiving a load about the rotary shaft, the smallest gap with the holding member in the same side as the orbiting scroll is less than the smallest gap with the holding member in the opposite side to the orbiting scroll.
  • a position of the gap between the first body portion 131 of the main frame 13 and the first body portion 141 of the sub-frame 14 may be between L1 and L2 as illustrated in FIG. 9.
  • L1 is a position of an end surface the third body portion 143 of the sub-frame 14 in the orbiting scroll 12 side. When the end surface is inclined, it may be the lowest position of the end surface.
  • L1 is an example of a position of an end surface of a rotary shaft bearing of the support member in the orbiting scroll side.
  • L2 is a position of a surface on which the orbiting wrap 122 of the plate 121 of the orbiting scroll 12 is formed. When this surface is inclined, it may be the uppermost position of the surface.
  • L2 is an example of a position of a surface on which the plate of the orbiting scroll is engaged with the fixed scroll.
  • the sub-frame 14 may include a thrust bearing 144 having an orbiting scroll support surface 144a supporting the orbiting scroll 12.
  • the thrust bearing 144 may have an elastically deformable shape.
  • an outer circumferential side of the thrust bearing 144 of the sub-frame 14 may be inclined and thus when being in contact with one surface of the orbiting scroll 12, on which the orbiting scroll 12 is not formed, the thrust bearing 144 of the sub-frame 14 may be elastically deformed. In this way, the thrust load is distributed to suppress local contact.
  • the shape of the thrust bearing 144 shown in FIG. 9 is not limited thereto, and thus the thrust bearing 144 may have a variety of shapes as long as being elastically deformed.
  • the thrust bearing 144 is an example of a part of the support member for supporting the orbiting scroll
  • the shape of the thrust bearing 144 of FIG. 9 is an example of a shape that is elastically deformed upon being in contact with a surface, on which the plate of the orbiting scroll is not engaged with the fixed scroll, due to the inclination of the orbiting scroll.
  • FIG. 10 illustrates an axial cross-sectional view of a compression portion and a rotary shaft according to an implementation example of the scroll compressor.
  • a compression portion 10 according to an implementation of the scroll compressor 2 may include a fixed scroll 11, an orbiting scroll 12, a main frame 13, a sub-frame 14, and an Oldham ring 15 as illustrated in FIG. 1.
  • the Oldham ring 15 is coupled to or engaged with the orbiting scroll 12 and the sub-frame 14.
  • one pair (two pieces) of Oldham ring guide grooves 121g are formed on a lower surface of the plate 121 of the orbiting scroll 12 in a substantially straight line.
  • One pair (two pieces) of key portions 15b formed on an upper surface of a ring portion 15a of the Oldham ring 15 may be slidably coupled to or engaged with the Oldham ring guide grooves 121g.
  • one pair (two pieces) of Oldham ring guide grooves 141g having a phase difference of approximately 90 ° with the Oldham ring guide groove 121g of the orbiting scroll 12 are formed on an upper surface of the first body portion 141 of the sub-frame 14 in a substantially straight line.
  • One pair (two pieces) of key portions 15c formed on a lower surface of the ring portion 15a of the Oldham ring 15 may be slidably coupled to or engaged with the Oldham ring guide grooves 141g.
  • the orbiting scroll 12 may perform an orbital movement without pivoting.
  • FIG. 11 illustrates an axial cross-sectional view of a compression portion and a rotary shaft according to an implementation of the scroll compressor.
  • a compression portion 10 according to an implementation of the scroll compressor 2 may include a fixed scroll 11, an orbiting scroll 12, a main frame 13, a sub-frame 14, and an Oldham ring 15 as illustrated in FIG. 1.
  • the Oldham ring 15 is coupled to or engaged with the orbiting scroll 12 and the sub-frame 14.
  • one pair (two pieces) of Oldham ring guide grooves 121g are formed on a lower surface of the plate 121 of the orbiting scroll 12 in a substantially straight line.
  • One pair (two pieces) of key portions 15b formed on an upper surface of a ring portion 15a of the Oldham ring 15 may be slidably coupled to or engaged with the Oldham ring guide grooves 121g.
  • one pair (two pieces) of Oldham ring guide grooves 131g having a phase difference of approximately 90 ° with the Oldham ring guide groove 121g of the orbiting scroll 12 are formed on an upper surface of the first body portion 131 of the main frame 13 in a substantially straight line.
  • One pair (two pieces) of key portions 15d formed on a lower surface of the ring portion 15a of the Oldham ring 15 may be slidably coupled to or engaged with the Oldham ring guide grooves 131g.
  • the orbiting scroll 12 may perform an orbital movement without pivoting.
  • FIG. 12 illustrates an axial cross-sectional view of a compression portion and a rotary shaft according to an implementation of the scroll compressor.
  • a compression portion 10 according to an implementation of the scroll compressor 2 may include a fixed scroll 11, an orbiting scroll 12, a main frame 13, a sub-frame 14, and an Oldham ring 15 as illustrated in FIG. 1.
  • the Oldham ring 15 is coupled to or engaged with the orbiting scroll 12 and the fixed scroll 11.
  • one pair (two pieces) of Oldham ring guide grooves 121g are formed on a lower surface of the plate 121 of the orbiting scroll 12 in a substantially straight line.
  • One pair (two pieces) of key portions 15b formed on an upper surface of a ring portion 15a of the Oldham ring 15 may be slidably coupled to or engaged with the Oldham ring guide grooves 121g.
  • one pair (two pieces) of Oldham ring guide grooves 112g having a phase difference of approximately 90 ° with the Oldham ring guide groove 121g of the orbiting scroll 12 are formed on a lower surface of the plate 112 of the fixed scroll 11 in a substantially straight line.
  • One pair (two pieces) of key portions 15e formed on an upper surface of the ring portion 15a of the Oldham ring 15 may be slidably coupled to or engaged with the Oldham ring guide grooves 112g.
  • the orbiting scroll 12 may perform an orbital movement without pivoting.
  • a space surrounded by the main frame 13 and the sub-frame 14 is formed by two sealing members between the main frame 13 and the sub-frame 14.
  • the sub-frame 14 may be pushed against the orbiting scroll 12 by guiding a certain pressure (intermediate pressure) from the compression chamber 16 during the compression operation in this space.
  • two methods may be mainly used, and it will be described in detail with some modifications.
  • FIG. 13 illustrates an axial cross-sectional view of a compression portion and a rotary shaft of a modification of the scroll compressor according to an embodiment of the disclosure.
  • FIG. 13 illustrates an axial cross-sectional view of the compression portion 10 and the rotary shaft 23 according to a modification of the scroll compressor 2.
  • a compression portion 10 according to a modification of the scroll compressor 2 may include a fixed scroll 11, an orbiting scroll 12, a main frame 13, and a sub-frame 14, as illustrated in FIG. 6.
  • the orbiting scroll 12 orbits by being engaged with the fixed scroll 11 so as to form a compression chamber 16.
  • the compression chamber 16 sucks and compresses a low pressure refrigerant as indicated by an arrow in a through hole 111a in the radial direction, and discharges a high pressure refrigerant as indicated by an arrow in a through hole 112a in a vertical direction.
  • a description of the Oldham ring 15 will be omitted.
  • a sealing member 171a configured to seal a gap between a body portion 123 of the orbiting scroll 12 and a third body portion 143 of the sub-frame 14 is provided. According to a modification, by providing the sealing member 171a, a chamber 171 is formed and the chamber 171 is maintained at a high pressure.
  • sealing members 172a and 172b configured to seal a gap between the main frame 13 and the sub-frame 14 may be provided in the compression portion 10 so as to form a chamber 172 between the main frame 13 and the sub-frame 14.
  • the sealing member 172a configured to seal a gap between a second body portion 132 of the main frame 13 and the first body portion 141 of the sub-frame 14 is provided, and at the same time, the sealing member 172b configured to seal a gap between a third body portion 133 of the main frame 13 and the third body portion 143 of the sub-frame 14 is provided.
  • These sealing members 172a and 172b correspond to the two sealing members described above.
  • the chamber 172 is formed by providing the sealing members 172a and 172b.
  • passages 181, 182 and 183 configured to guide refrigerant discharged from the compression chamber 16 to the chamber 172 may be provided.
  • the first passage 181, the second passage 182, and the third passage 183 configured to guide a refrigerant at a certain pressure from the compression chamber 16 to the chamber 172 are provided.
  • the first passage 181 may be provided in the orbiting scroll 12 to communicate with the compression chamber 16.
  • the first passage 181 is a passage passing through the inside of the orbiting scroll 12 and is an example of an internal passage of the orbiting scroll. The first passage 181 moves the refrigerant out of the compression chamber 16 and introduces the refrigerant into the second passage 182.
  • the second passage 182 may be provided in the fixed scroll 11 to connect the first passage 181 to the third passage 183.
  • the second passage 182 is a passage passing through the fixed scroll 11 and is an example of an internal passage of the fixed scroll.
  • the second passage 182 moves the refrigerant introduced from the first passage 181 and introduces the refrigerant into the third passage 183.
  • the third passage 183 may be provided in the main frame 13 to communicate with the chamber 172.
  • the third passage 183 is a passage passing through the main frame 13 and is an example of an internal passage of the holding member.
  • the third passage 183 moves the refrigerant introduced from the second passage 182 and introduces the refrigerant into the chamber 172. Accordingly, the pressure in the chamber 172 is maintained at a certain intermediate pressure.
  • FIG. 14 is a top view illustrating an end portion of a plate of the orbiting scroll in the compression portion when viewed from the top, according to a modification of the scroll compressor according to an embodiment of the disclosure.
  • FIG. 14 illustrates a plan view of the end portion of the plate 121 of the orbiting scroll 12 when viewed from the top.
  • an inlet 181a of the first passage 181 is provided in a region 125a (a region on the right side of a dotted line arc) facing the compression chamber 16, and an outlet 181b of the first passage 181 is provided in a region 125b (a region on the left side of the dotted line arc) being in contact with the body portion 111 of the fixed scroll 11.
  • the first passage 181 is not actually visible, but the first passage 181 is shown in dotted lines in the drawing for clarity.
  • the inlet 181a of the first passage 181 is illustrated to be arranged in a region fitted in two orbiting wraps 122 which are the outmost and adjacent to each other, but the position of the inlet 181a is not limited thereto. Therefore, a position of the inlet 181a may be selected according to the magnitude of the intermediate pressure to be directed to the chamber 172. Therefore, the desired intermediate pressure refrigerant in the compression chamber 16 flows to the first passage 181.
  • FIG. 15 is a bottom view illustrating a body portion of the fixed scroll in the compression portion when viewed from the bottom, according to a modification of the scroll compressor according to an embodiment of the disclosure.
  • FIG. 15 illustrates a bottom view of the body portion 111 of the fixed scroll 11 when viewed from the bottom.
  • an inlet 182a of the second passage 182 is provided in a region 115a (a region on the right side of a dotted line arc) being in contact with the plate 121 of the orbiting scroll 12 and an outlet 182b of the second passage 182 is provided in a region 115b (a region on the left side of the dotted line arc) being in contact with the main frame 13.
  • the second passage 182 is not actually visible, but the second passage 182 is shown in dotted lines in the drawing for clarity.
  • the inlet 182a of the second passage 182 is provided in a point on a track 181c of the outlet 181b of the first passage 181 upon the orbit of the orbiting scroll 12. Therefore, a certain range of intermediate pressure refrigerant in the compression chamber 16 that the inlet 181a faces flows from the first passage 181 to the second passage 182.
  • FIG. 16 illustrates an axial cross-sectional view of a compression portion and a rotary shaft of a modification of the scroll compressor according to an embodiment of the disclosure.
  • FIG. 16 illustrates an axial cross-sectional view of the compression portion 10 and the rotary shaft 23 according to a modification of the scroll compressor 2.
  • a compression portion 10 according to a modification of the scroll compressor 2 may further include a counter bore 184, which is arranged between the first passage 181 and the second passage 182 in comparison with the compression portion 10 according to a modification of the scroll compressor 2 illustrated in FIG. 13.
  • FIG. 17 is a bottom view illustrating a body portion of a fixed scroll in the compression portion when viewed from the bottom, according to a modification of the scroll compressor according to an embodiment of the disclosure.
  • an inlet 182a of the second passage 182 is provided in a region 115a (a region on the right side of a dotted line arc) being in contact with the plate 121 of the orbiting scroll 12 and an outlet 182b of the second passage 182 is provided in a region 115b (a region on the left side of the dotted line arc) being in contact with the main frame 13.
  • the second passage 182 is not actually visible, but the second passage 182 is shown in dotted lines in the drawing for clarity.
  • the inlet 182a of the second passage 182 is provided to be in contact with the counter bore 184 corresponding to an example of a groove portion covering an entire of a track 181c of the outlet 181b of the first passage 181 upon the orbit of the orbiting scroll 12. Therefore, an intermediate pressure refrigerant in the compression chamber 16 that the inlet 181a faces flows from the first passage 181 to the second passage 182.
  • the inlet 182a of the second passage 182 is provided to be in contact with the counter bore 184 covering an entire of the track 181c of the outlet 181b of the first passage 181 upon the orbit of the orbiting scroll 12, but is not limited thereto.
  • the inlet 182a of the second passage 182 is provided to be in contact with the counter bore 184 covering a part of of the track 181c of the outlet 181b of the first passage 181 upon the orbit of the orbiting scroll 12. That is, the inlet 182a of the second passage 182 may be in communication with the outlet 181b of the first passage 181 for at least a part of a cycle in which the orbiting scroll 12 orbits.
  • the first passage 181 configured to move the refrigerant out of the compression chamber 16 and introduce the refrigerant into the second passage 182 in the fixed scroll 11 is provided in the orbiting scroll 12
  • the second passage 182 configured to introduce the refrigerant introduced from the first passage 181 in the orbiting scroll 12 to the third passage 183 in the main frame 13 is provided in the fixed scroll 11, but is not limited thereto.
  • a passage configured to move a refrigerant out of the compression chamber 16 and directly introduce the refrigerant into the third passage 183 of the main frame 13 is provided in the fixed scroll 11.
  • it is configured to introduce the intermediate pressure from the compression chamber 16 to the chamber 172 by forming the chamber 172 between the main frame 13 and the sub-frame 14 by sealing the gap between the main frame 13 and the sub-frame 14 by using the sealing member 172a and 172b, on the assumption of the shape of the main frame 13 and the sub-frame 14 as illustrated in FIGS. 6, 10 and 12, but is not limited thereto.
  • it may be configured to introduce the intermediate pressure from the compression chamber 16 to the chamber by forming the chamber between the main frame 13 and the sub-frame 14 by sealing the gap between the main frame 13 and the sub-frame 14 by using the two sealing members, on the assumption of the shape of the main frame 13 and the sub-frame 14 as illustrated in FIG. 11.
  • the intermediate pressure may be introduced from the compression chamber 16 to the chamber 172.
  • the space formed by the chamber 142a and the chamber 121b of FIG. 5 corresponds to the chamber 172 of FIGS. 13 to 16
  • the intermediate pressure may be introduced from the compression chamber 16 to the chamber 172.
  • introducing the intermediate pressure from the compression chamber 16 to the chamber 172 by forming the chamber 172 between the main frame 13 and the sub-frame 14 by sealing the gap between the main frame 13 and the sub-frame 14 by using the sealing member 172a and 172b may include introducing the intermediate pressure from the compression chamber 16 to the chamber 172 by forming an inner space at least between the main frame 13 and the sub-frame 14 by sealing at least a gap between the main frame 13 and the sub-frame 14 by using the sealing mechanism.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)

Abstract

L'invention concerne un compresseur à spirales pouvant optimiser une position d'application d'une charge à partir d'un élément de support vers une spirale orbitale. Le compresseur à spirales comprend une spirale fixe fixée à l'intérieur d'un corps, une spirale orbitale conçue pour orbiter en prise avec la spirale fixe, un arbre rotatif conçu pour permettre à la spirale orbitale d'orbiter, un élément de retenue conçu pour retenir la spirale fixe à partir d'un côté opposé à la spirale orbitale, et un élément de support agencé entre l'arbre rotatif et l'élément de retenue afin de porter la spirale orbitale au moyen d'une charge appliquée à une position éloignée d'un centre de la spirale orbitale.
EP19864598.8A 2018-09-28 2019-09-26 Compresseur à spirales Active EP3824186B1 (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
JP2018183776 2018-09-28
JP2019001138A JP2020056394A (ja) 2018-09-28 2019-01-08 スクロール圧縮機
KR1020190112190A KR102671683B1 (ko) 2018-09-28 2019-09-10 스크롤 압축기
PCT/KR2019/012532 WO2020067739A1 (fr) 2018-09-28 2019-09-26 Compresseur à spirales

Publications (3)

Publication Number Publication Date
EP3824186A1 true EP3824186A1 (fr) 2021-05-26
EP3824186A4 EP3824186A4 (fr) 2021-09-22
EP3824186B1 EP3824186B1 (fr) 2023-08-23

Family

ID=70106804

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19864598.8A Active EP3824186B1 (fr) 2018-09-28 2019-09-26 Compresseur à spirales

Country Status (4)

Country Link
EP (1) EP3824186B1 (fr)
JP (1) JP2020056394A (fr)
KR (1) KR102671683B1 (fr)
CN (1) CN112771272B (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20230046430A (ko) * 2021-09-30 2023-04-06 삼성전자주식회사 스크롤 압축기
KR102376644B1 (ko) 2022-01-24 2022-03-21 주식회사 우드메탈 높낮이 조절 책상 및 걸상
KR102454708B1 (ko) 2022-02-28 2022-10-14 주식회사 우드메탈 높낮이 조절 책걸상
KR102385450B1 (ko) 2022-02-28 2022-04-12 주식회사 우드메탈 높낮이 조절 책걸상
KR102637329B1 (ko) 2023-12-28 2024-02-20 (주)캠퍼스라인 책걸상용 높이 조절장치

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5641978B2 (fr) 1973-05-07 1981-10-01
JP3661454B2 (ja) * 1998-11-20 2005-06-15 三菱電機株式会社 スクロ−ル圧縮機
JP3863685B2 (ja) * 1999-05-31 2006-12-27 三菱電機株式会社 スクロール圧縮機
JP5641978B2 (ja) * 2011-02-28 2014-12-17 三菱電機株式会社 スクロール圧縮機
DE112013006437B4 (de) * 2013-01-16 2019-10-31 Mitsubishi Electric Corporation Hermetischer Verdichter und Kältekreislaufvorrichtung vom Dampfkompressions-Typ mit einem derartigen hermetischen Verdichter
JP6274281B1 (ja) * 2016-08-31 2018-02-07 ダイキン工業株式会社 スクロール圧縮機

Also Published As

Publication number Publication date
KR20200037730A (ko) 2020-04-09
KR102671683B1 (ko) 2024-06-10
CN112771272B (zh) 2023-03-24
EP3824186B1 (fr) 2023-08-23
EP3824186A4 (fr) 2021-09-22
JP2020056394A (ja) 2020-04-09
CN112771272A (zh) 2021-05-07

Similar Documents

Publication Publication Date Title
EP3824186A1 (fr) Compresseur à spirales
WO2018164393A1 (fr) Compresseur à spirale
WO2017175945A1 (fr) Compresseur actionné par moteur
WO2018208024A1 (fr) Compresseur à spirale
WO2018190520A1 (fr) Compresseur à spirale
WO2017188557A1 (fr) Compresseur à spirales
WO2019045298A1 (fr) Compresseur à spirale
WO2021002629A1 (fr) Moteur et compresseur le comprenant
WO2017188575A1 (fr) Compresseur à spirale
WO2018194294A1 (fr) Compresseur rotatif
WO2017188576A1 (fr) Compresseur à spirale
WO2014123325A1 (fr) Compresseur rotatif à palette
WO2021045361A1 (fr) Compresseur rotatif et appareil domestique le comprenant
WO2017188574A1 (fr) Compresseur à spirale
WO2021015392A1 (fr) Compresseur à spirale
WO2020067739A1 (fr) Compresseur à spirales
WO2020116781A1 (fr) Compresseur à spirale haute pression
WO2018190544A1 (fr) Compresseur à spirale
WO2018199488A1 (fr) Compresseur à spirale
WO2021215652A1 (fr) Compresseur
WO2021010721A1 (fr) Compresseur à spirale
WO2021215651A1 (fr) Compresseur
WO2018174449A1 (fr) Compresseur hermétique
WO2023204354A1 (fr) Compresseur à spirales
WO2021040360A1 (fr) Compresseur à spirale

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: 20210216

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

A4 Supplementary search report drawn up and despatched

Effective date: 20210820

RIC1 Information provided on ipc code assigned before grant

Ipc: F04C 27/00 20060101ALI20210816BHEP

Ipc: F04C 23/00 20060101ALI20210816BHEP

Ipc: F01C 21/00 20060101ALI20210816BHEP

Ipc: F04C 29/12 20060101ALI20210816BHEP

Ipc: F04C 29/00 20060101ALI20210816BHEP

Ipc: F04C 18/02 20060101AFI20210816BHEP

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

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

Free format text: STATUS: GRANT OF PATENT IS INTENDED

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

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

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

INTG Intention to grant announced

Effective date: 20230629

AK Designated contracting states

Kind code of ref document: B1

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

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602019035826

Country of ref document: DE

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

Ref country code: DE

Payment date: 20230920

Year of fee payment: 5

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20230823

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1602864

Country of ref document: AT

Kind code of ref document: T

Effective date: 20230823

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

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231124

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

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231223

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

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231226

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231123

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231223

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231124

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

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

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

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

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

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

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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

Ref country code: LU

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

Effective date: 20230926

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20230930

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

Ref country code: LU

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

Effective date: 20230926

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823