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EP4163500A1 - Air compression assembly for air separation - Google Patents

Air compression assembly for air separation Download PDF

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Publication number
EP4163500A1
EP4163500A1 EP21201814.7A EP21201814A EP4163500A1 EP 4163500 A1 EP4163500 A1 EP 4163500A1 EP 21201814 A EP21201814 A EP 21201814A EP 4163500 A1 EP4163500 A1 EP 4163500A1
Authority
EP
European Patent Office
Prior art keywords
compressor
air
drive unit
compression system
booster
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.)
Withdrawn
Application number
EP21201814.7A
Other languages
German (de)
French (fr)
Inventor
Attilla Yildiz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Siemens Energy Global GmbH and Co KG
Original Assignee
Siemens Energy Global GmbH and Co KG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Siemens Energy Global GmbH and Co KG filed Critical Siemens Energy Global GmbH and Co KG
Priority to EP21201814.7A priority Critical patent/EP4163500A1/en
Priority to PCT/EP2022/077619 priority patent/WO2023061813A1/en
Publication of EP4163500A1 publication Critical patent/EP4163500A1/en
Withdrawn legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08—Centrifugal pumps
    • F04D17/10—Centrifugal pumps for compressing or evacuating
    • F04D17/12—Multi-stage pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/02—Units comprising pumps and their driving means
    • F04D25/024—Units comprising pumps and their driving means the driving means being assisted by a power recovery turbine
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
    • F04D25/163—Combinations of two or more pumps ; Producing two or more separate gas flows driven by a common gearing arrangement
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/58—Cooling; Heating; Diminishing heat transfer
    • F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
    • F04D29/5826—Cooling at least part of the working fluid in a heat exchanger
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J3/00—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
    • F25J3/02—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream
    • F25J3/04—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air
    • F25J3/04006—Providing pressurised feed air or process streams within or from the air fractionation unit
    • F25J3/04012—Providing pressurised feed air or process streams within or from the air fractionation unit by compression of warm gaseous streams; details of intake or interstage cooling
    • F25J3/04018—Providing pressurised feed air or process streams within or from the air fractionation unit by compression of warm gaseous streams; details of intake or interstage cooling of main feed air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J3/00—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
    • F25J3/02—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream
    • F25J3/04—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air
    • F25J3/04006—Providing pressurised feed air or process streams within or from the air fractionation unit
    • F25J3/04109—Arrangements of compressors and /or their drivers
    • F25J3/04115—Arrangements of compressors and /or their drivers characterised by the type of prime driver, e.g. hot gas expander
    • F25J3/04121—Steam turbine as the prime mechanical driver
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J3/00—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
    • F25J3/02—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream
    • F25J3/04—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air
    • F25J3/04006—Providing pressurised feed air or process streams within or from the air fractionation unit
    • F25J3/04109—Arrangements of compressors and /or their drivers
    • F25J3/04115—Arrangements of compressors and /or their drivers characterised by the type of prime driver, e.g. hot gas expander
    • F25J3/04127—Gas turbine as the prime mechanical driver
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J3/00—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
    • F25J3/02—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream
    • F25J3/04—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air
    • F25J3/04006—Providing pressurised feed air or process streams within or from the air fractionation unit
    • F25J3/04109—Arrangements of compressors and /or their drivers
    • F25J3/04115—Arrangements of compressors and /or their drivers characterised by the type of prime driver, e.g. hot gas expander
    • F25J3/04133—Electrical motor as the prime mechanical driver
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J3/00—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
    • F25J3/02—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream
    • F25J3/04—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air
    • F25J3/04006—Providing pressurised feed air or process streams within or from the air fractionation unit
    • F25J3/04109—Arrangements of compressors and /or their drivers
    • F25J3/04139—Combination of different types of drivers mechanically coupled to the same compressor, possibly split on multiple compressor casings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/70—Application in combination with
    • F05D2220/72—Application in combination with a steam turbine
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2230/00—Processes or apparatus involving steps for increasing the pressure of gaseous process streams
    • F25J2230/20—Integrated compressor and process expander; Gear box arrangement; Multiple compressors on a common shaft

Definitions

  • a geared compressor usually includes three compression stages and two intermediate coolers.
  • the other geared compressor typically includes four to six airends and three to five intercoolers.
  • the geared compressors have many mechanical components (ring gear, pinion shaft, large housings, etc.) which result in high costs.
  • an intermediate gear is usually used between the steam turbine and the geared compressor.
  • MAC main air compressor
  • BAC booster air compressor
  • Conventional MACs are usually designed as at least three-stage geared compressors. Arrangements with a geared compressor or geared compressor are already from the DE 102010020145 A1 , DE 102009015862 A1 , DE 102014225136 A1 , DE 102015200439 A1 , DE 102015203287 A1 known.
  • Such compression systems are correspondingly expensive because usually a gear and at least two compressor shafts are required, on the shaft ends of which the corresponding compressors can be attached.
  • the high installation effort, the maintenance costs and the amount of the investment are undesirable from an economic point of view.
  • the invention has set itself the task of reducing investment costs without significantly impairing the efficiency of such systems.
  • a compressor module within the meaning of the invention is a compressor or a compressor stage and, in the case of the radial compressor or centrifugal compressor, comprises at least one impeller.
  • the main air compressor and the booster air compressor each have at least one compressor module that is driven by the respective drive unit.
  • the invention is essentially concerned with the compression of air for air separation, which must meet the specific requirements of air separation, and with the drive of this compression process.
  • a supplier it is a mandatory requirement for a supplier to provide a main air compressor and at least one, preferably two, so-called booster air compressors (BAC).
  • BAC booster air compressors
  • the separate compressor train of the booster air compressor is a geared compressor with one large gear and several on the large gear torque-transmitting planetary gears formed.
  • the large gear wheel is coupled in a torque-transmitting manner to the second drive unit via a common second shaft.
  • the geared compressor has at least two planetary gearwheels, to which two compressor modules are coupled in a torque-transmitting manner.
  • the main air compressor has two compressor modules on the compressor train, the first drive unit and the two compressor modules having a common first shaft, the two compressor modules being coupled to the first drive unit in a torque-transmitting manner via the common first shaft.
  • the invention proposes reducing the number of compressor modules in the main air compressor from three to two, which leads to a reduction in investment costs.
  • the first drive unit is arranged between the two compressor modules.
  • the first drive unit is designed as a steam turbine.
  • the second drive unit is designed as an electric motor.
  • the two compressor modules are fluidically connected to one another, with an intercooler being arranged between the two compressor modules, the intercooler being used to cool the is formed in operation from the compressor module outflowing process fluid.
  • the booster air compressor has a number of compressor modules, one compressor module being fluidically connected to the compressor module of the main air compressor (MAC).
  • a second intermediate cooler is arranged between the compressor module of the main air compressor and the compressor module of the booster air compressor.
  • an intercooler is arranged between the compressor modules of the booster air compressor.
  • the figure shows an embodiment of an air compression system for air separation according to the invention.
  • main air compressor main air compressor
  • booster air compressor booster air compressor
  • the air compression system 1 also includes a first drive unit 4 for driving at least one compressor module 5, 6 of the main air compressor 2.
  • the air compression system 1 also includes at least one second drive unit 7 for driving at least one compressor module 8, 9, 10, 11 of the booster air compressor 3.
  • the main air compressor 2 includes a first compressor line, which is coupled to the first drive unit 4 in a torque-transmitting manner, with the booster air compressor 3 including a separate compressor line, which is coupled to the second drive unit 7 in a torque-transmitting manner.
  • the two compressor trains of the main air compressor 2 and the booster air compressor 3 are fluidically connected to one another, there is no drive-side connection between the two compressor trains. This saves costs because no gears, clutches, etc. are required.
  • the separate compressor train of the booster air compressor 3 is designed with a geared compressor 12 .
  • the geared compressor 12 has a large wheel gear which is coupled in a torque-transmitting manner to the second drive unit 7 via a shaft 13 .
  • the geared compressor 12 also includes a plurality of planetary gears torque-transmittingly coupled to the pinion gear. Rotation of the large wheel gear results in rotation of the planetary gears.
  • Each planetary gear is coupled to at least one compressor module 8, 9, 10, 11 so that the rotation of the large wheel gear leads to the performance of the sealing work in the compressor modules 8, 9, 10, 11.
  • the main air compressor 2 has two compressor modules 5, 6, which form a compressor train with the first drive unit 4.
  • the first drive unit 4 and the two compressor modules 5, 6 have a common first shaft 13, the two compressor modules 5, 6 being coupled to the first drive unit 4 in a torque-transmitting manner via the common first shaft 13.
  • the large gear wheel is coupled to the second drive unit 7 in a torque-transmitting manner via a common second shaft 27 .
  • the first drive unit 4 is arranged between the first compression module 5 and the second compression module 6 .
  • the first drive unit 4 is designed as a steam turbine. In alternative embodiments, the first drive unit 4 can also be designed as an electric motor, gas turbine or the like.
  • the second drive unit 7 is designed as an electric motor. In alternative embodiments, the second drive unit 7 can also be designed as an electric motor, gas turbine or the like.
  • a flow medium flows into the first compression module 5 via a first line 14.
  • the flow medium can be air.
  • the pressure and the temperature of the flow medium are increased.
  • the flow medium flows via a second line 15 to a first intermediate cooler 16.
  • the flow medium is cooled.
  • the flow medium then flows to the second compressor module 6. There the flow medium is further compressed, with the pressure and the temperature increasing. The flow medium then flows via a third line 17 to a second intermediate cooler 18. The temperature of the flow medium is reduced in the second intermediate cooler.
  • the compression work in the main air compressor 2 would thus be completed.
  • the further compression work is carried out in the booster air compressor 3 .
  • the flow medium flows via a fourth line 19 into a third compressor module 8.
  • the pressure and the temperature of the flow medium are increased.
  • the flow medium then flows via a fifth line 20 to a third intermediate cooler 21, where the temperature of the flow medium is reduced again.
  • the flow medium flows into a fourth compressor module 9, where the pressure of the flow medium is further increased, with the temperature also rising.
  • the flow medium then flows to a fourth intercooler 22 where the temperature of the flow medium is reduced.
  • the flow medium flows via a sixth line 23 to a fifth Compressor module 10, wherein the pressure of the flow medium is increased, the temperature increases.
  • the flow medium then flows via a seventh line 24 to a fifth intercooler 25, where the temperature of the flow medium is reduced.
  • the flow medium flows to a sixth compressor module 11, where the pressure and temperature of the flow medium is increased.
  • the flow medium flows out of the air compression system via an eighth line 26 .

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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)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)

Abstract

Die Erfindung betrifft eine Luftverdichtungsanlage (1) für eine Luftzerlegung umfassend:mindestens einen Hauptluftverdichter (2) (MAC), mindestens einen Booster-Luftverdichter (3) (BAC), mindestens eine erste Antriebseinheit (4) zum Antrieb zumindest eines Verdichtermoduls (5, 6) des Hauptluftverdichters (2) (MAC), mindestens eine zweite Antriebseinheit (7) zum Antrieb zumindest eines Verdichtermoduls (8, 9, 10, 11) des Booster-Luftverdichter (3) (BAC), wobei der Hauptluftverdichter (2) (MAC) einen ersten Verdichterstrang umfasst, der mit der ersten Antriebseinheit (4) drehmomentübertragend gekoppelt ist, wobei der Booster-Luftverdichter (3) (BAC) einen separaten Verdichterstrang umfasst, der mit der zweiten Antriebseinheit (7) drehmomentübertragend gekoppelt ist.The invention relates to an air compression system (1) for air separation, comprising: at least one main air compressor (2) (MAC), at least one booster air compressor (3) (BAC), at least one first drive unit (4) for driving at least one compressor module (5, 6) of the main air compressor (2) (MAC), at least one second drive unit (7) for driving at least one compressor module (8, 9, 10, 11) of the booster air compressor (3) (BAC), the main air compressor (2) ( MAC) comprises a first compressor train which is coupled in a torque-transmitting manner to the first drive unit (4), the booster air compressor (3) (BAC) comprising a separate compressor train which is coupled in a torque-transmitting manner to the second drive unit (7).

Description

Die Erfindung betrifft eine Luftverdichtungsanlage für eine Luftzerlegung umfassend:

  • mindestens einen Hauptluftverdichter (MAC),
  • mindestens einen Booster-Luftverdichter (BAC),
  • mindestens eine erste Antriebseinheit zum Antrieb zumindest eines Verdichtermoduls des Hauptluftverdichters (MAC),
  • mindestens eine zweite Antriebseinheit zum Antrieb zumindest eines Verdichtermoduls des Booster-Luftverdichters (BAC) .
The invention relates to an air compression system for air separation, comprising:
  • at least one main air compressor (MAC),
  • at least one booster air compressor (BAC),
  • at least one first drive unit for driving at least one compressor module of the main air compressor (MAC),
  • at least one second drive unit for driving at least one compressor module of the booster air compressor (BAC).

Aus der WO 2011/141439 A1 ist bereits eine Anordnung mit einem mehrstufigen Getriebeverdichter insbesondere zur Luftzerlegung bekannt. Bei einem derartigen Kompressor-Strang einer Luftverdichtungsanlage für eine Luftzerlegung werden sehr viele mechanische Komponenten, beispielsweise Getriebegehäuse mit Getriebeelementen und Kupplungen, etc. verwendet. Diese Bauteile dienen häufig nicht unmittelbar dem Zweck der Druckerhöhung eines Volumenstroms an Luft. Stattdessen sind diese Elemente notwendig, die eigentliche konstruktive Lösung zu realisieren, insbesondere, die einzelnen Verdichter mit einer geeigneten Drehzahl zu betreiben. Viele dieser Bauteile erzeugen neben hohen Investitionskosten auch insbesondere mechanische Verlustleistungen, die in Form von Wärme abgeführt werden, muss. Dementsprechend sind in der Regel großvolumige Ölanlagen zur Schmierung von Lagern und auch zur Kühlung des Getriebeöls erforderlich.From the WO 2011/141439 A1 an arrangement with a multi-stage geared compressor, in particular for air separation, is already known. A large number of mechanical components, for example gear housings with gear elements and clutches, etc., are used in such a compressor train of an air compression system for air separation. These components often do not directly serve the purpose of increasing the pressure of a volume flow of air. Instead, these elements are necessary to implement the actual design solution, in particular to operate the individual compressors at a suitable speed. In addition to high investment costs, many of these components also generate mechanical power losses, which must be dissipated in the form of heat. Accordingly, large-volume oil systems are usually required to lubricate bearings and also to cool the gear oil.

Es ist bekannt, Luftzerlegungsanlagen mit zwei Getriebeverdichtern auszubilden, wobei der eine Getriebeverdichter für die Verdichtung der Hauptluft und der andere Getriebeverdichter für die Verdichtung von Zusatzluft ausgebildet ist, wobei beide Getriebeverdichter mit einer Dampfturbine angetrieben werden. Der eine Getriebeverdichter umfasst in der Regel drei Verdichtungsstufen und zwei Zwischenkühler. Der andere Getriebeverdichter umfasst in der Regel vier bis sechs Verdichterstufen und drei bis fünf Zwischenkühler. Die Getriebeverdichter haben viele mechanische Komponenten (Hohlrad, Ritzelwelle, große Gehäuse usw.), die zu hohen Kosten führen. Außerdem wird meistens ein Zwischengetriebe zwischen der Dampfturbine und des Getriebeverdichters eingesetzt.It is known to design air separation plants with two geared compressors, one geared compressor for compressing the main air and the other geared compressor for compressing additional air, with both geared compressors being driven by a steam turbine. A geared compressor usually includes three compression stages and two intermediate coolers. The other geared compressor typically includes four to six airends and three to five intercoolers. The geared compressors have many mechanical components (ring gear, pinion shaft, large housings, etc.) which result in high costs. In addition, an intermediate gear is usually used between the steam turbine and the geared compressor.

Insbesondere für Anlagen zur Zerlegung von Luft in die einzelnen Bestandteile werden große Verdichtungsleistungen benötigt. In der Regel erfolgt ein derartiger Verdichtungsprozess in zwei miteinander verknüpften Verdichtungsanlagen einem sogenannten Main-Air-Compressor (MAC = Hauptluftverdichter) und einem Booster-Air-Compressor (BAC = > zusätzliche Verdichtung). Herkömmliche MAC werden in der Regel als mindestens dreistufige Getriebeverdichter ausgeführt.
Anordnungen mit einem Getriebeverdichter bzw. Getriebeverdichter sind bereits aus den DE 102010020145 A1 , DE 102009015862 A1 , DE 102014225136 A1 , DE 102015200439 A1 , DE 102015203287 A1 bekannt.Large compression capacities are required in particular for systems for separating air into its individual components. As a rule, such a compression process takes place in two interconnected compression systems, a so-called main air compressor (MAC = main air compressor) and a booster air compressor (BAC = > additional compression). Conventional MACs are usually designed as at least three-stage geared compressors.
Arrangements with a geared compressor or geared compressor are already from the DE 102010020145 A1 , DE 102009015862 A1 , DE 102014225136 A1 , DE 102015200439 A1 , DE 102015203287 A1 known.

Derartige Verdichtungsanlagen sind dementsprechend teuer, weil in der Regel ein Getriebe und mindestens zwei Verdichterwellen benötigt werden, an dessen Wellenenden die entsprechenden Verdichter angebracht werden können. Der hohe Installationsaufwand, die Wartungskosten und die Höhe der Investition schlechthin sind schon aus wirtschaftlichen Gesichtspunkten unerwünscht.Such compression systems are correspondingly expensive because usually a gear and at least two compressor shafts are required, on the shaft ends of which the corresponding compressors can be attached. The high installation effort, the maintenance costs and the amount of the investment are undesirable from an economic point of view.

Die Erfindung hat es sich ausgehend von den bekannten Problemen und Nachteilen des Standes der Technik im Bereich der Luftverdichtungsanlage für eine Luftzerlegung zur Aufgabe gemacht, Investitionskosten zu senken, ohne den Wirkungsgrad derartiger Anlagen nennenswert zu verschlechtern.Based on the known problems and disadvantages of the prior art in the field of air compression systems for air separation, the invention has set itself the task of reducing investment costs without significantly impairing the efficiency of such systems.

Die Aufgabe wird gelöst durch eine Luftverdichtungsanlage für eine Luftzerlegung umfassend:

  • mindestens einen Hauptluftverdichter (MAC),
  • mindestens einen Booster-Luftverdichter (BAC),
  • mindestens eine erste Antriebseinheit zum Antrieb zumindest eines Verdichtermoduls des Hauptluftverdichters (MAC),
  • mindestens eine zweite Antriebseinheit zum Antrieb zumindest eines Verdichtermoduls des Booster-Luftverdichter (BAC), wobei der Hauptluftverdichter (MAC) einen ersten Verdichterstrang umfasst, der mit der ersten Antriebseinheit drehmomentübertragend gekoppelt ist,
wobei der Booster-Luftverdichter (BAC) einen separaten Verdichterstrang umfasst, der mit der zweiten Antriebseinheit drehmomentübertragend gekoppelt ist.The task is solved by an air compression system for air separation comprising:
  • at least one main air compressor (MAC),
  • at least one booster air compressor (BAC),
  • at least one first drive unit for driving at least one compressor module of the main air compressor (MAC),
  • at least one second drive unit for driving at least one compressor module of the booster air compressor (BAC), wherein the main air compressor (MAC) comprises a first compressor train which is coupled to the first drive unit in a torque-transmitting manner,
wherein the booster air compressor (BAC) includes a separate compressor train torque-transmittingly coupled to the second drive unit.

Die rückbezogenen Unteransprüche betreffen vorteilhafte Weiterbildungen der Erfindung.The dependent claims relate to advantageous developments of the invention.

Ein Verdichtermodul im Sinne der Erfindung ist ein Verdichter oder eine Verdichterstufe und umfasst im Fall des Radialverdichters bzw. Zentrifugalverdichters mindestens ein Laufrad. Der Hauptluftverdichter und der Booster-Luftverdichter weisen jeweils mindestens ein Verdichtermodul auf, dass von der jeweiligen Antriebseinheit angetrieben wird.A compressor module within the meaning of the invention is a compressor or a compressor stage and, in the case of the radial compressor or centrifugal compressor, comprises at least one impeller. The main air compressor and the booster air compressor each have at least one compressor module that is driven by the respective drive unit.

Während eine Luftzerlegung einen sehr komplexen Verfahrensablauf aufweisen kann, beschäftigt sich die Erfindung im Wesentlichen mit der Verdichtung von Luft für eine Luftzerlegung, die den bestimmten Anforderungen einer Zerlegung von Luft genügen muss und mit dem Antrieb dieses Verdichtungsvorgangs. Dem industriellen Standard folgend, ist es für einen Anbieter eine zwingende Voraussetzung, einen Hauptluftverdichter (main air compressor) und mindestens einen, bevorzugt zwei sogenannte Booster-Luftverdichter (Booster Air Compressor BAC) bereitzustellen.While air separation can have a very complex process sequence, the invention is essentially concerned with the compression of air for air separation, which must meet the specific requirements of air separation, and with the drive of this compression process. Following the industrial standard, it is a mandatory requirement for a supplier to provide a main air compressor and at least one, preferably two, so-called booster air compressors (BAC).

Besondere Vorteile der Erfindung ergeben sich insbesondere als eine Auflösung der Strang-Struktur mehrstufiger Getriebeverdichter, wie aus dem zitierten Stand der Technik bekannt. In einer ersten vorteilhaften Weiterbildung ist der separate Verdichterstrang des Booster-Luftverdichter (BAC) als Getriebeverdichter mit einem Großzahnrad und mehrere an dem Großzahnrad drehmomentübertragende Planeten-Zahnräder ausgebildet.Particular advantages of the invention arise in particular when the train structure of multi-stage geared compressors is dissolved, as is known from the cited prior art. In a first advantageous development, the separate compressor train of the booster air compressor (BAC) is a geared compressor with one large gear and several on the large gear torque-transmitting planetary gears formed.

In einer weiteren vorteilhaften Weiterbildung ist das Großzahnrad über eine gemeinsame zweite Welle mit der zweiten Antriebseinheit drehmomentübertragend gekoppelt.In a further advantageous development, the large gear wheel is coupled in a torque-transmitting manner to the second drive unit via a common second shaft.

In einer weiteren vorteilhaften Weiterbildung weist der Getriebeverdichter mindestens zwei Planeten-Zahnräder auf, an dem jeweils zwei Verdichtermodule drehmomentübertragend gekoppelt sind.In a further advantageous development, the geared compressor has at least two planetary gearwheels, to which two compressor modules are coupled in a torque-transmitting manner.

In einer weiteren vorteilhaften Weiterbildung weist der Hauptluftverdichter (MAC) zwei Verdichtermodule an dem Verdichterstrang auf, wobei die erste Antriebseinheit und die zwei Verdichtermodule eine gemeinsame erste Welle aufweisen, wobei die zwei Verdichtermodule über die gemeinsame erste Welle drehmomentübertragend mit der ersten Antriebseinheit gekoppelt sind.In a further advantageous development, the main air compressor (MAC) has two compressor modules on the compressor train, the first drive unit and the two compressor modules having a common first shaft, the two compressor modules being coupled to the first drive unit in a torque-transmitting manner via the common first shaft.

Mit der Erfindung wird vorgeschlagen, die Anzahl der Verdichtermodule im Hauptluftverdichter von drei auf zwei zu reduzieren, was zu einer Reduzierung der Investitionskosten führt.The invention proposes reducing the number of compressor modules in the main air compressor from three to two, which leads to a reduction in investment costs.

In einer vorteilhaften Weiterbildung ist die erste Antriebseinheit zwischen den zwei Verdichtermodulen angeordnet.In an advantageous development, the first drive unit is arranged between the two compressor modules.

In einer weiteren vorteilhaften Weiterbildung ist die erste Antriebseinheit als Dampfturbine ausgebildet.In a further advantageous development, the first drive unit is designed as a steam turbine.

In einer weiteren vorteilhaften Weiterbildung ist die zweite Antriebseinheit als Elektromotor ausgebildet.In a further advantageous development, the second drive unit is designed as an electric motor.

In einer weiteren vorteilhaften Weiterbildung sind die zwei Verdichtermodule strömungstechnisch miteinander verbunden, wobei zwischen den beiden Verdichtermodulen ein Zwischenkühler angeordnet ist, wobei der Zwischenkühler zum Kühlen des im Betrieb aus dem Verdichtermodul ausströmenden Prozessfluids ausgebildet ist.In a further advantageous development, the two compressor modules are fluidically connected to one another, with an intercooler being arranged between the two compressor modules, the intercooler being used to cool the is formed in operation from the compressor module outflowing process fluid.

In einer weiteren vorteilhaften Weiterbildung weist der Booster-Luftverdichter (BAC) mehrere Verdichtermodule auf, wobei ein Verdichtermodul strömungstechnisch mit dem Verdichtermodul des Hauptluftverdichters (MAC) verbunden ist.In a further advantageous development, the booster air compressor (BAC) has a number of compressor modules, one compressor module being fluidically connected to the compressor module of the main air compressor (MAC).

In einer weiteren vorteilhaften Weiterbildung ist zwischen dem Verdichtermodul des Hauptluft-verdichters und dem Verdichtermodul des Booster-Luftverdichter ein zweiter Zwischenkühler angeordnet.In a further advantageous development, a second intermediate cooler is arranged between the compressor module of the main air compressor and the compressor module of the booster air compressor.

In einer weiteren vorteilhaften Weiterbildung ist zwischen den Verdichtermodulen des Booster-Luftverdichters jeweils ein Zwischenkühler angeordnet.In a further advantageous development, an intercooler is arranged between the compressor modules of the booster air compressor.

Im Folgenden ist die Erfindung anhand spezieller Ausführungsbeispiele unter Bezugnahme auf Zeichnungen näher erläutert.The invention is explained in more detail below using specific exemplary embodiments with reference to drawings.

Die oben beschriebenen Eigenschaften, Merkmale und Vorteile dieser Erfindung sowie die Art und Weise, wie diese erreicht werden, werden klarer und deutlicher verständlich im Zusammenhang mit der folgenden Beschreibung der Ausführungsbeispiele, die im Zusammenhang mit den Zeichnungen näher erläutert werden.The properties, features and advantages of this invention described above, and the manner in which they are achieved, will become clearer and more clearly understood in connection with the following description of the exemplary embodiments, which are explained in more detail in connection with the drawings.

Gleiche Bauteile oder Bauteile mit gleicher Funktion sind dabei mit gleichen Bezugszeichen gekennzeichnet.Identical components or components with the same function are identified with the same reference symbols.

Ausführungsbeispiele der Erfindung werden nachfolgend anhand der Zeichnungen beschrieben. Diese sollen die Ausführungsbeispiele nicht maßstäblich darstellen, vielmehr ist die Zeichnung, wo zur Erläuterung dienlich, in schematisierter und/oder leicht verzerrter Form ausgeführt. Im Hinblick auf Ergänzungen der in der Zeichnung unmittelbar erkennbaren Lehren wird auf den einschlägigen Stand der Technik verwiesen.Exemplary embodiments of the invention are described below with reference to the drawings. These are not intended to represent the exemplary embodiments to scale, rather the drawing, where useful for explanation, is in schematic and/or slightly distorted form. With regard to additions to the teachings that can be seen directly in the drawing, reference is made to the relevant state of the art.

Es zeigt:

Figur
eine schematische Darstellung der erfindungsgemäßen Luftverdichtungsanlage für eine Luftzerlegung.
It shows:
figure
a schematic representation of the air compression system according to the invention for air separation.

Die Figur zeigt eine erfindungsgemäße Ausführung einer Luftverdichtungsanlage für eine Luftzerlegung.The figure shows an embodiment of an air compression system for air separation according to the invention.

Die in der Figur 1 dargestellte Luftverdichtungsanlage 1 für eine Luftzerlegung sieht mindestens einen Hauptluftverdichter 2, der auch als Main-Air-Compressor (MAC = Hauptluftverdichter) bezeichnet wird und mindestens einen Booster-Luftverdichter 3, der auch als Booster-Air-Compressor (BAC = > zusätzliche Verdichtung) bezeichnet wird, vor.The air compression system 1 for air separation shown in Figure 1 has at least one main air compressor 2, which is also referred to as the main air compressor (MAC = main air compressor) and at least one booster air compressor 3, which is also referred to as the booster air compressor (BAC => additional compression) before.

Die Luftverdichtungsanlage 1 umfasst des Weiteren eine erste Antriebseinheit 4 zum Antrieb zumindest eines Verdichtermoduls 5, 6 des Hauptluftverdichters 2.The air compression system 1 also includes a first drive unit 4 for driving at least one compressor module 5, 6 of the main air compressor 2.

Die Luftverdichtungsanlage 1 umfasst des Weiteren mindestens eine zweite Antriebseinheit 7 zum Antrieb zumindest eines Verdichtermoduls 8, 9, 10, 11 des Booster-Luftverdichters 3.The air compression system 1 also includes at least one second drive unit 7 for driving at least one compressor module 8, 9, 10, 11 of the booster air compressor 3.

Der Hauptluftverdichter 2 umfasst einen ersten Verdichterstrang, der mit der ersten Antriebseinheit 4 drehmomentübertragend gekoppelt ist, wobei der Booster-Luftverdichter 3 einen separaten Verdichterstrang umfasst, der mit der zweiten Antriebseinheit 7 drehmomentübertragend gekoppelt ist. Die beiden Verdichterstränge des Hauptluftverdichters 2 und des Booster-Luftverdichter 3 sind zwar strömungstechnisch miteinander verbunden, allerdings besteht keine antriebseitige Verbindung zwischen den beiden Verdichtersträngen. Dadurch werden Kosten eingespart, da keine Getriebe, Kupplungen usw. benötigt werden.The main air compressor 2 includes a first compressor line, which is coupled to the first drive unit 4 in a torque-transmitting manner, with the booster air compressor 3 including a separate compressor line, which is coupled to the second drive unit 7 in a torque-transmitting manner. Although the two compressor trains of the main air compressor 2 and the booster air compressor 3 are fluidically connected to one another, there is no drive-side connection between the two compressor trains. This saves costs because no gears, clutches, etc. are required.

Der separate Verdichterstrang des Booster-Luftverdichters 3 ist mit einem Getriebeverdichter 12 ausgebildet. Der Getriebeverdichter 12 weist hierbei ein Großradzahnrad auf, das über eine Welle 13 mit der zweiten Antriebseinheit 7 drehmomentübertragend gekoppelt ist. Des Weiteren weist der Getriebeverdichter 12 mehrere Planeten-Zahnräder auf, die drehmomentübertragend mit dem Großradzahnrad gekoppelt sind. Eine Drehung des Großradzahnrades führt zu einer Drehung der Planeten-Zahnräder. Jedes Planeten-Zahnrad ist zumindest mit einem Verdichtermodul 8, 9, 10, 11 gekoppelt, so dass die Drehung des Großradzahnrades zur Verrichtung der Dichtungsarbeit in den Verdichtermodulen 8, 9, 10, 11 führt.The separate compressor train of the booster air compressor 3 is designed with a geared compressor 12 . The geared compressor 12 has a large wheel gear which is coupled in a torque-transmitting manner to the second drive unit 7 via a shaft 13 . The geared compressor 12 also includes a plurality of planetary gears torque-transmittingly coupled to the pinion gear. Rotation of the large wheel gear results in rotation of the planetary gears. Each planetary gear is coupled to at least one compressor module 8, 9, 10, 11 so that the rotation of the large wheel gear leads to the performance of the sealing work in the compressor modules 8, 9, 10, 11.

Der Hauptluftverdichter 2 weist zwei Verdichtermodule 5, 6 auf, die mit der ersten Antriebseinheit 4 einen Verdichterstrang bilden. Die erste Antriebseinheit 4 und die zwei Verdichtermodule 5, 6 weisen eine gemeinsame erste Welle 13 auf, wobei die zwei Verdichtermodule 5, 6 über die gemeinsame erste Welle 13 drehmomentübertragend mit der ersten Antriebseinheit 4 gekoppelt sind.The main air compressor 2 has two compressor modules 5, 6, which form a compressor train with the first drive unit 4. The first drive unit 4 and the two compressor modules 5, 6 have a common first shaft 13, the two compressor modules 5, 6 being coupled to the first drive unit 4 in a torque-transmitting manner via the common first shaft 13.

Das Großzahnrad ist über eine gemeinsame zweite Welle 27 mit der zweiten Antriebseinheit 7 drehmomentübertragend gekoppelt.The large gear wheel is coupled to the second drive unit 7 in a torque-transmitting manner via a common second shaft 27 .

Die erste Antriebseinheit 4 ist hierbei zwischen dem ersten Verdichtungsmodul 5 und dem zweiten Verdichtungsmodul 6 angeordnet.In this case, the first drive unit 4 is arranged between the first compression module 5 and the second compression module 6 .

Die erste Antriebseinheit 4 ist als Dampfturbine ausgebildet. Die erste Antriebseinheit 4 kann in alternativen Ausführungsformen auch als elektrischer Motor, Gasturbine oder vergleichbarem ausgebildet sein.The first drive unit 4 is designed as a steam turbine. In alternative embodiments, the first drive unit 4 can also be designed as an electric motor, gas turbine or the like.

Die zweite Antriebseinheit 7 ist als elektrischer Motor ausgebildet. Die zweite Antriebseinheit 7 kann in alternativen Ausführungsformen auch als elektrischer Motor, Gasturbine oder vergleichbarem ausgebildet sein.The second drive unit 7 is designed as an electric motor. In alternative embodiments, the second drive unit 7 can also be designed as an electric motor, gas turbine or the like.

Im Folgenden wird die Funktionsweise der Luftverdichtungsanlage 1 erläutert.The functioning of the air compression system 1 is explained below.

Ein Strömungsmedium strömt über eine erste Leitung 14 in das erste Verdichtungsmodul 5. Das Strömungsmedium kann Luft sein. In dem ersten Verdichtungsmodul 5 wird der Druck und die Temperatur des Strömungsmediums erhöht. Über eine zweite Leitung 15 strömt das Strömungsmedium zu einem ersten Zwischenkühler 16. Im ersten Zwischenkühler 16 wird das Strömungsmedium abgekühlt.A flow medium flows into the first compression module 5 via a first line 14. The flow medium can be air. In the first compression module 5, the pressure and the temperature of the flow medium are increased. The flow medium flows via a second line 15 to a first intermediate cooler 16. In the first intermediate cooler 16, the flow medium is cooled.

Anschließend strömt das Strömungsmedium zu dem zweiten Verdichtermodul 6. Dort wird das Strömungsmedium weiter verdichtet, wobei sich der Druck und die Temperatur erhöht. Das Strömungsmedium strömt anschließend über eine dritte Leitung 17 zu einem zweiten Zwischenkühler 18. In dem zweiten Zwischenkühler wird die Temperatur des Strömungsmediums verringert.The flow medium then flows to the second compressor module 6. There the flow medium is further compressed, with the pressure and the temperature increasing. The flow medium then flows via a third line 17 to a second intermediate cooler 18. The temperature of the flow medium is reduced in the second intermediate cooler.

Die Verdichtungsarbeit in dem Hauptluftverdichter 2 wäre somit abgeschlossen. Die weitere Verdichtungsarbeit wird in dem Booster-Luftverdichter 3 durchgeführt.The compression work in the main air compressor 2 would thus be completed. The further compression work is carried out in the booster air compressor 3 .

Dazu strömt das Strömungsmedium über eine vierte Leitung 19 in ein drittes Verdichtermodul 8. Im dritten Verdichtermodul 8 wird der Druck und die Temperatur des Strömungsmediums erhöht. Anschließend strömt das Strömungsmedium über eine fünfte Leitung 20 zu einem dritten Zwischenkühler 21, wo die Temperatur des Strömungsmediums wieder verringert wird.For this purpose, the flow medium flows via a fourth line 19 into a third compressor module 8. In the third compressor module 8, the pressure and the temperature of the flow medium are increased. The flow medium then flows via a fifth line 20 to a third intermediate cooler 21, where the temperature of the flow medium is reduced again.

Nach dem dritten Zwischenkühler 21 strömt das Strömungsmedium in ein viertes Verdichtermodul 9, wo der Druck des Strömungsmediums weiter erhöht wird, wobei dabei auch die Temperatur ansteigt.After the third intercooler 21, the flow medium flows into a fourth compressor module 9, where the pressure of the flow medium is further increased, with the temperature also rising.

Anschließend strömt das Strömungsmedium zu einem vierten Zwischenkühler 22, wo die Temperatur des Strömungsmediums verringert wird. Nach dem vierten Zwischenkühler 22 strömt das Strömungsmedium über eine sechste Leitung 23 zu einem fünften Verdichtermodul 10, wobei der Druck des Strömungsmediums erhöht wird, wobei sich die Temperatur erhöht.The flow medium then flows to a fourth intercooler 22 where the temperature of the flow medium is reduced. After the fourth intercooler 22, the flow medium flows via a sixth line 23 to a fifth Compressor module 10, wherein the pressure of the flow medium is increased, the temperature increases.

Anschließend strömt das Strömungsmedium über eine siebte Leitung 24 zu einem fünften Zwischenkühler 25, wo die Temperatur des Strömungsmediums verringert wird.The flow medium then flows via a seventh line 24 to a fifth intercooler 25, where the temperature of the flow medium is reduced.

Nach dem fünften Zwischenkühler 25 strömt das Strömungsmedium zu einem sechsten Verdichtermodul 11, wo der Druck und die Temperatur des Strömungsmediums vergrößert wird.After the fifth intercooler 25, the flow medium flows to a sixth compressor module 11, where the pressure and temperature of the flow medium is increased.

Nach dem sechsten Verdichtermodul 11 strömt das Strömungsmedium über eine achte Leitung 26 aus der Luftverdichtungsanlage heraus.After the sixth compressor module 11 , the flow medium flows out of the air compression system via an eighth line 26 .

Claims (12)

Luftverdichtungsanlage (1) für eine Luftzerlegung umfassend: - mindestens einen Hauptluftverdichter (2) (MAC), - mindestens einen Booster-Luftverdichter (3) (BAC), - mindestens eine erste Antriebseinheit (4) zum Antrieb zumindest eines Verdichtermoduls (5, 6) des Hauptluftverdichters (2) (MAC), - mindestens eine zweite Antriebseinheit (7) zum Antrieb zumindest eines Verdichtermoduls (8, 9, 10, 11) des Booster-Luftverdichter (3) (BAC) dadurch gekennzeichnet,
dass der Hauptluftverdichter (2) (MAC) einen ersten Verdichterstrang umfasst, der mit der ersten Antriebseinheit (4) drehmomentübertragend gekoppelt ist, wobei der Booster-Luftverdichter (3) (BAC) einen separaten Verdichterstrang umfasst, der mit der zweiten Antriebseinheit (7) drehmomentübertragend gekoppelt ist.Air compression system (1) for air separation, comprising: - at least one main air compressor (2) (MAC), - at least one booster air compressor (3) (BAC), - at least one first drive unit (4) for driving at least one compressor module (5, 6) of the main air compressor (2) (MAC), - at least one second drive unit (7) for driving at least one compressor module (8, 9, 10, 11) of the booster air compressor (3) (BAC) characterized,
that the main air compressor (2) (MAC) comprises a first compressor line, which is torque-transmittingly coupled to the first drive unit (4), wherein the booster air compressor (3) (BAC) comprises a separate compressor line, which is connected to the second drive unit (7) is coupled to transmit torque. Luftverdichtungsanlage (1) für eine Luftzerlegung nach Anspruch 1,
wobei der separate Verdichterstrang des Booster-Luftverdichter (3) (BAC) als Getriebeverdichter (12) mit einem Großzahnrad und mehrere an dem Großzahnrad drehmomentübertragende Planeten-Zahnräder ausgebildet ist.Air compression system (1) for air separation according to claim 1,
wherein the separate compressor train of the booster air compressor (3) (BAC) is designed as a geared compressor (12) with a large gear wheel and a plurality of planetary gear wheels transmitting torque on the large gear wheel. Luftverdichtungsanlage (1) für eine Luftzerlegung nach Anspruch 2,
wobei das Großzahnrad über eine gemeinsame zweite Welle (27) mit der zweiten Antriebseinheit (7) drehmomentübertragend gekoppelt ist.Air compression system (1) for air separation according to claim 2,
wherein the large gear wheel is coupled in a torque-transmitting manner to the second drive unit (7) via a common second shaft (27). Luftverdichtungsanlage (1) für eine Luftzerlegung nach einem der Ansprüche 1 bis 3,
wobei der Getriebeverdichter (12) mindestens zwei Planeten-Zahnräder aufweist, an dem jeweils zwei Verdichtermodule (8, 9, 10, 11) drehmomentübertragend gekoppelt sind.Air compression system (1) for air separation according to one of Claims 1 to 3,
wherein the geared compressor (12) has at least two planetary gear wheels, on each of which two compressor modules (8, 9, 10, 11) are coupled to transmit torque. Luftverdichtungsanlage (1) für eine Luftzerlegung nach einem der vorhergehenden Ansprüche 1 bis 4, wobei der Hauptluftverdichter (2) (MAC) zwei Verdichtermodule (5, 6) an dem Verdichterstrang aufweist, wobei die erste Antriebseinheit (4) und die zwei Verdichtermodule (5, 6) eine gemeinsame erste Welle (13) aufweisen, wobei die zwei Verdichtermodule (5, 6) über die gemeinsame erste Welle (13) drehmomentübertragend mit der ersten Antriebseinheit (4) gekoppelt sind. Air compression system (1) for air separation according to one of the preceding claims 1 to 4, wherein the main air compressor (2) (MAC) has two compressor modules (5, 6) on the compressor train, wherein the first drive unit (4) and the two compressor modules (5, 6) have a common first shaft (13), wherein the two compressor modules (5, 6) transmit torque to the first drive unit (4) via the common first shaft (13) are coupled. Luftverdichtungsanlage (1) für eine Luftzerlegung nach Anspruch 5,
wobei die erste Antriebseinheit (4) zwischen den zwei Verdichtermodulen (5, 6) angeordnet ist.Air compression system (1) for air separation according to claim 5,
wherein the first drive unit (4) is arranged between the two compressor modules (5, 6). Luftverdichtungsanlage (1) für eine Luftzerlegung nach einem der vorhergehenden Ansprüche,
wobei die erste Antriebseinheit (4) als Dampfturbine ausgebildet ist.Air compression system (1) for air separation according to one of the preceding claims,
wherein the first drive unit (4) is designed as a steam turbine. Luftverdichtungsanlage (1) für eine Luftzerlegung nach einem der vorhergehenden Ansprüche,
wobei die zweite Antriebseinheit (7) als Elektromotor ausgebildet ist.Air compression system (1) for air separation according to one of the preceding claims,
wherein the second drive unit (7) is designed as an electric motor. Luftverdichtungsanlage (1) für eine Luftzerlegung nach einem der vorhergehenden Ansprüche 1 - 8,
wobei die zwei Verdichtermodule (5, 6) strömungstechnisch miteinander verbunden sind und zwischen den beiden Verdichtermodulen (5, 6) ein Zwischenkühler (16) angeordnet ist, wobei der Zwischenkühler (16) zum Kühlen des im Betrieb aus dem Verdichtermodul (5) ausströmenden Prozessfluids ausgebildet ist.Air compression system (1) for air separation according to one of the preceding claims 1 - 8,
wherein the two compressor modules (5, 6) are fluidically connected to one another and an intermediate cooler (16) is arranged between the two compressor modules (5, 6), the intermediate cooler (16) for cooling the process fluid flowing out of the compressor module (5) during operation is trained. Luftverdichtungsanlage (1) für eine Luftzerlegung nach einem der vorhergehenden Ansprüche,
wobei der Booster-Luftverdichter (3) (BAC) mehrere Verdichtermodule (8, 9, 10, 11) aufweist, wobei ein Verdichtermodul (8, 9, 10, 11) strömungstechnisch mit dem Verdichtermodul (5, 6) des Hauptluftverdichters (2) (MAC) verbunden ist.Air compression system (1) for air separation according to one of the preceding claims,
wherein the booster air compressor (3) (BAC) has a plurality of compressor modules (8, 9, 10, 11), wherein a compressor module (8, 9, 10, 11) is fluidically connected to the compressor module (5, 6) of the main air compressor (2) (MAC) is connected. Luftverdichtungsanlage (1) für eine Luftzerlegung nach Anspruch 10,
wobei die zwischen dem Verdichtermodul (5, 6) des Hauptluftverdichters (2) und dem Verdichtermodul (8, 9, 10, 11) des Booster-Luftverdichters (3) ein zweiter Zwischenkühler (18) angeordnet ist.Air compression system (1) for air separation according to claim 10,
a second intermediate cooler (18) being arranged between the compressor module (5, 6) of the main air compressor (2) and the compressor module (8, 9, 10, 11) of the booster air compressor (3). Luftverdichtungsanlage (1) für eine Luftzerlegung nach einem der Ansprüche 4 bis 11,
wobei zwischen den Verdichtermodulen (8, 9, 10, 11) des Booster-Luftverdichter (3) jeweils ein Zwischenkühler (21, 22, 25) angeordnet ist.Air compression system (1) for air separation according to one of Claims 4 to 11,
an intermediate cooler (21, 22, 25) being arranged between the compressor modules (8, 9, 10, 11) of the booster air compressor (3).
EP21201814.7A 2021-10-11 2021-10-11 Air compression assembly for air separation Withdrawn EP4163500A1 (en)

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EP21201814.7A EP4163500A1 (en) 2021-10-11 2021-10-11 Air compression assembly for air separation
PCT/EP2022/077619 WO2023061813A1 (en) 2021-10-11 2022-10-05 Air compression system for an air separation process

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EP3636932A1 (en) * 2018-10-10 2020-04-15 Siemens Aktiengesellschaft Air compression assembly for air fractionation

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