CA2142440A1 - Cryogenic air separation - Google Patents
Cryogenic air separationInfo
- Publication number
- CA2142440A1 CA2142440A1 CA002142440A CA2142440A CA2142440A1 CA 2142440 A1 CA2142440 A1 CA 2142440A1 CA 002142440 A CA002142440 A CA 002142440A CA 2142440 A CA2142440 A CA 2142440A CA 2142440 A1 CA2142440 A1 CA 2142440A1
- Authority
- CA
- Canada
- Prior art keywords
- gear
- compressor
- common
- driving
- expander
- 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.)
- Abandoned
Links
- 238000000926 separation method Methods 0.000 title claims description 9
- 244000309464 bull Species 0.000 claims abstract description 12
- 230000006835 compression Effects 0.000 claims abstract description 11
- 238000007906 compression Methods 0.000 claims abstract description 11
- 239000007788 liquid Substances 0.000 claims description 6
- 239000006227 byproduct Substances 0.000 claims description 4
- 230000008878 coupling Effects 0.000 claims description 4
- 238000010168 coupling process Methods 0.000 claims description 4
- 238000005859 coupling reaction Methods 0.000 claims description 4
- 239000012530 fluid Substances 0.000 claims description 4
- 239000012263 liquid product Substances 0.000 claims description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 8
- 239000007789 gas Substances 0.000 description 5
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 238000004821 distillation Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Classifications
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- 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
- F25J3/04406—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 using a dual pressure main column system
- F25J3/04412—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 using a dual pressure main column system in a classical double column flowsheet, i.e. with thermal coupling by a main reboiler-condenser in the bottom of low pressure respectively top of high pressure column
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/12—Combinations with mechanical gearing
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- 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
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- 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
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- 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
- F25J3/04024—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 purified feed air, so-called boosted air
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- 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
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- 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
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- 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
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- 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
- F25J3/04248—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion
- F25J3/04284—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams
- F25J3/0429—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams of feed air, e.g. used as waste or product air or expanded into an auxiliary column
- F25J3/04296—Claude expansion, i.e. expanded into the main or high pressure column
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- 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
- F25J3/04248—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion
- F25J3/04284—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams
- F25J3/0429—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams of feed air, e.g. used as waste or product air or expanded into an auxiliary column
- F25J3/04303—Lachmann expansion, i.e. expanded into oxygen producing or low pressure column
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- 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
- F25J3/04248—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion
- F25J3/04284—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams
- F25J3/04309—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams of nitrogen
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- 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
- F25J3/04248—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion
- F25J3/04284—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams
- F25J3/04309—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams of nitrogen
- F25J3/04315—Lowest pressure or impure nitrogen, so-called waste nitrogen expansion
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- 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
- F25J3/04248—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion
- F25J3/04375—Details relating to the work expansion, e.g. process parameter etc.
- F25J3/04381—Details relating to the work expansion, e.g. process parameter etc. using work extraction by mechanical coupling of compression and expansion so-called companders
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- 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
- F25J3/04248—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion
- F25J3/04375—Details relating to the work expansion, e.g. process parameter etc.
- F25J3/04393—Details relating to the work expansion, e.g. process parameter etc. using multiple or multistage gas work expansion
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- 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
- F25J2200/00—Processes or apparatus using separation by rectification
- F25J2200/20—Processes or apparatus using separation by rectification in an elevated pressure multiple column system wherein the lowest pressure column is at a pressure well above the minimum pressure needed to overcome pressure drop to reject the products to atmosphere
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- 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
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- 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
- F25J2240/00—Processes or apparatus involving steps for expanding of process streams
- F25J2240/02—Expansion of a process fluid in a work-extracting turbine (i.e. isentropic expansion), e.g. of the feed stream
- F25J2240/12—Expansion of a process fluid in a work-extracting turbine (i.e. isentropic expansion), e.g. of the feed stream the fluid being nitrogen
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- 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
- F25J2250/00—Details related to the use of reboiler-condensers
- F25J2250/30—External or auxiliary boiler-condenser in general, e.g. without a specified fluid or one fluid is not a primary air component or an intermediate fluid
- F25J2250/42—One fluid being nitrogen
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- 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
- F25J2290/00—Other details not covered by groups F25J2200/00 - F25J2280/00
- F25J2290/62—Details of storing a fluid in a tank
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Separation By Low-Temperature Treatments (AREA)
Abstract
A cryogenic air separation-unit (10) comprises a number of compression stages (12, 14, 16) at least one of which is driven by two or more expander turbines (18, 20, 22) acting in parallel or series and linked for driving one or more compression stages (12) via a common or bull gear (34). One of said compression stages (12) may be linked directly to one of the expander turbines (18) via a gear (32, 36) which acts to form the output gear of the turbine and the input gear of the compressor.
Description
- 21424~10 94B110/lMB - 1 -CRYOGENIC AIR SEPARA TION
The present invention relal~s to cryogenic air separation and relates particularly, but not exclusively, to the operation of expander turbine driven compressors used in such a process.
A typical cryogenic air separation unit (ASU) comprises a number of compressors for compressing incoming air, a number of compressors for compressing nitrogen and a number of expander turbines used for expanding compressed air or nitrog-en so as to lower the temperature and pressure thereof prior to its suppty to one or other of the high pressure or low pressure distillation columns or heat exchangers. It is well known to use some of the energy released during gas expansion in the expander turbines to drive a compressor stage, however, in certain arrangements the power available from the expander turbine is insufficient to meet the requirements of the compressor. Additionally, in some arrangements, it is not possible to individually load each turbine. Alsoin some arrangements a small flow of nitrogen is required resulting in expensivestandalone compressors It is an object of the present invention to provide a cryogenic air separation apparatus which reduces and possibly eliminates both or one of the above mentioned problem.
Accordingly, the present invention provides a cryogenic air separation apparatuscomprising two or more compression stages and two or more expander turbines in which said two or more expander turbines are linked in series or parallel to drive one or more compressor stages.
Preferably, said expander turbines are linked to said compressor via a common (bull) gear, each expander turbine having an output (driving) gear for driving said common gear and said one or more compressors having an input gear driven by said common (bull) gear.
_ 21424~0 94B 1 1 0/l M B - 2 -Conveniently, said common (bull) gear comprises an externally toothed gear and said compressor input gear is driven from the same external teeth.
Advantageously, the apparatus further includes a motor for driving said common gear so as to drive said compressor as and when desired.
In a particularly useful arrangement, the apparatus further includes a generatordriven from said common gear as and when desired. Also the apparatus may include a clutch or fluid coupling to disconnect the motor or generator when desired .
In certain process conditions the motor may act as a generator.
In certain circumstances, an expander turbine may be driven by gas expanded from a liquid state or by gas taken at pressure from a condenser column.
Conveniently, the liquid gas comprises liquid product or liquid by-product.
The present invention will now be more particularly described by way of example only with reference to the accompanying drawings, in which:
Figure 1 is a schematic representation of a cryogenic air separation unit incorporating features of the present invention, and Figures 2, 3 and 4 illustrate three alternative arrangements of the present invention.
Referring briefly to Figure 1, a cryogenic air separation unit (ASU) 10 comprises a number of compression stages 12, 14, 16 for compressing incoming air A and a number of expander turbines 18, 20, 22 for expanding compressed air so as to reduce its temperature to that required in various stages of the cryogenic distillation process. Further components include a heat exchanger 24 and high _ 21424~0 94B1 10/lMB - 3 -and low pressure condenser columns-26, 28. The actual operation of the ASU
forms no part of the present application and is therefore not described in detail herein, however, the following brief explanation is provided for the purpose of ensuring the readers understanding of Figure 1 attached hereto: Air is compressed in one or more compression stages 12 and part is passed through heat exchanger 24 and then direct to the high pressure column 26 so as to produce 'strip' nitrogen for the low pressure column. Surplus air is compressed by compression stage 14 and then split with part being directed to expansion turbine 18 for expansion and cooling therein prior to its introduction into the low pressure rectification column. Surplus air from compression stage 14 is directedto a compression stage 16, passed through heat exchanger 24 but removed part way therethrough and passed to expansion turbine 20 prior to being passed to the high pressure column where it supplements the airflow from compression stage 12. A supplementary turbine 22 driven by an expanded source of liquid product or by-product 30 may be provided for reasons which will be explained in detail late herein. Alternatively, a turbine 17 may be provided for expanding high pressure nitrogen directly from one or other of the two columns. The compressors 12, 14, 16 and turbines 18, 20, 22 are provided with respective driven and driving gears 32, 36 connected in a manner described below.
The operation of the present method of compressor driving is probably best illustrated by reference to Figures 2 to 4. In Figure 2, it will be seen that the driving gear 32 of one or other of the compressors 12, 14, 16 (hereinafter referred to as the compressor 12) is engaged for being driven by a bull or common gear 34. Two or more of the expander turbines 18, 20, 22 are connected for driving the bull gear 34 via driving gears 36. One or other of theoutput gears 36 may form the input gear 32 of the compressor 12. In the Figure 3 arrangement, the third expansion turbine 22 is added to the driving force and connected for driving the bull gear 34 via output gear 36. A further additional feature is shown in Figure 4 and comprises an optional motor/generator combination 38, 40. Such components may be provided either separately or together and when provided together may be provided as individual units or combined together as one motor/generator combination and may include a clutch or fluid coupling 19 to disconnect the motor/generator Operation of the present apparatus is simple with two or more turbines 18, 20, 22 driving bull gear 34 which in turn drives compressor 12 and/or compressor 14, 16, 17. The combined output from the turbines being sufficient to drive the compressor. Supplementary turbines 17 and 22 are added in the Figure 3 embodiment and acts to boost the driving force as and when desired by allowing expanded product or by-product gas to pass therethrough so as to drive the turbines 17, 22 and its associated driving gear 36 in a manner which facilitates the driving of bull gear 34. The provision of the motor/generator combination, shown in Figure 4, allows the motor to be used to boost the driving force of the turbines when the driving force is undesirably reduced, such as, for example when the ASU plant is turned down. When surplus energy is available, power may be generated by driving generator 40 directly form bull gear 34. As stated earlier, the bullgear may be connected to the motor generator 38, 40 by a clutch or fluid coupling which may be used to disconnect the motor generator when the expander power matches the compressor power and power balance is achieved.
The present invention relal~s to cryogenic air separation and relates particularly, but not exclusively, to the operation of expander turbine driven compressors used in such a process.
A typical cryogenic air separation unit (ASU) comprises a number of compressors for compressing incoming air, a number of compressors for compressing nitrogen and a number of expander turbines used for expanding compressed air or nitrog-en so as to lower the temperature and pressure thereof prior to its suppty to one or other of the high pressure or low pressure distillation columns or heat exchangers. It is well known to use some of the energy released during gas expansion in the expander turbines to drive a compressor stage, however, in certain arrangements the power available from the expander turbine is insufficient to meet the requirements of the compressor. Additionally, in some arrangements, it is not possible to individually load each turbine. Alsoin some arrangements a small flow of nitrogen is required resulting in expensivestandalone compressors It is an object of the present invention to provide a cryogenic air separation apparatus which reduces and possibly eliminates both or one of the above mentioned problem.
Accordingly, the present invention provides a cryogenic air separation apparatuscomprising two or more compression stages and two or more expander turbines in which said two or more expander turbines are linked in series or parallel to drive one or more compressor stages.
Preferably, said expander turbines are linked to said compressor via a common (bull) gear, each expander turbine having an output (driving) gear for driving said common gear and said one or more compressors having an input gear driven by said common (bull) gear.
_ 21424~0 94B 1 1 0/l M B - 2 -Conveniently, said common (bull) gear comprises an externally toothed gear and said compressor input gear is driven from the same external teeth.
Advantageously, the apparatus further includes a motor for driving said common gear so as to drive said compressor as and when desired.
In a particularly useful arrangement, the apparatus further includes a generatordriven from said common gear as and when desired. Also the apparatus may include a clutch or fluid coupling to disconnect the motor or generator when desired .
In certain process conditions the motor may act as a generator.
In certain circumstances, an expander turbine may be driven by gas expanded from a liquid state or by gas taken at pressure from a condenser column.
Conveniently, the liquid gas comprises liquid product or liquid by-product.
The present invention will now be more particularly described by way of example only with reference to the accompanying drawings, in which:
Figure 1 is a schematic representation of a cryogenic air separation unit incorporating features of the present invention, and Figures 2, 3 and 4 illustrate three alternative arrangements of the present invention.
Referring briefly to Figure 1, a cryogenic air separation unit (ASU) 10 comprises a number of compression stages 12, 14, 16 for compressing incoming air A and a number of expander turbines 18, 20, 22 for expanding compressed air so as to reduce its temperature to that required in various stages of the cryogenic distillation process. Further components include a heat exchanger 24 and high _ 21424~0 94B1 10/lMB - 3 -and low pressure condenser columns-26, 28. The actual operation of the ASU
forms no part of the present application and is therefore not described in detail herein, however, the following brief explanation is provided for the purpose of ensuring the readers understanding of Figure 1 attached hereto: Air is compressed in one or more compression stages 12 and part is passed through heat exchanger 24 and then direct to the high pressure column 26 so as to produce 'strip' nitrogen for the low pressure column. Surplus air is compressed by compression stage 14 and then split with part being directed to expansion turbine 18 for expansion and cooling therein prior to its introduction into the low pressure rectification column. Surplus air from compression stage 14 is directedto a compression stage 16, passed through heat exchanger 24 but removed part way therethrough and passed to expansion turbine 20 prior to being passed to the high pressure column where it supplements the airflow from compression stage 12. A supplementary turbine 22 driven by an expanded source of liquid product or by-product 30 may be provided for reasons which will be explained in detail late herein. Alternatively, a turbine 17 may be provided for expanding high pressure nitrogen directly from one or other of the two columns. The compressors 12, 14, 16 and turbines 18, 20, 22 are provided with respective driven and driving gears 32, 36 connected in a manner described below.
The operation of the present method of compressor driving is probably best illustrated by reference to Figures 2 to 4. In Figure 2, it will be seen that the driving gear 32 of one or other of the compressors 12, 14, 16 (hereinafter referred to as the compressor 12) is engaged for being driven by a bull or common gear 34. Two or more of the expander turbines 18, 20, 22 are connected for driving the bull gear 34 via driving gears 36. One or other of theoutput gears 36 may form the input gear 32 of the compressor 12. In the Figure 3 arrangement, the third expansion turbine 22 is added to the driving force and connected for driving the bull gear 34 via output gear 36. A further additional feature is shown in Figure 4 and comprises an optional motor/generator combination 38, 40. Such components may be provided either separately or together and when provided together may be provided as individual units or combined together as one motor/generator combination and may include a clutch or fluid coupling 19 to disconnect the motor/generator Operation of the present apparatus is simple with two or more turbines 18, 20, 22 driving bull gear 34 which in turn drives compressor 12 and/or compressor 14, 16, 17. The combined output from the turbines being sufficient to drive the compressor. Supplementary turbines 17 and 22 are added in the Figure 3 embodiment and acts to boost the driving force as and when desired by allowing expanded product or by-product gas to pass therethrough so as to drive the turbines 17, 22 and its associated driving gear 36 in a manner which facilitates the driving of bull gear 34. The provision of the motor/generator combination, shown in Figure 4, allows the motor to be used to boost the driving force of the turbines when the driving force is undesirably reduced, such as, for example when the ASU plant is turned down. When surplus energy is available, power may be generated by driving generator 40 directly form bull gear 34. As stated earlier, the bullgear may be connected to the motor generator 38, 40 by a clutch or fluid coupling which may be used to disconnect the motor generator when the expander power matches the compressor power and power balance is achieved.
Claims (10)
1. A cryogenic air separation apparatus comprising two or more compression stages and two or more expander turbines in which said two or more expander turbines are linked in parallel or series to drive one or more compressor stages.
2. An apparatus as claimed in Claim 1 in which said expander turbines are linked to said compressor via a common (bull) gear, each expander turbine having an output (driving) gear for driving said common gear and said compressor or compressors having an input gear driven by said common (bull) gear.
3. An apparatus as claimed in Claim 1 or Claim 2 in which said common gear comprises an externally toothed gear and said compressor input gear is driven from said external teeth.
4. An apparatus as claimed in any one of the preceding claims further including a motor for driving said common gear so as to drive said compressor as and when desired.
5. An apparatus as claimed in any one of the preceding claims further including a generator driven from said common gear as and when desired.
6. An apparatus as claimed in any one of the preceding claims further including a clutch or fluid coupling for disconnecting said motor and or generator from said common gear.
7. An apparatus as claimed in any one of Claims 1 to 6 in which an expander turbine is driven by gas expanded from a liquid state.
8. An apparatus as claimed in Claim 7 in which said liquid gas comprises liquid product or liquid by-product.
9. An apparatus as claimed in any one of the preceding claims in which the output (driving) gear of an expander turbine forms the input gear of said compressor.
10. An apparatus substantially as described herein with reference to and as illustrated in Figures 1 to 4 of the accompanying drawings.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9404991A GB9404991D0 (en) | 1994-03-15 | 1994-03-15 | Cryogenic air separation |
GB9404991.3 | 1994-03-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA2142440A1 true CA2142440A1 (en) | 1995-09-16 |
Family
ID=10751849
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002142440A Abandoned CA2142440A1 (en) | 1994-03-15 | 1995-02-13 | Cryogenic air separation |
Country Status (9)
Country | Link |
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EP (1) | EP0672877A1 (en) |
AU (1) | AU1231595A (en) |
CA (1) | CA2142440A1 (en) |
CZ (1) | CZ65095A3 (en) |
GB (1) | GB9404991D0 (en) |
HU (1) | HU9500720D0 (en) |
PL (1) | PL307668A1 (en) |
SK (1) | SK32095A3 (en) |
ZA (1) | ZA951696B (en) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5924307A (en) * | 1997-05-19 | 1999-07-20 | Praxair Technology, Inc. | Turbine/motor (generator) driven booster compressor |
US5901579A (en) * | 1998-04-03 | 1999-05-11 | Praxair Technology, Inc. | Cryogenic air separation system with integrated machine compression |
US6116027A (en) * | 1998-09-29 | 2000-09-12 | Air Products And Chemicals, Inc. | Supplemental air supply for an air separation system |
US6393865B1 (en) * | 2000-09-27 | 2002-05-28 | Air Products And Chemicals, Inc. | Combined service main air/product compressor |
US6484533B1 (en) * | 2000-11-02 | 2002-11-26 | Air Products And Chemicals, Inc. | Method and apparatus for the production of a liquid cryogen |
DE10060678A1 (en) * | 2000-12-06 | 2002-06-13 | Linde Ag | Machine system for work relaxation of two process streams |
DE10139097A1 (en) * | 2001-08-09 | 2003-02-20 | Linde Ag | Method and device for producing oxygen by low-temperature separation of air |
US20030123972A1 (en) * | 2001-10-09 | 2003-07-03 | Quetel Ralph L. | Method of standardizing compressor design |
JP4242131B2 (en) | 2002-10-18 | 2009-03-18 | パナソニック株式会社 | Refrigeration cycle equipment |
DE102006012241A1 (en) * | 2006-03-15 | 2007-09-20 | Linde Ag | Method and apparatus for the cryogenic separation of air |
EP2369281A1 (en) * | 2010-03-09 | 2011-09-28 | Linde Aktiengesellschaft | Method and device for cryogenic decomposition of air |
KR101603218B1 (en) | 2010-03-16 | 2016-03-15 | 한화테크윈 주식회사 | Turbine system |
AU2011283126C1 (en) | 2010-07-30 | 2017-09-14 | Exxonmobil Upstream Research Company | Systems and methods for using multiple cryogenic hydraulic turbines |
CN102758653B (en) * | 2011-04-28 | 2015-06-24 | 中国科学院工程热物理研究所 | Multilevel centripetal turbine system |
EP3014077B1 (en) | 2013-06-28 | 2018-01-17 | Mitsubishi Heavy Industries Compressor Corporation | Axial flow expander |
WO2014210409A1 (en) | 2013-06-28 | 2014-12-31 | Exxonmobil Upstream Research Company | Systems and methods of utilizing axial flow expanders |
US20150211539A1 (en) | 2014-01-24 | 2015-07-30 | Air Products And Chemicals, Inc. | Systems and methods for compressing air |
US20160245585A1 (en) * | 2015-02-24 | 2016-08-25 | Henry E. Howard | System and method for integrated air separation and liquefaction |
CN111406192B (en) * | 2017-11-29 | 2022-04-08 | 乔治洛德方法研究和开发液化空气有限公司 | Cryogenic rectification method and apparatus for producing pressurized air by expander booster braked in conjunction with nitrogen expander |
CN108223031A (en) * | 2017-12-26 | 2018-06-29 | 王尚锦 | S-CO2Brayton cycle turbine, compressor and generator integral type unit |
CN110985337A (en) * | 2019-12-02 | 2020-04-10 | 东方电气集团东方汽轮机有限公司 | Integrated driving unit and operation method thereof |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3477239A (en) * | 1967-05-16 | 1969-11-11 | Messer Griesheim Gmbh | Multistage compression drive in gas separation |
DE4234739C1 (en) * | 1992-10-15 | 1993-11-25 | Gutehoffnungshuette Man | Gearbox multi-shaft turbo compressor with feedback stages |
-
1994
- 1994-03-15 GB GB9404991A patent/GB9404991D0/en active Pending
-
1995
- 1995-01-26 EP EP95300488A patent/EP0672877A1/en not_active Withdrawn
- 1995-02-13 CA CA002142440A patent/CA2142440A1/en not_active Abandoned
- 1995-02-17 AU AU12315/95A patent/AU1231595A/en not_active Abandoned
- 1995-03-01 ZA ZA951696A patent/ZA951696B/en unknown
- 1995-03-10 SK SK320-95A patent/SK32095A3/en unknown
- 1995-03-10 HU HU9500720A patent/HU9500720D0/en unknown
- 1995-03-13 CZ CZ95650A patent/CZ65095A3/en unknown
- 1995-03-13 PL PL95307668A patent/PL307668A1/en unknown
Also Published As
Publication number | Publication date |
---|---|
SK32095A3 (en) | 1995-10-11 |
HU9500720D0 (en) | 1995-05-29 |
EP0672877A1 (en) | 1995-09-20 |
CZ65095A3 (en) | 1996-01-17 |
PL307668A1 (en) | 1995-09-18 |
GB9404991D0 (en) | 1994-04-27 |
ZA951696B (en) | 1996-02-08 |
AU1231595A (en) | 1995-09-21 |
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