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EP4088030B1 - Scroll compressor - Google Patents

Scroll compressor Download PDF

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Publication number
EP4088030B1
EP4088030B1 EP20700566.1A EP20700566A EP4088030B1 EP 4088030 B1 EP4088030 B1 EP 4088030B1 EP 20700566 A EP20700566 A EP 20700566A EP 4088030 B1 EP4088030 B1 EP 4088030B1
Authority
EP
European Patent Office
Prior art keywords
pressure chamber
channel
scroll
oil return
gas connection
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.)
Active
Application number
EP20700566.1A
Other languages
German (de)
French (fr)
Other versions
EP4088030A1 (en
Inventor
Lukas LÖHMER
Phillip BARTH
Jan BERWANGER
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.)
Pierburg GmbH
Original Assignee
Pierburg GmbH
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Filing date
Publication date
Application filed by Pierburg GmbH filed Critical Pierburg GmbH
Publication of EP4088030A1 publication Critical patent/EP4088030A1/en
Application granted granted Critical
Publication of EP4088030B1 publication Critical patent/EP4088030B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • F04C18/0246Details concerning the involute wraps or their base, e.g. geometry
    • F04C18/0253Details concerning the base
    • 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
    • F04C23/02Pumps characterised by combination with, or adaptation to, specific driving engines or motors
    • 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
    • F04C29/02Lubrication; Lubricant separation
    • F04C29/026Lubricant separation
    • 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
    • F04C2240/30Casings or housings
    • 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
    • F04C2240/40Electric motor
    • 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
    • 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
    • F04C29/02Lubrication; Lubricant separation
    • F04C29/028Means for improving or restricting lubricant flow

Definitions

  • the invention relates to a scroll compressor with a compressor housing, a high-pressure chamber, a low-pressure chamber, which is fluidly connected to the high-pressure chamber via an oil return channel, an oil return throttle being provided in the oil return channel, an orbiting displacement spiral arranged on a driven eccentric unit, which in a fixed spiral intervenes, a sliding disk being arranged between the orbiting displacement spiral and the compressor housing, and a counter-pressure chamber adjacent to the displacement spiral, which is fluidly connected to the high-pressure chamber via a gas connection channel, a gas connection throttle being provided in the gas connection channel.
  • Such scroll compressors are from the prior art, for example from EP 3 404 264 A1 , well known and include a high pressure chamber, a low pressure chamber, an orbiting displacement spiral and a fixed spiral interacting with the displacement spiral.
  • a sliding disk is arranged between the orbiting displacement spiral and a compressor housing.
  • the orbiting displacement spiral engages with the fixed spiral in such a way that compression chambers are formed between the displacement spiral and the fixed spiral, which accommodate a working fluid.
  • a counter-pressure chamber is provided between the compressor housing and the displacement spiral. The pressure prevailing in the counter-pressure chamber and acting on the displacement spiral causes a resultant force in the axial direction, causing the displacement spiral is pressed against the fixed spiral and thus the spirals are sealed to one another.
  • the pressure prevailing in the counter-pressure chamber is built up by a fluidic connection between the counter-pressure chamber and the high-pressure chamber, with the high-pressure fluid flowing into the counter-pressure chamber via a gas connection channel connecting the high-pressure chamber with the counter-pressure chamber.
  • a gas connection throttle is arranged in the gas connection channel, which controls the mass flow of the fluid flowing into the counter-pressure chamber.
  • the scroll compressor includes an oil return channel, which fluidly connects the high-pressure chamber with the low-pressure chamber.
  • An oil intended for lubricating the components in the scroll compressor is separated from the compressed fluid via a separator arranged in the high-pressure chamber and returned to the low-pressure chamber via the oil return channel, so that the returned oil can be used again to lubricate the components.
  • an oil return throttle is arranged in the oil return channel.
  • the oil return throttle is formed by a separate component, which is manufactured through an additional manufacturing process and must be mounted in the oil return channel during assembly, which increases the manufacturing and assembly costs of the scroll compressor.
  • the task is therefore to provide a scroll compressor which has reduced manufacturing and assembly costs.
  • the sliding disk having the oil return throttle and/or the gas connection throttle, the manufacture and assembly of the scroll compressor is simplified and thereby the manufacturing and assembly costs are reduced.
  • the sliding disk takes over the throttling function in the oil return channel and/or in the gas connection channel, with the oil return throttle or the gas connection throttle being implemented through a simple and inexpensively manufactured opening in the sliding disk and no additional components for executing the oil return throttle and/or the Gas connection throttle is required.
  • the sliding disk thus reduces the sliding friction between the orbiting displacement spiral and the compressor housing as well as throttling the fluid flowing into the counter-pressure chamber and/or the oil flowing back into the low-pressure chamber.
  • the oil return throttle or the gas connection throttle is an opening provided on the sliding disk, the opening having a smaller diameter than the oil return channel or the gas connection channel.
  • the sliding disk can be equipped with the oil return throttle and/or the gas connection throttle in a simple and cost-effective manner, such a throttle being able to be produced by a simple and cost-effective manufacturing process, for example using a laser. This creates a throttle for the oil return channel and/or for the gas connection channel, with no additional components that would increase the manufacturing and assembly costs being required.
  • the oil return channel and/or the gas connection channel extends at least in sections through the fixed spiral.
  • the gas connection channel extends from the high-pressure chamber via a gas channel in the fixed spiral, through the sliding disk and via a gas channel in the compressor housing to the counter-pressure chamber.
  • the oil return channel extends from the high-pressure chamber via an oil channel in the fixed spiral, through the sliding disk and via an oil channel in the compressor housing to the low-pressure chamber.
  • the oil return channel and/or the gas connection channel can be guided directly from the high-pressure chamber to the counter-pressure chamber or the low-pressure chamber.
  • the high-pressure chamber preferably has an oil separation chamber in which an oil separator is arranged, with an inlet of the oil return channel being arranged at the lowest point of the oil separation chamber.
  • the oil separator separates the oil dissolved in the gas, with the oil-free gas rising and flowing through an outlet into a cooling circuit.
  • the separated oil sinks to the bottom of the oil separation chamber and flows back into the low-pressure chamber via the oil return channel.
  • the oil can be used to lubricate the components of the scroll compressor.
  • an inlet of the gas connection channel is arranged in front of the oil separator in the flow direction of the gas-oil mixture.
  • the gas with oil dissolved in it is conveyed into the counter-pressure chamber, whereby the components adjacent to the counter-pressure chamber, in particular bearing elements, are transported through the oil be lubricated.
  • the inlet of the gas connection channel can be arranged downstream of the oil separator in the flow direction of the gas-oil mixture.
  • a filter is provided in the oil return channel and/or gas connection channel.
  • the returning oil and/or the gas flowing into the counter-pressure chamber may contain particles which arise, for example, from wear of the components moving relative to one another.
  • the particles can lead to clogging of the oil return throttle or the gas connection throttle or to abrasive wear of the components moving relative to one another.
  • the filter can be used to filter out the particles from the oil or gas and prevent clogging of the oil return channel or the gas connection channel as well as abrasive wear on the components moving relative to one another.
  • the displacement spiral preferably has a circumferential groove on the side facing the sliding disk, in which a sliding ring is arranged, the sliding ring resting on the sliding disk. This allows the friction between the sliding disk and the displacement spiral to be reduced during the orbiting movement of the displacement spiral.
  • the sliding disk is positively connected to the drive housing perpendicular to a longitudinal axis.
  • the compressor housing has at least one fixing bolt and the sliding disk has a fixing opening corresponding to the fixing bolt.
  • the fixing bolt can reliably prevent twisting and radial displacement of the sliding disk.
  • the fixing bolt can be a separate component pressed into an opening in the compressor housing or can be made in one piece with the compressor housing.
  • the sliding disk has at least one guide opening through which a guide pin attached to the compressor housing and guiding the orbiting displacement spiral extends.
  • the guide pin engages eccentrically in an opening of the displacement spiral, whereby the displacement spiral is guided by the guide pin during the orbiting movement, with a rotational movement of the displacement spiral being prevented by the guide pin.
  • the oil return throttle and/or the gas connection throttle has a diameter that is many times smaller than the diameter of the fixing bolt or the guide pin.
  • the oil or gas mass flow can be controlled by the size of the diameter of the oil return throttle and/or the gas connection throttle.
  • the orbiting displacement spiral is connected via the eccentric unit to a rotor shaft of a rotor of an electric motor, the electric motor being arranged in the low-pressure chamber.
  • the electric motor is cooled, thereby increasing the service life of the scroll compressor.
  • a scroll compressor for an air conditioning system of a motor vehicle which has a gas connection channel extending from the high-pressure chamber to the counter-pressure chamber and/or an oil return channel extending from the high-pressure chamber to the low-pressure chamber, with a gas connection arranged in the gas connection channel and/or an oil return channel arranged in the oil return channel.
  • Throttle is provided in a simple and cost-effective manner by the sliding disk, thereby reducing the assembly and manufacturing costs of the scroll compressor.
  • the scroll compressor 2 comprises a multi-part compressor housing 10 with a first compressor housing part 12, a second compressor housing part 14 which adjoins the first compressor housing part 12 axially and a third compressor housing part 16 which adjoins the second compressor housing part 14.
  • the first compressor housing part 12, the second compressor housing part 14 and the Third compressor housing part 16 delimits an engine compartment 18.
  • the second compressor housing part 14 and the third compressor housing part 16 delimit a compressor compartment 20.
  • An electric motor 22 with a stator 24 and a rotor 26 is arranged in the engine compartment 18.
  • the rotor 26 is attached to a rotor shaft 28.
  • the rotor shaft 28 extends from the engine compartment 18 through a central opening 29 of the second compressor housing part 14 into the compressor compartment 20.
  • the rotor shaft 28 is rotatably mounted in two shaft bearings 40, 42 via two end-side shaft bearing sections 30, 34 about a rotor shaft rotation axis.
  • the first shaft bearing 40 is arranged in the engine compartment 18 and supports the first shaft bearing section 30.
  • the second shaft bearing 42 is arranged in the compressor compartment 20 and supports the second shaft bearing section 34.
  • a shaft sealing ring 43 is provided on the side of the second shaft bearing 42 facing the engine compartment 18 , which rests on the radial inside of the rotor shaft 28 and is supported on the radial outside by the second compressor housing part 14.
  • the shaft sealing ring 43 fluidly seals the engine compartment 18 from a counter-pressure chamber 82 of the compressor compartment 20.
  • a compressor unit 58 is arranged in the compressor chamber 20 and has an orbiting displacement spiral 60 and a fixed spiral 62.
  • the orbiting displacement spiral 60 is arranged via an eccentric shaft bearing 64 on an eccentric unit 50 attached to the rotor shaft 28 and rests via a sliding disk 70 on a surface of the second compressor housing part 14 facing the compressor chamber 20, the displacement spiral 60 being on the side facing the sliding disk 70 has a sliding ring 142 arranged in a circumferential groove 140.
  • the fixed scroll 62 is fixedly disposed in the compressor housing 10, with the fixed scroll 62 being axially supported by the second compressor housing part 14 and the third compressor housing part 16.
  • a refrigerant is introduced through a compressor inlet 85 into the engine compartment 18 of the scroll compressor 2, with the refrigerant flowing through the engine compartment 18 into the compressor compartment 20.
  • the orbiting displacement spiral 60 and the fixed spiral 62 are designed such that they delimit a compression chamber 63 and, through the orbiting movement of the displacement spiral 60, a refrigerant is conveyed from a radially outer inlet 66 of the compression chamber 63 to a radially inner outlet 68 of the compression chamber 63 and thereby is compacted.
  • the compressor chamber 20 has a high-pressure chamber 80 and a counter-pressure chamber 82.
  • the high-pressure chamber 80 is delimited by the third compressor housing part 16 and by the fixed spiral 62 and is fluidly arranged between the outlet 68 and a compressor outlet 84, with the refrigerant flowing from the outlet 68 via the high-pressure chamber 80 to the compressor outlet 84.
  • the refrigerant flows into a coolant circuit of a motor vehicle.
  • the high-pressure chamber 80 has an oil separation chamber 86, which is fluidly arranged immediately in front of the compressor outlet 84 and has an oil separator 88.
  • the oil separator 88 is designed as a cyclone separator, with the refrigerant flowing through the oil separator 88 to the compressor outlet 84 and the oil released from the refrigerant settling at the bottom of the oil separation chamber 86, i.e. at the lowest point of the oil separation chamber 86.
  • an inlet 89 of an oil return channel 90 is provided at the bottom of the oil separation chamber 86, which fluidly connects the oil separation chamber 86 and thus the high-pressure chamber 80 with a low-pressure chamber 87, the engine compartment 18 forming the low-pressure chamber 87.
  • the oil return channel 90 extends through the third compressor housing part 16, the fixed spiral 62 and through the second compressor housing part 14, with a filter 130 being arranged in the oil return channel 90.
  • the counter-pressure chamber 82 is delimited by the second compressor housing part 14 and the orbiting displacement spiral 60, the pressure prevailing in the counter-pressure chamber 82 acting on the axially displaceable, orbiting displacement spiral 60, resulting in an axial load on the displacement spiral.
  • This axial load leads to an improved seal between the end faces of the orbiting displacement spiral 60 and the fixed spiral 62.
  • the counter-pressure chamber 82 is connected to the gas connection channel 100 via a gas connection channel 100 High pressure chamber 80 fluidly connected.
  • the gas connection channel 100 runs from the high-pressure chamber 80 through the fixed spiral 62 and through the second compressor housing part 14.
  • a gas connection throttle is arranged in the gas connection channel 100, which controls the mass flow of the gas flowing into the counter-pressure chamber 82.
  • the oil return channel 90 and the gas connection channel 100 run through the sliding disk 70 arranged between the second compressor housing part 14 and the fixed spiral 62, the sliding disk 70, which in Figure 2 is shown, an oil return throttle 92 and a gas connection throttle 96.
  • the sliding disk 70 has a first bore 94 in its radially outer region and a second bore 98 spaced apart from the first bore 94 in the circumferential direction.
  • the first bore 94 has a smaller diameter than the rest of the oil return line 90, so that the first bore 94 forms the oil return throttle 92.
  • the second bore 98 has a smaller diameter than the rest of the gas connection line 100, so that the second bore 98 forms the gas connection throttle 96.
  • the oil mass flow through the oil return channel 90 is thus controlled by the oil return throttle 92 and the gas mass flow into the counter-pressure chamber 82 is controlled by the gas connection throttle 96.
  • the sliding disk 70 has two fixing openings 102, 104 in the radially outer region and six guide openings 110, 112, 114, 116, 118, 120 in the radially inner region, the fixing openings 102, 104 and the guide openings 110, 112, 114, 116, 118, 120 have a significantly larger diameter than the bores 94, 98.
  • a fixing bolt 103 attached to the second compressor housing part 14 engages in each of the two fixing openings 102, 104 a, whereby the sliding disk 70 is fixed perpendicular to a longitudinal axis 106 of the scroll compressor 2.
  • the six guide openings 110, 112, 114, 116, 118, 120 are each penetrated by a guide pin 122 attached to the second compressor housing part 14, the guide pins 122 engaging eccentrically in guide holes 124 provided on the displacement spiral 60.
  • the guide bores 124 have a larger diameter than the guide pins 122, with the guide pins 122 sliding on the respective inner peripheral surface of the guide bore 124 during the orbiting movement of the displacement spiral 60.
  • a plain bearing sleeve 126 is arranged in the guide bores 124.
  • a scroll compressor 2 is thus created, which can be produced with reduced manufacturing and assembly effort, the oil return throttle 92 and the gas connection throttle 96 being provided in a simple and cost-effective manner by the sliding disk 70 and no additional components and associated manufacturing and assembly steps are required.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)

Description

Die Erfindung betrifft einen Spiralverdichter mit einem Verdichtergehäuse, einer Hochdruckkammer, einer Niederdruckkammer, welche über einen Ölrückführungskanal mit der Hochdruckkammer fluidisch verbunden ist, wobei in dem Ölrückführungskanal eine Ölrückführungs-Drossel vorgesehen ist, einer an einer angetriebenen Exzentereinheit angeordneten und orbitierenden Verdrängerspirale, welche in eine feststehende Spirale eingreift, wobei zwischen der orbitierenden Verdrängerspirale und dem Verdichtergehäuse eine Gleitscheibe angeordnet ist, und einer an die Verdrängerspirale angrenzende Gegendruckkammer, welche über einen Gasverbindungskanal mit der Hochdruckkammer fluidisch verbunden ist, wobei in dem Gasverbindungskanal eine Gasverbindungs-Drossel vorgesehen ist.The invention relates to a scroll compressor with a compressor housing, a high-pressure chamber, a low-pressure chamber, which is fluidly connected to the high-pressure chamber via an oil return channel, an oil return throttle being provided in the oil return channel, an orbiting displacement spiral arranged on a driven eccentric unit, which in a fixed spiral intervenes, a sliding disk being arranged between the orbiting displacement spiral and the compressor housing, and a counter-pressure chamber adjacent to the displacement spiral, which is fluidly connected to the high-pressure chamber via a gas connection channel, a gas connection throttle being provided in the gas connection channel.

Derartige Spiralverdichter sind aus dem Stand der Technik, beispielsweise aus der EP 3 404 264 A1 , hinlänglich bekannt und umfassen eine Hochdruckkammer, eine Niederdruckkammer, eine orbitierende Verdrängerspirale und eine mit der Verdrängerspirale zusammenwirkende, feststehende Spirale. Zwischen der orbitierenden Verdrängerspirale und einem Verdichtergehäuse ist eine Gleitscheibe angeordnet. Die orbitierende Verdrängerspirale greift in die feststehende Spirale derart ein, dass zwischen der Verdrängerspirale und der feststehenden Spirale Verdichtungskammern gebildet werden, welche ein Arbeitsfluid aufnehmen. Zwischen dem Verdichtergehäuse und der Verdrängerspirale ist eine Gegendruckkammer vorgesehen. Der in der Gegendruckkammer herrschende und auf die Verdrängerspirale wirkende Druck verursacht eine resultierende Kraft in axialer Richtung, wodurch die Verdrängerspirale gegen die feststehende Spirale gedrückt wird und somit die Spiralen zueinander abgedichtet werden.Such scroll compressors are from the prior art, for example from EP 3 404 264 A1 , well known and include a high pressure chamber, a low pressure chamber, an orbiting displacement spiral and a fixed spiral interacting with the displacement spiral. A sliding disk is arranged between the orbiting displacement spiral and a compressor housing. The orbiting displacement spiral engages with the fixed spiral in such a way that compression chambers are formed between the displacement spiral and the fixed spiral, which accommodate a working fluid. A counter-pressure chamber is provided between the compressor housing and the displacement spiral. The pressure prevailing in the counter-pressure chamber and acting on the displacement spiral causes a resultant force in the axial direction, causing the displacement spiral is pressed against the fixed spiral and thus the spirals are sealed to one another.

Der in der Gegendruckkammer herrschende Druck wird durch eine fluidische Verbindung zwischen der Gegendruckkammer und der Hochdruckkammer aufgebaut, wobei das unter hohem Druck stehende Fluid über einen die Hochdruckkammer mit der Gegendruckkammer verbindenden Gasverbindungskanal in die Gegendruckkammer strömt. In dem Gasverbindungskanal ist eine Gasverbindungs-Drossel angeordnet, welche den Massenstrom des in die Gegendruckkammer strömenden Fluids steuert. Nachteilhaft an einer derartigen Gasverbindungs-Drossel ist, dass diese durch eine separate Komponente gebildet wird, wobei durch das Vorsehen einer derartigen separaten Gasverbindungs-Drossel sowohl die Herstellungs- als auch die Montagekosten des Spiralverdichters erhöht wird.The pressure prevailing in the counter-pressure chamber is built up by a fluidic connection between the counter-pressure chamber and the high-pressure chamber, with the high-pressure fluid flowing into the counter-pressure chamber via a gas connection channel connecting the high-pressure chamber with the counter-pressure chamber. A gas connection throttle is arranged in the gas connection channel, which controls the mass flow of the fluid flowing into the counter-pressure chamber. The disadvantage of such a gas connection throttle is that it is formed by a separate component, with the provision of such a separate gas connection throttle increasing both the manufacturing and assembly costs of the scroll compressor.

Des Weiteren umfasst der Spiralverdichter einen Ölrückführungskanal, welcher die Hochdruckkammer mit der Niederdruckkammer fluidisch verbindet. Dabei wird ein zur Schmierung der Komponenten in dem Spiralverdichter vorgesehenes Öl aus dem verdichteten Fluid über einen in der Hochdruckkammer angeordneten Abscheider abgetrennt und über den Ölrückführungskanal in die Niederdruckkammer zurückgeführt, so dass das zurückgeführte Öl erneut zur Schmierung der Komponenten verwendet werden kann. Zur Steuerung des Rückflussmassenstroms des abgetrennten Öls ist im Ölrückführungskanal eine Ölrückführungs-Drossel angeordnet. Die Ölrückführungs-Drossel wird durch eine separate Komponente gebildet, welche durch einen zusätzlichen Herstellungsprozess hergestellt und bei der Montage aufwendig in den Ölrückführungskanal montiert werden muss, wodurch der Herstellungs- und der Montageaufwand des Spiralverdichters erhöht wird.Furthermore, the scroll compressor includes an oil return channel, which fluidly connects the high-pressure chamber with the low-pressure chamber. An oil intended for lubricating the components in the scroll compressor is separated from the compressed fluid via a separator arranged in the high-pressure chamber and returned to the low-pressure chamber via the oil return channel, so that the returned oil can be used again to lubricate the components. To control the return mass flow of the separated oil, an oil return throttle is arranged in the oil return channel. The oil return throttle is formed by a separate component, which is manufactured through an additional manufacturing process and must be mounted in the oil return channel during assembly, which increases the manufacturing and assembly costs of the scroll compressor.

Es stellt sich daher die Aufgabe, einen Spiralverdichter bereitzustellen, welcher einen reduzierten Herstellungs- und Montageaufwand aufweist.The task is therefore to provide a scroll compressor which has reduced manufacturing and assembly costs.

Diese Aufgabe wird durch einen Spiralverdichter mit den Merkmalen des Hauptanspruchs 1 gelöst.This task is achieved by a scroll compressor with the features of main claim 1.

Dadurch, dass der Ölrückführungskanal und/oder der Gasverbindungskanal sich durch die Gleitscheibe erstreckt, wobei die Gleitscheibe die Ölrückführungs-Drossel und/oder die Gasverbindungs-Drossel aufweist, wird die Herstellung und die Montage des Spiralverdichters vereinfacht und dadurch die Herstellungs- und Montagekosten reduziert. Dabei übernimmt die Gleitscheibe die Drosselfunktion im Ölrückführungskanal und/oder im Gasverbindungskanal, wobei die Ölrückführungs-Drossel oder die Gasverbindungs-Drossel durch eine einfach und kostengünstig hergestellte Öffnung in der Gleitscheibe ausgeführt ist und keine zusätzlichen Bauteile zur Ausführung der Ölrückführungs-Drossel und/oder der Gasverbindungs-Drossel erforderlich sind. Damit wird durch die Gleitscheibe die Reduzierung der Gleitreibung zwischen der orbitierenden Verdrängerspirale und dem Verdichtergehäuse sowie die Drosselung des in die Gegendruckkammer strömenden Fluids und/oder des in die Niederdruckkammer rückströmenden Öls erzielt.Because the oil return channel and/or the gas connection channel extends through the sliding disk, the sliding disk having the oil return throttle and/or the gas connection throttle, the manufacture and assembly of the scroll compressor is simplified and thereby the manufacturing and assembly costs are reduced. The sliding disk takes over the throttling function in the oil return channel and/or in the gas connection channel, with the oil return throttle or the gas connection throttle being implemented through a simple and inexpensively manufactured opening in the sliding disk and no additional components for executing the oil return throttle and/or the Gas connection throttle is required. The sliding disk thus reduces the sliding friction between the orbiting displacement spiral and the compressor housing as well as throttling the fluid flowing into the counter-pressure chamber and/or the oil flowing back into the low-pressure chamber.

Vorzugsweise ist die Ölrückführungs-Drossel oder die Gasverbindungs-Drossel eine an der Gleitscheibe vorgesehene Öffnung, wobei die Öffnung einen kleineren Durchmesser als der Ölrückführungskanal oder der Gasverbindungskanal aufweist. Dadurch kann die Gleitscheibe auf eine einfache und kostengünstige Weise mit der Ölrückführungs-Drossel und/oder der Gasverbindungs-Drossel ausgestattet werden, wobei durch einen einfachen und kostengünstigen Herstellungsprozess, beispielsweise mittels eines Lasers, eine derartige Drossel hergestellt werden kann. Damit wird eine Drossel für den Ölrückführungskanal und/oder für den Gasverbindungskanal geschaffen, wobei keine zusätzlichen Komponenten, welche die Herstellungs- und Montagekosten erhöhen würden, benötigt werden.Preferably, the oil return throttle or the gas connection throttle is an opening provided on the sliding disk, the opening having a smaller diameter than the oil return channel or the gas connection channel. As a result, the sliding disk can be equipped with the oil return throttle and/or the gas connection throttle in a simple and cost-effective manner, such a throttle being able to be produced by a simple and cost-effective manufacturing process, for example using a laser. This creates a throttle for the oil return channel and/or for the gas connection channel, with no additional components that would increase the manufacturing and assembly costs being required.

Vorzugsweise erstreckt sich der Ölrückführungskanal und/oder der Gasverbindungskanal zumindest abschnittsweise durch die feststehende Spirale. In einer bevorzugten Ausgestaltung erstreckt sich der Gasverbindungskanal ausgehend von der Hochdruckkammer über einen Gaskanal in der feststehenden Spirale, durch die Gleitscheibe und über einen Gaskanal im Verdichtergehäuse zur Gegendruckkammer. In einer bevorzugten Ausgestaltung erstreckt sich der Ölrückführungskanal ausgehend von der Hochdruckkammer über einen Ölkanal in der feststehenden Spirale, durch die Gleitscheibe und über einen Ölkanal im Verdichtergehäuse zur Niederdruckkammer.Preferably, the oil return channel and/or the gas connection channel extends at least in sections through the fixed spiral. In a preferred embodiment, the gas connection channel extends from the high-pressure chamber via a gas channel in the fixed spiral, through the sliding disk and via a gas channel in the compressor housing to the counter-pressure chamber. In a preferred embodiment, the oil return channel extends from the high-pressure chamber via an oil channel in the fixed spiral, through the sliding disk and via an oil channel in the compressor housing to the low-pressure chamber.

Dadurch, dass die Gleitscheibe unmittelbar an die feststehende Spirale angrenzt und die feststehende Spirale unmittelbar an die Hochdruckkammer angrenzt, kann der Ölrückführungskanal und/oder der Gasverbindungskanal auf direktem Wege ausgehend von der Hochdruckkammer zur Gegendruckkammer oder der Niederdruckkammer geleitet werden.Because the sliding disk is directly adjacent to the fixed spiral and the fixed spiral is directly adjacent to the high-pressure chamber, the oil return channel and/or the gas connection channel can be guided directly from the high-pressure chamber to the counter-pressure chamber or the low-pressure chamber.

Vorzugsweise weist die Hochdruckkammer eine Ölabscheidekammer auf, in welcher ein Ölabscheider angeordnet ist, wobei am tiefsten Punkt der Ölabscheidekammer ein Einlass des Ölrückführungskanals angeordnet ist. Der Ölabscheider trennt das in dem Gas gelöste Öl ab, wobei das ölfreie Gas aufsteigt und durch einen Auslass in einen Kühlkreislauf strömt. Das abgetrennte Öl sinkt auf den Boden der Ölabscheidekammer ab und strömt über den Ölrückführungskanal wieder in die Niederdruckkammer. Ausgehend von der Niederdruckkammer kann das Öl zur Schmierung der Komponenten des Spiralverdichters verwendet werden.The high-pressure chamber preferably has an oil separation chamber in which an oil separator is arranged, with an inlet of the oil return channel being arranged at the lowest point of the oil separation chamber. The oil separator separates the oil dissolved in the gas, with the oil-free gas rising and flowing through an outlet into a cooling circuit. The separated oil sinks to the bottom of the oil separation chamber and flows back into the low-pressure chamber via the oil return channel. Starting from the low pressure chamber, the oil can be used to lubricate the components of the scroll compressor.

Vorzugsweise ist ein Einlass des Gasverbindungskanals in Strömungsrichtung des Gas-Öl-Gemisches vor dem Ölabscheider angeordnet. Dadurch wird das Gas mit darin gelöstem Öl in die Gegendruckkammer gefördert, wodurch die an die Gegendruckkammer angrenzenden Komponenten, insbesondere Lagerelemente, durch das Öl geschmiert werden. Alternativ kann der Einlass des Gasverbindungskanals in Strömungsrichtung des Gas-Öl-Gemisches nach dem Ölabscheider angeordnet sein.Preferably, an inlet of the gas connection channel is arranged in front of the oil separator in the flow direction of the gas-oil mixture. As a result, the gas with oil dissolved in it is conveyed into the counter-pressure chamber, whereby the components adjacent to the counter-pressure chamber, in particular bearing elements, are transported through the oil be lubricated. Alternatively, the inlet of the gas connection channel can be arranged downstream of the oil separator in the flow direction of the gas-oil mixture.

In einer bevorzugten Ausgestaltung ist im Ölrückführungskanal und/oder Gasverbindungskanal ein Filter vorgesehen. In dem zurückführenden Öl und/oder im in die Gegendruckkammer strömenden Gas können Partikel enthalten sein, welche beispielsweise durch einen Verschleiß der zueinander bewegten Komponenten entstehen. Die Partikel können zu einem Verstopfen der Ölrückführungs-Drossel bzw. der Gasverbindungs-Drossel oder zu einem abrasiven Verschleiß der relativ zueinander bewegenden Komponenten führen. Durch den Filter können die Partikel aus dem Öl bzw. dem Gas herausgefiltert werden und ein Verstopfen des Ölrückführungskanals bzw. des Gasverbindungskanals sowie der abrasive Verschleiß der relativ zueinander bewegten Komponenten verhindert werden.In a preferred embodiment, a filter is provided in the oil return channel and/or gas connection channel. The returning oil and/or the gas flowing into the counter-pressure chamber may contain particles which arise, for example, from wear of the components moving relative to one another. The particles can lead to clogging of the oil return throttle or the gas connection throttle or to abrasive wear of the components moving relative to one another. The filter can be used to filter out the particles from the oil or gas and prevent clogging of the oil return channel or the gas connection channel as well as abrasive wear on the components moving relative to one another.

Vorzugsweise weist die Verdrängerspirale an der der Gleitscheibe zugewandten Seite eine umlaufende Nut auf, in welcher ein Gleitring angeordnet ist, wobei der Gleitring an der Gleitscheibe anliegt. Dadurch kann die Reibung zwischen der Gleitscheibe und der Verdrängerspirale während der orbitierenden Bewegung der Verdrängerspirale reduziert werden.The displacement spiral preferably has a circumferential groove on the side facing the sliding disk, in which a sliding ring is arranged, the sliding ring resting on the sliding disk. This allows the friction between the sliding disk and the displacement spiral to be reduced during the orbiting movement of the displacement spiral.

Vorzugsweise ist die Gleitscheibe senkrecht zu einer Längsachse formschlüssig mit dem Antriebsgehäuse verbunden. In einer bevorzugten Ausgestaltung weist das Verdichtergehäuse mindestens einen Fixierungsbolzen auf und die Gleitscheibe eine zum Fixierungsbolzen korrespondierende Fixierungsöffnung auf. Durch den Fixierungsbolzen können ein Verdrehen und eine radiale Verschiebung der Gleitscheibe zuverlässig verhindert werden. Der Fixierungsbolzen kann ein separates, in eine Öffnung des Verdichtergehäuses eingepresstes Bauteil sein oder einstückig mit dem Verdichtergehäuse hergestellt sein.Preferably, the sliding disk is positively connected to the drive housing perpendicular to a longitudinal axis. In a preferred embodiment, the compressor housing has at least one fixing bolt and the sliding disk has a fixing opening corresponding to the fixing bolt. The fixing bolt can reliably prevent twisting and radial displacement of the sliding disk. The fixing bolt can be a separate component pressed into an opening in the compressor housing or can be made in one piece with the compressor housing.

Vorzugsweise weist die Gleitscheibe mindestens eine Führungsöffnung auf, durch welche sich ein am Verdichtergehäuse befestigter und die orbitierenden Verdrängerspirale führender Führungsstift erstreckt. Der Führungsstift greift exzentrisch in eine Öffnung der Verdrängerspirale ein, wodurch die Verdrängerspirale während der orbitierenden Bewegung durch den Führungsstift geführt wird, wobei eine Rotationsbewegung der Verdrängerspirale durch den Führungsstift verhindert wird.Preferably, the sliding disk has at least one guide opening through which a guide pin attached to the compressor housing and guiding the orbiting displacement spiral extends. The guide pin engages eccentrically in an opening of the displacement spiral, whereby the displacement spiral is guided by the guide pin during the orbiting movement, with a rotational movement of the displacement spiral being prevented by the guide pin.

Vorzugsweise weist die Ölrückführungs-Drossel und/oder die Gasverbindungs-Drossel einen Durchmesser auf, welcher um ein Vielfaches kleiner ist als der Durchmesser des Fixierungsbolzens oder des Führungsstifts. Durch die Größe des Durchmessers der Ölrückführungs-Drossel und/oder der Gasverbindungs-Drossel kann der Öl- bzw. Gasmassenstrom gesteuert werden.Preferably, the oil return throttle and/or the gas connection throttle has a diameter that is many times smaller than the diameter of the fixing bolt or the guide pin. The oil or gas mass flow can be controlled by the size of the diameter of the oil return throttle and/or the gas connection throttle.

Vorzugsweise ist die orbitierende Verdrängerspirale über die Exzentereinheit mit einer Rotorwelle eines Rotors eines Elektromotors verbunden, wobei der Elektromotor in der Niederdruckkammer angeordnet ist. Durch die Anordnung des Elektromotors in der Niederdruckkammer wird der Elektromotor gekühlt und dadurch die Lebensdauer des Spiralverdichters erhöht.Preferably, the orbiting displacement spiral is connected via the eccentric unit to a rotor shaft of a rotor of an electric motor, the electric motor being arranged in the low-pressure chamber. By arranging the electric motor in the low-pressure chamber, the electric motor is cooled, thereby increasing the service life of the scroll compressor.

Es wird somit ein Spiralverdichter für eine Klimaanlage eines Kraftfahrzeugs geschaffen, welcher einen von der Hochdruckkammer zur Gegendruckkammer erstreckenden Gasverbindungskanal und/oder einen von der Hochdruckkammer zur Niederdruckkammer erstreckenden Ölrückführungskanal aufweist, wobei eine im Gasverbindungskanal angeordnete Gasverbindungs- und/oder eine im Ölrückführungskanal angeordnete Ölrückführungs-Drossel auf eine einfache und kostengünstige Weise durch die Gleitscheibe bereitgestellt wird und dadurch die Montageund Herstellungskosten des Spiralverdichters reduziert werden.A scroll compressor for an air conditioning system of a motor vehicle is thus created, which has a gas connection channel extending from the high-pressure chamber to the counter-pressure chamber and/or an oil return channel extending from the high-pressure chamber to the low-pressure chamber, with a gas connection arranged in the gas connection channel and/or an oil return channel arranged in the oil return channel. Throttle is provided in a simple and cost-effective manner by the sliding disk, thereby reducing the assembly and manufacturing costs of the scroll compressor.

Ein Ausführungsbeispiel eines erfindungsgemäßen Spiralverdichters ist in der Figur dargestellt und nachfolgend beschrieben.

  • Figur 1 zeigt eine Schnittansicht eines erfindungsgemäßen Spiralverdichters, und
  • Figur 2 zeigt eine Draufsicht einer Gleitscheibe des Spiralverdichters aus Figur 1.
An exemplary embodiment of a scroll compressor according to the invention is shown in the figure and described below.
  • Figure 1 shows a sectional view of a scroll compressor according to the invention, and
  • Figure 2 shows a top view of a sliding disk of the scroll compressor Figure 1 .

Ein Ausführungsbeispiel eines erfindungsgemäßen Spiralverdichters wird nachfolgend anhand der beigefügten Figuren beschrieben.An exemplary embodiment of a scroll compressor according to the invention is described below with reference to the attached figures.

Der Spiralverdichter 2 umfasst ein mehrteiliges Verdichtergehäuse 10 mit einem ersten Verdichtergehäuseteil 12, einem axial an das erste Verdichtergehäuseteil 12 anschließenden, zweiten Verdichtergehäuseteil 14 und einem an das zweite Verdichtergehäuseteil 14 anschließenden, dritten Verdichtergehäuseteil 16. Das erste Verdichtergehäuseteil 12, das zweite Verdichtergehäuseteil 14 und das dritte Verdichtergehäuseteil 16 begrenzen eine Motorraum 18. Das zweite Verdichtergehäuseteil 14 und das dritte Verdichtergehäuseteil 16 begrenzen einen Verdichterraum 20.The scroll compressor 2 comprises a multi-part compressor housing 10 with a first compressor housing part 12, a second compressor housing part 14 which adjoins the first compressor housing part 12 axially and a third compressor housing part 16 which adjoins the second compressor housing part 14. The first compressor housing part 12, the second compressor housing part 14 and the Third compressor housing part 16 delimits an engine compartment 18. The second compressor housing part 14 and the third compressor housing part 16 delimit a compressor compartment 20.

In dem Motorraum 18 ist ein Elektromotor 22 mit einem Stator 24 und einem Rotor 26 angeordnet. Der Rotor 26 ist auf einer Rotorwelle 28 befestigt. Die Rotorwelle 28 erstreckt sich ausgehend von dem Motorraum 18 durch eine zentrale Öffnung 29 des zweiten Verdichtergehäuseteils 14 in den Verdichterraum 20. Die Rotorwelle 28 ist über zwei endseitige Wellenlagerabschnitte 30, 34 um eine Rotorwellendrehachse drehbar in zwei Wellenlagern 40, 42 gelagert. Das erste Wellenlager 40 ist in dem Motorraum 18 angeordnet und lagert den ersten Wellenlagerabschnitt 30. Das zweite Wellenlager 42 ist in dem Verdichterraum 20 angeordnet und lagert den zweiten Wellenlagerabschnitt 34. An der dem Motorraum 18 zugewandten Seite des zweiten Wellenlagers 42 ist ein Wellendichtring 43 vorgesehen, der auf der radialen Innenseite an der Rotorwelle 28 anliegt und auf der radialen Außenseite durch das zweite Verdichtergehäuseteil 14 gestützt wird. Der Wellendichtring 43 dichtet den Motorraum 18 fluidisch gegenüber einer Gegendruckkammer 82 des Verdichterraums 20 ab.An electric motor 22 with a stator 24 and a rotor 26 is arranged in the engine compartment 18. The rotor 26 is attached to a rotor shaft 28. The rotor shaft 28 extends from the engine compartment 18 through a central opening 29 of the second compressor housing part 14 into the compressor compartment 20. The rotor shaft 28 is rotatably mounted in two shaft bearings 40, 42 via two end-side shaft bearing sections 30, 34 about a rotor shaft rotation axis. The first shaft bearing 40 is arranged in the engine compartment 18 and supports the first shaft bearing section 30. The second shaft bearing 42 is arranged in the compressor compartment 20 and supports the second shaft bearing section 34. A shaft sealing ring 43 is provided on the side of the second shaft bearing 42 facing the engine compartment 18 , which rests on the radial inside of the rotor shaft 28 and is supported on the radial outside by the second compressor housing part 14. The shaft sealing ring 43 fluidly seals the engine compartment 18 from a counter-pressure chamber 82 of the compressor compartment 20.

In dem Verdichterraum 20 ist eine Verdichtereinheit 58 angeordnet, welche eine orbitierende Verdrängerspirale 60 und eine feststehende Spirale 62 aufweist. Die orbitierende Verdrängerspirale 60 ist über ein Exzenterwellenlager 64 an einer an der Rotorwelle 28 befestigten Exzentereinheit 50 angeordnet und liegt über eine Gleitscheibe 70 an einer dem Verdichterraum 20 zugewandten Fläche des zweiten Verdichtergehäuseteils 14 an, wobei die Verdrängerspirale 60 an der der Gleitscheibe 70 zugewandten Seite einen in einer umlaufende Nut 140 angeordneten Gleitring 142 aufweist.A compressor unit 58 is arranged in the compressor chamber 20 and has an orbiting displacement spiral 60 and a fixed spiral 62. The orbiting displacement spiral 60 is arranged via an eccentric shaft bearing 64 on an eccentric unit 50 attached to the rotor shaft 28 and rests via a sliding disk 70 on a surface of the second compressor housing part 14 facing the compressor chamber 20, the displacement spiral 60 being on the side facing the sliding disk 70 has a sliding ring 142 arranged in a circumferential groove 140.

Die feststehende Spirale 62 ist fest in dem Verdichtergehäuse 10 angeordnet, wobei die feststehende Spirale 62 axial durch das zweite Verdichtergehäuseteil 14 und das dritte Verdichtergehäuseteil 16 gestützt wird.The fixed scroll 62 is fixedly disposed in the compressor housing 10, with the fixed scroll 62 being axially supported by the second compressor housing part 14 and the third compressor housing part 16.

Im Betrieb des Spiralverdichters 2 wird ein Kältemittel durch einen Verdichtereinlass 85 in den Motorraum 18 des Spiralverdichter 2 eingeleitet, wobei das Kältemittel durch den Motorraum 18 in den Verdichterraum 20 strömt. Durch eine Rotation der Rotorwelle 28 und damit des Exzenters 50 um die Rotordrehachse wird eine orbitierende Bewegung der Verdrängerspirale 60 erzeugt. Die orbitierende Verdrängerspirale 60 und die feststehende Spirale 62 sind derart ausgebildet, dass diese eine Verdichtungskammer 63 begrenzen und durch die orbitierende Bewegung der Verdrängerspirale 60 ein Kältemittel von einem radial außenliegenden Einlass 66 der Verdichtungskammer 63 zu einem radial innenliegenden Auslass 68 der Verdichtungskammer 63 gefördert und dabei verdichtet wird.During operation of the scroll compressor 2, a refrigerant is introduced through a compressor inlet 85 into the engine compartment 18 of the scroll compressor 2, with the refrigerant flowing through the engine compartment 18 into the compressor compartment 20. By rotating the rotor shaft 28 and thus the eccentric 50 about the rotor axis of rotation, an orbiting movement of the displacement spiral 60 is generated. The orbiting displacement spiral 60 and the fixed spiral 62 are designed such that they delimit a compression chamber 63 and, through the orbiting movement of the displacement spiral 60, a refrigerant is conveyed from a radially outer inlet 66 of the compression chamber 63 to a radially inner outlet 68 of the compression chamber 63 and thereby is compacted.

Der Verdichterraum 20 weist eine Hochdruckkammer 80 und eine Gegendruckkammer 82 auf. Die Hochdruckkammer 80 ist durch das dritte Verdichtergehäuseteil 16 und durch die feststehende Spirale 62 begrenzt und fluidisch zwischen dem Auslass 68 und einem Verdichterauslass 84 angeordnet, wobei das Kältemittel ausgehend vom Auslass 68 über die Hochdruckkammer 80 zum Verdichterauslass 84 strömt. Ausgehend vom Verdichterauslass 84 strömt das Kältemittel in einen Kühlmittelkreislauf eines Kraftfahrzeugs. Die Hochdruckkammer 80 weist eine Ölabscheidekammer 86 auf, welche fluidisch unmittelbar vor dem Verdichterauslass 84 angeordnet ist und einen Ölabscheider 88 aufweist. Der Ölabscheider 88 ist als Zyklon-Abscheider ausgeführt, wobei das Kältemittel durch den Ölabscheider 88 zum Verdichterauslass 84 strömt und das von dem Kältemittel gelöste Öl sich am Boden der Ölabscheidekammer 86, d.h. am untersten Punkt der Ölabscheidekammer 86, absetzt.The compressor chamber 20 has a high-pressure chamber 80 and a counter-pressure chamber 82. The high-pressure chamber 80 is delimited by the third compressor housing part 16 and by the fixed spiral 62 and is fluidly arranged between the outlet 68 and a compressor outlet 84, with the refrigerant flowing from the outlet 68 via the high-pressure chamber 80 to the compressor outlet 84. Starting from the compressor outlet 84, the refrigerant flows into a coolant circuit of a motor vehicle. The high-pressure chamber 80 has an oil separation chamber 86, which is fluidly arranged immediately in front of the compressor outlet 84 and has an oil separator 88. The oil separator 88 is designed as a cyclone separator, with the refrigerant flowing through the oil separator 88 to the compressor outlet 84 and the oil released from the refrigerant settling at the bottom of the oil separation chamber 86, i.e. at the lowest point of the oil separation chamber 86.

Zur Abführung des in der Ölabscheidekammer 86 abgesetzten Öls ist am Boden der Ölabscheidekammer 86 ein Einlass 89 eines Ölrückführungskanal 90 vorgesehen, welcher die Ölabscheidekammer 86 und damit die Hochdruckkammer 80 mit einer Niederdruckkammer 87 fluidisch verbindet, wobei der Motorraum 18 die Niederdruckkammer 87 bildet. Der Ölrückführungskanal 90 erstreckt sich durch das dritte Verdichtergehäuseteil 16, die feststehende Spirale 62 und durch das zweite Verdichtergehäuseteil 14, wobei im Ölrückführungskanal 90 ein Filter 130 angeordnet ist.To remove the oil deposited in the oil separation chamber 86, an inlet 89 of an oil return channel 90 is provided at the bottom of the oil separation chamber 86, which fluidly connects the oil separation chamber 86 and thus the high-pressure chamber 80 with a low-pressure chamber 87, the engine compartment 18 forming the low-pressure chamber 87. The oil return channel 90 extends through the third compressor housing part 16, the fixed spiral 62 and through the second compressor housing part 14, with a filter 130 being arranged in the oil return channel 90.

Die Gegendruckkammer 82 ist durch das zweite Verdichtergehäuseteil 14 und die orbitierende Verdrängerspirale 60 begrenzt, wobei der in der Gegendruckkammer 82 herrschende Druck auf die axial verschiebbare, orbitierende Verdrängerspirale 60 wirkt und daraus eine Axialbelastung auf die Verdrängerspirale resultiert. Diese Axialbelastung führt zu einer verbesserten Abdichtung zwischen den Stirnflächen der orbitierenden Verdrängerspirale 60 und der feststehenden Spirale 62. Die Gegendruckkammer 82 ist über einen Gasverbindungskanal 100 mit der Hochdruckkammer 80 fluidisch verbunden. Der Gasverbindungskanal 100 verläuft ausgehend von der Hochdruckkammer 80 durch die feststehende Spirale 62 und durch das zweite Verdichtergehäuseteil 14. Im dem Gasverbindungskanal 100 ist eine Gasverbindungs-Drossel angeordnet, welche den Massenstrom des in die Gegendruckkammer 82 strömenden Gases steuert.The counter-pressure chamber 82 is delimited by the second compressor housing part 14 and the orbiting displacement spiral 60, the pressure prevailing in the counter-pressure chamber 82 acting on the axially displaceable, orbiting displacement spiral 60, resulting in an axial load on the displacement spiral. This axial load leads to an improved seal between the end faces of the orbiting displacement spiral 60 and the fixed spiral 62. The counter-pressure chamber 82 is connected to the gas connection channel 100 via a gas connection channel 100 High pressure chamber 80 fluidly connected. The gas connection channel 100 runs from the high-pressure chamber 80 through the fixed spiral 62 and through the second compressor housing part 14. A gas connection throttle is arranged in the gas connection channel 100, which controls the mass flow of the gas flowing into the counter-pressure chamber 82.

Erfindungsgemäß verläuft der Ölrückführungskanal 90 und der Gasverbindungskanal 100 durch die zwischen dem zweiten Verdichtergehäuseteil 14 und der feststehenden Spirale 62 angeordneten Gleitscheibe 70, wobei die Gleitscheibe 70, welche in Figur 2 gezeigt ist, eine Ölrückführungs-Drossel 92 und eine Gasverbindungs-Drossel 96 aufweist.According to the invention, the oil return channel 90 and the gas connection channel 100 run through the sliding disk 70 arranged between the second compressor housing part 14 and the fixed spiral 62, the sliding disk 70, which in Figure 2 is shown, an oil return throttle 92 and a gas connection throttle 96.

Hierfür weist die Gleitscheibe 70 in ihrem radial äußeren Bereich eine erste Bohrung 94 und zur ersten Bohrung 94 in Umfangsrichtung beabstandet eine zweite Bohrung 98 auf. Die erste Bohrung 94 weist einen kleineren Durchmesser als der sonstige Verlauf der Ölrückführungsleitung 90 auf, so dass die erste Bohrung 94 die Ölrückführungs-Drossel 92 bildet. Die zweite Bohrung 98 weist einen kleineren Durchmesser als der sonstige Verlauf der Gasverbindungsleitung 100 auf, so dass die zweite Bohrung 98 die Gasverbindungs-Drossel 96 bildet. Damit wird durch die Ölrückführungs-Drossel 92 der Ölmassenstrom durch den Ölrückführungskanal 90 gesteuert und durch die Gasverbindungs-Drossel 96 der Gasmassenstrom in die Gegendruckkammer 82 gesteuert.For this purpose, the sliding disk 70 has a first bore 94 in its radially outer region and a second bore 98 spaced apart from the first bore 94 in the circumferential direction. The first bore 94 has a smaller diameter than the rest of the oil return line 90, so that the first bore 94 forms the oil return throttle 92. The second bore 98 has a smaller diameter than the rest of the gas connection line 100, so that the second bore 98 forms the gas connection throttle 96. The oil mass flow through the oil return channel 90 is thus controlled by the oil return throttle 92 and the gas mass flow into the counter-pressure chamber 82 is controlled by the gas connection throttle 96.

Des Weiteren weist die Gleitscheibe 70 im radial äußeren Bereich zwei Fixierungsöffnungen 102, 104 und im radial inneren Bereich sechs Führungsöffnungen 110, 112, 114, 116, 118, 120 auf, wobei die Fixierungsöffnungen 102, 104 und die Führungsöffnungen 110, 112, 114, 116, 118, 120 einen wesentlich größeren Durchmesser als die Bohrungen 94, 98 aufweisen. In die beiden Fixierungsöffnungen 102, 104 greift jeweils ein am zweiten Verdichtergehäuseteil 14 befestigter Fixierungsbolzen 103 ein, wodurch die Gleitscheibe 70 senkrecht zu einer Längsachse 106 des Spiralverdichters 2 fixiert wird. Die sechs Führungsöffnungen 110, 112, 114, 116, 118, 120 durchdringt jeweils ein am zweiten Verdichtergehäuseteil 14 befestigter Führungsstift 122, wobei die Führungsstifte 122 exzentrisch in jeweils eine an der Verdrängerspirale 60 vorgesehene Führungsbohrungen 124 eingreifen. Die Führungsbohrungen 124 weisen einen größeren Durchmesser als die Führungsstifte 122 auf, wobei die Führungsstifte 122 während der orbitierenden Bewegung der Verdrängerspirale 60 an der jeweiligen Innenumfangsfläche der Führungsbohrung 124 gleiten. Zur Reduzierung der Reibung zwischen den Führungsstiften 122 und der Verdrängerspirale 60 ist in den Führungsbohrungen 124 jeweils eine Gleitlagerhülse 126 angeordnet.Furthermore, the sliding disk 70 has two fixing openings 102, 104 in the radially outer region and six guide openings 110, 112, 114, 116, 118, 120 in the radially inner region, the fixing openings 102, 104 and the guide openings 110, 112, 114, 116, 118, 120 have a significantly larger diameter than the bores 94, 98. A fixing bolt 103 attached to the second compressor housing part 14 engages in each of the two fixing openings 102, 104 a, whereby the sliding disk 70 is fixed perpendicular to a longitudinal axis 106 of the scroll compressor 2. The six guide openings 110, 112, 114, 116, 118, 120 are each penetrated by a guide pin 122 attached to the second compressor housing part 14, the guide pins 122 engaging eccentrically in guide holes 124 provided on the displacement spiral 60. The guide bores 124 have a larger diameter than the guide pins 122, with the guide pins 122 sliding on the respective inner peripheral surface of the guide bore 124 during the orbiting movement of the displacement spiral 60. To reduce the friction between the guide pins 122 and the displacement spiral 60, a plain bearing sleeve 126 is arranged in the guide bores 124.

Es wird somit ein Spiralverdichter 2 geschaffen, welcher durch einen reduzierten Herstellungs- und Montageaufwand hergestellt werden kann, wobei die Ölrückführungs-Drossel 92 und die Gasverbindungs-Drossel 96 auf eine einfache und kostengünstige Weise durch die Gleitscheibe 70 bereitgestellt werden und dazu keine zusätzlichen Komponenten und damit verbundene Herstellungs- und Montageschritte erforderlich sind.A scroll compressor 2 is thus created, which can be produced with reduced manufacturing and assembly effort, the oil return throttle 92 and the gas connection throttle 96 being provided in a simple and cost-effective manner by the sliding disk 70 and no additional components and associated manufacturing and assembly steps are required.

Es sollte deutlich sein, dass der Schutzbereich nicht auf das beschriebene Ausführungsbeispiel beschränkt ist, sondern verschiedene Modifikationen denkbar sind. So kann beispielsweise die Gleitscheibe 70, das Verdichtergehäuse 10 oder die Verdichtereinheit 58 anders ausgeführt sein.It should be clear that the scope of protection is not limited to the exemplary embodiment described, but various modifications are conceivable. For example, the sliding disk 70, the compressor housing 10 or the compressor unit 58 can be designed differently.

Claims (14)

  1. Scroll compressor with
    a compressor housing (10),
    a high-pressure chamber (80),
    a low-pressure chamber (87) which is fluidically connected to the high-pressure chamber (80) via an oil return channel (90), an oil return throttle (92) being provided in the oil return channel (90),
    an orbiting displacement scroll (60) which is arranged on a driven eccentric unit (50) and engages in a fixed scroll (62), a sliding disc (70) being arranged between the orbiting displacement scroll (60) and the compressor housing (10), and
    a back-pressure chamber (82) which adjoins the displacement scroll (60) and is fluidically connected to the high-pressure chamber (80) via a gas connection channel (100), wherein a gas connection throttle (96) being provided in the gas connection channel (100),
    characterised in that
    the oil return channel (90) and/or the gas connection channel (100) extends through the sliding disc (70), wherein the sliding disc (70) has the oil return throttle (92) and/or the gas connection throttle (96).
  2. The scroll compressor according to claim 1, wherein
    the oil return throttle (92) or the gas connection throttle (96) is an opening (94, 98) provided on the sliding disc (70), wherein the opening (94, 98) has a smaller diameter than the oil return channel (90) or the gas connection channel (100).
  3. The scroll compressor according to claim 1 or 2, wherein
    the oil return channel (90) and/or the gas connection channel (100) extends at least partially through the stationary scroll (92).
  4. Scroll compressor according to claim 3, wherein
    the gas connection channel (100) extends from the high-pressure chamber (80) via a gas channel in the fixed scroll (62), through the sliding disc (70) and via a gas channel in the compressor housing (10) to the back-pressure chamber (82).
  5. Scroll compressor according to claim 3, wherein
    the oil return channel (90) extends from the high-pressure chamber (80) via an oil channel in the fixed scroll (62), through the sliding disc (70) and via an oil channel in the compressor housing (10) to the low-pressure chamber (87).
  6. Scroll compressor according to one of the preceding claims, wherein the high-pressure chamber (80) has an oil separation chamber (86) in which an oil separator (88) is arranged, an inlet (89) of the oil return channel (90) being arranged at the lowest point of the oil separation chamber (86).
  7. Scroll compressor according to one of the preceding claims, wherein an inlet (101) of the gas connection channel (100) is arranged upstream of the oil separator (88) in the direction of flow of the gas.
  8. Scroll compressor according to one of the preceding claims, wherein a filter (130) is provided in the oil return channel (90) and/or in the gas connection channel (100).
  9. Scroll compressor according to one of the preceding claims, wherein the displacement scroll (60) comprises, on the side facing the sliding disc (70), a circumferential groove (140) in which a sliding ring (142) is arranged, wherein the sliding ring (142) bears against the sliding disc (70).
  10. Scroll compressor according to one of the preceding claims,
    wherein
    the sliding disc (70) is positively connected to the compressor housing (10) perpendicular to a longitudinal axis (106).
  11. Scroll compressor according to claim 10, wherein
    the compressor housing (10) comprises at least one fixing bolt (103) and the sliding disc (70) comprises a fixing opening (102, 104) corresponding to the fixing bolt (103).
  12. Scroll compressor according to one of the preceding claims,
    wherein
    the sliding disc (70) comprises at least one guide opening (110, 112, 114, 116, 118, 120) through which a guide pin (122) attached to the compressor housing (10) and guiding the orbiting displacement scroll (60) extends.
  13. Scroll compressor according to claim 11 or 12, wherein
    the oil return throttle (92) and/or the gas connection throttle (94) comprises a diameter which is several times smaller than the diameter of the fixing bolt (103) or the guide pin (122).
  14. Scroll compressor according to one of the preceding claims,
    wherein
    the orbiting displacement scroll (60) is connected via the eccentric unit (50) to a rotor shaft (28) of a rotor (26) of an electric motor (22), wherein the electric motor (22) is arranged in the low-pressure chamber (87).
EP20700566.1A 2020-01-09 2020-01-09 Scroll compressor Active EP4088030B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/EP2020/050435 WO2021139890A1 (en) 2020-01-09 2020-01-09 Spiral compressor

Publications (2)

Publication Number Publication Date
EP4088030A1 EP4088030A1 (en) 2022-11-16
EP4088030B1 true EP4088030B1 (en) 2024-03-06

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ID=69159774

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Application Number Title Priority Date Filing Date
EP20700566.1A Active EP4088030B1 (en) 2020-01-09 2020-01-09 Scroll compressor

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US (1) US11965506B2 (en)
EP (1) EP4088030B1 (en)
WO (1) WO2021139890A1 (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1464841B1 (en) * 2003-03-31 2012-12-05 Kabushiki Kaisha Toyota Jidoshokki Hermetic compressor
JP5637151B2 (en) * 2012-01-20 2014-12-10 株式会社豊田自動織機 Differential pressure valve and electric compressor provided with differential pressure valve
JP6135126B2 (en) 2012-12-26 2017-05-31 株式会社豊田自動織機 Scroll compressor
KR101642178B1 (en) * 2013-07-02 2016-07-25 한온시스템 주식회사 Scroll compressor
DE102017105175B3 (en) * 2017-03-10 2018-08-23 OET GmbH Positive displacement machine according to the spiral principle, method for operating a positive displacement machine, positive displacement spiral, vehicle air conditioning system and vehicle
DE102017110913B3 (en) 2017-05-19 2018-08-23 OET GmbH Displacement machine according to the spiral principle, method for operating a positive displacement machine, vehicle air conditioning and vehicle

Also Published As

Publication number Publication date
WO2021139890A1 (en) 2021-07-15
EP4088030A1 (en) 2022-11-16
US11965506B2 (en) 2024-04-23
US20230349379A1 (en) 2023-11-02

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