Process and apparatus for separating air using a split heat exchanger

Abstract

Process and apparatus for the separation of a compressed feed air stream to produce an oxygen product using a distillation column having a lower-pressure column and a higher-pressure column, a higher-pressure heat exchanger and a lower-pressure heat exchanger where the gaseous nitrogen expander receives a nitrogen-enriched fraction from a position intermediate the warmer end and the colder end of the higher-pressure heat exchanger.

Claims

1. A process for the separation of a compressed feed air stream to produce an oxygen product and optionally a nitrogen product, the process comprising: providing a multi-column distillation system comprising a lower-pressure column and a higher-pressure column; passing a first portion of the compressed feed air stream into a first end of a first heat exchanger section, cooling the first portion of the compressed feed air stream in the first heat exchanger section, and withdrawing the first portion of the compressed feed air stream from a second end of the first heat exchanger section passing the first portion of the compressed feed air stream withdrawn from the second end of the first heat exchanger section to at least one of the higher-pressure column or the lower-pressure column; passing a second portion of the compressed feed air stream into a first end of a second heat exchanger section, cooling the second portion of the compressed feed air stream in the second heat exchanger section, and withdrawing the second portion from a second end of the second heat exchanger section passing the second portion of the compressed feed air stream withdrawn from the second end of the second heat exchanger section to the higher-pressure column; withdrawing an oxygen-enriched fraction from the higher-pressure column; passing the oxygen-enriched fraction withdrawn from the higher-pressure column to the lower-pressure column; withdrawing an oxygen-rich fraction from the lower-pressure column; passing the oxygen-rich fraction withdrawn from the lower-pressure column to the second end of the first heat exchanger section, heating the oxygen-rich fraction in the first heat exchanger section, and withdrawing the oxygen-rich fraction from the first end of the first heat exchanger section as the oxygen product; withdrawing a nitrogen-enriched fraction from the higher-pressure column; passing the nitrogen-enriched fraction withdrawn from the higher-pressure column to the second end of the first heat exchanger section, heating the nitrogen-enriched fraction in the first heat exchanger section, and withdrawing the nitrogen-enriched fraction from a position intermediate the first end and the second end of the first heat exchanger section; and expanding the nitrogen-enriched fraction withdrawn from the position intermediate the first end and the second end of the first heat exchanger section in an expander to produce work and reduce the pressure of the nitrogen-enriched fraction; withdrawing a nitrogen-rich byproduct from the lower-pressure column; passing a first fraction of the nitrogen-rich byproduct withdrawn from the lower-pressure column to a first end of a first subcooler heat exchanger section, heating the first fraction of the nitrogen-rich byproduct in the first subcooler heat exchanger section, and withdrawing the first fraction of the nitrogen-rich byproduct from a second end of the first subcooler heat exchanger section; passing a first portion of the nitrogen-rich byproduct from the second end of the first subcooler heat exchanger section to the second end of the first heat exchanger section, heating the first portion of the nitrogen-rich byproduct in the first heat exchanger section, and withdrawing the first portion of the nitrogen-rich byproduct from the first end of the first heat exchanger section as a first nitrogen-rich discharge byproduct gas; passing a second portion of the first fraction of the nitrogen-rich byproduct from the second end of the first subcooler heat exchanger section to the second end of the second heat exchanger section, heating the second portion of the first fraction of the nitrogen-rich byproduct in the second heat exchanger section, and withdrawing the second portion of the first fraction of the nitrogen-rich byproduct from the first end of the second heat exchanger section as a third nitrogen-rich discharge product gas; wherein passing a second fraction of the nitrogen-rich byproduct withdrawn from the lower-pressure column to a first end of a second subcooler heat exchanger section, heating the second fraction of the nitrogen-rich byproduct in the second subcooler heat exchanger section, and withdrawing the second fraction of the nitrogen-rich byproduct from a second end of the second subcooler heat exchanger section; wherein passing the second fraction of the nitrogen-rich byproduct from the second end of the second subcooler heat exchanger section to the second end of the second heat exchanger section, heating the second fraction of the nitrogen-rich byproduct in the second heat exchanger section, and withdrawing the second fraction of the nitrogen-rich byproduct from the first end of the second heat exchanger section as a second nitrogen-rich discharge byproduct gas; wherein the expanded nitrogen-enriched fraction or a first portion thereof is passed to the second end of the second heat exchanger section, heated in the second heat exchanger section, and withdrawn from the first end of the second heat exchanger section; and wherein the second portion of the first fraction of the nitrogen-rich byproduct passed to the second end of the second heat exchanger section and the expanded nitrogen-enriched fraction or first portion thereof passed to the second end of the second heat exchanger section are blended at a location that is upstream of the second heat exchanger section and downstream of the first and second subcooler heat exchanger sections and subsequently passed together to the second end of the second heat exchanger section.

2. The process according to claim 1 wherein the pressure of the second portion of the compressed feed air stream is less than the pressure of the first portion of the compressed air feed stream.

3. The process according to claim 1 wherein a higher-pressure heat exchanger comprises the first heat exchanger section; and wherein a lower-pressure heat exchanger comprises the second heat exchanger section, wherein the maximum operating pressure in the lower-pressure heat exchanger is lower than the maximum operating pressure in the higher-pressure heat exchanger.

4. The process according to claim 1 further comprising: passing a third portion of the compressed feed air stream into the first end of the first heat exchanger section, cooling the third portion of the compressed feed air stream in the first heat exchanger section, and withdrawing the third portion of the compressed air feed stream from a position intermediate the first end and the second end of the first heat exchanger section; expanding the third portion of the compressed feed air stream withdrawn from the position intermediate the first end and the second end of the first heat exchanger section in a second expander to produce work and reduce the pressure of the third portion of the compressed feed air stream; and passing the third portion after expanding to at least one of the higher-pressure column or the lower-pressure column.

5. The process according to claim 4 wherein the second portion of the compressed feed air stream withdrawn from the second end of the second heat exchanger section and the third portion after expanding are blended prior to each being passed together to the higher-pressure column.

6. The process according to claim 1 wherein a nitrogen product is produced, the process further comprising: withdrawing a nitrogen-rich fraction from the higher-pressure column; passing a first portion of the nitrogen-rich fraction to a reboiler-condenser of the multi-column distillation system, condensing the first portion of the nitrogen-rich fraction in the reboiler-condenser, and withdrawing the first portion of the nitrogen-rich fraction from the reboiler-condenser; passing a part of the first portion of the nitrogen-rich fraction withdrawn from the reboiler-condenser to the second end of the second subcooler heat exchanger section, cooling the part of the first portion of the nitrogen-rich fraction in the second subcooler heat exchanger section, and withdrawing the part of the first portion of the nitrogen-rich fraction from the first end of the second subcooler heat exchanger section; passing the part of the first portion of the nitrogen-rich fraction withdrawn from the first end of the second subcooler heat exchanger section to the lower-pressure column; and passing a second portion of the nitrogen-rich fraction to the second end of the second heat exchanger section, heating the second portion of the nitrogen-rich fraction in the second heat exchanger section, and withdrawing the second portion of the nitrogen-rich fraction from the first end of the second heat exchanger section as the nitrogen product.

7. The process of claim 1, wherein the second portion of the first fraction of the nitrogen-rich byproduct passed to the second end of the second heat exchanger section and the expanded nitrogen-enriched fraction or first portion thereof passed to the second end of the second heat exchanger section that are blended at the location that is upstream of the second heat exchanger section and downstream of the first and second subcooler heat exchanger sections and subsequently passed together to the second end of the second heat exchanger section is performed such that the first portion of the first fraction of the nitrogen-rich byproduct is not mixed with the expanded nitrogen-enriched fraction or first portion thereof and is not passed through the second heat exchanger section after being output from the first subcooler heat exchanger section.

8. The process of claim 1, wherein the second portion of the first fraction of the nitrogen-rich byproduct passed to the second end of the second heat exchanger section and the expanded nitrogen-enriched fraction or first portion thereof passed to the second end of the second heat exchanger section that are blended at the location that is upstream of the second heat exchanger section and downstream of the first and second subcooler heat exchanger sections and subsequently passed together to the second end of the second heat exchanger section is performed in accordance with a blending process that includes: blending the expanded nitrogen-enriched fraction with the first fraction of the nitrogen-rich byproduct to form a nitrogen-rich mixture upstream of the first and second heat exchange sections and downstream of the first subcooler heat exchanger section and subsequently splitting the nitrogen-rich mixture such that a first portion of the nitrogen-rich mixture including the first portion of the first fraction of the nitrogen-rich byproduct and a second portion of the expanded nitrogen-enriched fraction is passed to the second end of the first heat exchanger section and a second portion of the nitrogen-rich mixture including the first portion of the first fraction of the nitrogen-rich byproduct and the first portion of the expanded nitrogen-enriched fraction is passed to the second end of the second heat exchanger section.

Description

BRIEF DESCRIPTION OF SEVERAL VIEWS OF THE DRAWINGS

(1) FIG. 1 is a process flow diagram for the present process for separating a compressed feed air stream to produce an oxygen product with high-pressure and low-pressure heat exchangers.

(2) FIGS. 2A-C are other process flow diagrams for the present process for separating a compressed feed air stream to produce an oxygen product with high-pressure and low-pressure heat exchangers.

(3) FIGS. 3A-D are process flow diagrams for various heat exchanger networks for the present process.

(4) FIG. 4 is a process flow diagram for the present process for separating a compressed feed air stream to produce an oxygen product with high-pressure and low-pressure heat exchangers.

(5) FIG. 5 is a process flow diagram for a comparative process for separating a compressed feed air stream to produce an oxygen product.

(6) FIG. 6 is a process flow diagram for a prior art process for separating a compressed feed air stream to produce an oxygen product.

(7) FIG. 7 is a process flow diagram for a comparative process for separating a compressed feed air stream to produce an oxygen product.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

(8) The ensuing detailed description provides preferred exemplary embodiments only, and is not intended to limit the scope, applicability, or configuration of the invention. Rather, the ensuing detailed description of the preferred exemplary embodiments will provide those skilled in the art with an enabling description for implementing the preferred exemplary embodiments of the invention, it being understood that various changes may be made in the function and arrangement of elements without departing from the scope of the invention as defined by the claims.

(9) The articles a and an as used herein mean one or more when applied to any feature in embodiments of the present invention described in the specification and claims. The use of a and an does not limit the meaning to a single feature unless such a limit is specifically stated. The article the preceding singular or plural nouns or noun phrases denotes a particular specified feature or particular specified features and may have a singular or plural connotation depending upon the context in which it is used.

(10) The adjective any means one, some, or all indiscriminately of whatever quantity.

(11) The term and/or placed between a first entity and a second entity includes any of the meanings of (1) only the first entity, (2) only the second entity, and (3) the first entity and the second entity. The term and/or placed between the last two entities of a list of 3 or more entities means at least one of the entities in the list including any specific combination of entities in this list. For example, A, B and/or C has the same meaning as A and/or B and/or C and comprises the following combinations of A, B and C: (1) only A, (2) only B, (3) only C, (4) A and B and not C, (5) A and C and not B, (6) B and C and not A, and (7) A and B and C.

(12) The phrase at least one of preceding a list of features or entities means one or more of the features or entities in the list of entities, but not necessarily including at least one of each and every entity specifically listed within the list of entities and not excluding any combinations of entities in the list of entities. For example, at least one of A, B, or C (or equivalently at least one of A, B, and C or equivalently at least one of A, B, and/or C) has the same meaning as A and/or B and/or C and comprises the following combinations of A, B and C: (1) only A, (2) only B, (3) only C, (4) A and B and not C, (5) A and C and not B, (6) B and C and not A, and (7) A and B and C.

(13) The term plurality means two or more than two.

(14) The phrase at least a portion means a portion or all. The at least a portion of a stream may have the same composition with the same concentration of each of the species as the stream from which it is derived. The at least a portion of a stream may have a different concentration of species than that of the stream from which it is derived. The at least a portion of a stream may include only specific species of the stream from which it is derived.

(15) As used herein a divided portion of a stream is a portion having the same chemical composition and species concentrations as the stream from which it was taken.

(16) As used herein a separated portion of a stream is a portion having a different chemical composition and different species concentrations than the stream from which it was taken.

(17) As used herein, first, second, third, etc. are used to distinguish from among a plurality of steps and/or features, and is not indicative of the total number, or relative position in time and/or space unless expressly stated as such.

(18) The term depleted means having a lesser mole % concentration of the indicated component than the original stream from which it was formed. Depleted does not mean that the stream is completely lacking the indicated component.

(19) The terms rich or enriched means having a greater mole % concentration of the indicated component than the original stream from which it was formed.

(20) As used herein, indirect heat transfer is heat transfer from one stream to another stream where the streams are not mixed together. Indirect heat transfer includes, for example, transfer of heat from a first fluid to a second fluid in a heat exchanger where the fluids are separated by plates or tubes.

(21) As used herein, direct heat transfer is heat transfer from one stream to another stream where the streams are intimately mixed together. Direct heat transfer includes, for example, humidification where water is sprayed directly into a hot air stream and the heat from the air evaporates the water.

(22) Illustrative embodiments of the invention are described below. While the invention is susceptible to various modifications and alternative forms, specific embodiments thereof have been shown by way of example in the drawings and are herein described in detail. It should be understood, however that the description herein of specific embodiments is not intended to limit the invention to the particular forms disclosed, but on the contrary, the invention is to cover all modifications, equivalents, and alternatives falling within the scope of the invention as defined by the appended claims.

(23) For the purposes of simplicity and clarity, detailed descriptions of well-known devices, circuits, and methods are omitted so as not to obscure the description of the present process and apparatus with unnecessary detail.

(24) The present process and apparatus are described with reference to the figures, wherein like reference numbers refer to like elements throughout the figures. Reference numbers for common elements in the figures may be included without explicit description of the common element when discussing each figure. The understanding of the common elements is readily understood from the description of the elements in a related figure.

(25) FIGS. 1, 2A-C, 3A-D, and 4, illustrate various embodiments of the present process and apparatus for separation of a compressed feed air stream 105 to produce an oxygen product 170, and an optional nitrogen product 180. The figures illustrate both required and optional features of the present process and apparatus.

(26) The compressed feed air stream 105 may be formed by compressing air 100 in a main air compressor 102 and removing impurities, such as CO.sub.2 and H.sub.2O from the air in adsorption unit 104.

(27) The compressed feed air stream 105 is divided into two or more portions. A first portion 107a may be compressed in one or more booster compressors 110 and the compressed first portion 107b passed into a first (warmer) end of a first heat exchanger section 184. The first portion 107b is cooled in the first heat exchanger section 184, and subsequently withdrawn from a second (colder) end of the first heat exchanger section 184. The compressed first portion 107b may be at least partially condensed in the first heat exchanger section 184. The thermodynamic state of the fluid (107c) leaving the second (colder) end of heat exchanger section 184 is generally all liquid for any pressure below the critical pressure of air. For pressures greater than the critical pressure of air, the temperature is generally as cold or colder than the critical temperature (approximately 140 C.) and preferably below 160 C. The first heat exchanger section 184 may be part or all of a so-called higher-pressure heat exchanger. The higher-pressure heat exchanger may be a so-called plate-fin heat exchanger or any other type of suitable heat exchanger known in the art.

(28) The first portion 107c withdrawn from the second (colder) end of the first heat exchanger section 184 is passed to a multi-column separation system comprising a lower-pressure column 188 and a higher-pressure column 190. The first portion 107c may be passed to the higher-pressure column 190 and/or the lower-pressure column of the multi-column separation system. The first portion 107c may be a liquid stream, a supercritical dense fluid, or a partially condensed stream. In FIGS. 1, 2A-C, 3A-D, and 4, the first portion 107c is passed to the higher-pressure column 190. The first portion 107c withdrawn from the second (colder) end of the heat exchanger 184 may be expanded prior to being passed to the higher-pressure column 190 and/or the lower-pressure column 188. The first portion 107c of the compressed feed air stream 105 may be expanded in a valve 112, dense fluid expander, or other device known in the art to expand a fluid. The first portion 107c may is introduced into the higher-pressure column 190 and/or the lower-pressure column 188 as a predominantly liquid air feed. Alternatively (not shown) the first portion 107c may be cooled in first subcooler heat exchange section 192, supplementing or replacing stream 124. In yet another alternative (not shown), the first portion 107c may be cooled in the second subcooler heat exchange section 194.

(29) A second portion 108a of the compressed feed air stream 105 is passed into a first (warmer) end of a second heat exchanger section 186. The pressure of the second portion 108a of the compressed feed air stream 105 may be less than the pressure of the first portion 107b of the compressed feed air stream (105). The second portion 108a is cooled in the second heat exchanger section 186, and subsequently withdrawn from a second (colder) end of the second heat exchanger section 186. The thermodynamic state of the fluid leaving the second (colder) end of the second heat exchanger section 186 is generally subcritical pressure, typically 4 to 10 atmospheres pressure, and generally no more than 10 mole % liquid, and preferably no more than 3 mole % liquid. The second heat exchanger section 186 may be part or all of a so-called lower-pressure core heat exchanger. The lower-pressure core heat exchanger may be a so-called plate-fin heat exchanger or any other type of heat exchanger known in the art.

(30) The lower-pressure heat exchanger may have a lower operating pressure rating than the higher-pressure heat exchanger. As a result, the lower-pressure heat exchanger may be a lower cost unit than the higher-pressure heat exchanger. Capital cost savings for the heat exchanger system can be achieved for heat exchanger systems using a higher-pressure heat exchanger and a lower-pressure heat exchanger as compared to a heat exchanger system where all of the heat exchangers are rated for higher pressure operation.

(31) The first heat exchanger section 184 and the second heat exchanger section 186 are part of physically and thermodynamically separate heat exchangers. A first heat exchanger comprises first exchanger section 184 and the second heat exchanger comprises the second heat exchanger section 186. The first heat exchanger may be rated for higher pressures than the second heat exchanger. Though it is obvious to one of ordinary skill in the art, the first heat exchanger section is also physically and thermodynamically separate from the second heat exchanger section.

(32) The second portion 108b withdrawn from the second (colder) end of the second heat exchanger section 186 is passed to the higher-pressure column 190 of the multi-column separation system.

(33) As shown in FIGS. 1, 2A, 2B, 2C, and 4, a third portion 109a of the compressed feed air stream 105 may be compressed in one or more booster compressors 114 and passed into the first (warmer) end of the first heat exchanger section 184. The third portion 109b may be cooled in the first heat exchanger section 184, and subsequently withdrawn from a position intermediate the first (warmer) end and the second (colder) end of the first heat exchanger section 184.

(34) While booster compressor 110 and booster compressor 114 are shown as separate machines in FIGS. 1, 2A, 2B, 2C, and 4, the two booster compressors can be a single machine. Both the high pressure air stream 107b and the medium pressure air stream 109b may be at the same pressure and come from the final stage discharge of the single booster compressor. Alternatively, stream 109b may be discharged from an intermediate stage of a single multi-stage booster compressor and stream 107b from the final stage of the single multi-stage booster compressor. The booster compressors may be driven by one or both of expander 132 or expander 116.

(35) The third portion 109c withdrawn from the position intermediate the first (warmer) end and the second (colder) end of the first heat exchanger section 184 may be expanded in an expander 116 where it is further cooled, while producing work. The third portion 109d after expanding may be passed to the higher-pressure column 190 and/or the lower-pressure column 188. Expander 116 may be a dissipative, generator-loaded, or process-loaded expander.

(36) As shown in FIGS. 1, 2A-C, and 4, the third portion 109d after expanding and the second portion 108b may be blended prior to being passed to the higher-pressure column 190. The combined stream comprising the second portion 108b and third portion 109d may be introduced as a predominantly vapor feed air into the higher-pressure column 190 at an elevation in the higher-pressure column 190 below that of the first portion 107c of the compressed feed air stream 105.

(37) As shown in FIGS. 1, 2A-C, and 4, an oxygen-enriched fraction 122 is withdrawn as a liquid from the bottom section of the higher-pressure column 190 and passed to a lower-pressure column 188 of the multi-column separation system. The oxygen-enriched fraction 122 may be introduced into a middle section of the lower-pressure column 188.

(38) The higher-pressure column 190 and the lower-pressure column 188 are each distillation-type columns. They can be constructed of systems and materials that are well known in the art (for example: sieve trays, bubble-cap trays, valve trays, random packing, structured packing). The higher-pressure column 190 is so-called higher-pressure because it has an operating pressure higher than the lower-pressure column 188. The lower-pressure column 188 is so-called lower-pressure because it has an operating pressure lower than the higher-pressure column 190. The multi-column separation system may also include one or more additional columns for producing an argon byproduct. At least one additional column may be a standalone column, or part of the lower pressure column 188 where a physical barrier is installed in the lower-pressure column to separate the sections in the lower pressure column.

(39) As shown in FIGS. 1, 2A-C, and 4, an oxygen-rich fraction 166 is withdrawn from a bottom section of the lower pressure column 188. The oxygen-rich fraction 166 is passed to the second (colder) end of the first heat exchanger section 184, heated in the first heat exchanger section 184, and subsequently withdrawn from the first (warmer) end of the first heat exchanger section 184 as oxygen product 170. The pressure of the oxygen-rich fraction 166 withdrawn from the lower pressure column 188 may be increased by passing the oxygen-rich fraction 166 through pump 168. The oxygen-rich fraction 166 may be a liquid stream or a supercritical dense fluid.

(40) As shown in FIGS. 1, 2A-C, and 4, a nitrogen-enriched fraction 128a is withdrawn from the higher-pressure column 190. As shown in the figures, the nitrogen-enriched fraction 128a may be withdrawn from the higher-pressure column 190 at an elevation below the elevation that the nitrogen-rich fraction 127 is withdrawn. Alternatively, the nitrogen-enriched fraction 128a may be withdrawn from the same location as nitrogen-rich fraction 127 and have the same composition as nitrogen-rich fraction 127.

(41) The nitrogen-enriched fraction 128a withdrawn from the higher-pressure column 190 is passed to the second (colder) end of the first heat exchanger section 184, heated in the first heat exchanger section 184, and withdrawn from a position intermediate the first (warmer) end and the second (colder) end of the first heat exchanger section 184.

(42) The nitrogen-enriched fraction 128b withdrawn from the position intermediate the first (warmer) end and the second (colder) end of the first heat exchanger section 184 is expanded in an expander 132 to produce work and reduce the pressure of the nitrogen-enriched fraction 128b. Expander 132 may be a dissipative, generator-loaded, or process-loaded expander.

(43) At least a first portion 128e of the expanded nitrogen-enriched fraction 128c is passed to the second (colder) end of the second heat exchanger section 186, heated in the second heat exchanger section 186, and withdrawn from the first (warmer) end of the second heat exchanger section 186. In the embodiments shown in FIGS. 1, 2A, 2B, and 3A-D, all of the expanded nitrogen-enriched fraction 128c is passed to the second (colder) end of the second heat exchanger section 186. In the embodiments shown in FIGS. 2C, and 4, the nitrogen-enriched fraction 128c is blended with another stream 152b, described below, and a first portion 128e of the expanded nitrogen-enriched fraction 128c (as part of the blend) is passed to the second (colder) end of the second heat exchanger section 186 and a second portion 128d of the expanded nitrogen-enriched fraction 128c (as part of the blend) is passed to the second (colder) end of the first heat exchanger section 184.

(44) In the embodiments shown in FIGS. 2C, 3A, 3B, and 4, a first portion 128e of the expanded nitrogen-enriched fraction 128c is passed to the second (colder) end of the second heat exchanger section 186, heated in the second heat exchanger section 186, and withdrawn from the first (warmer) end of the second heat exchanger section 186 as part of waste stream 260. A second portion 128d of the expanded nitrogen-enriched fraction 128c is passed to the second (colder) end of the first heat exchanger section 184, heated in the first heat exchanger section 184, and withdrawn from the first (warmer) end of the first heat exchanger section 184 as a part of waste stream 162.

(45) As shown in FIGS. 1, 2A-C, and 4, a nitrogen-rich byproduct 150 may be withdrawn from the upper region of the lower-pressure column 188. The nitrogen-rich byproduct 150 may be divided into a first fraction 152a and a second fraction 151a. The upper region is defined as section bound by point where nitrogen-enriched intermediate stream 124 enters the lower-pressure column and the lower-pressure column top end. Typically, the top end is the location where stream 148 enters the lower-pressure column.

(46) The first fraction 152a of the nitrogen-rich byproduct 150 may be passed to a first (colder) end of a first subcooler heat exchanger section 192, heated in the first subcooler heat exchanger section 192, and withdrawn from a second (warmer) end of the first subcooler heat exchanger section 192.

(47) In the embodiments shown in FIGS. 1, 2A, and 2B, the at least a portion of the first fraction 152b of the nitrogen-rich byproduct 150 is passed from the second (warmer) end of the first subcooler heat exchanger section 192 to the second (colder) end of the first heat exchanger section 184, heated in the first heat exchanger section 184, and withdrawn from the first (warmer) end of the first heat exchanger section 184 as a first nitrogen-rich discharge byproduct gas 162.

(48) In the embodiments shown in FIGS. 2A and 2B, a second portion 152d of the first fraction 152b of the nitrogen-rich byproduct 150 is passed from the second (warmer) end of the first subcooler heat exchanger section 192 to the second (colder) end of the second heat exchanger section 186, heated in the second heat exchanger section 186, and withdrawn from the first (warmer) end of the second heat exchanger section 186 as a third nitrogen-rich discharge product gas 260.

(49) In the embodiment shown in FIG. 2B, the second portion 152d of the first fraction 152b of the nitrogen-rich byproduct 150 is blended with the expanded nitrogen-enriched fraction 128c from the expander 132 and passed together through the second (colder) end of the second heat exchanger section 186.

(50) In the embodiments shown in FIGS. 2C and 4, the first fraction 152b of the nitrogen-rich byproduct 150 from the second (warmer) end of the first subcooler heat exchanger section 192 is blended with the nitrogen-enriched fraction 128c from the expander 132 to form a nitrogen-rich mixture 258. A first portion 259 of the nitrogen-rich mixture 258 is passed to the second (colder) end of the first heat exchanger section 184, heated in the first heat exchanger section 184, and withdrawn from the first (warmer) end of the first heat exchanger section 184 as a first nitrogen-rich discharge gas 162. A second portion 256 of the nitrogen-rich mixture 258 is passed to the second (colder) end of the second heat exchanger section 186, heated in the second heat exchanger section 186, and withdrawn from the first (warmer) end of the second heat exchanger section 186 as a second nitrogen-rich discharge gas 260.

(51) The advantage of blending the first fraction 152b of the nitrogen-rich byproduct 150 with the nitrogen-enriched fraction 128c from the expander 132 is to provide the greatest flexibility to control the flow split of streams 128c and 152b between the first heat exchanger section 184 and the second heat exchanger section 186. This flexibility will lead to the most efficient operation.

(52) As shown in each of the embodiments of FIGS. 1-4, the second fraction 151a of the nitrogen-rich byproduct 150 may be passed to a first (colder) end of a second subcooler heat exchanger section 194, heated in the second subcooler heat exchanger section 194, and withdrawn from a second (warmer) end of the second subcooler heat exchanger section 194.

(53) The second fraction 151b of the nitrogen-rich byproduct 150 may be passed from the second (warmer) end of the second subcooler heat exchanger section 194 to the second (colder) end of the second heat exchanger section 186, heated in the second heat exchanger section 186, and withdrawn from the first (warmer) end of the second heat exchanger section 186 as a second nitrogen-rich discharge byproduct gas 158.

(54) In an alternative embodiment, a low pressure nitrogen product can be produced by withdrawing a nitrogen-rich gas stream (not shown) from the top end of upper region of the lower-pressure column 188, optionally heating this nitrogen-rich gas stream in the first subcooler heat exchanger section 192 and/or second subcooler heat exchanger section 194, or a third subcooler heat exchanger, and subsequently heating the nitrogen-rich gas stream further in the first heat exchanger section 184 and/or the second heat exchanger section 186. In this case, the nitrogen-rich byproduct 150 may be removed from the lower-pressure column 188 as a vapor-side draw from a location in the upper region below where the nitrogen-rich gas stream is withdrawn. If the flow rate of the nitrogen-rich gas stream is of sufficient magnitude, one of the first fraction 152a of the nitrogen-rich byproduct 150 and the second fraction 151a of the nitrogen-rich byproduct 150 may be eliminated and replaced with this nitrogen-rich gas stream.

(55) As shown in each of the embodiments of FIGS. 1, 2A, 2B, 2C, and 4, a nitrogen-rich fraction 127 may be withdrawn from the top end of the higher-pressure column 190. A second portion 129 of the nitrogen-rich fraction 127 may be passed to the second (colder) end of the second heat exchanger section 186, heated in the second heat exchanger section 186, and subsequently withdrawn from the first (warmer) end of the second heat exchanger section 186 as a gaseous nitrogen product 180. Alternatively, second portion 129 may be heated in the second heat exchanger section 186.

(56) Though not shown, it is well known in the art to produce gaseous nitrogen product 180 using an alternate technique called pumped-LIN. With this technique, an additional liquid is withdrawn from stream 144, optionally pumped to a pressure greater than that of the higher-pressure column (190) and may be subsequently passed to the second (colder) end of the first heat exchanger section 184, heated in the first heat exchanger section 184, and subsequently withdrawn from the first (warmer) end of the first heat exchanger section 184 as a gaseous nitrogen product 180.

(57) The nitrogen-rich fraction 127 or a first portion 140 of the nitrogen-rich fraction 127 withdrawn from the top end of the higher-pressure column 190 may be passed to a reboiler-condenser 142 of the multi-column distillation system. The nitrogen-rich fraction 127 or a first portion 140 of the nitrogen-rich fraction 127 may be condensed in the reboiler-condenser 142, and withdrawn from the reboiler-condenser 142 as nitrogen-rich liquid 144. The reboiler-condenser 142 thermally couples the lower-pressure column 188 and the higher-pressure column 190.

(58) A large part (greater than 40 mole %) of the nitrogen-rich liquid (144) is returned to the top of the higher-pressure column 190 as reflux. A part 146 of the nitrogen-rich liquid (144) may be passed to a second (warmer) end of the second subcooler heat exchanger section 194, cooled in the second subcooler heat exchanger section 194, and withdrawn from the first (colder) end of the second subcooler heat exchanger section 194. The part 146 of the nitrogen-rich liquid (144) withdrawn from the first (colder) end of the second subcooler heat exchanger section 194 may be passed to the top end of the lower-pressure column 188 as reflux. Alternatively, a part 146 of the nitrogen-rich liquid (144) may be passed to a second (warmer) end of the first subcooler heat exchanger section 192, cooled in the first subcooler heat exchanger section 192, and withdrawn from the first (colder) end of the first subcooler heat exchanger section 192.

(59) While the figures show stream 146 which is passed through the second subcooler heat exchanger section 194 being formed from the stream withdrawn from the reboiler-condenser, this stream may alternatively be taken from an intermediate location in the higher-pressure column. For example, stream 146 may be taken as a liquid draw from the location of stream 128a off-take. In such an event, all of the nitrogen-rich liquid (144) is returned to the top of the higher-pressure column 190 as reflux.

(60) As shown in each of the embodiments of FIGS. 1, 2A, 2B, 2C, and 4, a nitrogen-enriched intermediate 124 may be withdrawn from the higher-pressure column 190 from an elevation in the higher-pressure column which is above that of the predominantly liquid air feed. The nitrogen-enriched intermediate 124 may be passed to the second (warmer) end of the first subcooler heat exchanger section 192, cooled in the first subcooler heat exchanger section 192, withdrawn from the first (colder) end of the first subcooler heat exchanger section 192, and passed to an intermediate section of the lower-pressure column 188. Alternatively, the nitrogen-enriched intermediate 124 may be passed to the second (warmer) end of the second subcooler heat exchanger section 194, cooled in the second subcooler heat exchanger section 194, withdrawn from the first (colder) end of the second subcooler heat exchanger section 194, and passed to an intermediate section of the lower-pressure column 188.

(61) The first subcooler heat exchanger section 192 may be structurally integrated with the first heat exchanger section 184.

(62) The second subcooler heat exchanger section 194 may be structurally integrated with the second heat exchanger section 186.

(63) The integration of the subcooler heat exchanger sections 192, 194 with the heat exchanger sections 184, 186 is described with reference to FIGS. 3A-D. FIG. 3A illustrates the same heat exchanger subprocess of FIG. 2A where the subcooler heat exchanger sections 192 and 194 are separate from the heat exchanger sections 184 and 186.

(64) In the embodiment shown in FIG. 3B, the second subcooler heat exchanger section 194 is integrated with the second heat exchanger section 186 as a single heat exchanger 386. The horizontal dotted line shown in the heat exchanger 386 represents the boundary, or interface, between the second subcooler heat exchanger section 194 and the second heat exchanger section 186.

(65) The part 146 of the nitrogen-rich liquid fraction (144) is passed to the second (warmer) end of the second subcooler heat exchanger section 194 of the heat exchanger 386, bypassing the second heat exchanger section 186, and is withdrawn from the first (colder) end of the second subcooler heat exchanger section 194 of the heat exchanger 386. The second fraction 151a of the nitrogen-rich byproduct 150 is passed to the first (colder) end of the second subcooler heat exchanger section 194 of the heat exchanger 386 and is withdrawn from the first (warmer) end of the second heat exchanger section 186 of the heat exchanger 386. The expanded nitrogen-enriched fraction 128c, the second portion 152d of the first fraction 152a of the nitrogen-rich byproduct 150, and the second portion 129 of the nitrogen-rich fraction 127 are each passed to the second (colder) end of the second heat exchanger section 186 of the heat exchanger 386, bypassing the second subcooler heat exchanger section 194, and withdrawn from the first (warmer) end of the second heat exchanger section 186 of the heat exchanger 386. The second portion 108b of the compressed feed air stream is passed to the first (warmer) end of the second heat exchanger section 186 and is withdrawn from the second (colder) end of the second heat exchanger section 186 of the heat exchanger 386 bypassing the second subcooler heat exchanger section 194 of the heat exchanger 386.

(66) This type of heat exchanger arrangement is commonly used to reduce capital costs. The heat transfer efficiency of the heat exchanger arrangement shown in FIG. 3B for the second subcooler heat exchanger section 194 and second heat exchanger section 186 is essentially equivalent to the heat exchanger arrangement shown in FIG. 3A.

(67) In the embodiment shown in FIG. 3C, the first subcooler heat exchanger section 192 is integrated with the first heat exchanger section 184 as a single heat exchanger 384. The horizontal dotted line shown in the heat exchanger 384 represents the boundary between the first subcooler heat exchanger section 192 and the first heat exchanger section 184. The dotted line represents the interface between the second (warmer) end of the first subcooler heat exchanger section 192 and the second (colder) end of the first heat exchanger section 184.

(68) The first fraction 152a of the nitrogen-rich byproduct 150 is passed to the first (colder) end of the first subcooler heat exchanger section 192 of the heat exchanger 384. A first portion 152c of the first fraction 152b of the nitrogen-rich byproduct 150 passes from the second (warmer) end of the first subcooler heat exchanger section 192 of the heat exchanger 384 to the second (colder) end of the first heat exchanger section 184 and is withdrawn from the first (warmer) end of the first heat exchanger section 184 of the heat exchanger 384 as the first nitrogen-rich discharge byproduct gas 162. A second portion 152d of the first fraction 152b of the nitrogen-rich byproduct 150 is withdrawn from the second (warmer) end of the first subcooler heat exchanger section 184 of the heat exchanger 384 bypassing the first heat exchanger section 184. The nitrogen-enriched fraction 128c and the oxygen-rich fraction 166 are each passed to the second (colder) end of the first heat exchanger section 184 of the heat exchanger 384, bypassing the first subcooler heat exchanger section 192, and withdrawn from the first (warmer) end of the first heat exchanger section 184 of the heat exchanger 384.

(69) This type of heat exchanger arrangement is commonly used to reduce capital costs. The heat transfer efficiency of the heat exchanger arrangement shown in FIG. 3C for the first subcooler heat exchanger section 192 and first heat exchanger section 184 is essentially equivalent to the heat exchanger arrangement shown in FIG. 3A.

(70) In the embodiment shown in FIG. 3D, first subcooler heat exchanger section 192 is integrated with the first heat exchanger section 184 as a single heat exchanger 384 and the second subcooler heat exchanger section 194 is integrated with the second heat exchanger section 186 as a single heat exchanger 386. The description for the integrated heat exchanger 384 for FIG. 3C and the description for the integrated heat exchanger 386 for FIG. 3B applies to the integrated heat exchangers 384 and 386. The heat transfer efficiency of the heat exchanger arrangement shown in FIG. 3D for the integrated heat exchangers 384 and 386 are essentially equivalent to the heat exchanger arrangement shown in FIG. 3A for separated heat exchangers.

(71) In the embodiment shown in FIG. 4, the integrated heat exchanger 386 in FIG. 3B is applied to the process flow diagram of FIG. 2C.

(72) The apparatus according to the present disclosure comprises a multi-column distillation system comprising a lower-pressure column 188 and a higher-pressure column 190, a first heat exchanger, a second heat exchanger, and an expander 132.

(73) The first heat exchanger comprises a first heat exchanger section 184. The first heat exchanger section 184 has a first (warmer) end and a second (colder) end. The first (warmer) end is operatively disposed to receive a first portion 107b of the compressed feed air stream 105. The apparatus may comprise a booster compressor 110 and the first (warmer) end may be operatively disposed to receive the first portion 107b from a booster compressor 110. At least one of the lower-pressure column 188 or the higher-pressure column 190 is operatively disposed to receive the first portion 107c of the compressed feed air stream 105 from the second (colder) end of the first heat exchanger section 184. The second (colder) end of the first heat exchanger section 184 is operatively disposed to receive an oxygen-rich fraction 166 from the lower-pressure column 188 and the first (warmer) end of the first heat exchanger section 184 is operatively disposed to discharge the oxygen product 170. The second (colder) end of the first heat exchanger section 184 is operatively disposed to receive a nitrogen-enriched fraction 128a from the higher-pressure column 190.

(74) The second heat exchanger comprises a second heat exchanger section 186. The second heat exchanger may have a lower operating pressure rating than the first heat exchanger. The second heat exchanger section 186 has a first (warmer) end and a second (colder) end. The first (warmer) end is operatively disposed to receive a second portion 108a of the compressed feed air stream 105. The pressure of the second portion 108a of the compressed feed air stream 105 may be less than the pressure of the first portion 107b of the compressed feed air stream 105. The higher-pressure column 190 is operatively disposed to receive the second portion 108b of the compressed feed air stream 105 from the second (colder) end of the second heat exchanger section 186.

(75) The expander 132 has an inlet and an outlet. The inlet of the expander 132 is operatively disposed to receive the nitrogen-enriched fraction 128b withdrawn from a position intermediate the first (warmer) end and the second (colder) end of the first heat exchanger section 184.

(76) As shown in FIG. 1, the second (colder) end of the second heat exchanger section 186 may be operatively disposed to receive the at least a portion of the nitrogen-enriched fraction 128c from the outlet of the expander 132.

(77) As shown in FIGS. 2C and 4, the second (colder) end of the second heat exchanger section 186 may be operatively disposed to receive a first portion 128e of the expanded nitrogen-enriched fraction 128c from the outlet of the expander 132, and the second (colder) end of the first heat exchanger section 184 may be operatively disposed to receive a second portion 128d of the nitrogen-enriched fraction 128c from the outlet of the expander 132.

(78) As shown in FIGS. 1 to 4, the apparatus may further comprise a second expander 116 having an inlet and an outlet. The first (warmer) end of the first heat exchanger section 184 may be operatively disposed to receive a third portion 109b of the compressed feed air stream 105 and discharge the third portion 109c from a position intermediate the first (warmer) end and the second (colder) end of the first heat exchanger section 184. The inlet of the second expander 116 may be operatively disposed to receive the third portion 109c withdrawn from the position intermediate the first (warmer) end and the second (colder) end of the first heat exchanger section 184. At least one of the higher-pressure column 190 or the lower-pressure column 188 may be operatively disposed to receive the third portion 109d from the outlet of the second expander 116.

(79) As shown in FIGS. 1 to 4, the apparatus may further comprise a first subcooler heat exchanger section 192 and a second subcooler heat exchanger section 194.

(80) The first subcooler heat exchanger section 192 has a first (colder) end and a second (warmer) end. The first (colder) end of the first subcooler heat exchanger section 192 may be operatively disposed to receive a first fraction 152a of a nitrogen-rich byproduct 150 from the upper region of the lower-pressure column and discharge the first fraction 152b from the second (warmer) end of the first subcooler heat exchanger section 192. The second (colder) end of the first heat exchanger section 184 may be operatively disposed to receive the at least a portion of first fraction 152b from the second (warmer) end of the first subcooler heat exchanger section 192.

(81) The second subcooler heat exchanger section 194 has a first (colder) end and a second (warmer) end. The first (colder) end of the second subcooler heat exchanger section 194 may be operatively disposed to receive a second fraction 151a of the nitrogen-rich byproduct 150 and discharge the second fraction 151b from the second (warmer) end of the second subcooler heat exchanger section 194. The second (colder) end of the second heat exchanger section 186 may be operatively disposed to receive at the second fraction 151b from the second (warmer) end of the second subcooler heat exchanger section 194.

(82) As shown in FIG. 4, the second (colder) end of the second heat exchanger section 186 may be operatively disposed to receive a second portion 152d of the first fraction 152b from the second (warmer) end of the first subcooler heat exchanger section 192 and the second (colder) end of the first heat exchanger section 184 may be operatively disposed to receive a first portion 152c of the first fraction 152b from the second (warmer) end of the first subcooler heat exchanger section 192.

Example

(83) Computer simulations for various heat exchanger configurations were conducted using Aspen Plus.

(84) The basis for the simulations are as follows:

(85) TABLE-US-00001 Ambient Pressure (bara) 1.0 Ambient Temperature ( C.) 25 Cooling Water Supply ( C.) 25 Oxygen Product (stream 170) Flow rate (nm.sup.3/h) 100,000 Pressure (bara) 65 Nitrogen Product (stream 180) Flow rate (nm.sup.3/h) 5,000 Pressure (bara) 5.0

(86) Some key results are summarized in Table 1.

(87) The results shown in the 1.sup.st column, Case 1, corresponds to the process shown in FIG. 5, where the first and second heat exchanger sections are combined into one single heat exchanger section 584 and first and second subcooler heat exchanger sections are combined into one single subcooler heat exchanger section 596. Reference numbers for streams in FIG. 5 in common with the earlier figures have the same reference number as in the earlier figures. Note that there is no need to split nitrogen-rich byproduct 150 as it flows through the heat exchanger system (150-551, 558). This case represents the lowest power achievable. This is because combining all the streams into one, single heat exchanger provides the greatest flexibility to thermally balance the heat loads and therefore achieve highest thermodynamic efficiency. It is typical that when splitting the heat exchanger system into two parallel heat exchangers, the lowest power achievable can only approach, but will not meet that of Case 1.

(88) The results shown in the 2.sup.nd column, Case 2, represents the prior art and corresponds to the process shown FIG. 6. The process of FIG. 6 is similar to that of FIG. 1 but follows the teachings of EP 2824407. In particular, expander 132 receives its flow from the second heat exchanger section 186. Also note that second subcooler heat heat exchanger section 194 has been integrated with second heat exchanger section 186 to create second heat exchanger 386. The power penalty compared to Case 1, 1146 kW, is greatest and is due primarily to the ineffective use of expander 132 resulting in high air expander flow 109b.

(89) The results shown in the 3.sup.rd column, Case 3, corresponds to an embodiment of the invention as shown in FIG. 1, where expander 132 receives its flow from the first heat exchanger section 184. Of note, this configuration enables the inlet temperature to expander 132 (stream 128b) to be warmer compared to the prior art and approaches that of the Case 1. In addition, the flow of stream 128b is slightly larger compared to the prior art Case 2. The resultant refrigeration produced by expander 132 is thus greater than that of Case 2, and results in a reduction of (compressed) air expander flow (stream 109b). The power is reduced by 384 kW compared to Case 2 (Prior Art).

(90) The results shown in the 4th column, Case 4, are for a comparative case shown in FIG. 7. The results show the modest effect of only splitting stream 258 between the two heat exchangers. Case 4 can be envisioned as the embodiment of FIG. 4 except expander 132 draws its flow from the second heat exchanger section 186, as in the prior art case. The power is reduced by 120 kW compared to Case 2 (Prior Art).

(91) The results shown in the 5.sup.th column, Case 5, correspond to an embodiment of the invention as shown in FIG. 4. In this case, not only does expander 132 receive its flow from the first heat exchanger section 184, but also expander 132 discharge stream 128c, after having been mixed with low pressure nitrogen stream 152b, is split between the first and second heat exchangers sections. By making both changes, further benefits can be achieved over simply combining the individual benefits of case 3 and 4. The power is reduced by 741 kW compared to Case 2 (Prior Art). This power is nearly comparable to that of the Case 1. It is noteworthy that the expander 132 flow, and temperatures approach closely those of the Case 1hence the further reduction of (compressed) air expander flow compared to the Prior Art.

(92) TABLE-US-00002 TABLE 1 Case 1 Case 2 Case 3 Case 4 Case 5 FIG. 5 FIG. 6 FIG. 1 FIG. 7 FIG. 4 Power kW 56,417 57,563 57,175 57,443 56,882 Penalty compared to Case 1 kW 1,146 758 1,026 405 Improvement compared to Case 2 kW 1,146 388 120 741 Dry Air flow (105) Nm.sup.3/hr 483,477 481,731 482,950 482,137 483,705 MP Air flow (108a) Nm.sup.3/hr 309,030 278,692 292,946 280,165 295,738 MP Air pressure (108a) bara 5.6 5.6 5.6 5.6 5.5 JT Air flow (107b) Nm.sup.3/hr 135,003 114,274 129,088 114,571 127,441 JT Air pressure (107b) bara 75 75 75 75 75 Air Expander flow (109b) Nm.sup.3/hr 39,444 88,764 60,916 87,401 60,526 Air Expander pressure (109b) bara 35 35 35 35 35 N.sub.2 Expander flow (128b) Nm.sup.3/hr 56,124 45,790 49,521 47,201 53,856 T into expander (128b) C. 123 163 123 160 125 T out of expander (128c) C. 168 194 168 193 168 Lower pressure N.sub.2-enriched (136) Nm.sup.3/hr 56,124 45,790 49,521 First N.sub.2 discharge (158) Nm.sup.3/hr 321,748 246,440 258,460 152,290 153,762 Second N.sub.2 discharge (162) Nm.sup.3/hr 83,895 69,361 81,709 65,208 Third N2 discharge (260) Nm.sup.3/hr 142,535 159,131