The present invention relates to a process and to a plant for producing pressurized air gases by cryogenic air distillation.
Certain (type 1) processes, such as those described in EP-A-0 504 029, produce oxygen at high pressure (>15 bar) using a single compressor to compress the air to a pressure well above the pressure of the medium-pressure column.
These processes are suitable for a context in which investment costs are of prime importance, as they have the drawback of consuming a very large amount of energy when no liquid production is required.
Other (type 2) processes, using a high air pressure only for producing pressurized gaseous oxygen, are disclosed in U.S. Pat. No. 5,475,980 and have a better specific energy for producing gaseous oxygen at high pressure, without producing liquid (or with a low production of liquid). They use cryogenic compression of air pressurized by means of a blower mechanically linked to an expansion turbine.
However, this energy advantage is counterbalanced by an investment substantially greater than that of type 1, as this is an expensive process in terms of exchanger volume. This is because in general a large fraction (60% to 80%) of the main air stream undergoes adiabatic cryogenic compression before being reintroduced into the main exchange line.
Finally, these types of process seem to be economically advantageous, and the choice will depend on the intended utilization of the energy, available at low or high cost.
In this document, the term “condensation” includes pseudo-condensation and the term “vaporization” includes pseudo-vaporization.
Temperatures are considered as being similar if they differ by at most 10° C., preferably at most 5° C.
The exchange line is the main exchanger where the gases produced by the column system are warmed and/or where the air intended for distillation is cooled.
The invention includes both methods and apparatus to achieve the desired results, as described, but is not limited to the various embodiments disclosed.
It is an object of the invention to propose an alternative for producing process schemes allowing the energy performance to be improved over type-1 processes, while retaining an exchange volume requirement of less than that of cold-compression, type-2 schemes, as described above.
According to the invention, only a fraction of the air (the fraction that liquefies at the cold end) undergoes cryogenic compression, which minimizes the increase in volume of the exchanger. However, this allows the main air pressure to be very substantially reduced, since the air output by the cryogenic booster remains at a pressure sufficient to vaporize oxygen.
One of the objects of the invention is to provide a process for separating air by cryogenic distillation in a system of columns, comprising a double column or a triple column, the column operating at the highest pressure operating at a pressure called medium pressure, in which:
For a further understanding of the nature and objects for the present invention, reference should be made to the following detailed description, taken in conjunction with the accompanying drawings, in which like elements are given the same or analogous reference numbers and wherein:
The invention includes methods and apparatus for the cryogenic separation of air, as described above.
According to other, optional aspects:
Another object of the invention is to provide a cryogenic-distillation air-separation plant comprising:
The turbine constituting the drive device or forming part of the latter may be an air expansion turbine, in particular a blowing turbine or a nitrogen expansion turbine.
The invention will be described in greater detail with respect to the drawings,
A nitrogen-enriched gas stream 31, coming from the medium-pressure column 100, is warmed in the exchange line, exits therefrom at a temperature higher than the inlet temperature of the Claude turbine 17, and is sent to an expansion turbine 119. The nitrogen expanded substantially at the low pressure and substantially at the temperature of the cold end of the exchange line is reintroduced into the exchange line, where it warms up or joins a nitrogen-enriched gas 33 withdrawn from the low-pressure column, and the nitrogen stream 29 formed is warmed while passing through the entire exchange line.
The nitrogen turbine 119 is coupled to the cold booster 23, while the Claude turbine 17 is coupled to the hot booster 5.
The expansion turbine 119 is not an essential element of the invention and the drive for the cold booster 23 may be replaced by an electric motor. Likewise, the expansion turbine 119 may be replaced with an air-expansion turbine.
The column system of
The medium-pressure column 100 operates at a pressure of 5.5 bar, but it may operate at higher pressure.
The gaseous air 35 coming from the turbine 17 is sent into the bottom of the medium-pressure column 100.
The liquefied air 37 is expanded in the valve 39 and divided into two, one portion being sent to the medium-pressure column 100 and the remainder to the low-pressure column 200.
Rich liquid 51, lower lean liquid 53 and upper lean liquid 55 are sent from the medium-pressure column 100 into the low-pressure column 200 after in-valve expansion and subcooling steps.
Oxygen-enriched liquid 57 and nitrogen-enriched liquid 59 are possibly withdrawn from the double column as final products.
Oxygen-enriched liquid is pressurized by the pump 500 and sent, as pressurized liquid 25, towards the exchange line 9. Alternatively or additionally, other, pressurized or non-pressurized, liquids, such as other liquid oxygen streams at a different pressure, liquid nitrogen and liquid argon, may be vaporized in the exchange line 9.
Waste nitrogen 27 is withdrawn from the top of the low-pressure column and is warmed in the exchange line 9, after having been used to subcool the reflux liquids 51, 53, 55.
The column may optionally produce argon by treating a stream withdrawn from the low-pressure column 200.
As a variant, as shown in dotted lines, a portion 41 of the high-pressure air, not boosted in the booster 23, may liquefy in the exchange line by heat exchange with the oxygen, which vaporizes, is expanded in a valve 43 down to the medium pressure, and is mixed with the liquefied air 37. It will be understood that if the air is at a supercritical pressure on leaving the booster 5 liquefaction will take place only after expansion in the valves 39, 43.
The hot booster 5 is again coupled to the Claude turbine, but the cold booster 23 is coupled to the blowing turbine.
The liquid-air expansion valves are also different in
As in
This kind of process is more suitable for the production of low-purity oxygen.
In
The remaining portion 2 of the air at about 15 bar (and therefore between 10 and 50% of the total high-pressure flow) is cooled in the exchange line 9 down to an intermediate temperature above the intake temperature of the Claude turbine 17 and is then boosted in the cold booster 23. This air then liquefies in the exchange line 9. As in
It will be understood that many additional changes in the details, materials, steps and arrangement of parts, which have been herein described in order to explain the nature of the invention, may be made by those skilled in the art within the principle and scope of the invention as expressed in the appended claims. Thus, the present invention is not intended to be limited to the specific embodiments in the examples given above.
Number | Date | Country | Kind |
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03 50142 | May 2003 | FR | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/FR2004/050146 | 4/6/2004 | WO | 00 | 11/4/2005 |
Publishing Document | Publishing Date | Country | Kind |
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WO2004/099691 | 11/18/2004 | WO | A |
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3285028 | Newton | Nov 1966 | A |
3605422 | Pryor | Sep 1971 | A |
4303428 | Vandenbussche | Dec 1981 | A |
4869742 | Thorogood | Sep 1989 | A |
5329776 | Grenier | Jul 1994 | A |
5400600 | Grenier | Mar 1995 | A |
5475980 | Grenier et al. | Dec 1995 | A |
5515687 | Arriulou | May 1996 | A |
5596885 | Grenier | Jan 1997 | A |
5941098 | Guillard | Aug 1999 | A |
6253576 | Herron et al. | Jul 2001 | B1 |
6336345 | Corduan | Jan 2002 | B1 |
20050126221 | Ha | Jun 2005 | A1 |
Number | Date | Country |
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199 51 521 | May 2001 | DE |
0 504 029 | Sep 1992 | EP |
0 644 388 | Mar 1995 | EP |
0 932 000 | Jul 1999 | EP |
Entry |
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International Search Report for PCT/FR2004/050146. |
Number | Date | Country | |
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20060277944 A1 | Dec 2006 | US |