WO2014189240A1 - Scroll compressor - Google Patents
Scroll compressor Download PDFInfo
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- WO2014189240A1 WO2014189240A1 PCT/KR2014/004460 KR2014004460W WO2014189240A1 WO 2014189240 A1 WO2014189240 A1 WO 2014189240A1 KR 2014004460 W KR2014004460 W KR 2014004460W WO 2014189240 A1 WO2014189240 A1 WO 2014189240A1
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- WIPO (PCT)
- Prior art keywords
- compression chamber
- bypass holes
- compression
- scroll compressor
- larger
- Prior art date
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/02—Rotary-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
- F04C18/0207—Rotary-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
- F04C18/0246—Details concerning the involute wraps or their base, e.g. geometry
- F04C18/0253—Details concerning the base
- F04C18/0261—Details of the ports, e.g. location, number, geometry
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C14/00—Control of, monitoring of, or safety arrangements for, machines, pumps or pumping installations
- F04C14/24—Control of, monitoring of, or safety arrangements for, machines, pumps or pumping installations characterised by using valves controlling pressure or flow rate, e.g. discharge valves or unloading valves
- F04C14/26—Control of, monitoring of, or safety arrangements for, machines, pumps or pumping installations characterised by using valves controlling pressure or flow rate, e.g. discharge valves or unloading valves using bypass channels
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/02—Rotary-piston machines or engines 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
- F01C1/0207—Rotary-piston machines or engines 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
- F01C1/0215—Rotary-piston machines or engines 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/02—Rotary-piston machines or engines 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
- F01C1/0207—Rotary-piston machines or engines 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
- F01C1/0246—Details concerning the involute wraps or their base, e.g. geometry
- F01C1/0253—Details concerning the base
- F01C1/0261—Details of the ports, e.g. location, number, geometry
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C15/00—Component parts, details or accessories of machines, pumps or pumping installations, not provided for in groups F04C2/00 - F04C14/00
- F04C15/06—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/02—Rotary-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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/02—Rotary-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
- F04C18/0207—Rotary-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
- F04C18/0215—Rotary-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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/02—Rotary-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
- F04C18/0207—Rotary-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
- F04C18/0246—Details concerning the involute wraps or their base, e.g. geometry
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C28/00—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids
- F04C28/24—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids characterised by using valves controlling pressure or flow rate, e.g. discharge valves or unloading valves
- F04C28/26—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids characterised by using valves controlling pressure or flow rate, e.g. discharge valves or unloading valves using bypass channels
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/12—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/80—Other components
- F04C2240/808—Electronic circuits (e.g. inverters) installed inside the machine
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2270/00—Control; Monitoring or safety arrangements
- F04C2270/19—Temperature
- F04C2270/195—Controlled or regulated
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2270/00—Control; Monitoring or safety arrangements
- F04C2270/80—Diagnostics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2270/00—Control; Monitoring or safety arrangements
- F04C2270/86—Detection
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C23/00—Combinations 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
- F04C23/008—Hermetic pumps
Definitions
- the present disclosure relates to a scroll compressor, and more particularly, to a scroll compressor formed to have different volume reduction gradients for both compression chambers.
- Scroll compressor is a compressor in which an compression chamber continuously moving between a fixed wrap and an orbiting wrap while an orbiting scroll performs orbiting movement with respect to a fixed scroll in a state that the fixed wrap of the fixed scroll is engaged with the orbiting wrap of the orbiting scroll is formed to inhale and compress refrigerant.
- the scroll compressor continuously performs inhalation, compression and discharge, and thus has excellent characteristics in terms of vibration and noise generated during its operational process compared to other types of compressors.
- the behavior characteristic of a scroll compressor is determined by its type of the fixed wrap and orbiting wrap.
- the fixed wrap and orbiting wrap may have an arbitrary shape, but typically have an involute curved shape that can be easily processed.
- the involute curve denotes a curve corresponding to a trajectory drawn by a cross section of thread when unloosing thread wound around a base circle having an arbitrary radius.
- the capacity change rate is constant because a thickness of the wrap is constant and thus the number of turns should be increased to obtain a high compression ratio, but in this case, there is a drawback of increasing the size of the compressor at the same time.
- a orbiting wrap is typically formed at one side of a disk-shaped end plate and a boss portion is formed at a rear surface on which the orbiting wrap is not formed and connected to a rotation shaft for orbiting the circular scroll.
- Such a shape may form a orbiting wrap over a substantially overall area of the end plate, thereby decreasing a diameter of the end plate portion for obtaining the same compression ratio.
- the operating point to which a repulsive force of refrigerant is applied and the operating point to which a reaction force for cancelling out the repulsive force is applied are separated from each other in an axial direction, thereby causing a problem of increasing vibration or noise while the behavior of the circular scroll is unstabilized during the operational process.
- a so-called shaft penetration scroll compressor in which a position at which the rotation shaft 1 and the circular scroll 2 are coupled to each other is formed on the same surface as that of the orbiting wrap 2a.
- the operating point of a repulsive force and the operating point of the reaction force are applied at the same position, thereby solving a problem that the circular scroll 2 is inclined.
- An object of the present disclosure is to provide a scroll compressor capable of minimizing over-compression loss in a compression chamber with a larger volume reduction gradient when volume reduction gradients (or compression gradients) of both compression chambers are different from each other.
- a scroll compressor having both compression chambers with different volume reduction gradients, wherein the entire cross-sectional area of bypass holes formed at a compression chamber with a larger volume reduction gradient between the both compression chambers is formed to be larger than that of bypass holes at the other compression chamber.
- the number of bypass holes formed at a compression chamber with a larger volume reduction gradient between the both compression chambers may be formed to be greater than that of bypass holes formed at the other compression chamber.
- the individual cross-sectional area of bypass holes formed at a compression chamber with a larger volume reduction gradient between the both compression chambers may be formed to be larger than that of bypass holes formed at the other compression chamber.
- a scroll compressor including a fixed scroll having a fixed wrap; a orbiting scroll tooth-coupled to the fixed wrap to have a orbiting wrap forming a first and a second compression chamber on an outer and an inner surface thereof, and a rotating shaft coupling portion is formed at a central portion thereof to perform orbiting movement with respect to the fixed scroll; a rotating shaft having an eccentric portion in which the eccentric portion is coupled to a rotating shaft coupling portion of the orbiting scroll to be overlapped with the orbiting wrap in a radial direction; and a driving unit configured to drive the rotating shaft, wherein bypass holes passing through the first and the second compression chamber to the outside are formed at the fixed scroll, and the entire cross-sectional area of bypass holes passing through the second compression chamber among the bypass holes is formed to be larger than that of bypass holes passing through the first compression chamber.
- the number of bypass holes passing through the second compression chamber may be formed to be greater than that of bypass holes passing through the first compression chamber.
- the individual cross-sectional area of bypass holes passing through the second compression chamber may be formed to be larger than that of bypass holes passing through the first compression chamber.
- a protruding portion may be formed on an inner circumferential surface at an inner end portion of the fixed wrap, and a recess portion brought into contact with protruding portion to form a compression chamber may be formed on an outer circumferential surface of the rotating shaft coupling portion.
- a scroll compressor formed with two pairs of compression chambers in which the two pairs of compression chambers are discharged through one discharge port, and bypass holes bypassing part of refrigerant prior to discharging refrigerant compressed in each compression chamber through the discharge port are formed at the each compression chamber, wherein the entire cross-sectional areas of bypass holes formed at the both compression chambers are different from each other.
- volume reduction gradients of the both compression chambers may be different from each other.
- the entire cross-sectional area of bypass holes formed at a compression chamber with a larger volume reduction gradient between the both compression chambers may be formed to be larger than that of bypass holes at the other compression chamber.
- the number of bypass holes formed at a compression chamber with a larger volume reduction gradient between the both compression chambers may be formed to be greater than that of bypass holes formed at the other compression chamber.
- the individual cross-sectional area of bypass holes formed at a compression chamber with a larger volume reduction gradient between the both compression chambers may be formed to be larger than that of bypass holes formed at the other compression chamber.
- the entire cross-sectional area of bypass holes formed at a compression chamber with a larger volume reduction gradient between the both compression chambers may be formed to be larger than that of bypass holes at the other compression chamber to prevent over-compression at the compression chamber with a larger volume reduction gradient, thereby enhancing the entire efficiency of the compressor.
- FIG. 1 is a longitudinal cross-sectional view illustrating a compression unit in a shaft penetration scroll compressor in the related art.
- FIG. 2 is a plan view illustrating bypass holes communicated with each compression chamber in a shaft penetration scroll compressor according to FIG. 1.
- FIG. 3 is a longitudinal cross-sectional view illustrating a shaft penetration scroll compressor according to the present disclosure.
- FIG. 4 is a plan view illustrating a compression unit in a shaft penetration scroll compressor according to FIG. 3.
- FIG. 5 is a plan view illustrating bypass holes communicated with each compression chamber in a shaft penetration scroll compressor according to FIG. 3.
- FIGS. 6 and 7 are a compression diagram and a volume diagram for a shaft penetration scroll compressor according to FIG. 3.
- FIG. 3 is a longitudinal cross-sectional view illustrating a shaft penetration scroll compressor according to the present disclosure
- FIG. 4 is a plan view illustrating a compression unit in a shaft penetration scroll compressor according to FIG. 3
- FIG. 5 is a plan view illustrating bypass holes communicated with each compression chamber in a shaft penetration scroll compressor according to FIG. 3.
- a drive motor 20 may be installed within a sealed container 10, and a main frame 30 and a sub-frame 40 may be installed at both an upper and a lower side of the drive motor 20, and a fixed scroll 50 may be fixed and installed at an upper side of the main frame 30, and a orbiting scroll 60 may be installed between the fixed scroll 50 and the main frame 30 engaged with the fixed scroll 50 and coupled to a rotating shaft 23 of the drive motor 20 to compress refrigerant while performing orbiting movement.
- the sealed container 10 may include a cylindrically shaped casing 11 and an upper shell 12 and a lower shell 13 bonded and coupled to cover an upper and a lower portion of the casing 11.
- a suction pipe 14 may be installed on a lateral surface of the casing 10, and a discharge pipe 15 may be installed at an upper portion of the upper shell 12.
- the lower shell 13 functions as an oil chamber for storing oil supplied to efficiently operate the compressor.
- the drive motor 20 may include a stator 21 fixed on an inner surface of the casing 10 and a rotor 22 positioned within the stator 21 to be rotated by an interaction with the stator 21.
- a rotating shaft 23 rotated with the rotor 22 at the same time may be coupled to the center of the rotor 22.
- An oil passage (F) may be formed in a penetrated manner at a central portion of the rotating shaft 23 along the length direction of the rotor 22, and an oil pump 24 for supplying oil stored in the lower shell 13 to the upper portion thereof may be installed at a lower portion of the rotating shaft 23.
- a pin portion 23c may be eccentrically formed at an upper end of the rotating shaft 23.
- An outer circumferential surface of the fixed scroll 50 may be pushed and fixed between the casing 10 and the upper shell 12 in a shrink fit manner or coupled to the casing 10 and the upper shell 12 by welding. Furthermore, a fixed wrap 54 tooth-coupled to a orbiting wrap 64 which will be described later to form a first compression chamber (S1) on an outer surface of the orbiting wrap 64 and a second compression chamber (S2) on an inner surface thereof, respectively, may be formed on a bottom surface of the end plate portion 52 of the fixed scroll 50.
- the orbiting scroll 60 may be engaged with the fixed scroll 50 to be supported by an upper surface of the main frame 30.
- the orbiting scroll 60 may be formed with a substantially circular shaped end plate portion 62, and the orbiting wrap 64 may be formed on an upper surface of the end plate portion 62 to form two pairs of compression chambers (S1, S2) tooth-coupled to the fixed wrap 54 to continuously move.
- a substantially circular shaped rotating shaft coupling portion 66 to which the pin portion 23c of the rotating shaft 23 is rotatably inserted and coupled may be formed at a central portion of the end plate portion 62.
- the eccentric portion 23c of the rotating shaft 23 is inserted and coupled to the rotating shaft coupling portion 66, and the fixed wrap 54, orbiting wrap 64 and the eccentric portion 23c of the rotating shaft 23 may be installed to be overlapped in a radial direction of the compressor.
- a repulsive force of refrigerant is applied to the fixed wrap 54 and orbiting wrap 64 during compression, and a compression force is applied between the rotating shaft coupling portion 66 and eccentric portion 23c as a reaction force to this.
- the repulsive force and compression force of refrigerant may be applied to the same lateral surface with respect to the end plate portion 62 and thus offseted to each other.
- the fixed wrap 54 and orbiting wrap 64 may be formed with an involute curve, but may be formed to have another curve other than the involute curve according to circumstances.
- the center of the rotating shaft coupling portion 66 is referred to as "O" and two contact points are referred to as P1 and P2, respectively, it is seen that angle defined by two straight lines connecting two contact points (P1, P2) to the center (O) of the rotating shaft coupling portion is less than 360 degrees, and distance l between each contact point to a normal vector is greater than "0". Accordingly, it may have a smaller volume compared to a case where the first compression chamber (S1) prior to its discharge has the fixed wrap 54 and orbiting wrap 64 formed with an involute curve, thereby increasing its compression ratio.
- a protruding portion 55 protruded toward the rotating shaft coupling portion 66 may be formed adjacent to an inner end portion of the fixed wrap 54, and a contact portion 55a formed to be protruded from the protruding portion 55 may be further formed on the protruding portion 55. Accordingly, an inner end portion of the fixed wrap may be formed to have a thickness greater than that of the other portion thereof.
- a recess portion 67 engaged with the protruding portion 55 may be formed on the rotating shaft coupling portion 66.
- One side wall of the recess portion 67 may form one side contact point (P1) of the first compression chamber (S1) while being brought into contact with the contact portion 55a of the protruding portion 55.
- undescribed reference numerals 52a, 52b and 56 refer to a first bypass hole, a second bypass hole and a discharge port, respectively.
- a shaft penetration scroll compressor when power is applied to the drive motor 20 to rotate the rotating shaft 23, the orbiting scroll 60 eccentrically coupled to the rotating shaft 23 performs orbiting movement along a predetermined path, and the first compression chamber (S1) and second compression chamber (S2) formed between the orbiting scroll 60 and the fixed scroll 50 reduce their volume while continuously moving around the orbiting movement, thereby repeating a series of processes of continuously inhaling, compressing and discharging refrigerant.
- each bypass hole 52a, 52b may be formed at the fixed scroll 50 to bypass part of refrigerant compressed in a region having an intermediate pressure between a suction pressure (Ps) and a discharge pressure (Pd) in advance prior to discharging refrigerant from each compression chamber (S1, S2).
- a volume reduction gradient (or compression gradient) of the first compression chamber (S1) is increased compared to that of the second compression chamber (S2).
- over-compression which is larger than the other compression chamber (S2) occurs to reduce compression efficiency, and therefore, the entire cross-sectional area of the bypass holes 52a communicated with the first compression chamber (S1) may be formed to be larger than that of the bypass holes 52b communicated with the second compression chamber (S2), thereby preventing over-compression in the first compression chamber (S1).
- bypass holes communicated with the first compression chamber (S1) may be formed to be greater than that of bypass holes communicated with the second compression chamber (S2), thereby preventing over-compression loss at the first compression chamber (S1) occurring while a volume reduction gradient of the first compression chamber (S1) is abruptly reduced compared to that of the second compression chamber (S2).
- a diameter of the first bypass hole 52a should be formed to be less than a wrap thickness of the fixed wrap 54 to prevent refrigerant leakage between both compression chambers.
- the entire cross-sectional area of first bypass holes formed at the first compression chamber with a larger volume reduction gradient between the both compression chambers may be formed to be larger than that of second bypass holes at the second compression chamber to prevent over-compression at the first compression chamber, thereby enhancing the entire efficiency of the compressor.
Abstract
Description
Claims (12)
- A scroll compressor having both compression chambers with different volume reduction gradients, wherein the entire cross-sectional area of bypass holes formed at a compression chamber with a larger volume reduction gradient between the both compression chambers is formed to be larger than that of bypass holes at the other compression chamber.
- The scroll compressor of claim 1, wherein the number of bypass holes formed at a compression chamber with a larger volume reduction gradient between the both compression chambers is formed to be greater than that of bypass holes formed at the other compression chamber.
- The scroll compressor of claim 1, wherein the individual cross-sectional area of bypass holes formed at a compression chamber with a larger volume reduction gradient between the both compression chambers is formed to be larger than that of bypass holes formed at the other compression chamber.
- A scroll compressor, comprising:a fixed scroll having a fixed wrap;a orbiting scroll tooth-coupled to the fixed wrap to have a orbiting wrap forming a first and a second compression chamber on an outer and an inner surface thereof, and a rotating shaft coupling portion is formed at a central portion thereof to perform orbiting movement with respect to the fixed scroll;a rotating shaft having an eccentric portion in which the eccentric portion is coupled to a rotating shaft coupling portion of the orbiting scroll to be overlapped with the orbiting wrap in a radial direction; anda driving unit configured to drive the rotating shaft,wherein bypass holes passing through the first and the second compression chamber to the outside are formed at the fixed scroll, andthe entire cross-sectional area of bypass holes passing through the second compression chamber among the bypass holes is formed to be larger than that of bypass holes passing through the first compression chamber.
- The scroll compressor of claim 4, wherein the number of bypass holes passing through the second compression chamber is formed to be greater than that of bypass holes passing through the first compression chamber.
- The scroll compressor of claim 4, wherein the individual cross-sectional area of bypass holes passing through the second compression chamber is formed to be larger than that of bypass holes passing through the first compression chamber.
- The scroll compressor of any one of claims 4 to 6, wherein a protruding portion is formed on an inner circumferential surface at an inner end portion of the fixed wrap, and a recess portion brought into contact with protruding portion to form a compression chamber is formed on an outer circumferential surface of the rotating shaft coupling portion.
- A scroll compressor formed with two pairs of compression chambers in which the two pairs of compression chambers are discharged through one discharge port, and bypass holes bypassing part of refrigerant prior to discharging refrigerant compressed in each compression chamber through the discharge port are formed at the each compression chamber,wherein the entire cross-sectional areas of bypass holes formed at the both compression chambers are different from each other.
- The scroll compressor of claim 8, wherein the volume reduction gradients of the both compression chambers are different from each other.
- The scroll compressor of claim 9, wherein the entire cross-sectional area of bypass holes formed at a compression chamber with a larger volume reduction gradient between the both compression chambers is formed to be larger than that of bypass holes at the other compression chamber.
- The scroll compressor of claim 10, wherein the number of bypass holes formed at a compression chamber with a larger volume reduction gradient between the both compression chambers is formed to be greater than that of bypass holes formed at the other compression chamber.
- The scroll compressor of claim 10, wherein the individual cross-sectional area of bypass holes formed at a compression chamber with a larger volume reduction gradient between the both compression chambers is formed to be larger than that of bypass holes formed at the other compression chamber.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201480024407.6A CN105190042B (en) | 2013-05-21 | 2014-05-19 | Screw compressor |
US14/782,080 US9683568B2 (en) | 2013-05-21 | 2014-05-19 | Scroll compressor having an area of bypass holes formed at a compression chamber with a larger volume reduction gradient larger than an area of bypass holes at the other compression chamber |
US15/624,841 US10125767B2 (en) | 2013-05-21 | 2017-06-16 | Scroll compressor with bypass portions |
US16/186,221 US11047386B2 (en) | 2013-05-21 | 2018-11-09 | Scroll compressor with bypass portions |
US16/848,188 US11473579B2 (en) | 2013-05-21 | 2020-04-14 | Scroll compressor with bypass portions |
US17/941,743 US11739752B2 (en) | 2013-05-21 | 2022-09-09 | Scroll compressor with bypass portions |
Applications Claiming Priority (2)
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KR1020130057316A KR102056371B1 (en) | 2013-05-21 | 2013-05-21 | Scroll compressor |
KR10-2013-0057316 | 2013-05-21 |
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US14/782,080 A-371-Of-International US9683568B2 (en) | 2013-05-21 | 2014-05-19 | Scroll compressor having an area of bypass holes formed at a compression chamber with a larger volume reduction gradient larger than an area of bypass holes at the other compression chamber |
US15/624,841 Continuation-In-Part US10125767B2 (en) | 2013-05-21 | 2017-06-16 | Scroll compressor with bypass portions |
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WO2014189240A1 true WO2014189240A1 (en) | 2014-11-27 |
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PCT/KR2014/004460 WO2014189240A1 (en) | 2013-05-21 | 2014-05-19 | Scroll compressor |
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US (1) | US9683568B2 (en) |
KR (1) | KR102056371B1 (en) |
CN (1) | CN105190042B (en) |
WO (1) | WO2014189240A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
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EP3415765A1 (en) * | 2017-06-14 | 2018-12-19 | LG Electronics Inc. | Scroll compressor |
WO2021040360A1 (en) * | 2019-08-27 | 2021-03-04 | Samsung Electronics Co., Ltd. | Scroll compressor |
US11473579B2 (en) * | 2013-05-21 | 2022-10-18 | Lg Electronics Inc. | Scroll compressor with bypass portions |
Families Citing this family (6)
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CN208996964U (en) * | 2015-09-14 | 2019-06-18 | 特灵国际有限公司 | Compressor and heat transfer loop |
JP6765508B2 (en) * | 2017-03-29 | 2020-10-07 | 三菱電機株式会社 | Scroll compressor and manufacturing method of scroll compressor |
WO2019022037A1 (en) * | 2017-07-27 | 2019-01-31 | パナソニックIpマネジメント株式会社 | Scroll compressor |
JP6865861B2 (en) * | 2018-01-30 | 2021-04-28 | 三菱電機株式会社 | Scroll compressor |
KR102497530B1 (en) * | 2018-05-28 | 2023-02-08 | 엘지전자 주식회사 | Scroll compressor having enhanced discharge structure |
WO2021117173A1 (en) * | 2019-12-12 | 2021-06-17 | 三菱電機株式会社 | Scroll compressor and refrigeration cycle device |
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KR101282227B1 (en) | 2011-09-21 | 2013-07-09 | 엘지전자 주식회사 | Scroll compressor |
KR20130031734A (en) | 2011-09-21 | 2013-03-29 | 엘지전자 주식회사 | Scroll compressor |
-
2013
- 2013-05-21 KR KR1020130057316A patent/KR102056371B1/en active IP Right Grant
-
2014
- 2014-05-19 US US14/782,080 patent/US9683568B2/en active Active
- 2014-05-19 WO PCT/KR2014/004460 patent/WO2014189240A1/en active Application Filing
- 2014-05-19 CN CN201480024407.6A patent/CN105190042B/en active Active
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JPH04255589A (en) * | 1991-02-08 | 1992-09-10 | Toshiba Corp | Scroll type compressor |
JPH09217690A (en) * | 1996-02-14 | 1997-08-19 | Matsushita Electric Ind Co Ltd | Scroll gas compressor |
US6379123B1 (en) * | 1997-05-12 | 2002-04-30 | Matsushita Electric Industrial Co., Ltd. | Capacity control scroll compressor |
JP2001200795A (en) * | 2000-01-17 | 2001-07-27 | Matsushita Electric Ind Co Ltd | Scroll compressor |
US20130089449A1 (en) * | 2011-10-11 | 2013-04-11 | Sanghun SEONG | Scroll compressor with bypass hole |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11473579B2 (en) * | 2013-05-21 | 2022-10-18 | Lg Electronics Inc. | Scroll compressor with bypass portions |
US11739752B2 (en) | 2013-05-21 | 2023-08-29 | Lg Electronics Inc. | Scroll compressor with bypass portions |
EP3415765A1 (en) * | 2017-06-14 | 2018-12-19 | LG Electronics Inc. | Scroll compressor |
CN110741163A (en) * | 2017-06-14 | 2020-01-31 | Lg电子株式会社 | Scroll compressor having a discharge port |
CN110741163B (en) * | 2017-06-14 | 2022-04-26 | Lg电子株式会社 | Scroll compressor having a discharge port |
WO2021040360A1 (en) * | 2019-08-27 | 2021-03-04 | Samsung Electronics Co., Ltd. | Scroll compressor |
US11286931B2 (en) | 2019-08-27 | 2022-03-29 | Samsung Electronics Co., Ltd. | Scroll compressor having a shaft support portion including a closing portion |
Also Published As
Publication number | Publication date |
---|---|
CN105190042A (en) | 2015-12-23 |
CN105190042B (en) | 2017-06-16 |
KR20140136795A (en) | 2014-12-01 |
KR102056371B1 (en) | 2019-12-16 |
US9683568B2 (en) | 2017-06-20 |
US20160040667A1 (en) | 2016-02-11 |
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