EP2142806B1 - Compressor system for underwater use in the offshore area - Google Patents

Compressor system for underwater use in the offshore area Download PDF

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Publication number
EP2142806B1
EP2142806B1 EP08759450.3A EP08759450A EP2142806B1 EP 2142806 B1 EP2142806 B1 EP 2142806B1 EP 08759450 A EP08759450 A EP 08759450A EP 2142806 B1 EP2142806 B1 EP 2142806B1
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EP
European Patent Office
Prior art keywords
housing
compressor system
cooling
compressor
electric motor
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
EP08759450.3A
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German (de)
French (fr)
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EP2142806A1 (en
Inventor
Maria Bade
Joachim Mucha
Axel MÖHLE
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Siemens AG
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Siemens AG
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Publication of EP2142806A1 publication Critical patent/EP2142806A1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08Centrifugal pumps
    • F04D17/10Centrifugal pumps for compressing or evacuating
    • F04D17/12Multi-stage pumps
    • F04D17/122Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/06Units comprising pumps and their driving means the pump being electrically driven
    • F04D25/0686Units comprising pumps and their driving means the pump being electrically driven specially adapted for submerged use
    • 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
    • F04D29/58Cooling; Heating; Diminishing heat transfer
    • F04D29/5806Cooling the drive system
    • 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
    • F04D29/58Cooling; Heating; Diminishing heat transfer
    • F04D29/582Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
    • F04D29/5826Cooling at least part of the working fluid in a heat exchanger
    • 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
    • F04D29/58Cooling; Heating; Diminishing heat transfer
    • F04D29/586Cooling; Heating; Diminishing heat transfer specially adapted for liquid pumps
    • F04D29/588Cooling; Heating; Diminishing heat transfer specially adapted for liquid pumps cooling or heating the machine

Definitions

  • the invention relates to a compressor system, in particular for the promotion of gases or gas / oil mixtures in the offshore sector.
  • the compressor system has a seawater-resistant housing with at least one access opening for gases or gas / oil mixtures to be compressed and with at least one outlet opening for the compressed gases or gas / oil mixtures. It has a compressor arranged in the housing, which is connected on the input side to the access opening and on the output side to the output opening.
  • an electric motor is arranged with a stator core which can be cooled via an inner side of the housing and with a rotor core for driving the compressor.
  • German patent DE 37 29 486 C1 is a compressor unit for the production of natural gas in the offshore area with drive by a high-frequency motor for the compression of gases is known, which is suitable for large water depths.
  • the high-frequency motor of the compressor unit is magnetically mounted and drives the compressor stages in a common gas-tight housing. The cooling of the engine, the bearings and the compressor stages takes place through the liquid surrounding the common housing.
  • German patent application DE 42 09 118 A1 is an electric motor with a motor pressure housing, filled with gas. under high pressure, known.
  • a capsule is provided which surrounds the rotor rods on the drive side and / or side.
  • a compressor which has a compressor unit and an electric motor driving the same via a common shaft.
  • the shaft is mounted on a liquid cooled axle.
  • the compressor systems can be driven by an electric motor or by a gas turbine.
  • the electric motor is preferably a brushless asynchronous motor.
  • a high-speed turbine is used for compression, in which case the turbine and the electric motor are preferably arranged on a common shaft.
  • the brush and gearless drive allows virtually maintenance-free operation of such compressor systems.
  • screw or reciprocating compressors can be used for compression.
  • the considered compressor systems may be installed in coastal petrochemical facilities, on drilling platforms or under water. In the latter case, the drive of the compressor is typically carried out with an electric motor.
  • the supply of the gas or the gas / oil mixture is usually via a pipe which is flanged to the outside of the housing of the compressor system. In a corresponding manner, the further transport of the compressed gas or gas / oil mixture takes place on the output side via another Pipeline.
  • a pressure hose can be used instead of a pipe.
  • the high electrical connection capacity of the electric motors used in the range of several 100 kW requires cooling of the electric motors.
  • an oil recooling system is used, which is connected as a separate unit via oil supply lines and oil return lines to the compressor system.
  • Such compressor systems are disadvantageously expansive because of the externally arranged oil recooling.
  • Another disadvantage is that the external oil recooling systems may leak over time.
  • the oil feed pipes and the oil return pipes themselves may become leaky, in particular due to corrosion caused by sea water or due to mechanical effects, such as corrosion. by waves.
  • pressure-tight connection connections of the pipelines to the housing of the compressor system can become leaky over time. Escaping oil and oil / gas mixtures in this context represents a potential ecological hazard to the surrounding waters.
  • the stator core is spaced from the inside of the housing.
  • the stator in this case forms with at least one opposite part of the inside of the housing an annular cooling chamber.
  • a coolant is present in the cooling chamber.
  • the coolant is a liquid, especially an oil, e.g. a silicone or mineral oil. In addition to the high specific heat capacity, this has an advantageous electrically insulating effect with regard to the live winding ends.
  • other cooling liquids may be used, such as e.g. Water based coolants.
  • the coolant may alternatively be a refrigerant, such as e.g. Freon® R134a.
  • the coolant is a sol, that is, a liquid / gas mixture.
  • cooling passages extending essentially axially to the axis of rotation of the electric motor are provided in the stator core.
  • the compressor system comprises a circulation pump for the coolant.
  • the compressor system for the intended use is installed such that the axis of rotation of the electric motor is substantially in the vertical direction.
  • the present arrangement causes automatically adjusts a cooling circuit within the cooling chamber. Because the heating of the coolant in the respective cooling channels causes it to rise and flow out of the upper axial face of the stator core. Subsequent coolant forcibly conveys the heated coolant to the inside of the housing that is cold compared to the coolant temperature. The subsequent cooling causes an increase in specific gravity and a decrease in the coolant. At the lower end of the cooling chamber, the cooled coolant is sucked in the direction of the axially lower end face of the stator core. The cooling circuit is closed.
  • the cold outside of the outside of the housing which has typical temperatures in the single-digit Celsius range, acts as a heat sink.
  • the large temperature gradient between heated coolant and cold seawater causes a large heat flow from the coolant through the housing wall to the seawater.
  • baffles For the purpose of directing the circulating liquid flow forming in the cooling chamber, baffles, e.g. be arranged at the axial ends of the stator.
  • the housing has an outer housing side, on which a plurality of cooling fins is arranged.
  • the cooling fins cause a significant increase in the cooling surface to the sea water.
  • the enlarged cooling surface may, depending on the shape and number of existing cooling fins, be a multiple of the otherwise existing outer surface of the housing of the compressor system.
  • the cooling fins are away from the outside of the housing.
  • the housing has a cylindrical shape.
  • the heat sinks are radially away from the outside of the housing.
  • With “radial" directions are referred to the axis of symmetry of the cylindrical housing to and away from her.
  • the axis of symmetry coincides with the axis of rotation of the electric motor.
  • FIG. 1 shows a sectional view of a non-inventive compressor system 1 along the axis of rotation DA of an electric motor 7 and a compressor eighth
  • a housing 2 is seawater resistant.
  • the housing 2 is preferably made of steel and may have a protective coating to prevent corrosion.
  • the steel used may alternatively or additionally be a stainless steel.
  • the housing 2 may be made of a seawater resistant aluminum.
  • the housing is pressure-tight, in accordance with the intended for operation of the compressor system 1 depth of use under the sea water level or on the seabed.
  • the pressure-tight requirements relate not only to the housing 2 itself, but also implementations in the housing, such as for power and control cables for power supply and for controlling and / or monitoring of the compressor system. 1
  • the housing 2 has, for example, an access opening 3 for the gases or gas / oil mixtures to be compressed and an outlet opening 4 for the compressed gases or gas / oil mixtures.
  • a plurality of openings 3, 4 may be present.
  • At the two openings 3, 4 are usually connecting elements, such as couplings or flanges, mounted in order to connect to these pipes or pressure hoses.
  • the connection elements and the pipes are to be designed in a technically robust manner with regard to the respectively required pressure tightness.
  • the compressor 8 is arranged, which is the input side connected to the access opening 3 and the output side to the output port 4.
  • the arrows shown in the region of the openings 3, 4 indicate the flow directions.
  • the compressor 8 has a turbine 81 with turbine blades not further specified. Their diameter decreases in the axial direction, that is, in the flow direction, whereby the pressure increases due to the compression at the same time.
  • the reference numeral 83 denotes a high-pressure discharge. From there, via a pipe connection, not further described, inside the housing 2, the transport of the compressed gas to the exit opening 3 takes place.
  • the electric motor 7 is further arranged for driving the compressor 8.
  • the electric motor 7 has a stator 71 and a rotor package 72. Furthermore, in the example of the FIG. 1 both the compressor 8 and the electric motor 7 on a common, guided in bearings 6 shaft 5.
  • the stator 71 of the electric motor 7 is cooled via a housing inner side GI of the housing 2 of the compressor system 1.
  • cooling takes place via a stator outer side SA, which rests flush against the inside of the housing GI.
  • the arrows entered in the contact area between the outside of the stator SA and the inside of the housing GI symbolize the heat flow.
  • a good thermal conductivity mass such as a good thermal conductivity paste, a grease or the like.
  • the compressor system 1 shown is installed such that the axis of rotation DA of the electric motor 7 extends substantially in the vertical direction. It can alternatively be aligned in a horizontal position.
  • the housing 2 has a housing outside GA, on which a plurality of projecting cooling fins 21 is arranged.
  • the cooling fins 21 are radially away from the housing outside GA.
  • the compressor system 1 according to the invention and an embodiment according to FIG. 2 and FIG. 3 have such a cylindrical design.
  • FIG. 2 shows a sectional view of a compressor system according to the invention 1.
  • the compressor system 1 shown is in turn mounted vertically with respect to the axis of rotation DA of the electric motor 7.
  • stator 71 In contrast to the compressor system according to FIG. 1 is the stator 71 according to the invention from the inside GI of the housing 2 spaced.
  • the mean radial distance is preferably in a range of 5 cm to 15 cm. Depending on the electrical connection performance of the electric motor 7, the distance values can also be above, for example, at 20 cm, or below, such as at 3 cm.
  • the stator 71 forms with at least one opposite part of the housing inner side GI an annular cooling chamber 9, in which a coolant 9 is present.
  • the cooling chamber 9 In the cooling chamber 9 are also the winding heads 73 of the stator 71, which protrude axially from the stator 71.
  • the cooling chamber 9 has in the example of FIG. 2 only one chamber up. It may alternatively have a plurality of chambers, in which case adjacent chambers are separated from each other by a radially axially extending bulkhead.
  • the cooling chamber 9 is formed by two ripeness 91, 92 and a circular disk 94.
  • the two ripen 91, 92 have an inner diameter which corresponds to the inner diameter of the stator 71.
  • the first hoop 91 is sealed to a lower axial end face of the stator pack 71, such as e.g. welded.
  • the axis of symmetry of this hoop 91 is aligned with the axis of rotation DA of the electric motor 7.
  • the axial height of the first hoop 91 corresponds to almost the axial distance of the stator 71 to a bottom plate 22 of the housing 2.
  • the lower edge of the first hoop 91 can via a sealing ring 93 for Bottom plate 22 to be sealed towards sealed or welded to the bottom plate 22.
  • the second hoop 92 is similarly attached to the upper axial end of the stator core 71.
  • the circular disk 94 has an inner diameter which corresponds approximately to the inner diameter of the maturity 91, 92.
  • the outer diameter corresponds approximately to the inner diameter of the housing 2.
  • the second hoop 92 and the circular disk 94 are preferably welded together tightly and together form a flange 92, 94.
  • the outer edge of the circular disk 94 and the flange 92, 94 can via another Gasket 95 may be sealed to the inside of the housing GI or tightly welded to the inside of the housing GI.
  • the maturity 91, 92, the circular disk 94, a radial inner side of the stator core 71 and the inside of the housing GI thus form a hollow cylinder.
  • a coolant preferably an oil
  • a so-called transformer oil based on mineral oil or silicone oil comes into consideration.
  • the entire cooling chamber 9 is filled with the cooling liquid.
  • a compensating vessel for the cooling liquid may be present to compensate for a temperature-induced change in volume of the coolant.
  • the coolant may alternatively be a refrigerant, such as a Freon®. It is particularly advantageous in terms environmental compatibility a CFC-free Freon®, such as Freon® R134a.
  • the cooling chamber 9 is filled with a sol, that is, with a liquid / gas mixture.
  • cooling passages 75 extending essentially axially to the axis of rotation DA of the electric motor 7 are present in the stator pack 71. Because of the embedding of the stator 71 in the coolant, these are also filled with the coolant.
  • a circulation of the coolant in the cooling chamber 9 is established. This is represented by flow arrows.
  • the coolant heated in the cooling channels 75 rises upward and cools in the reverse direction from top to bottom along the cold inside of the housing GI again.
  • the thermally particularly critical winding heads 73 are surrounded by the circulating coolant and thus effectively cooled.
  • the horizontal arrows symbolize the heat transfer from the coolant, continue on the wall of the housing 2 in the sea water, which surrounds the outside of the housing GA 2.
  • the adjusting in the cooling chamber 9 cooling circuit can also be referred to as a primary cooling circuit, while adjusts to the outside of the housing, but only in the case of a stationary water, a counterflow, which sweeps from bottom to top along the outside of the housing GA.
  • the cooling by the seawater can also be called secondary cooling.
  • the compressor system 1 may comprise a circulation pump for the coolant.
  • the circulating pump is e.g. a centrifugal pump which is mounted in or on the cooling chamber 9.
  • cooling fins 21 are formed on the outside of the housing 2 GA shorter in length. They extend only in the axial "hot" region of the housing 2, which is opposite to the cooling chamber 9.
  • the cooling of the compressor 8 takes place in this context on the gases to be compressed or gas / oil mixtures themselves.
  • FIG. 3 shows a sectional view of a compressor system 1 according to a third embodiment of the invention.
  • the cooling chamber 9 is substantially torus-shaped, wherein the cooling chamber 9 curved cooling chamber walls 96, 97 which favor the circulating flow through their shape.
  • the cooling capacity of this embodiment is therefore larger in comparison to the second embodiment with the same construction volume.
  • the cooling chamber walls 96, 97 fulfill in addition to the formation of the cooling chamber 9 and a Strömungsleitfunktion.
  • Reference numerals 98, 99 denote further sealing rings for sealing the cooling chamber walls 96, 97 with the inside of the housing GI.
  • the cooling chamber walls 96, 97 may be tightly welded to the inside of the housing GI.
  • FIG. 4 shows a side view of the compressor system 1 according to FIG. 3 according to the in FIG. 3 marked line of vision IV.
  • FIG. 4 shows the view into the access opening 3, that is in the direction of the compressor.
  • the stator 71 has a plurality of circumferentially uniformly distributed cooling channels 75 on.
  • the cooling channels 75 are arranged with respect to their radial position to the winding heads 73 on both sides of the winding heads 73 (see also FIG. 2 and FIG. 3 ).
  • the arrangement of the cooling channels 75 is preferably carried out in the magnetically less active region of the stator 71.
  • the plurality of cooling channels 75 allows effective cooling of the stator 71 from the inside out.
  • cooling fins 21 On the outer side of the housing GA there is a large number of cooling fins 21 arranged radially away from the outside of the housing to see.
  • the cooling fins 21 cause a drastic increase in the cooling surface available for cooling by seawater.
  • the cooling fins 21 are an integral part of the housing 2 of the compressor system 1.
  • the housing 2 is made of a casting.
  • the compressor system according to the invention is also suitable for high-speed compressor systems at speeds of up to 15,000 rpm and powers of a few 100 kW up to 10 MW and more.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Motor Or Generator Cooling System (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)

Description

Die Erfindung betrifft ein Verdichtersystem, insbesondere zur Förderung von Gasen oder Gas-/Ölgemischen im Offshore-Bereich. Das Verdichtersystem weist ein seewasserfestes Gehäuse mit zumindest einer Zugangsöffnung für zu verdichtende Gase oder Gas-/Ölgemische und mit zumindest einer Ausgangsöffnung für die verdichteten Gase oder Gas-/Ölgemische auf. Es weist einen im Gehäuse angeordneten Verdichter auf, welcher eingangsseitig mit der Zugangsöffnung und ausgangsseitig mit der Ausgangsöffnung verbunden ist. Im Gehäuse ist ein Elektromotor mit einem über eine Innenseite des Gehäuses kühlbaren Statorpaket und mit einem Rotorpaket zum Antreiben des Verdichters angeordnet.The invention relates to a compressor system, in particular for the promotion of gases or gas / oil mixtures in the offshore sector. The compressor system has a seawater-resistant housing with at least one access opening for gases or gas / oil mixtures to be compressed and with at least one outlet opening for the compressed gases or gas / oil mixtures. It has a compressor arranged in the housing, which is connected on the input side to the access opening and on the output side to the output opening. In the housing, an electric motor is arranged with a stator core which can be cooled via an inner side of the housing and with a rotor core for driving the compressor.

Aus dem deutschen Patent DE 37 29 486 C1 ist eine Kompressoreinheit zur Förderung von Erdgas im Offshore-Bereich mit Antrieb durch einen Hochfrequenzmotor zur Verdichtung von Gasen bekannt, die für große Wassertiefen geeignet ist. Der Hochfrequenzmotor der Kompressoreinheit ist magnetisch gelagert und treibt in einem gemeinsamen nach außen gasdichten Gehäuse die Kompressorstufen an. Die Kühlung des Motors, der Lager sowie der Kompressorstufen erfolgt durch die das gemeinsame Gehäuse umgebende Flüssigkeit.From the German patent DE 37 29 486 C1 is a compressor unit for the production of natural gas in the offshore area with drive by a high-frequency motor for the compression of gases is known, which is suitable for large water depths. The high-frequency motor of the compressor unit is magnetically mounted and drives the compressor stages in a common gas-tight housing. The cooling of the engine, the bearings and the compressor stages takes place through the liquid surrounding the common housing.

Aus der deutschen Offenlegungsschrift DE 196 23 553 A1 ist eine flüssigkeitsgekühlte elektrische Maschine bekannt, die als Unterwassermotor in spaltrohrloser Bauweise ausgebildet ist und vollständig mit Motorfüllflüssigkeit niedriger Viskosität gefüllt ist. Zur Optimierung der Wärmeverteilung innerhalb des Stators sind Kühlrohre vorgesehen, die parallel zum Luftspalt zwischen Stator und Rotor verlaufen. Die gesamte für Kühlzwecke verwendete Motorfüllflüssigkeit strömt parallel durch die Kühlrohre und den Luftspalt.From the German patent application DE 196 23 553 A1 is a liquid-cooled electric machine is known which is designed as a submersible motor in spaltrohrloser construction and is completely filled with motor filling liquid of low viscosity. To optimize the heat distribution within the stator cooling tubes are provided which extend parallel to the air gap between the stator and rotor. The entire engine fill fluid used for cooling flows in parallel through the cooling tubes and the air gap.

Aus der deutschen Offenlegungsschrift DE 42 09 118 A1 ist ein Elektromotor mit einem Motor-Druckgehäuse, gefüllt mit Gas . unter hohem Druck, bekannt. Um die in dem Elektromotor anfallende Verlustwärme zu verringern, ist eine Kapsel vorgesehen, die die Rotorstäbe antriebsseitig und/oder nebenseitig umschließt.From the German patent application DE 42 09 118 A1 is an electric motor with a motor pressure housing, filled with gas. under high pressure, known. In order to reduce the heat loss incurred in the electric motor, a capsule is provided which surrounds the rotor rods on the drive side and / or side.

Aus dem französischen Patent FR 1 181 680 A ist ein Kompressor bekannt, der eine Kompressoreinheit und einen diese über eine gemeinsame Welle antreibenden Elektromotor aufweist. Die Welle ist auf einer flüssigkeitsgekühlten Achse gelagert.From the French patent FR 1 181 680 A For example, a compressor is known which has a compressor unit and an electric motor driving the same via a common shaft. The shaft is mounted on a liquid cooled axle.

Die Offshore-Förderung, das heißt die Förderung von Öl und Gas in küstennahen Gewässern, stellt hohe Anforderungen an Verdichtersysteme. Sie müssen rauem Klima, korrodierenden Umweltbedingungen sowie unberechenbaren Gaszusammensetzungen gewachsen sein. Die Verdichtersysteme können mit einem Elektromotor oder mit einer Gasturbine angetrieben werden. Der Elektromotor ist vorzugsweise ein bürstenloser Asynchronmotor. Üblicherweise wird zum Verdichten eine schnelllaufende Turbine verwendet, wobei in diesem Falle die Turbine und der Elektromotor vorzugsweise auf einer gemeinsamen Welle angeordnet sind. Der bürsten- und getriebelose Antrieb erlaubt einen nahezu wartungsfreien Betrieb derartiger Verdichtersysteme. Alternativ können auch Schrauben- oder Kolbenkompressoren zum Verdichten verwendet werden.Offshore production, ie the extraction of oil and gas in offshore waters, places high demands on compressor systems. They have to cope with harsh climates, corrosive environmental conditions and unpredictable gas compositions. The compressor systems can be driven by an electric motor or by a gas turbine. The electric motor is preferably a brushless asynchronous motor. Usually, a high-speed turbine is used for compression, in which case the turbine and the electric motor are preferably arranged on a common shaft. The brush and gearless drive allows virtually maintenance-free operation of such compressor systems. Alternatively, screw or reciprocating compressors can be used for compression.

Die betrachteten Verdichtersysteme können in Einrichtungen der Petrochemie an der Küste, auf Bohrplattformen oder auch unter Wasser installiert sein. Im letzteren Fall erfolgt der Antrieb des Verdichters typischerweise mit einem Elektromotor.The considered compressor systems may be installed in coastal petrochemical facilities, on drilling platforms or under water. In the latter case, the drive of the compressor is typically carried out with an electric motor.

Die Zuführung des Gases bzw. des Gas-/Ölgemisches erfolgt üblicherweise über eine Rohrleitung, welche an der Gehäuseaußenseite des Verdichtersystems angeflanscht ist. In entsprechender Weise erfolgt der Weitertransport des verdichteten Gases bzw. Gas-/Ölgemisches ausgangsseitig über eine weitere Rohrleitung. Alternativ kann anstelle einer Rohrleitung ein Druckschlauch verwendet werden.The supply of the gas or the gas / oil mixture is usually via a pipe which is flanged to the outside of the housing of the compressor system. In a corresponding manner, the further transport of the compressed gas or gas / oil mixture takes place on the output side via another Pipeline. Alternatively, a pressure hose can be used instead of a pipe.

Die hohe elektrische Anschlussleistung der verwendeten Elektromotoren im Bereich von mehreren 100 kW macht eine Kühlung der Elektromotoren erforderlich. Üblicherweise wird eine Ölrückkühlanlage verwendet, welche als separate Einheit über Ölzulaufleitungen und Ölrücklaufleitungen an das Verdichtersystem angeschlossen ist. Derartige Verdichtersysteme sind wegen der außerhalb angeordneten Ölrückkühlanlagen nachteilig raumgreifend.The high electrical connection capacity of the electric motors used in the range of several 100 kW requires cooling of the electric motors. Typically, an oil recooling system is used, which is connected as a separate unit via oil supply lines and oil return lines to the compressor system. Such compressor systems are disadvantageously expansive because of the externally arranged oil recooling.

Ein weiterer Nachteil ist, dass die externen Ölrückkühlanlagen mit der Zeit undicht werden können. Zum einen können die Ölzulaufleitungen und die Ölrücklaufleitungen selbst undicht werden, insbesondere durch eine meerwasserbedingte Korrosion oder durch mechanische Einwirkungen, wie z.B. durch Wellenschlag. Zum anderen können auch druckdicht ausgeführte Anschlussverbindungen der Rohrleitungen am Gehäuse des Verdichtersystems mit der Zeit undicht werden. Austretendes Öl sowie Öl-/Gasgemische stellt in diesem Zusammenhang eine potentielle ökologische Gefahr für die umgebenden Gewässer dar.Another disadvantage is that the external oil recooling systems may leak over time. On the one hand, the oil feed pipes and the oil return pipes themselves may become leaky, in particular due to corrosion caused by sea water or due to mechanical effects, such as corrosion. by waves. On the other hand, pressure-tight connection connections of the pipelines to the housing of the compressor system can become leaky over time. Escaping oil and oil / gas mixtures in this context represents a potential ecological hazard to the surrounding waters.

Es ist eine Aufgabe der Erfindung ein Verdichtersystem anzugeben, bei welchem die zuvor beschriebenen Nachteile vermieden werden.It is an object of the invention to provide a compressor system in which the disadvantages described above are avoided.

Die Aufgabe der Erfindung wird durch ein Verdichtersystem mit den Merkmalen des Anspruchs 1 gelöst. Weitere vorteilhafte Ausführungsformen sind in den abhängigen Ansprüchen 2 bis 6 angegeben.The object of the invention is achieved by a compressor system having the features of claim 1. Further advantageous embodiments are specified in the dependent claims 2 to 6.

Erfindungsgemäß ist das Statorpaket von der Innenseite des Gehäuses beabstandet. Das Statorpaket bildet in diesem Fall mit zumindest einem gegenüberliegenden Teil der Gehäuseinnenseite eine ringförmige Kühlkammer aus. In der Kühlkammer ist ein Kühlmittel vorhanden.According to the invention, the stator core is spaced from the inside of the housing. The stator in this case forms with at least one opposite part of the inside of the housing an annular cooling chamber. In the cooling chamber, a coolant is present.

Damit ist der Vorteil verbunden, dass der Wärmeübergangswiderstand vom Statorpaket zum Gehäuse wegen der vollständigen Einbettung des Statorpakets im Kühlmittel und wegen der Benetzung der Gehäuseinnenseite mit dem Kühlmittel drastisch reduziert wird. Der Grund dafür ist, dass das Statorpaket mit seinen besonders heißen Stellen, wie z.B. mit seinen axial überstehenden Wickelköpfen, komplett im Kühlmittel eingetaucht ist. Die Kühlung dieser heißen und kritischen Stellen ist daher besonders effektiv. Mit "axial" sind Richtungen parallel zur Drehachse des Elektromotors bezeichnet.This has the advantage that the heat transfer resistance from the stator to the housing is drastically reduced because of the complete embedding of the stator in the coolant and because of the wetting of the inside of the housing with the coolant. The reason for this is that the stator pack with its particularly hot spots, such as with its axially projecting winding heads, completely immersed in the coolant. The cooling of these hot and critical points is therefore particularly effective. With "axial" directions are designated parallel to the axis of rotation of the electric motor.

Vorzugsweise ist das Kühlmittel eine Flüssigkeit, insbesondere ein Öl, wie z.B. ein Silikon- oder Mineralöl. Neben der hohen spezifischen Wärmekapazität wirkt dieses in Hinblick auf die spannungsführenden Wickelköpfe vorteilhaft elektrisch isolierend. Alternativ können andere Kühlflüssigkeiten verwendet werden, wie z.B. Kühlflüssigkeiten auf Wasserbasis. Das Kühlmittel kann alternativ ein Kältemittel sein, wie z.B. Freon® R134a. In diesem Fall ist das Kühlmittel ein Sol, das heißt ein Flüssigkeits-/Gasgemisch.Preferably, the coolant is a liquid, especially an oil, e.g. a silicone or mineral oil. In addition to the high specific heat capacity, this has an advantageous electrically insulating effect with regard to the live winding ends. Alternatively, other cooling liquids may be used, such as e.g. Water based coolants. The coolant may alternatively be a refrigerant, such as e.g. Freon® R134a. In this case, the coolant is a sol, that is, a liquid / gas mixture.

Nach einer Ausführungsform sind im Statorpaket im Wesentlichen axial zur Drehachse des Elektromotors verlaufende Kühlkanäle vorhanden. Dadurch ist in vorteilhafter Weise eine Kühlung im Inneren des Statorpakets möglich.According to one embodiment, cooling passages extending essentially axially to the axis of rotation of the electric motor are provided in the stator core. As a result, cooling in the interior of the stator is possible in an advantageous manner.

Einer weiteren Ausführungsform zufolge weist das Verdichtersystem eine Umwälzpumpe für das Kühlmittel auf. Durch die Umwälzung wird eine gleichmäßigere und auch höhere Kühlleistung erzielt.According to another embodiment, the compressor system comprises a circulation pump for the coolant. By the circulation a more even and also higher cooling achievement is achieved.

Nach einer bevorzugten Ausführungsform ist das Verdichtersystem für den bestimmungsgemäßen Einsatz derart installiert, dass die Drehachse des Elektromotors im Wesentlichen in vertikaler Richtung verläuft. Selbiges trifft auf die Kühlkanäle zu. Die vorliegende Anordnung bewirkt, dass sich selbsttätig ein Kühlkreislauf innerhalb der Kühlkammer einstellt. Denn die Erwärmung des Kühlmittels in den jeweiligen Kühlkanälen bewirkt, dass dieses aufsteigt und aus der oberen axialen Stirnseite des Statorpakets herausströmt. Nachströmendes Kühlmittel befördert das erhitzte Kühlmittel zwangläufig zu der im Vergleich zur Kühlmitteltemperatur kalten Gehäuseinnenseite. Die nachfolgende Abkühlung bewirkt eine Erhöhung des spezifischen Gewichts und ein Absinken des Kühlmittels. Am unteren Ende der Kühlkammer angelangt wird das abgekühlte Kühlmittel in Richtung zur axialen unteren Stirnseite des Statorpakets angesaugt. Der Kühlkreislauf ist damit geschlossen. Dabei wirkt das die Gehäuseaußenseite umspülende kalte Meerwasser mit typischen Temperaturen im einstelligen Celsius-Bereich als Wärmesenke. Der große Temperaturgradient zwischen erhitztem Kühlmittel und kaltem Meerwasser bewirkt einen großen Wärmestrom vom Kühlmittel über die Gehäusewandung zum Meerwasser.According to a preferred embodiment, the compressor system for the intended use is installed such that the axis of rotation of the electric motor is substantially in the vertical direction. The same applies to the cooling channels. The present arrangement causes automatically adjusts a cooling circuit within the cooling chamber. Because the heating of the coolant in the respective cooling channels causes it to rise and flow out of the upper axial face of the stator core. Subsequent coolant forcibly conveys the heated coolant to the inside of the housing that is cold compared to the coolant temperature. The subsequent cooling causes an increase in specific gravity and a decrease in the coolant. At the lower end of the cooling chamber, the cooled coolant is sucked in the direction of the axially lower end face of the stator core. The cooling circuit is closed. At the same time, the cold outside of the outside of the housing, which has typical temperatures in the single-digit Celsius range, acts as a heat sink. The large temperature gradient between heated coolant and cold seawater causes a large heat flow from the coolant through the housing wall to the seawater.

Zur gezielten Lenkung der sich in der Kühlkammer ausbildenden zirkulierenden Flüssigkeitsströmüng können auch Leitbleche z.B. an den axialen Enden des Statorpakets angeordnet sein.For the purpose of directing the circulating liquid flow forming in the cooling chamber, baffles, e.g. be arranged at the axial ends of the stator.

Nach einer weiteren vorteilhaften Ausführungsform weist das Gehäuse eine Gehäuseaußenseite auf, an der eine Vielzahl von Kühlrippen angeordnet ist. Die Kühlrippen bewirken eine erhebliche Vergrößerung der Kühlfläche zum Meerwasser hin. Die vergrößerte Kühlfläche kann, je nach Ausformung und Anzahl der vorhandenen Kühlrippen, ein Vielfaches der sonst vorliegenden Außenfläche des Gehäuses des Verdichtersystems sein. Vorzugsweise weisen die Kühlrippen von der Außenseite des Gehäuses weg.According to a further advantageous embodiment, the housing has an outer housing side, on which a plurality of cooling fins is arranged. The cooling fins cause a significant increase in the cooling surface to the sea water. The enlarged cooling surface may, depending on the shape and number of existing cooling fins, be a multiple of the otherwise existing outer surface of the housing of the compressor system. Preferably, the cooling fins are away from the outside of the housing.

Vorzugsweise weist das Gehäuse eine zylindrische Bauform auf. In diesem Fall weisen die Kühlkörper radial von der Gehäuseaußenseite weg. Mit "radial" sind Richtungen auf die Symmetrieachse des zylindrischen Gehäuses zu und von ihr weg bezeichnet. Typischerweise fällt die Symmetrieachse mit der Drehachse des Elektromotors zusammen.Preferably, the housing has a cylindrical shape. In this case, the heat sinks are radially away from the outside of the housing. With "radial" directions are referred to the axis of symmetry of the cylindrical housing to and away from her. Typically, the axis of symmetry coincides with the axis of rotation of the electric motor.

Weitere vorteilhafte Eigenschaften der Erfindung ergeben sich aus deren beispielhafter Erläuterung anhand der Figuren. Es zeigen

FIG 1
eine Schnittdarstellung eines nicht erfindungsgemäßen Verdichtersystems entlang der Drehachse eines Elektromotors und eines Verdichters,
FIG 2
eine Schnittdarstellung eines erfindungsgemäßen Verdichtersystems,
FIG 3
eine Schnittdarstellung eines Verdichtersystems gemäß einer Ausführungsform der Erfindung und
FIG 4
eine Seitenansicht des Verdichtersystems gemäß FIG 3 entsprechend der in FIG 3 eingezeichneten Blickrichtung IV.
Further advantageous features of the invention will become apparent from the exemplification thereof with reference to the figures. Show it
FIG. 1
a sectional view of a non-inventive compressor system along the axis of rotation of an electric motor and a compressor,
FIG. 2
a sectional view of a compressor system according to the invention,
FIG. 3
a sectional view of a compressor system according to an embodiment of the invention and
FIG. 4
a side view of the compressor system according to FIG. 3 according to the in FIG. 3 marked line of vision IV.

FIG 1 zeigt eine Schnittdarstellung eines nicht erfindungsgemäßen Verdichtersystems 1 entlang der Drehachse DA eines Elektromotors 7 und eines Verdichters 8. FIG. 1 shows a sectional view of a non-inventive compressor system 1 along the axis of rotation DA of an electric motor 7 and a compressor eighth

Die in den Figuren FIG 1 bis FIG 3 dargestellten Verdichtersysteme sind insbesondere zur Förderung von Gasen und/oder Gas-/Ölgemischen im Offshore-Bereich ausgebildet. Insbesondere ist ein Gehäuse 2 seewasserfest ausgeführt. Das Gehäuse 2 ist vorzugsweise aus Stahl gefertigt und kann zur Vermeidung von Korrosion einen Schutzanstrich aufweisen. Der verwendete Stahl kann alternativ oder zusätzlich ein nichtrostender Stahl sein. Alternativ kann das Gehäuse 2 aus einem seewasserfesten Aluminium hergestellt sein. Vorzugsweise ist das Gehäuse druckdicht ausgeführt, und zwar entsprechend der zum Betrieb des Verdichtersystems 1 vorgesehenen Einsatztiefe unter dem Meerwasserspiegel oder am Meeresgrund. Die druckdichten Anforderungen betreffen nicht nur das Gehäuse 2 selbst, sondern auch Durchführungen im Gehäuse, wie z.B. für Strom- und Steuerungskabel zur Energieversorgung und zur Steuerung und/oder Überwachung des Verdichtersystems 1.The in the figures 1 to FIG. 3 shown compressor systems are designed in particular for the promotion of gases and / or gas / oil mixtures in the offshore sector. In particular, a housing 2 is seawater resistant. The housing 2 is preferably made of steel and may have a protective coating to prevent corrosion. The steel used may alternatively or additionally be a stainless steel. Alternatively, the housing 2 may be made of a seawater resistant aluminum. Preferably, the housing is pressure-tight, in accordance with the intended for operation of the compressor system 1 depth of use under the sea water level or on the seabed. The pressure-tight requirements relate not only to the housing 2 itself, but also implementations in the housing, such as for power and control cables for power supply and for controlling and / or monitoring of the compressor system. 1

Das Gehäuse 2 weist beispielhaft eine Zugangsöffnung 3 für die zu verdichtenden Gase oder Gas-/Ölgemische und eine Ausgangsöffnung 4 für die verdichteten Gase oder Gas-/Ölgemische auf. Es können alternativ auch mehrere Öffnungen 3, 4 vorhanden sein. An den beiden Öffnungen 3, 4 sind üblicherweise Anschlusselemente, wie z.B. Kupplungen oder Flansche, angebracht, um an diese Leitungsrohre oder Druckschläuche anschließen zu können. Die Anschlusselemente sowie die Leitungsrohre sind hinsichtlich der jeweils geforderten Druckdichtigkeit in entsprechender Weise technisch robust auszulegen.The housing 2 has, for example, an access opening 3 for the gases or gas / oil mixtures to be compressed and an outlet opening 4 for the compressed gases or gas / oil mixtures. Alternatively, a plurality of openings 3, 4 may be present. At the two openings 3, 4 are usually connecting elements, such as couplings or flanges, mounted in order to connect to these pipes or pressure hoses. The connection elements and the pipes are to be designed in a technically robust manner with regard to the respectively required pressure tightness.

Im Gehäuse 2 ist der Verdichter 8 angeordnet, welcher eingangsseitig mit der Zugangsöffnung 3 und ausgangsseitig mit der Ausgangsöffnung 4 verbunden ist. Die im Bereich der Öffnungen 3, 4 dargestellten Pfeile zeigen die Strömungsrichtungen an. Im Beispiel der FIG 1 weist der Verdichter 8 eine Turbine 81 mit nicht weiter bezeichneten Turbinenblättern auf. Deren Durchmesser nimmt in axialer Richtung, das heißt in Strömungsrichtung ab, wobei durch die Verdichtung zugleich der Druck zunimmt. Mit dem Bezugszeichen 83 ist eine Hochdruckausleitung bezeichnet. Von dort aus erfolgt über eine nicht weiter bezeichnete Rohrverbindung im Inneren des Gehäuses 2 der Transport des verdichteten Gases zur Ausgangsöffnung 3 hin.In the housing 2, the compressor 8 is arranged, which is the input side connected to the access opening 3 and the output side to the output port 4. The arrows shown in the region of the openings 3, 4 indicate the flow directions. In the example of FIG. 1 For example, the compressor 8 has a turbine 81 with turbine blades not further specified. Their diameter decreases in the axial direction, that is, in the flow direction, whereby the pressure increases due to the compression at the same time. The reference numeral 83 denotes a high-pressure discharge. From there, via a pipe connection, not further described, inside the housing 2, the transport of the compressed gas to the exit opening 3 takes place.

Im Gehäuse 2 ist weiterhin der Elektromotor 7 zum Antreiben des Verdichters 8 angeordnet. Der Elektromotor 7 weist ein Statorpaket 71 sowie ein Rotorpaket 72 auf. Weiterhin weisen im Beispiel der FIG 1 sowohl der Verdichter 8 als auch der Elektromotor 7 eine gemeinsame, in Lagern 6 geführte Welle 5 auf.In the housing 2, the electric motor 7 is further arranged for driving the compressor 8. The electric motor 7 has a stator 71 and a rotor package 72. Furthermore, in the example of the FIG. 1 both the compressor 8 and the electric motor 7 on a common, guided in bearings 6 shaft 5.

Das Statorpaket 71 des Elektromotors 7 ist über eine Gehäuseinnenseite GI des Gehäuses 2 des Verdichtersystems 1 kühlbar. Im Beispiel der FIG 1 erfolgt die Kühlung über eine Statoraußenseite SA, welche bündig an der Gehäuseinnenseite GI anliegt. Die im Kontaktbereich zwischen Statoraußenseite SA und Gehäuseinnenseite GI eingetragenen Pfeile versinnbildlichen den Wärmestrom. Um die Kühlleistung zu erhöhen, kann zwischen der Statoraußenseite SA und der Gehäuseinnenseite GI eine gut wärmeleitfähige Masse eingebracht sein, wie z.B. eine gut wärmeleitende Paste, ein Fett oder dergleichen.The stator 71 of the electric motor 7 is cooled via a housing inner side GI of the housing 2 of the compressor system 1. In the example of FIG. 1 cooling takes place via a stator outer side SA, which rests flush against the inside of the housing GI. The arrows entered in the contact area between the outside of the stator SA and the inside of the housing GI symbolize the heat flow. To increase the cooling capacity, can between the stator outside SA and the inside of the housing GI be introduced a good thermal conductivity mass, such as a good thermal conductivity paste, a grease or the like.

Das gezeigte Verdichtersystem 1 ist derart installiert, dass die Drehachse DA des Elektromotors 7 im Wesentlichen in vertikaler Richtung verläuft. Sie kann alternativ auch in waagrechter Position ausgerichtet sein.The compressor system 1 shown is installed such that the axis of rotation DA of the electric motor 7 extends substantially in the vertical direction. It can alternatively be aligned in a horizontal position.

Des Weiteren weist das Gehäuse 2 eine Gehäuseaußenseite GA, an welcher eine Vielzahl von abstehenden Kühlrippen 21 angeordnet ist. Bei dem vorliegenden Fall einer zylindrischen Bauform des Gehäuses 2 weisen die Kühlrippen 21 radial von der Gehäuseaußenseite GA weg. Auch das erfindungsgemäße Verdichtersystem 1 und eine Ausführungsform dessen gemäß FIG 2 und FIG 3 weisen eine derartige zylindrische Bauform auf.Furthermore, the housing 2 has a housing outside GA, on which a plurality of projecting cooling fins 21 is arranged. In the present case of a cylindrical design of the housing 2, the cooling fins 21 are radially away from the housing outside GA. Also, the compressor system 1 according to the invention and an embodiment according to FIG. 2 and FIG. 3 have such a cylindrical design.

FIG 2 zeigt eine Schnittdarstellung eines erfindungsgemäßen Verdichtersystems 1. Das gezeigte Verdichtersystem 1 ist in Bezug auf die Drehachse DA des Elektromotors 7 wiederum vertikal installiert. FIG. 2 shows a sectional view of a compressor system according to the invention 1. The compressor system 1 shown is in turn mounted vertically with respect to the axis of rotation DA of the electric motor 7.

Im Unterschied zum Verdichtersystem gemäß FIG 1 ist das Statorpaket 71 gemäß der Erfindung von der Innenseite GI des Gehäuses 2 beabstandet. Der mittlere radiale Abstand liegt vorzugsweise in einem Bereich von 5 cm bis 15 cm. Je nach elektrischer Anschlussleistung des Elektromotors 7 können die Abstandswerte auch darüber liegen, wie z.B. bei 20 cm, oder darunter liegen, wie z.B. bei 3 cm. Das Statorpaket 71 bildet mit zumindest einem gegenüberliegenden Teil der Gehäuseinnenseite GI eine ringförmige Kühlkammer 9 aus, in welcher ein Kühlmittel 9 vorhanden ist. In der Kühlkammer 9 liegen auch die Wickelköpfe 73 des Statorpakets 71, welche axial aus dem Statorpaket 71 herausragen. Die Kühlkammer 9 weist im Beispiel der FIG 2 nur eine Kammer auf. Sie kann alternativ mehrere Kammern aufweisen, wobei in diesem Fall benachbarte Kammern jeweils durch ein radialaxial verlaufendes Schott von einander getrennt sind.In contrast to the compressor system according to FIG. 1 is the stator 71 according to the invention from the inside GI of the housing 2 spaced. The mean radial distance is preferably in a range of 5 cm to 15 cm. Depending on the electrical connection performance of the electric motor 7, the distance values can also be above, for example, at 20 cm, or below, such as at 3 cm. The stator 71 forms with at least one opposite part of the housing inner side GI an annular cooling chamber 9, in which a coolant 9 is present. In the cooling chamber 9 are also the winding heads 73 of the stator 71, which protrude axially from the stator 71. The cooling chamber 9 has in the example of FIG. 2 only one chamber up. It may alternatively have a plurality of chambers, in which case adjacent chambers are separated from each other by a radially axially extending bulkhead.

Die Kühlkammer 9 ist durch zwei Reife 91, 92 und eine Kreisscheibe 94 gebildet. Die beiden Reife 91, 92 weisen einen Innendurchmesser auf, der dem Innendurchmesser des Statorpakets 71 entspricht. Der erste Reif 91 ist an einer unteren axialen Stirnseite des Statorpakets 71 abgedichtet angebracht, wie z.B. angeschweißt. Die Symmetrieachse dieses Reifs 91 fluchtet mit der Drehachse DA des Elektromotors 7. Die axiale Höhe des ersten Reifs 91 entspricht nahezu dem axialen Abstand des Statorpakets 71 zu einer Bodenplatte 22 des Gehäuses 2. Der untere Rand des ersten Reifs 91 kann über einen Dichtungsring 93 zur Bodenplatte 22 hin abgedichtet sein oder mit der Bodenplatte 22 dicht verschweißt sein.The cooling chamber 9 is formed by two ripeness 91, 92 and a circular disk 94. The two ripen 91, 92 have an inner diameter which corresponds to the inner diameter of the stator 71. The first hoop 91 is sealed to a lower axial end face of the stator pack 71, such as e.g. welded. The axis of symmetry of this hoop 91 is aligned with the axis of rotation DA of the electric motor 7. The axial height of the first hoop 91 corresponds to almost the axial distance of the stator 71 to a bottom plate 22 of the housing 2. The lower edge of the first hoop 91 can via a sealing ring 93 for Bottom plate 22 to be sealed towards sealed or welded to the bottom plate 22.

Der zweite Reif 92 ist in entsprechender Weise am oberen axialen Ende des Statorpakets 71 angebracht. Die Kreisscheibe 94 weist einen Innendurchmesser auf, der in etwa dem Innendurchmesser der Reife 91, 92 entspricht. Der Außendurchmesser entspricht in etwa dem Innendurchmesser des Gehäuses 2. Der zweite Reif 92 und die Kreisscheibe 94 sind vorzugsweise mit einander dicht verschweißt und bilden gemeinsam einen Flansch 92, 94. Der Außenrand der Kreisscheibe 94 bzw. des Flansches 92, 94 kann über einen weiteren Dichtungsring 95 zur Gehäuseinnenseite GI abgedichtet sein oder mit der Gehäuseinnenseite GI dicht verschweißt sein. Die Reife 91, 92, die Kreisscheibe 94, eine radiale Innenseite des Statorpakets 71 und die Gehäuseinnenseite GI bilden somit einen Hohlzylinder.The second hoop 92 is similarly attached to the upper axial end of the stator core 71. The circular disk 94 has an inner diameter which corresponds approximately to the inner diameter of the maturity 91, 92. The outer diameter corresponds approximately to the inner diameter of the housing 2. The second hoop 92 and the circular disk 94 are preferably welded together tightly and together form a flange 92, 94. The outer edge of the circular disk 94 and the flange 92, 94 can via another Gasket 95 may be sealed to the inside of the housing GI or tightly welded to the inside of the housing GI. The maturity 91, 92, the circular disk 94, a radial inner side of the stator core 71 and the inside of the housing GI thus form a hollow cylinder.

In der Kühlkammer 9 ist ein Kühlmittel, vorzugsweise ein Öl, als Kühlflüssigkeit vorhanden. Insbesondere kommt ein sogenanntes Trafoöl auf Mineralölbasis oder Silikonölbasis in Betracht. Vorzugsweise ist die gesamte Kühlkammer 9 mit der Kühlflüssigkeit gefüllt. Im Gehäuse 2 und außerhalb der Kühlkammer 9 kann ein Ausgleichsgefäß für die Kühlflüssigkeit vorhanden sein, um eine temperaturbedingte Volumenänderung des Kühlmittels auszugleichen.In the cooling chamber 9, a coolant, preferably an oil, is present as the cooling fluid. In particular, a so-called transformer oil based on mineral oil or silicone oil comes into consideration. Preferably, the entire cooling chamber 9 is filled with the cooling liquid. In the housing 2 and outside the cooling chamber 9, a compensating vessel for the cooling liquid may be present to compensate for a temperature-induced change in volume of the coolant.

Das Kühlmittel kann alternativ zum Öl auch ein Kältemittel sein, wie z.B. ein Freon®. Besonders vorteilhaft ist hinsichtlich der Umweltverträglichkeit ein FCKW-freies Freon®, wie z.B. Freon® R134a. In diesem Fall ist die Kühlkammer 9 mit einem Sol gefüllt, das heißt mit einem Flüssigkeits-/Gasgemisch.The coolant may alternatively be a refrigerant, such as a Freon®. It is particularly advantageous in terms environmental compatibility a CFC-free Freon®, such as Freon® R134a. In this case, the cooling chamber 9 is filled with a sol, that is, with a liquid / gas mixture.

Des Weiteren sind im Statorpaket 71 im Wesentlichen axial zur Drehachse DA des Elektromotors 7 verlaufende Kühlkanäle 75 vorhanden. Wegen der Einbettung des Statorpakets 71 in dem Kühlmittel sind diese gleichfalls mit dem Kühlmittel gefüllt. Während des Betriebs des Verdichtersystems 1 stellt sich eine Zirkulation des Kühlmittels in der Kühlkammer 9 ein. Dies ist durch Strömungspfeile dargestellt. Dabei steigt das in den Kühlkanälen 75 erhitzte Kühlmittel nach oben und kühlt sich in umgekehrter Richtung von oben nach unten entlang der kalten Gehäuseinnenseite GI wieder ab. Dabei werden die thermisch besonders kritischen Wickelköpfe 73 durch das zirkulierende Kühlmittel umspült und damit wirksam gekühlt.Furthermore, cooling passages 75 extending essentially axially to the axis of rotation DA of the electric motor 7 are present in the stator pack 71. Because of the embedding of the stator 71 in the coolant, these are also filled with the coolant. During operation of the compressor system 1, a circulation of the coolant in the cooling chamber 9 is established. This is represented by flow arrows. In this case, the coolant heated in the cooling channels 75 rises upward and cools in the reverse direction from top to bottom along the cold inside of the housing GI again. In this case, the thermally particularly critical winding heads 73 are surrounded by the circulating coolant and thus effectively cooled.

Die waagrechten Pfeile symbolisieren den Wärmetransport vom Kühlmittel, weiter über die Wandung des Gehäuses 2 in das Meerwasser, welches die Außenseite GA des Gehäuses 2 umspült. Der sich in der Kühlkammer 9 einstellende Kühlkreislauf kann auch als Primärkühlkreislauf bezeichnet werden, während sich an der Gehäuseaußenseite, allerdings nur im Falle eines ruhenden Gewässers, eine Gegenströmung einstellt, welche von unten nach oben entlang der Gehäuseaußenseite GA entlang streicht. Die Kühlung durch das Meerwasser kann auch als Sekundärkühlung bezeichnet werden.The horizontal arrows symbolize the heat transfer from the coolant, continue on the wall of the housing 2 in the sea water, which surrounds the outside of the housing GA 2. The adjusting in the cooling chamber 9 cooling circuit can also be referred to as a primary cooling circuit, while adjusts to the outside of the housing, but only in the case of a stationary water, a counterflow, which sweeps from bottom to top along the outside of the housing GA. The cooling by the seawater can also be called secondary cooling.

Zur weiteren Steigerung der Kühlleistung kann das Verdichtersystem 1 eine Umwälzpumpe für das Kühlmittel aufweisen. Die Umwälzpumpe ist z.B. eine Kreiselpumpe, welche in oder an der Kühlkammer 9 angebracht ist.To further increase the cooling capacity, the compressor system 1 may comprise a circulation pump for the coolant. The circulating pump is e.g. a centrifugal pump which is mounted in or on the cooling chamber 9.

Im Vergleich zur FIG 1 sind die Kühlrippen 21 an der Außenseite GA des Gehäuses 2 hinsichtlich ihrer Länge kürzer ausgebildet. Sie erstrecken sich nur in dem axialen "heißen" Bereich des Gehäuses 2, welcher der Kühlkammer 9 gegenüberliegt. Die Kühlung des Verdichters 8 erfolgt in diesem Zusammenhang über die zu verdichtenden Gase bzw. Gas-/Ölgemische selbst.In comparison to FIG. 1 the cooling fins 21 are formed on the outside of the housing 2 GA shorter in length. They extend only in the axial "hot" region of the housing 2, which is opposite to the cooling chamber 9. The cooling of the compressor 8 takes place in this context on the gases to be compressed or gas / oil mixtures themselves.

FIG 3 zeigt eine Schnittdarstellung eines Verdichtersystems 1 gemäß einer dritten Ausführungsform der Erfindung. FIG. 3 shows a sectional view of a compressor system 1 according to a third embodiment of the invention.

Im Vergleich zur FIG 2 ist die Kühlkammer 9 im Wesentlichen torusförmig ausgebildet, wobei die Kühlkammer 9 gebogene Kühlkammerwände 96, 97 aufweist, welche durch ihre Formgebung den zirkulierenden Strömungsverlauf begünstigen. Die Kühlleistung dieser Ausführungsform ist daher im Vergleich zur zweiten Ausführungsform bei gleichem Bauvolumen größer. Die Kühlkammerwände 96, 97 erfüllen neben der Ausbildung der Kühlkammer 9 auch eine Strömungsleitfunktion. Mit den Bezugszeichen 98, 99 sind weitere Dichtungsringe zur Abdichtung der Kühlkammerwände 96, 97 mit der Gehäuseinnenseite GI bezeichnet. Alternativ können die Kühlkammerwände 96, 97 mit der Gehäuseinnenseite GI dicht verschweißt sein.In comparison to FIG. 2 the cooling chamber 9 is substantially torus-shaped, wherein the cooling chamber 9 curved cooling chamber walls 96, 97 which favor the circulating flow through their shape. The cooling capacity of this embodiment is therefore larger in comparison to the second embodiment with the same construction volume. The cooling chamber walls 96, 97 fulfill in addition to the formation of the cooling chamber 9 and a Strömungsleitfunktion. Reference numerals 98, 99 denote further sealing rings for sealing the cooling chamber walls 96, 97 with the inside of the housing GI. Alternatively, the cooling chamber walls 96, 97 may be tightly welded to the inside of the housing GI.

FIG 4 zeigt eine Seitenansicht des Verdichtersystems 1 gemäß FIG 3 entsprechend der in FIG 3 eingezeichneten Blickrichtung IV. FIG. 4 shows a side view of the compressor system 1 according to FIG. 3 according to the in FIG. 3 marked line of vision IV.

FIG 4 zeigt den Blick in die Zugangsöffnung 3, das heißt in Richtung auf den Verdichter. Wie FIG 4 weiter zeigt, weist das Statorpaket 71 eine Vielzahl in Umfangrichtung gleichmäßig verteilt angeordneter Kühlkanäle 75 auf. Die Kühlkanäle 75 sind hinsichtlich ihrer radialen Lage zu den Wickelköpfe 73 zu beiden Seiten der Wickelköpfe 73 angeordnet (vgl. dazu auch FIG 2 und FIG 3). Die Anordnung der Kühlkanäle 75 erfolgt vorzugsweise im magnetisch weniger aktiven Bereich des Statorpakets 71. Die Vielzahl von Kühlkanälen 75 ermöglicht eine effektive Kühlung des Statorpakets 71 quasi von innen heraus. FIG. 4 shows the view into the access opening 3, that is in the direction of the compressor. As FIG. 4 shows further, the stator 71 has a plurality of circumferentially uniformly distributed cooling channels 75 on. The cooling channels 75 are arranged with respect to their radial position to the winding heads 73 on both sides of the winding heads 73 (see also FIG. 2 and FIG. 3 ). The arrangement of the cooling channels 75 is preferably carried out in the magnetically less active region of the stator 71. The plurality of cooling channels 75 allows effective cooling of the stator 71 from the inside out.

An der Gehäuseaußenseite GA ist eine Vielzahl von radial von der Gehäuseaußenseite weg weisend angeordneten Kühlrippen 21 zu sehen. Die Kühlrippen 21 bewirken eine drastische Erhöhung der zur Kühlung durch Meerwasser zur Verfügung stehenden Kühlfläche. Vorzugsweise sind die Kühlrippen 21 integraler Bestandteil des Gehäuses 2 des Verdichtersystems 1. Insbesondere ist das Gehäuse 2 aus einem Guss gefertigt.On the outer side of the housing GA there is a large number of cooling fins 21 arranged radially away from the outside of the housing to see. The cooling fins 21 cause a drastic increase in the cooling surface available for cooling by seawater. Preferably, the cooling fins 21 are an integral part of the housing 2 of the compressor system 1. In particular, the housing 2 is made of a casting.

Das erfindungsgemäße Verdichtersystem eignet sich auch für schnelllaufende Verdichtersysteme bei Drehzahlen bis zu 15000 U/min und Leistungen von einigen 100 kW bis zu 10 MW und mehr.The compressor system according to the invention is also suitable for high-speed compressor systems at speeds of up to 15,000 rpm and powers of a few 100 kW up to 10 MW and more.

Claims (6)

  1. Compressor system, especially for transporting gases or gas/oil mixtures in the offshore area, with a seawater-proof housing (2) with at least one entry opening (3) for the gases or gas/oil mixtures which are to be compressed, and with at least one discharge opening (4) for the compressed gases or gas/oil mixtures, with a compressor (8) which is arranged in the housing (2) and which on the inlet side is connected to the entry opening (3) and on the outlet side is connected to the discharge opening (4), and with an electric motor (7), which is arranged in the housing (2), with a stator packet (71) which can be cooled via an inner side (GI) of the housing (2), and with a rotor packet (72) for driving Compressor (8),
    characterized in that
    - the stator packet (71) is at a distance from the inner side (GI) of the housing (2),
    - the stator packet (71) with at least one oppositely disposed part of the housing inner side (GI) forms an annular cooling chamber (9), and
    - a cooling medium is provided in the cooling chamber (9).
  2. Compressor system according to Claim 1, characterized in that the cooling medium is an oil.
  3. Compressor system according to Claim 1 or 2, characterized in that cooling passages (75) which extend essentially axially to the rotational axis (DA) of the electric motor (7) are provided in the stator packet (71).
  4. Compressor system according to one of the preceding claims, characterized in that Compressor system has a circulating pump for the cooling medium.
  5. Compressor system according to one of the preceding claims, characterized in that Compressor system in the asintended application is installed in such a way that the rotational axis (DA) of the electric motor (7) extends essentially in the vertical direction.
  6. Compressor system according to one of the preceding claims, characterized in that the housing (2) has a housing outer side (GA) and a multiplicity of cooling fins (21) are arranged on the housing outer side (GA).
EP08759450.3A 2007-05-09 2008-05-07 Compressor system for underwater use in the offshore area Active EP2142806B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007021720.1A DE102007021720B4 (en) 2007-05-09 2007-05-09 Compressor system for underwater use in the offshore sector
PCT/EP2008/055629 WO2008138829A1 (en) 2007-05-09 2008-05-07 Compressor system for underwater use in the offshore area

Publications (2)

Publication Number Publication Date
EP2142806A1 EP2142806A1 (en) 2010-01-13
EP2142806B1 true EP2142806B1 (en) 2018-02-28

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US (1) US8313316B2 (en)
EP (1) EP2142806B1 (en)
CN (1) CN101675249B (en)
BR (1) BRPI0811221B1 (en)
CA (1) CA2686794A1 (en)
DE (1) DE102007021720B4 (en)
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WO (1) WO2008138829A1 (en)

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Publication number Publication date
BRPI0811221A2 (en) 2014-10-29
RU2470190C2 (en) 2012-12-20
EP2142806A1 (en) 2010-01-13
BRPI0811221B1 (en) 2019-09-03
US20100239441A1 (en) 2010-09-23
CN101675249B (en) 2013-01-09
RU2009145531A (en) 2011-06-20
CN101675249A (en) 2010-03-17
DE102007021720B4 (en) 2014-01-23
WO2008138829A1 (en) 2008-11-20
CA2686794A1 (en) 2008-11-20
US8313316B2 (en) 2012-11-20
DE102007021720A1 (en) 2008-11-13

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