EP3775567B1 - Method for controlling at least one radial blower in a cooling system, and radial blower - Google Patents

Method for controlling at least one radial blower in a cooling system, and radial blower Download PDF

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Publication number
EP3775567B1
EP3775567B1 EP19716110.2A EP19716110A EP3775567B1 EP 3775567 B1 EP3775567 B1 EP 3775567B1 EP 19716110 A EP19716110 A EP 19716110A EP 3775567 B1 EP3775567 B1 EP 3775567B1
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EP
European Patent Office
Prior art keywords
shaft
radial
housing
vibrometer
radial fan
Prior art date
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EP19716110.2A
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German (de)
French (fr)
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EP3775567A1 (en
Inventor
Andreas Lehr
Michael Bütikofer
David Muri
Christian Ambühl
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Teqtoniq GmbH
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Teqtoniq GmbH
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Publication of EP3775567A1 publication Critical patent/EP3775567A1/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/001Testing thereof; Determination or simulation of flow characteristics; Stall or surge detection, e.g. condition monitoring
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02Surge control
    • F04D27/0269Surge control by changing flow path between different stages or between a plurality of compressors; load distribution between compressors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/05Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/051Axial thrust balancing
    • F04D29/0513Axial thrust balancing hydrostatic; hydrodynamic thrust bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/05Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/056Bearings
    • F04D29/057Bearings hydrostatic; hydrodynamic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/30Control parameters, e.g. input parameters
    • F05D2270/334Vibration measurements

Definitions

  • the invention relates to a method for controlling at least one radial fan in a refrigeration system and a refrigeration system.
  • a radial fan for a gas laser comprises between a first and second radial bearing, in particular a radial gas bearing, a motor which is formed by a rotor and a stator.
  • An impeller is provided on a shaft in the housing of the radial fan, which is driven in rotation by the motor, in order to circulate the laser gas of a laser assembly.
  • This centrifugal fan further comprises an axial gas bearing which is positioned remotely from the impeller, with the motor having the first and second radial bearings arranged directly adjacent thereto being positioned between the axial gas bearing and the impeller.
  • a pressure medium is supplied to the radial gas bearings and the axial gas bearing through channels in the housing in order to form a hydrodynamic bearing.
  • Such radial fans are also suitable for integration into a refrigeration system.
  • a refrigeration system in particular the radial fan or fans, it is necessary for the operating points of the radial fans to be monitored.
  • the operating points of such a refrigeration system are constantly changing due to a continuously changing ambient temperature, the amount of heat to be cooled and the required temperature of the refrigeration system. These changes affect the centrifugal fans. Either the centrifugal fans can be overloaded and thus damaged, or the operating range is not optimally utilized.
  • This electric motor comprises a stator with a rotor which is mounted in bearing arrangements so that it can rotate relative to it, as well as a motor housing and a vibration sensor for recording vibrations occurring in the electric motor Vibrations caused by malfunctions in the bearing assemblies.
  • a single-stage centrifugal pump with an axial thrust compensation device is known, with an impeller connected to a shaft being arranged to rotate in the housing of the centrifugal pump.
  • At least one split ring seal arranged between the impeller and the housing forms a relief chamber, with the relief chamber being connected to the pressure region of the centrifugal pump by a pressure-transmitting connection.
  • a shaft seal is arranged between the shaft and the housing. This shaft is provided with at least one roller bearing that absorbs axial forces.
  • a turbo vacuum pump is known. This has a housing which is provided with a suction opening and a delivery opening. An evacuation pump arranged in the housing compresses the gas sucked in through the suction opening, which gas is discharged through the delivery opening. A motor is also provided to drive the evacuation pump.
  • This turbo compressor includes a housing with a cover, in which a rotor with an impeller arranged on the face side is positioned in a rotating manner.
  • a vibration sensor assigned to the blade ends of the impeller is provided in the cover in order to monitor the blade ends for possible blade breakage.
  • a turbo compressor is also known.
  • This turbocompressor includes a shaft which is rotatably supported by two radial foil air bearings spaced apart from one another.
  • An axial film air bearing is also provided. Vibrations are transmitted to a vibration sensor provided on the outer circumference of the metal plate via a metal plate, which is assigned to the axial film air bearing and the radial film air bearing adjacent thereto.
  • the invention is based on the object of proposing a method for controlling at least one radial fan in a refrigeration system and a radial fan, whereby a maximum energy efficiency of the radial fan or fans and thus of the refrigeration system is achieved.
  • the centrifugal fan comprises a housing in which a shaft is rotatably mounted, which at one end accommodates at least one impeller of a compressor that is attached to the housing and at least one radial bearing and at least one thrust gas bearing by which the shaft is rotatably supported in the housing and has a motor driven by a rotor and a stator, the motor being provided between the first and second radial bearings, a vibrometer for Shaft is aligned and another vibrometer is assigned to a front end of the shaft and positioned in the axis of rotation of the shaft and with the vibrometers, which are assigned to the shaft, operating points of the shaft are recorded and forwarded to a controller for determining an operating state of the radial fan.
  • the current operating state of the radial fan can be recorded and a critical operating state can also be monitored at the same time become. Due to the direct monitoring of the shaft, a corresponding control can be made possible based on the currently recorded operating situation in order to prevent a critical operating state or a limit value of the radial fan from being exceeded on the one hand and on the other hand to control an optimal efficiency value.
  • a critical limit value is preferably detected by the control of the radial fan and exceeding the limit value is prevented by the control of the radial fan itself or optionally by the control of the refrigeration system.
  • the controller can do this intervene to limit or reduce the speed of the motor in terms of its control in order to drive the shaft rotating below the critical limit value.
  • centrifugal fans are preferably connected to one another in a network using data lines.
  • a bus system is provided. This allows rapid communication and mutual exchange of the individual operating points.
  • one of the radial fans is preferably operated as the master and the other radial fans are operated as slaves.
  • the other radial fans operated as slaves are switched on by the master on the basis of its existing measured values in such a way that this network of radial fans works in a regulated energy minimum.
  • a further advantageous embodiment of the method provides that the signals recorded by the vibrometer are continuously evaluated. This allows full control and monitoring to be achieved.
  • a radial fan which comprises a housing in which a shaft is rotatably mounted, which at one end accommodates at least one impeller of a compressor which is attached to the housing and at least one radial bearing and at least one Has axial gas bearing, through which the shaft is rotatably supported on the housing, the shaft being driven by a motor having a rotor and stator, at least one vibrometer being provided which is associated with the shaft.
  • the vibrometer is aligned radially to the shaft of the centrifugal fan. As a result, vibrations occurring during rotation of the shaft can be determined.
  • a critical operating state of the shaft can be defined via the frequency and/or the amplitude of a vibrometer signal.
  • a further advantageous embodiment of the radial fan provides that the at least one vibrometer is assigned to the shaft between the rotor of the motor and the radial bearing or axial gas bearing provided adjacent thereto. As a result, critical operating states can be detected immediately adjacent to the generation of the rotational movement of the shaft.
  • a vibrometer is provided at a front end of the shaft. As a result, additional monitoring or a further parameter can be recorded in order to evaluate critical operating states.
  • the at least one vibrometer is preferably positioned in a housing opening so that it is assigned directly to the shaft.
  • the vibrometer is preferably provided in the housing opening so as to be pressure-tight.
  • FIG 1 a schematic sectional view of a radial fan 11 is shown.
  • This radial fan 11 radially accelerates a refrigerant from at least one impeller 16, 26 of a compressor 27 and directs it into lines of a refrigeration system 1, which is shown, for example, in figure 3 is shown.
  • This radial fan 11 radially accelerates the cooling medium from at least one impeller 16, 26 of a compressor 27 and compresses it into the gas pressure line 75 ( figure 3 ) the compression side of the refrigeration system 1 out.
  • the impeller 16, 26 is seated on a shaft 17 which is driven by a motor 20 in the central region of the motor housing 21.
  • This motor 20 consists of a rotor 18 connected to the shaft 17 and a stator 19 fastened to the motor housing 21.
  • the area which is arranged outside the impeller 16, 26 viewed from the shaft 17 forms the pressure side of the fan.
  • a radial bearing 22, 23, in particular a lower radial gas bearing 22 and an upper radial gas bearing 23, are arranged in the upper and lower region of the shaft 17, respectively.
  • These radial gas bearings 22, 23 include stationary bearing surfaces referred to as the radial stator 24. Furthermore, the shaft 17 in the area of the radial gas bearings 22, 23 rotating bearing surfaces 25.
  • the pressure medium for the gas bearings is advantageously the cooling medium.
  • An axial gas bearing 31 is provided between the impeller 16 of the compressor 27 and the lower radial gas bearing 22 .
  • This axial gas bearing 31 comprises a rotating disk 32 and axial stators 34 adjacent to the disk 32 or on its upper side and underside, each of which has stationary bearing surfaces 35 .
  • Disc 32 includes rotating bearing surfaces 36 opposed to stationary bearing surface 35 .
  • a duct 41 which is connected to the compression side of the refrigeration system 1, runs under the impeller 16.
  • the pressurized cooling medium is guided in a gaseous state under the impeller 16 through this duct 41 in order to counteract the axial gas bearing 31 to protect against the entry of particles.
  • the rotating bearing surfaces 25 of the radial gas bearing 22 and/or the rotating bearing surfaces 36 of the axial gas laser 31 preferably have surfaces that include grooves.
  • Herringbone patterns are preferably provided.
  • Such grooves or surface depressions are preferably introduced using an ultra-short pulse laser, in particular a picosecond laser. This enables processing with very short processing times. In addition, this processing step does not require any post-processing and meets the high requirements for precise design.
  • the very short laser pulses in the microsecond range result in a direct sublimation of the material. As a result, these grooves can be produced without reworking, in particular without burrs. In particular, an ion beam method is used. Alternatively, micro-machining can also be provided.
  • the radial fan 11 is aligned vertically in an installation situation in the refrigeration system 1 .
  • the compressor 27 is aligned downwards and the motor housing 21 is aligned vertically upwards.
  • the radial fan 11 can advantageously be arranged directly above a flooded evaporator 66 so that any condensate that may occur when the refrigeration system 1 is at a standstill flows back down into the evaporator 66 .
  • FIG 2 a schematically enlarged view of the axial gas bearing 31 and a connection of the compressor 27 to the motor housing 21 of the radial fan 11 is shown.
  • the compressor 27 with its housing 52 is connected to the motor housing 21 of the radial fan 11 without using a labyrinth seal or the like.
  • the supply of the pressurized cooling medium via the channel 41 is used to prevent particles from entering the axial gas bearing 31 .
  • the axial gas bearing 31 itself has such a narrow gap between the bearing surfaces 35 of the stator 34 and the bearing surfaces 36 of the rotating disk 32 that the axial gas bearing 31 itself forms a seal between a rotor chamber 46 in the housing 21 and a gas chamber 49 in the compressor 27 .
  • the rotor space 46 is formed between a through bore 47 in the motor housing 21 and the shaft 17 mounted therein.
  • the gas space 49 is formed between a housing section 51 of the motor housing 21 or housing 52 of the compressor 27 and the impeller 16 .
  • a housing 52 of the compressor 27 preferably encompasses the housing section 51 and is firmly connected to the motor housing 21 outside of this housing section 51 .
  • the cooling medium flows mainly in the direction of the gas space 49;
  • a seal between a pressure side of the compressor 27 and the motor housing 21 can thus be achieved by this arrangement.
  • the compressor 27 is preferably designed as a multi-stage compressor or turbo compressor.
  • a first stage forms the impeller 26, and the second stage forms the impeller 16.
  • the seal between the pressure side of the second stage or the impeller 16 of the compressor 27 and the motor housing 21 of the Radial fan 11 done.
  • the pressure connection 54 can preferably have a filter element. This serves to ensure that no particles get into the compressor 27 and/or the axial gas bearing 31 .
  • This radial fan 11 can also have a heating device 56 in the area of the axial gas bearing 31 or adjacent to an axial stator 34 or between the two axial stators 34 .
  • a heating device 56 serves to heat the axial gas bearing 31 to a temperature which is above the dew point of the cooling medium when the pressure is applied. This can prevent condensation of the cooling medium.
  • Such a heating device 56 can be designed as an electrically driven heater, such as by a resistance heating element or a PTC element.
  • a vibrometer 61 which is assigned to the shaft 17 , is preferably provided between the motor 20 and the lower radial gas bearing 22 .
  • This vibrometer 61 is a measuring device for quantifying mechanical vibrations.
  • Such a vibrometer 61 can be used to measure vibration frequency and vibration amplitude.
  • a so-called laser Doppler vibrometer can be used.
  • This vibrometer 61 is inserted into a housing opening 62 of the motor housing 21 and is preferably arranged in a pressure-tight manner. This can be done by means of an O-ring seal 63, for example. As a result, the pressure in the rotor space 46 for the hydrodynamic operation of the radial and axial gas bearings 22, 23, 31 can be maintained.
  • a measuring surface of the vibrometer 61 is aligned tangentially to the peripheral surface of the shaft 17 .
  • the measuring surface can advantageously also lie on a bearing sleeve surrounding a radial gas bearing 22 , 23 .
  • the frequency and the amplitude can be continuously detected by the vibrometer 61 and passed on to a controller 71 of the radial fan or the refrigeration system.
  • the current operating point or the operating points of the radial fan 11 prevailing during the cooling can be determined.
  • a comparison with a limit value can be carried out at the same time.
  • Such a limit value can be a critical operating state in which damage to the bearing or bearings or other components of the radial fan is to be expected. In particular to the effect that the shaft 17 in the motor housing 21 or the impellers 16, 26 in the compressor 27 are blocked.
  • a vibrometer 61 can also be provided between the motor 20 and the upper radial gas bearing 23 .
  • a further vibrometer 64 can be provided for additional monitoring of operating states of the radial fan 11, which is positioned in the axis of rotation of the shaft 17 and points to a front end of the shaft 17 with respect to a measuring surface. This also allows eccentricities in the rotating drive of the shaft 17 to be evaluated.
  • This additional vibrometer 64 is again positioned in a media-tight manner in a housing cover 65 in analogy to the vibrometer 61 .
  • FIG 3 a schematic view of a refrigeration system 1 is shown.
  • This refrigeration system 1 is only an example and works in particular according to the principle of evaporative cooling.
  • a refrigerant is located in an evaporator 66 .
  • the energy or heat required to evaporate the refrigerant is extracted from the environment.
  • the refrigerant absorbs this energy and turns into a gaseous state.
  • the refrigerant in the gaseous state is fed via a line 67 to one or, according to the exemplary embodiment, to a plurality of radial fans 11 which each have a compressor 27 .
  • the refrigerant is compressed to a high pressure and high temperature, which is higher than the inlet pressure and the inlet temperature before the compressor 11, respectively.
  • the refrigerant is then fed to a liquefier or a condenser 68 .
  • the refrigerant liquefied by cooling.
  • the refrigerant is then passed through a throttle element, in particular an expansion valve 69, at high pressure.
  • the refrigerant expands or is converted to low pressure and can be supplied to the evaporator 66 in the liquid state in order in turn to extract the heat from the environment.
  • the refrigeration system 1 is a closed refrigeration circuit.
  • a controller 71 of the refrigeration system 1 is provided, by means of which the individual radial fans 11 can be controlled.
  • the radial fans 11 are preferably each connected to the controller 71 by a bus system 72 .
  • the compressor control or a radial fan control preferably works according to the master-slave principle.
  • the master function is assigned to one of the radial fans 11 .
  • the other radial fans 11 are operated as so-called slaves in the network.
  • the controller 71 acquires the measured values of the sensors of the radial fan from the master. On the basis of these recorded or existing measured values, the further radial fans are switched on in each case, so that the network of radial fans 11 is operated at a regulated energy minimum. A protective function of each individual radial fan 11 is retained.
  • control and regulation algorithms are used in the controller 71 for controlling the radial fan 11 in such a way that no critical operating point can arise for the respective radial fan 11.
  • the radial fans 11 can also communicate with one another via the bus system 72 in order to independently control the achievement of an energy efficiency maximum based on the measured values present in the radial fan 11 itself, in particular based on the measured values present in the master radial fan 11.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Motor Or Generator Cooling System (AREA)

Description

Die Erfindung betrifft ein Verfahren zur Steuerung von zumindest einem Radialgebläse in einer Kälteanlage sowie einer Kälteanlage.The invention relates to a method for controlling at least one radial fan in a refrigeration system and a refrigeration system.

Aus der DE 10 2010 001 538 A1 ist ein Radialgebläse für einen Gaslaser bekannt. Ein solches Radialgebläse umfasst zwischen einem ersten und zweiten Radiallager, insbesondere einem Radialgaslager, einen Motor, der durch einen Rotor und einen Stator gebildet ist. An einer Welle im Gehäuse des Radialgebläses, welche durch den Motor rotierend angetrieben wird, ist ein Laufrad vorgesehen, um das Lasergas einer Laserbaugruppe umzuwälzen. Dieses Radialgebläse umfasst des Weiteren ein Axialgaslager, welches entfernt zum Laufrad positioniert ist, wobei zwischen dem Axialgaslager und dem Laufrad der Motor mit dem direkt benachbart dazu angeordneten ersten und zweiten Radiallager positioniert ist. Durch Kanäle im Gehäuse wird den Radialgaslagern und dem Axialgaslager ein Druckmedium zugeführt, um eine hydrodynamische Lagerung auszubilden.From the DE 10 2010 001 538 A1 a radial fan for a gas laser is known. Such a radial fan comprises between a first and second radial bearing, in particular a radial gas bearing, a motor which is formed by a rotor and a stator. An impeller is provided on a shaft in the housing of the radial fan, which is driven in rotation by the motor, in order to circulate the laser gas of a laser assembly. This centrifugal fan further comprises an axial gas bearing which is positioned remotely from the impeller, with the motor having the first and second radial bearings arranged directly adjacent thereto being positioned between the axial gas bearing and the impeller. A pressure medium is supplied to the radial gas bearings and the axial gas bearing through channels in the housing in order to form a hydrodynamic bearing.

Solche Radialgebläse eignen sich auch zu einer Einbindung in eine Kälteanlage. Beim Betrieb der Kälteanlage, insbesondere dem oder den Radialgebläsen, ist es erforderlich, dass die Betriebspunkte der Radialgebläse überwacht werden. Aufgrund von einer fortlaufend sich ändernden Umgebungstemperatur, zu kühlender Wärmemenge und geforderten Temperatur der Kälteanlage ändern sich die Betriebspunkte einer solchen Kälteanlage fortdauernd. Diese Änderungen wirken sich auf die Radialgebläse aus. Entweder kann es zu einer Überbelastung der Radialgebläse und somit zu Beschädigungen kommen oder der Betriebsbereich wird nicht optimal ausgenutzt.Such radial fans are also suitable for integration into a refrigeration system. During operation of the refrigeration system, in particular the radial fan or fans, it is necessary for the operating points of the radial fans to be monitored. The operating points of such a refrigeration system are constantly changing due to a continuously changing ambient temperature, the amount of heat to be cooled and the required temperature of the refrigeration system. These changes affect the centrifugal fans. Either the centrifugal fans can be overloaded and thus damaged, or the operating range is not optimally utilized.

Aus der DE 10 2013 102 648 A1 ist ein Elektromotor mit einer Funktionsüberwachung der Motorlager bekannt. Dieser Elektromotor umfasst einen Stator mit einem relativ zu diesem drehbar in Lageranordnungen gelagerten Rotor sowie ein Motorgehäuse und einen Schwingungssensor zur Aufnahme von im Elektromotor auftretenden Schwingungen, die durch Funktionsstörungen an den Lageranordnungen verursacht werden.From the DE 10 2013 102 648 A1 an electric motor with function monitoring of the motor bearings is known. This electric motor comprises a stator with a rotor which is mounted in bearing arrangements so that it can rotate relative to it, as well as a motor housing and a vibration sensor for recording vibrations occurring in the electric motor Vibrations caused by malfunctions in the bearing assemblies.

Aus der DE 10 2006 011 613 A1 ist eine einstufige Kreiselpumpe mit einer Axialschubausgleichseinrichtung bekannt, wobei im Gehäuse der Kreiselpumpe ein mit einer Welle verbundenes Laufrad rotierend angeordnet ist. Mindestens eine zwischen Laufrad und Gehäuse angeordnete Spaltringabdichtung bildet einen Entlastungsraum, wobei der Entlastungsraum mit einer druckübertragenden Verbindung an den Druckbereich der Kreiselpumpe angeschlossen ist. Zwischen Welle und Gehäuse ist eine Wellenabdichtung angeordnet. Diese Welle ist mit zumindest einem Axialkräfte aufnehmenden Wälzlager versehen.From the DE 10 2006 011 613 A1 a single-stage centrifugal pump with an axial thrust compensation device is known, with an impeller connected to a shaft being arranged to rotate in the housing of the centrifugal pump. At least one split ring seal arranged between the impeller and the housing forms a relief chamber, with the relief chamber being connected to the pressure region of the centrifugal pump by a pressure-transmitting connection. A shaft seal is arranged between the shaft and the housing. This shaft is provided with at least one roller bearing that absorbs axial forces.

Aus der DE 43 27 506 A1 ist eine Turbovakuumpumpe bekannt. Diese weist ein Gehäuse auf, das mit einer Ansaugöffnung und einer Förderöffnung versehen ist. Eine in dem Gehäuse angeordnete Evakuierungspumpe verdichtet das durch die Ansaugöffnung angesaugte Gas, welches durch die Förderöffnung abgeführt wird. Des Weiteren ist ein Motor für den Antrieb der Evakuierpumpe vorgesehen.From the DE 43 27 506 A1 a turbo vacuum pump is known. This has a housing which is provided with a suction opening and a delivery opening. An evacuation pump arranged in the housing compresses the gas sucked in through the suction opening, which gas is discharged through the delivery opening. A motor is also provided to drive the evacuation pump.

Aus der KR 2001 0081670 A ist ein Turbokompressor bekannt. Dieser Turbokompressor umfasst ein Gehäuse mit einem Deckel, in welchem ein Rotor mit jeweils einem stirnseitig daran angeordneten Laufrad rotierend positioniert ist. In dem Deckel ist den Schaufelenden des Laufrades zugeordnet ein Schwingungssensor vorgesehen, um die Schaufelenden auf einen möglichen Schaufelbruch hin zu überwachen.From the KR 2001 0081670 A a turbo compressor is known. This turbo compressor includes a housing with a cover, in which a rotor with an impeller arranged on the face side is positioned in a rotating manner. A vibration sensor assigned to the blade ends of the impeller is provided in the cover in order to monitor the blade ends for possible blade breakage.

Aus der KR 2016 0087299 A ist des Weiteren ein Turbokompressor bekannt. Dieser Turbokompressor umfasst eine Welle, welche durch zwei zueinander beabstandete radiale Folienluftlager rotierend gelagert ist. Des Weiteren ist ein axiales Folienluftlager vorgesehen. Über eine Metallplatte, welche dem axialen Folienluftlager und dem dazu benachbarten radialen Folienluftlager zugeordnet ist, werden Schwingungen an einen am Außenumfang der Metallplatte vorgesehenen Schwingungssensor übertragen.From the KR 2016 0087299 A a turbo compressor is also known. This turbocompressor includes a shaft which is rotatably supported by two radial foil air bearings spaced apart from one another. An axial film air bearing is also provided. Vibrations are transmitted to a vibration sensor provided on the outer circumference of the metal plate via a metal plate, which is assigned to the axial film air bearing and the radial film air bearing adjacent thereto.

Der Erfindung liegt die Aufgabe zugrunde, ein Verfahren zur Steuerung von zumindest einem Radialgebläse in einer Kälteanlage sowie ein Radialgebläse vorzuschlagen, wodurch ein Energieeffizienzmaximum des oder der Radialgebläse und somit der Kälteanlage erreicht wird.The invention is based on the object of proposing a method for controlling at least one radial fan in a refrigeration system and a radial fan, whereby a maximum energy efficiency of the radial fan or fans and thus of the refrigeration system is achieved.

Diese Aufgabe wird durch ein Verfahren zur Steuerung von zumindest einem Radialgebläse in einer Kälteanlage gelöst, bei welchem das Radialgebläse ein Gehäuse umfasst, in welchem eine Welle rotierend gelagert ist, die an einem Ende zumindest ein Laufrad eines Verdichters aufnimmt, der an dem Gehäuse befestigt ist und zumindest ein Radiallager und zumindest ein Axialgaslager umfasst, durch welche die Welle rotierend im Gehäuse gelagert ist und einen Motor aufweist, der durch einen Rotor und einen Stator angetrieben wird, wobei der Motor zwischen dem ersten und zweiten Radiallager vorgesehen ist, wobei ein Vibrometer zur Welle ausgerichtet wird und ein weiteres Vibrometer einem stirnseitigen Ende der Welle zugeordnet und in der Rotationsachse der Welle positioniert wird und mit den Vibrometern, welche der Welle zugeordnet sind, Betriebspunkte der Welle erfasst und an eine Steuerung zur Ermittlung eines Betriebszustandes des Radialgebläses weitergeleitet werden. Durch die Überwachung der Welle, durch welche das zumindest eine Laufrad des Radialgebläses angetrieben und die Kühlung aufgrund des durch das zumindest eine Laufrad beschleunigte und/oder verdichtete Druckmedium oder Kältemittel erzielt wird, kann der aktuelle Betriebszustand des Radialgebläses erfasst und gleichzeitig auch ein kritischer Betriebszustand überwacht werden. Durch die unmittelbare Überwachung der Welle kann aufgrund der aktuell erfassten Betriebssituation eine entsprechende Ansteuerung ermöglicht sein, um einerseits ein Überschreiten eines kritischen Betriebszustandes oder eines Grenzwertes des Radialgebläses zu verhindern und andererseits einen optimalen Effizienzwert anzusteuern.This object is achieved by a method for controlling at least one centrifugal fan in a refrigeration system, in which the centrifugal fan comprises a housing in which a shaft is rotatably mounted, which at one end accommodates at least one impeller of a compressor that is attached to the housing and at least one radial bearing and at least one thrust gas bearing by which the shaft is rotatably supported in the housing and has a motor driven by a rotor and a stator, the motor being provided between the first and second radial bearings, a vibrometer for Shaft is aligned and another vibrometer is assigned to a front end of the shaft and positioned in the axis of rotation of the shaft and with the vibrometers, which are assigned to the shaft, operating points of the shaft are recorded and forwarded to a controller for determining an operating state of the radial fan. By monitoring the shaft, by which the at least one impeller of the radial fan is driven and the cooling is achieved on the basis of the pressure medium or refrigerant accelerated and/or compressed by the at least one impeller, the current operating state of the radial fan can be recorded and a critical operating state can also be monitored at the same time become. Due to the direct monitoring of the shaft, a corresponding control can be made possible based on the currently recorded operating situation in order to prevent a critical operating state or a limit value of the radial fan from being exceeded on the one hand and on the other hand to control an optimal efficiency value.

Bevorzugt wird ein kritischer Grenzwert durch die Steuerung des Radialgebläses erfasst und ein Überschreiten des Grenzwertes durch die Steuerung des Radialgebläses selbst oder wahlweise durch die Steuerung der Kälteanlage verhindert. Die Steuerung kann dabei dahingehend eingreifen, dass der Motor bezüglich seiner Ansteuerung in der Drehzahl begrenzt oder reduziert wird, um unterhalb des kritischen Grenzwertes die Welle rotierend anzutreiben.A critical limit value is preferably detected by the control of the radial fan and exceeding the limit value is prevented by the control of the radial fan itself or optionally by the control of the refrigeration system. The controller can do this intervene to limit or reduce the speed of the motor in terms of its control in order to drive the shaft rotating below the critical limit value.

Des Weiteren werden bevorzugt bei mehreren in der Kälteanlage vorgesehenen Radialgebläsen durch die jeweiligen Vibrometer Betriebspunkte erfasst, die jeweiligen Betriebspunkte der Radialgebläse miteinander verglichen und auf die maximale Energieeffizienz des jeweiligen Radialgebläses eingestellt. Eine solche Ansteuerung und Überwachung weist den Vorteil auf, dass die jeweiligen Steuerungen für die Radialgebläse selbständig eine Kontrolle zur Erreichung eines Energieeffizienzmaximums durchführen, das heißt, dass jedes Radialgebläse unabhängig voneinander in seinem eigenen Energieeffizienzmaximum arbeiten kann und somit in der Gesamtheit eine optimale Effizienz der Kälteanlage erzielt wird. Dies führt dazu, dass ein Verbund von mehreren Radialgebläsen in einem geregelten Energieminimum für die Kälteanlage betrieben werden kann. Unabhängig davon bleibt bevorzugt die Selbstschutzfunktion jedes einzelnen Radialgebläses bezüglich dessen kritischen Grenzwertes aufrechterhalten.Furthermore, with several radial fans provided in the refrigeration system, operating points are preferably detected by the respective vibrometer, the respective operating points of the radial fans are compared with one another and adjusted to the maximum energy efficiency of the respective radial fan. Such control and monitoring has the advantage that the respective controllers for the radial fans independently carry out a check to achieve an energy efficiency maximum, i.e. that each radial fan can work independently of one another in its own energy efficiency maximum and thus optimal overall efficiency of the refrigeration system is achieved. This means that a network of several radial fans can be operated in a controlled energy minimum for the refrigeration system. Irrespective of this, the self-protection function of each individual radial fan is preferably maintained with regard to its critical limit value.

Bei mehreren Radialgebläsen in der Kälteanlage sind diese bevorzugt mit Datenleitungen in einem Netzwerk miteinander verbunden. Insbesondere ist ein Bus-System vorgesehen. Dadurch können eine schnelle Kommunikation und ein gegenseitiger Austausch der einzelnen Betriebspunkte ermöglicht sein.If there are several centrifugal fans in the refrigeration system, these are preferably connected to one another in a network using data lines. In particular, a bus system is provided. This allows rapid communication and mutual exchange of the individual operating points.

Des Weiteren werden bevorzugt bei mehreren Radialgebläsen in der Kälteanlage eines der Radialgebläse als Master und die weiteren Radialgebläse als Slave betrieben. Dadurch werden durch den Master auf Basis seiner vorhandenen Messwerte die weiteren als Slave betriebenen Radialgebläse jeweils entsprechend derart zugeschaltet, dass dieser Verbund der Radialgebläse in einem geregelten Energieminimum arbeitet.Furthermore, if there are several radial fans in the refrigeration system, one of the radial fans is preferably operated as the master and the other radial fans are operated as slaves. As a result, the other radial fans operated as slaves are switched on by the master on the basis of its existing measured values in such a way that this network of radial fans works in a regulated energy minimum.

Eine weitere vorteilhafte Ausgestaltung des Verfahrens sieht vor, dass die durch die Vibrometer erfassten Signale permanent ausgewertet werden. Dadurch kann eine vollständige Kontrolle und Überwachung erzielt werden.A further advantageous embodiment of the method provides that the signals recorded by the vibrometer are continuously evaluated. This allows full control and monitoring to be achieved.

Die der Erfindung zugrundeliegende Aufgabe wird des Weiteren durch ein Radialgebläse gelöst, welches ein Gehäuse umfasst, in welchem eine Welle rotierend gelagert ist, die an einem Ende zumindest ein Laufrad eines Verdichters aufnimmt, der an dem Gehäuse befestigt ist und zumindest ein Radiallager und zumindest ein Axialgaslager aufweist, durch welches die Welle rotierend am Gehäuse gelagert ist, wobei die Welle durch einen Motor mit einem Rotor und Stator angetrieben wird, wobei zumindest ein Vibrometer vorgesehen ist, welches der Welle zugeordnet ist. Durch die Ermittlung der Betriebspunkte unmittelbar an der Welle kann eine exakte Erfassung eines Betriebszustands des Radialgebläses erzielt werden. Dadurch können kritische Betriebspunkte oder ein Überschreiten von Grenzwerten der Lager und/oder des Radialgebläses sofort erkannt und diesen entgegengewirkt werden. Die von dem Vibrometer erfassten Daten werden an die Steuerung für das Radialgebläse weitergeleitet.The object on which the invention is based is also achieved by a radial fan, which comprises a housing in which a shaft is rotatably mounted, which at one end accommodates at least one impeller of a compressor which is attached to the housing and at least one radial bearing and at least one Has axial gas bearing, through which the shaft is rotatably supported on the housing, the shaft being driven by a motor having a rotor and stator, at least one vibrometer being provided which is associated with the shaft. By determining the operating points directly on the shaft, an exact detection of an operating state of the radial fan can be achieved. As a result, critical operating points or exceeding the limit values of the bearings and/or the radial fan can be recognized immediately and counteracted. The data recorded by the vibrometer are forwarded to the controller for the centrifugal fan.

Das Vibrometer ist radial zur Welle des Radialgebläses ausgerichtet. Dadurch können bei einer Rotation der Welle entstehende Schwingungen ermittelt werden. Ein kritischer Betriebszustand der Welle kann über die Frequenz und/oder die Amplitude eines Vibrometersignals definiert werden.The vibrometer is aligned radially to the shaft of the centrifugal fan. As a result, vibrations occurring during rotation of the shaft can be determined. A critical operating state of the shaft can be defined via the frequency and/or the amplitude of a vibrometer signal.

Eine weitere vorteilhafte Ausgestaltung des Radialgebläses sieht vor, dass das zumindest eine Vibrometer zwischen dem Rotor des Motors und dem benachbart dazu vorgesehenen Radiallager oder Axialgaslager der Welle zugeordnet ist. Dadurch können kritische Betriebszustände unmittelbar benachbart zur Erzeugung der Rotationsbewegung der Welle erfasst werden.A further advantageous embodiment of the radial fan provides that the at least one vibrometer is assigned to the shaft between the rotor of the motor and the radial bearing or axial gas bearing provided adjacent thereto. As a result, critical operating states can be detected immediately adjacent to the generation of the rotational movement of the shaft.

Des Weiteren ist an einem stirnseitigen Ende der Welle ein Vibrometer vorgesehen. Dadurch kann eine zusätzliche Überwachung beziehungsweise ein weiterer Parameter erfasst werden, um kritische Betriebszustände zu bewerten.Furthermore, a vibrometer is provided at a front end of the shaft. As a result, additional monitoring or a further parameter can be recorded in order to evaluate critical operating states.

Das zumindest eine Vibrometer ist bevorzugt in einer Gehäuseöffnung positioniert, sodass dieses unmittelbar der Welle zugeordnet ist. Bevorzugt ist das Vibrometer druckmediendicht in der Gehäuseöffnung vorgesehen. Dadurch kann einerseits das benachbart dazu angeordnete Radialgaslager und/oder Axialgaslager hydrodynamisch angetrieben werden, und andererseits ist eine unmittelbare Erfassung der Welle ermöglicht.The at least one vibrometer is preferably positioned in a housing opening so that it is assigned directly to the shaft. The vibrometer is preferably provided in the housing opening so as to be pressure-tight. As a result, on the one hand, the radial gas bearing and/or axial gas bearing arranged adjacent thereto can be driven hydrodynamically, and on the other hand, direct detection of the shaft is made possible.

Die Erfindung sowie weitere vorteilhafte Ausführungsformen und Weiterbildungen derselben werden im Folgenden anhand der in den Zeichnungen dargestellten Beispiele näher beschrieben und erläutert.The invention and other advantageous embodiments and developments thereof are described and explained in more detail below with reference to the examples shown in the drawings.

Es zeigen:

  • Figur 1 eine schematische Schnittansicht eines Radialgebläses,
  • Figur 2 eine schematisch vergrößerte Ansicht eines Axialgaslagers benachbart zum Verdichter, und
  • Figur 3 eine schematische Ansicht einer Kälteanlage.
Show it:
  • figure 1 a schematic sectional view of a radial fan,
  • figure 2 a schematic enlarged view of a thrust gas bearing adjacent to the compressor, and
  • figure 3 a schematic view of a refrigeration system.

In Figur 1 ist eine schematische Schnittdarstellung eines Radialgebläses 11 dargestellt. Durch dieses Radialgebläse 11 wird ein Kältemittel, von zumindest einem Laufrad 16, 26 eines Verdichters 27 radial beschleunigt und in Leitungen einer Kälteanlage 1 gelenkt, welche beispielhaft in Figur 3 dargestellt ist.In figure 1 a schematic sectional view of a radial fan 11 is shown. This radial fan 11 radially accelerates a refrigerant from at least one impeller 16, 26 of a compressor 27 and directs it into lines of a refrigeration system 1, which is shown, for example, in figure 3 is shown.

Durch dieses Radialgebläse 11 wird das Kühlmedium von zumindest einem Laufrad 16, 26 eines Verdichters 27 radial beschleunigt und komprimiert in die Gasdruckleitung 75 (Figur 3) der Kompressionsseite der Kälteanlage 1 geführt. Das Laufrad 16, 26 sitzt auf einer Welle 17, welche im mittleren Bereich des Motorengehäuses 21 von einem Motor 20 angetrieben wird. Dieser Motor 20 besteht aus einem mit der Welle 17 verbundenen Rotor 18 und einem am Motorengehäuse 21 befestigten Stator 19. Der Bereich, der von der Welle 17 her gesehen außerhalb des Laufrades 16, 26 angeordnet ist, bildet die Druckseite des Gebläses. Im oberen und unteren Bereich der Welle 17 sind jeweils ein Radiallager 22, 23, insbesondere ein unteres Radialgaslager 22 und ein oberes Radialgaslager 23, angeordnet. Diese Radialgaslager 22, 23 umfassen stationäre Lagerflächen, die als Radialstator 24 bezeichnet werden. Des Weiteren umfasst die Welle 17 im Bereich der Radialgaslager 22, 23 rotierende Lagerflächen 25. Das Druckmedium für die Gaslager ist vorteilhaft das Kühlmedium. Zwischen dem Laufrad 16 des Verdichters 27 und dem unteren Radialgaslager 22 ist ein Axialgaslager 31 vorgesehen. Dieses Axialgaslager 31 umfasst eine rotierende Scheibe 32 sowie benachbart zur Scheibe 32 beziehungsweise an deren Oberseite und Unterseite Axialstatoren 34, welche jeweils stationäre Lagerflächen 35 aufweisen. Die Scheibe 32 umfasst rotierende Lagerflächen 36, die der stationären Lagerfläche 35 gegenüberliegen. Zwischen Axialgaslager 31 und Laufrad 16 führt ein Kanal 41, der mit der Kompressionsseite der Kälteanlage 1 verbunden ist, unter das Laufrad 16. Durch diesen Kanal 41 wird das unter Druck stehende Kühlmedium in gasförmigem Zustand unter das Laufrad 16 geführt, um das Axialgaslager 31 gegen den Eintritt von Partikeln zu schützen.This radial fan 11 radially accelerates the cooling medium from at least one impeller 16, 26 of a compressor 27 and compresses it into the gas pressure line 75 ( figure 3 ) the compression side of the refrigeration system 1 out. The impeller 16, 26 is seated on a shaft 17 which is driven by a motor 20 in the central region of the motor housing 21. This motor 20 consists of a rotor 18 connected to the shaft 17 and a stator 19 fastened to the motor housing 21. The area which is arranged outside the impeller 16, 26 viewed from the shaft 17 forms the pressure side of the fan. A radial bearing 22, 23, in particular a lower radial gas bearing 22 and an upper radial gas bearing 23, are arranged in the upper and lower region of the shaft 17, respectively. These radial gas bearings 22, 23 include stationary bearing surfaces referred to as the radial stator 24. Furthermore, the shaft 17 in the area of the radial gas bearings 22, 23 rotating bearing surfaces 25. The pressure medium for the gas bearings is advantageously the cooling medium. An axial gas bearing 31 is provided between the impeller 16 of the compressor 27 and the lower radial gas bearing 22 . This axial gas bearing 31 comprises a rotating disk 32 and axial stators 34 adjacent to the disk 32 or on its upper side and underside, each of which has stationary bearing surfaces 35 . Disc 32 includes rotating bearing surfaces 36 opposed to stationary bearing surface 35 . Between the axial gas bearing 31 and the impeller 16, a duct 41, which is connected to the compression side of the refrigeration system 1, runs under the impeller 16. The pressurized cooling medium is guided in a gaseous state under the impeller 16 through this duct 41 in order to counteract the axial gas bearing 31 to protect against the entry of particles.

Bevorzugt weisen die rotierenden Lagerflächen 25 des Radialgaslagers 22 und/oder die rotierenden Lagerflächen 36 des Axialgaslasers 31 Oberflächen auf, die Nuten umfassen. Bevorzugt sind Fischgrätenmuster vorgesehen. Solche Nuten oder Oberflächenvertiefungen werden bevorzugt mit einem Ultrakurzpuls-Laser, insbesondere Pikosekunden-Laser, eingebracht. Dies ermöglicht eine Bearbeitung mit sehr kurzen Bearbeitungszeiten. Darüber hinaus ist dieser Bearbeitungsschritt nacharbeitungsfrei und erfüllt die hohen Anforderungen an die präzise Ausgestaltung. Durch die sehr kurzen Laserimpulse im Mikrosekundenbereich kommt es zu einer direkten Sublimierung des Materials. Dadurch kann eine nacharbeitungsfreie, insbesondere gratfreie, Herstellung dieser Nuten vorgesehen sein. Insbesondere wird ein lonenstrahlverfahren eingesetzt. Alternativ kann auch eine Mikrozerspanung vorgesehen sein.The rotating bearing surfaces 25 of the radial gas bearing 22 and/or the rotating bearing surfaces 36 of the axial gas laser 31 preferably have surfaces that include grooves. Herringbone patterns are preferably provided. Such grooves or surface depressions are preferably introduced using an ultra-short pulse laser, in particular a picosecond laser. This enables processing with very short processing times. In addition, this processing step does not require any post-processing and meets the high requirements for precise design. The very short laser pulses in the microsecond range result in a direct sublimation of the material. As a result, these grooves can be produced without reworking, in particular without burrs. In particular, an ion beam method is used. Alternatively, micro-machining can also be provided.

Das Radialgebläse 11 ist in einer Einbausituation in der Kälteanlage 1 vertikal ausgerichtet. Dabei sind der Verdichter 27 nach unten ausgerichtet und das Motorengehäuse 21 vertikal nach oben ausgerichtet. Das Radialgebläse 11 kann vorteilhaft direkt über einem überfluteten Verdampfer 66 angeordnet sein, sodass ggf. im Stillstand der Kälteanlage 1 entstehendes Kondensat nach unten in den Verdampfer 66 zurückfließt.The radial fan 11 is aligned vertically in an installation situation in the refrigeration system 1 . The compressor 27 is aligned downwards and the motor housing 21 is aligned vertically upwards. The radial fan 11 can advantageously be arranged directly above a flooded evaporator 66 so that any condensate that may occur when the refrigeration system 1 is at a standstill flows back down into the evaporator 66 .

In Figur 2 ist eine schematisch vergrößerte Ansicht des Axialgaslagers 31 sowie eine Anbindung des Verdichters 27 an das Motorengehäuse 21 des Radialgebläses 11 dargestellt. Die Anbindung des Verdichters 27 mit dessen Gehäuse 52 an das Motorengehäuse 21 des Radialgebläses 11 erfolgt ohne die Verwendung einer Labyrinthdichtung oder dergleichen. Die Zuführung des unter Druck stehenden Kühlmediums über den Kanal 41 wird dafür eingesetzt, einen Eintritt von Partikeln in das Axialgaslager 31 zu verhindern. Das Axialgaslager 31 selbst verfügt über einen so schmalen Spalt zwischen den Lagerflächen 35 des Stators 34 und den Lagerflächen 36 der rotierenden Scheibe 32, dass durch das Axialgaslager 31 selbst eine Abdichtung zwischen einem Rotorraum 46 im Gehäuse 21 und einem Gasraum 49 im Verdichter 27 gebildet wird. Der Rotorraum 46 ist in radialer Richtung gesehen zwischen einer Durchgangsbohrung 47 im Motorengehäuse 21 und der darin gelagerten Welle 17 gebildet. Der Gasraum 49 ist zwischen einem Gehäuseabschnitt 51 des Motorengehäuses 21 beziehungsweise Gehäuse 52 des Verdichters 27 und dem Laufrad 16 gebildet. Bevorzugt umgreift ein Gehäuse 52 des Verdichters 27 den Gehäuseabschnitt 51 und ist außerhalb dieses Gehäuseabschnitts 51 fest mit dem Motorengehäuse 21 verbunden.In figure 2 a schematically enlarged view of the axial gas bearing 31 and a connection of the compressor 27 to the motor housing 21 of the radial fan 11 is shown. The compressor 27 with its housing 52 is connected to the motor housing 21 of the radial fan 11 without using a labyrinth seal or the like. The supply of the pressurized cooling medium via the channel 41 is used to prevent particles from entering the axial gas bearing 31 . The axial gas bearing 31 itself has such a narrow gap between the bearing surfaces 35 of the stator 34 and the bearing surfaces 36 of the rotating disk 32 that the axial gas bearing 31 itself forms a seal between a rotor chamber 46 in the housing 21 and a gas chamber 49 in the compressor 27 . Seen in the radial direction, the rotor space 46 is formed between a through bore 47 in the motor housing 21 and the shaft 17 mounted therein. The gas space 49 is formed between a housing section 51 of the motor housing 21 or housing 52 of the compressor 27 and the impeller 16 . A housing 52 of the compressor 27 preferably encompasses the housing section 51 and is firmly connected to the motor housing 21 outside of this housing section 51 .

An dem Motorengehäuse 21 ist ein Druckanschluss 54 für das unter Druck stehende Kühlmedium vorgesehen, welches dem Kanal 41 zugeführt wird. In einem Bereich, in dem der Rotorraum 46 und der Gasraum 49 aneinandergrenzen, strömt das Kühlmedium hauptsächlich in Richtung des Gasraumes 49, in der Gegenrichtung wird der Gasstrom durch das Axiallager 31 abgehalten, welches den Rotorraum 46 abdichtet.A pressure connection 54 for the pressurized cooling medium, which is supplied to the channel 41 , is provided on the motor housing 21 . In an area in which the rotor space 46 and the gas space 49 adjoin one another, the cooling medium flows mainly in the direction of the gas space 49;

Durch diese Anordnung kann somit eine Abdichtung zwischen einer Druckseite des Verdichters 27 und dem Motorengehäuse 21 erfolgen. Der Verdichter 27 ist bevorzugt als ein mehrstufiger Verdichter oder Turboverdichter ausgebildet. Eine erste Stufe bildet das Laufrad 26, und die zweite Stufe bildet das Laufrad 16. Insbesondere kann die Abdichtung zwischen der Druckseite der zweiten Stufe beziehungsweise des Laufrades 16 des Verdichters 27 und dem Motorengehäuse 21 des Radialgebläses 11 erfolgen. Im Motorengehäuse kann so ein niedrigerer Druck als an der Druckseite des Verdichters 27 eingestellt werden, wodurch eine Kondensation des Kühlmediums in den Radiallagern 22, 23 verhindert wird. Des Weiteren kann bevorzugt der Druckanschluss 54 ein Filterelement aufweisen. Dieses dient dazu, dass keine Partikel in den Verdichter 27 und/oder das Axialgaslager 31 gelangen.A seal between a pressure side of the compressor 27 and the motor housing 21 can thus be achieved by this arrangement. The compressor 27 is preferably designed as a multi-stage compressor or turbo compressor. A first stage forms the impeller 26, and the second stage forms the impeller 16. In particular, the seal between the pressure side of the second stage or the impeller 16 of the compressor 27 and the motor housing 21 of the Radial fan 11 done. In this way, a lower pressure can be set in the motor housing than on the pressure side of the compressor 27, as a result of which condensation of the cooling medium in the radial bearings 22, 23 is prevented. Furthermore, the pressure connection 54 can preferably have a filter element. This serves to ensure that no particles get into the compressor 27 and/or the axial gas bearing 31 .

Dieses Radialgebläse 11 kann des Weiteren im Bereich des Axialgaslagers 31 oder an einen Axialstator 34 angrenzend oder zwischen den beiden Axialstatoren 34 eine Heizeinrichtung 56 aufweisen. Eine solche Heizeinrichtung 56 dient der Erwärmung des Axialgaslagers 31 auf eine Temperatur, die über dem Taupunkt des Kühlmediums bei einem anliegenden Druck liegt. Dadurch kann eine Kondensation des Kühlmediums verhindert werden. Eine solche Heizeinrichtung 56 kann als eine elektrisch angetriebene Heizung, wie beispielsweise durch ein Widerstands-Heizelement oder ein PTC-Element, ausgebildet sein.This radial fan 11 can also have a heating device 56 in the area of the axial gas bearing 31 or adjacent to an axial stator 34 or between the two axial stators 34 . Such a heating device 56 serves to heat the axial gas bearing 31 to a temperature which is above the dew point of the cooling medium when the pressure is applied. This can prevent condensation of the cooling medium. Such a heating device 56 can be designed as an electrically driven heater, such as by a resistance heating element or a PTC element.

Zwischen dem Motor 20 und dem unteren Radialgaslager 22 ist bevorzugt ein Vibrometer 61 vorgesehen, welches der Welle 17 zugeordnet ist. Bei diesem Vibrometer 61 handelt es sich um ein Messgerät zur Quantifizierung von mechanischen Schwingungen. Ein solches Vibrometer 61 kann zur Messung von Schwingungsfrequenz und Schwingungsamplitude verwendet werden. Beispielsweise kann ein sogenanntes Laser-Doppler-Vibrometer eingesetzt werden. Dieses Vibrometer 61 ist in eine Gehäuseöffnung 62 des Motorengehäuses 21 eingesetzt und vorzugsweise druckdicht angeordnet. Dies kann beispielsweise mittels einer O-Ringdichtung 63 erfolgen. Dadurch kann der Druck im Rotorraum 46 für den hydrodynamischen Betrieb des Radial- und Axialgaslagers 22, 23, 31 aufrechterhalten bleiben. Eine Messfläche des Vibrometers 61 ist tangential zur Umfangsfläche der Welle 17 ausgerichtet. Dabei kann die Messfläche vorteilhaft auch auf einer ein Radialgaslager 22, 23 umgebenden Lagerhülse liegen. Während des Betriebs des Radialgebläses 11 können durch das Vibrometer 61 permanent die Frequenz und die Amplitude erfasst und an eine Steuerung 71 des Radialgebläses oder der Kälteanlage weitergegeben werden. Dadurch kann der aktuelle Betriebspunkt beziehungsweise die während der Kühlung herrschenden Betriebspunkte des Radialgebläses 11 ermittelt werden. Zudem kann gleichzeitig ein Vergleich mit einem Grenzwert vorgenommen werden. Ein solcher Grenzwert kann ein kritischer Betriebszustand sein, bei dem mit einer Schädigung des oder der Lager oder weiteren Komponenten des Radialgebläses zu rechnen ist. Insbesondere dahingehend, dass ein Blockieren der Welle 17 im Motorengehäuse 21 oder der Laufräder 16, 26 im Verdichter 27 gegeben ist.A vibrometer 61 , which is assigned to the shaft 17 , is preferably provided between the motor 20 and the lower radial gas bearing 22 . This vibrometer 61 is a measuring device for quantifying mechanical vibrations. Such a vibrometer 61 can be used to measure vibration frequency and vibration amplitude. For example, a so-called laser Doppler vibrometer can be used. This vibrometer 61 is inserted into a housing opening 62 of the motor housing 21 and is preferably arranged in a pressure-tight manner. This can be done by means of an O-ring seal 63, for example. As a result, the pressure in the rotor space 46 for the hydrodynamic operation of the radial and axial gas bearings 22, 23, 31 can be maintained. A measuring surface of the vibrometer 61 is aligned tangentially to the peripheral surface of the shaft 17 . In this case, the measuring surface can advantageously also lie on a bearing sleeve surrounding a radial gas bearing 22 , 23 . During the operation of the radial fan 11, the frequency and the amplitude can be continuously detected by the vibrometer 61 and passed on to a controller 71 of the radial fan or the refrigeration system. As a result, the current operating point or the operating points of the radial fan 11 prevailing during the cooling can be determined. In addition, a comparison with a limit value can be carried out at the same time. Such a limit value can be a critical operating state in which damage to the bearing or bearings or other components of the radial fan is to be expected. In particular to the effect that the shaft 17 in the motor housing 21 or the impellers 16, 26 in the compressor 27 are blocked.

Alternativ kann ergänzend zwischen dem Motor 20 und dem oberen Radialgaslager 23 ebenfalls ein Vibrometer 61 vorgesehen sein.Alternatively, a vibrometer 61 can also be provided between the motor 20 and the upper radial gas bearing 23 .

Für eine zusätzliche Überwachung von Betriebszuständen des Radialgebläses 11 kann ein weiteres Vibrometer 64 vorgesehen sein, das in der Rotationsachse der Welle 17 positioniert ist und bezüglich einer Messfläche auf ein stirnseitiges Ende der Welle 17 weist. Auch dadurch können Exzentrizitäten bei dem rotierenden Antrieb der Welle 17 erfassend ausgewertet werden.A further vibrometer 64 can be provided for additional monitoring of operating states of the radial fan 11, which is positioned in the axis of rotation of the shaft 17 and points to a front end of the shaft 17 with respect to a measuring surface. This also allows eccentricities in the rotating drive of the shaft 17 to be evaluated.

Dieses zusätzliche Vibrometer 64 ist in Analogie zum Vibrometer 61 wiederum mediendicht in einem Gehäusedeckel 65 positioniert.This additional vibrometer 64 is again positioned in a media-tight manner in a housing cover 65 in analogy to the vibrometer 61 .

In Figur 3 ist eine schematische Ansicht einer Kälteanlage 1 dargestellt. Diese Kälteanlage 1 ist nur beispielhaft und arbeitet insbesondere nach dem Prinzip der Verdunstungskälte. In einem Verdampfer 66 befindet sich ein Kältemittel. Die notwendige Energie beziehungsweise Wärme zum Verdampfen des Kältemittels wird aus der Umgebung entzogen. Das Kältemittel nimmt diese Energie auf und geht in einen gasförmigen Zustand über. Über eine Leitung 67 wird das Kältemittel im gasförmigen Zustand einem oder gemäß dem Ausführungsbeispiel mehreren Radialgebläsen 11 zugeführt, welche jeweils einen Verdichter 27 aufweisen. Das Kältemittel wird auf einen hohen Druck und eine hohe Temperatur, die jeweils höher als der Eingangsdruck und die Eingangstemperatur vor dem Verdichter 11 ist, verdichtet. Darauffolgend wird das Kältemittel einem Verflüssiger beziehungsweise einem Kondensator 68 zugeführt. In diesem Verflüssiger wird das Kältemittel durch Abkühlung verflüssigt. Darauffolgend wird das Kältemittel mit hohem Druck durch ein Drosselorgan, insbesondere ein Expansionsventil 69, geleitet. Das Kältemittel expandiert beziehungsweise wird auf Niederdruck übergeführt und kann in flüssigem Zustand dem Verdampfer 66 zugeführt werden, um aus der Umgebung wiederum die Wärme zu entziehen. Es handelt sich bei der Kälteanlage 1 um einen geschlossenen Kältekreislauf.In figure 3 a schematic view of a refrigeration system 1 is shown. This refrigeration system 1 is only an example and works in particular according to the principle of evaporative cooling. A refrigerant is located in an evaporator 66 . The energy or heat required to evaporate the refrigerant is extracted from the environment. The refrigerant absorbs this energy and turns into a gaseous state. The refrigerant in the gaseous state is fed via a line 67 to one or, according to the exemplary embodiment, to a plurality of radial fans 11 which each have a compressor 27 . The refrigerant is compressed to a high pressure and high temperature, which is higher than the inlet pressure and the inlet temperature before the compressor 11, respectively. The refrigerant is then fed to a liquefier or a condenser 68 . In this condenser, the refrigerant liquefied by cooling. The refrigerant is then passed through a throttle element, in particular an expansion valve 69, at high pressure. The refrigerant expands or is converted to low pressure and can be supplied to the evaporator 66 in the liquid state in order in turn to extract the heat from the environment. The refrigeration system 1 is a closed refrigeration circuit.

Zur Ansteuerung der einzelnen Radialgebläse 11 ist eine Steuerung 71 der Kälteanlage 1 vorgesehen, durch welche die einzelnen Radialgebläse 11 ansteuerbar sind. Bevorzugt sind die Radialgebläse 11 jeweils durch ein Bussystem 72 mit der Steuerung 71 verbunden. Die Verdichtersteuerung beziehungsweise eine Radialgebläsesteuerung arbeitet bevorzugt nach dem Master-Slave-Prinzip. Einem der Radialgebläse 11 wird die Masterfunktion zugeordnet. Die weiteren Radialgebläse 11 werden als sogenannte Slave im Verbund betrieben. Die Steuerung 71 erfasst von dem Master die Messwerte der Sensoren des Radialgebläses. Ausgehend von diesen erfassten beziehungsweise vorhandenen Messwerten werden die weiteren Radialgebläse jeweils zugeschalten, sodass der Verbund der Radialgebläse 11 in einem geregelten Energieminimum betrieben wird. Dabei bleibt eine Schutzfunktion eines jeden einzelnen Radialgebläses 11 beibehalten.To control the individual radial fans 11, a controller 71 of the refrigeration system 1 is provided, by means of which the individual radial fans 11 can be controlled. The radial fans 11 are preferably each connected to the controller 71 by a bus system 72 . The compressor control or a radial fan control preferably works according to the master-slave principle. The master function is assigned to one of the radial fans 11 . The other radial fans 11 are operated as so-called slaves in the network. The controller 71 acquires the measured values of the sensors of the radial fan from the master. On the basis of these recorded or existing measured values, the further radial fans are switched on in each case, so that the network of radial fans 11 is operated at a regulated energy minimum. A protective function of each individual radial fan 11 is retained.

Um einen sicheren Betriebsbereich der Radialgebläse 11 in der Kälteanlage 1 zu erzielen, werden steuer- und regelungstechnische Algorithmen in der Steuerung 71 für die Ansteuerung der Radialgebläse 11 derart eingesetzt, dass für das jeweilige Radialgebläse 11 kein kritischer Betriebspunkt entstehen kann. Des Weiteren können die Radialgebläse 11 über das Bussystem 72 auch miteinander kommunizieren, um selbständig die Kontrolle zur Erreichung eines Energieeffizienzmaximums auf Basis der im Radialgebläse 11 selbst vorhandenen Messwerte, insbesondere auf Basis der im Master-Radialgebläse 11 vorhandenen Messwerte, zu erzielen.In order to achieve a safe operating range for the radial fan 11 in the refrigeration system 1, control and regulation algorithms are used in the controller 71 for controlling the radial fan 11 in such a way that no critical operating point can arise for the respective radial fan 11. Furthermore, the radial fans 11 can also communicate with one another via the bus system 72 in order to independently control the achievement of an energy efficiency maximum based on the measured values present in the radial fan 11 itself, in particular based on the measured values present in the master radial fan 11.

Claims (9)

  1. A method for controlling at least one radial fan (11) in a cooling system (1), in which the radial fan (11) comprises a housing (21) in which a shaft (17) is rotatably mounted which, on one end, receives at least one impeller (16, 26) of a compressor (27), which is fixed on the housing (21), and the housing (21) comprises at least one radial bearing (22, 23) and at least one axial gas bearing (31), by means of which the shaft (17) is rotatably mounted in the housing (21), and an engine (20) driven by a rotor (18) and stator (19), said engine driving the shaft (17), characterized in, that a vibrometer (61) is aligned radially to the shaft (17) and a further vibrometer (64) is allocated to an end-face of the shaft (17) and positioned in the rotational axis of the shaft (17) and that operating points of the shaft (17) are detected by the vibrometers (61, 64), which are allocated to the shaft (17), and are forwarded on to a controller (71) for ascertaining an operating state of the radial fan (11).
  2. The method of claim 1, characterized in, that a critical threshold value is recognised by the controller (71) of the radial fan (11), and exceeding the threshold values is prevented by the controller (71) of the radial fan (11) itself or alternatively by the controller (71) of a cooling system.
  3. The method of claim 1 or 2, characterized in, that the operating points are detected by several radial fans (11) provided in the cooling system by means of the respective at least one vibrometer (61, 64), and the respective operating points are compared to one another and set to the maximum energy efficiency of the respective radial fan (11).
  4. The method of any one of the preceding claims, characterized in, that several radial fans (11) are connected to one another in the cooling system with a network of data lines of a bus system for exchanging data.
  5. The method of any one of claim 3 or 4, characterized in, that one of the radial fans (11) is operated as a master and the further radial fans (11) as slaves.
  6. The method of any one of the preceding claims, characterized in, that the signals detected by the vibrometer (61, 64) are permanently evaluated, and the respective radial fan (11) is constantly monitored.
  7. A radial fan for a cooling system (1), comprising:
    - a housing (21) in which a shaft (17) is rotatably mounted which, on one end, receives at least one impeller (16, 26) of a compressor (27), which is fixed on the housing (21),
    - at least one radial bearing (22, 23) and having at least one axial gas bearing (31) by means of which the shaft (17) is rotatably mounted in the housing (21),
    - an engine (20) driven by a rotor (18) and a stator (19), said engine driving the shaft (17),
    - at least one vibrometer (61, 64) which is allocated to the shaft (17), characterized in,
    - that the at least one vibrometer (61) is aligned radially to the shaft (17),
    - that a further vibrometer (64) is allocated to the shaft (17) to an end-face of the shaft (17) and positioned in the rotational axis of the shaft (17).
  8. The radial fan of claim 7, characterized in, that the at least one vibrometer (61) is allocated to the shaft (17) between the rotor (18) of the engine (20) and the radial bearing (22, 23) or axial gas bearing (31) arranged adjacently thereto.
  9. The radial fan according to claim 7 or 8, wherein the at least one vibrometer (61, 64) is positioned in a housing opening (62) of the housing (21) and is provided in the housing opening (62) in a pressure medium-tight manner.
EP19716110.2A 2018-04-13 2019-04-02 Method for controlling at least one radial blower in a cooling system, and radial blower Active EP3775567B1 (en)

Applications Claiming Priority (2)

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DE102018108827.2A DE102018108827B3 (en) 2018-04-13 2018-04-13 Method for controlling at least one radial fan in a refrigeration system and radial fan
PCT/EP2019/058236 WO2019197209A1 (en) 2018-04-13 2019-04-02 Method for controlling at least one radial blower in a cooling system, and radial blower

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EP3775567B1 true EP3775567B1 (en) 2023-03-22

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EP (1) EP3775567B1 (en)
CN (1) CN111954762B (en)
CA (1) CA3096809A1 (en)
DE (1) DE102018108827B3 (en)
DK (1) DK3775567T3 (en)
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WO (1) WO2019197209A1 (en)

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DE102022204869A1 (en) * 2022-05-17 2023-11-23 Robert Bosch Gesellschaft mit beschränkter Haftung Method for operating an electrically driven compressor, control device

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TW201943966A (en) 2019-11-16
EP3775567A1 (en) 2021-02-17
DK3775567T3 (en) 2023-05-30
CA3096809A1 (en) 2019-10-17
CN111954762A (en) 2020-11-17
DE102018108827B3 (en) 2019-05-29
US20220307511A1 (en) 2022-09-29
CN111954762B (en) 2022-08-02
WO2019197209A1 (en) 2019-10-17
TWI801555B (en) 2023-05-11

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