The invention relates to a method for generating two purified air substreams at different pressures.
A “condenser-evaporator” denotes a heat exchanger in which a first condensing fluid stream comes into indirect heat exchange with a second evaporating fluid stream. Each condenser-evaporator has a liquefaction chamber and an evaporation chamber which consist of liquefaction passages or evaporation passages, respectively. In the liquefaction chamber, a first fluid stream is condensed (liquefied) and in the evaporation chamber, a second fluid stream is evaporated. Evaporation and liquefaction chambers are formed by groups of passages which are in a heat-exchange relationship with one another.
A condenser-evaporator can be constructed, for example, as a falling-film or bath evaporator. In a “falling-film evaporator”, the film that is to be evaporated flows from top to bottom through the evaporation chamber and is partially evaporated in the course of this. In a “bath evaporator” (sometimes also termed “circulation evaporator” or “thermosiphon evaporator”) the heat-exchanger block is in a liquid bath of the fluid that is to be evaporated. This flows owing to the thermosiphon effect from bottom to top through the evaporation passages and exits again at the top as a two-phase mixture. The remaining liquid flows outside the heat-exchanger block back into the liquid bath (in a bath evaporator, the evaporation chamber can comprise not only the evaporation passages but also the outer chamber around the heat-exchanger block).
The condenser-evaporator for the low-pressure column (the low-pressure column intermediate evaporator and the low-pressure column sump evaporator) can be arranged in the interior of the low-pressure column or in one or more separate containers.
EP 342436 A2 discloses compressing a total air stream (1) to a first total air pressure, dividing into two air substreams, boosting one of these and purifying the two air substreams in two purification appliances which are operated at different pressures for the compression.
The object of the invention is to design such a method and a corresponding device in such a manner that they are energetically particularly expedient to operate.
This object is achieved by the features of claim 1.
In the invention, the total air stream, before division thereof, is cooled by direct heat exchange with cooling water in the first direct contact cooler to a particularly low temperature which is, in particular, below the ambient temperature. Using conventional aftercoolers or intercoolers, such a low temperature cannot usually be achieved. At this particularly low temperature, the second air substream then enters the boosting. The corresponding volume reduction at the intake of the recompressor effects a noticeable improvement of the efficiency of the boosting and thereby saves energy.
Upstream of the first direct contact cooler, a conventional aftercooler can be connected, in which the total air stream, after the compression thereof to the first total air pressure, is cooled by indirect heat exchange with cooling water to a temperature which is generally higher than the ambient temperature. The cooling of the total air between compression and division to the two air substreams can, however, also be performed solely in the first direct contact cooler.
The heat exchange with cooling water for cooling the boosted second air substream (14) could alternatively in principle proceed indirectly. In the invention, this cooling, however, is carried out at least in part as direct heat exchange in a second direct contact cooler. Upstream of the second direct contact cooler, a conventional aftercooler can be connected, in which the boosted second air substream is cooled by indirect heat exchange with cooling water to a temperature which is generally higher than the ambient temperature. However, the cooling can alternatively be performed solely in the direct contact cooler.
All compression steps can be accomplished in a multistage manner and then each have preferably one conventional intercooling between each pair of successively following stages.
The invention further relates to the use of the above method for providing feed air at two different pressure levels for a low-temperature fractionation of air as claimed in claim 3.
The invention further relates to a device as claimed in claim 4. The device according to the invention can be supplemented by device features which correspond to the features of the dependent method claims.
The invention and further details of the invention will be described in more detail hereinafter with reference to an exemplary embodiment shown schematically in
Atmospheric air 1 is drawn in by suction in
The second air substream 11 is compressed in a booster 12 with aftercooler 13 from the first total air pressure (minus pressure drops) to a second total air pressure of 4.9 bar. The booster can have two or more stages with intercooling; for reasons of redundancy it is preferably constructed in two lines (both are not shown in the drawing). Each line of the main air compressor and the booster can be constructed as one machine having a shared drive, in particular as a geared compressor. The second air substream 14 is then cooled from 295 K to 290 K in a second direct contact cooler 15, more precisely in direct heat exchange with a warmer cooling water stream 16.
The first air substream is purified in a first purification appliance 18 which is operated at the first total air pressure, and then passed via line 19 at this pressure to the warm end of a main heat exchanger, which in the exemplary embodiment is formed by two blocks 20, 21 connected in parallel. The air cooled to about dew point forms a “first feed air stream”, which is fed to a first high-pressure column 23.
The first high-pressure column 23 is part of a distillation column system for nitrogen-oxygen separation which, in addition, has a second high-pressure column 24, a low-pressure column consisting of two sections 25, 26, a low-pressure column intermediate evaporator 27, a low-pressure column sump evaporator 28 and an auxiliary condenser 29. The low-pressure column intermediate evaporator 27 and the low-pressure column sump evaporator 28 are constructed as falling-film evaporators, and the auxiliary condenser 29 as a bath evaporator.
The precooled second air substream 17 is purified in a second purification appliance 30 which is operated at the second total air pressure. From the purified second air substream, via line 32, a small part can be withdrawn which is used as instrument air or for purposes outside the air fractionation. The remainder flows via line 33 to the main heat exchanger 20 and is there cooled. The cooled second air substream 34 is divided into a “second feed air stream” 35 which is introduced into the second high-pressure column 24, and into a “third feed air stream” 36, which is passed to the liquefaction chamber of the auxiliary condenser 29.
The at least partially, preferably substantially completely, condensed third substream 37 is introduced into a separator (phase separator) 38. The liquid fraction 39 is fed in a first part 40 to the first high-pressure column 23. In a second part 41, it is fed via a subcooling countercurrent heat exchanger 42 and line 43 into the low-pressure column 26.
Nitrogen-rich overhead gas 44 of the first high-pressure column 23 is condensed in a first part in the low-pressure column intermediate evaporator 27. Here, liquid nitrogen 46 that is obtained is applied in a first part 47 as reflux to the top of the first high-pressure column 23. A second part 48 is cooled in the subcooling countercurrent heat exchanger 42 and applied via line 49 as reflux to the top of the low-pressure column 26. A part 50 of the subcooled liquid can if required be obtained as liquid product (LIN).
A second part 51 of the nitrogen-rich overhead gas 44 of the first high-pressure column 23 is introduced into the main heat exchanger 20. At least a part 52 thereof is only warmed to an intermediate temperature and is then work-producingly expanded in a generator-braked compressed nitrogen turbine 53 from 2.7 bar to 1.25 bar. The outlet pressure of the turbine is already sufficient to force the work-producingly expanded stream 54 through the main heat exchanger 20 and via the lines 55, 56, 57 as regeneration gas through the first and the second purification appliances 18, 30.
A further part of the stream 51 is warmed to ambient temperature in the main heat exchanger 20 and obtained as gaseous pressurized nitrogen product (PGAN).
Nitrogen-rich overhead gas 58 of the second high-pressure column 24 is condensed in the low-pressure column sump evaporator 28. In this process, liquid nitrogen 59 that is obtained is applied in a first part 60 as reflux to the top of the second high-pressure column 24. A second part 61 is cooled in the subcooling countercurrent heat exchanger 42 and applied via line 62 as reflux to the top of the low-pressure column 26.
The sump liquids 63, 64 of the two high-pressure columns 23, 24 are combined, and fed via line 65, the subcooling countercurrent heat exchanger 42 and line 66 to the low-pressure column 26.
The sump liquid 66 of the low-pressure column 25 is introduced into the evaporation chamber of the low-pressure column sump evaporator 28 and there in part evaporated. The fraction 67 remaining liquid flows into the evaporation chamber of the auxiliary condenser 29 and is there in part evaporated. The evaporated fraction 68 is passed to the cold end of the main heat exchanger block 20, warmed to about ambient temperature and finally, via line 69, obtained as gaseous oxygen product (GOX) of a purity of 95 mol %. The fraction remaining liquid is, as a part 70, in a pump 71, evaporated and warmed to a pressure of 6 bar in the main heat exchanger block 21 and finally admixed to the gaseous oxygen product 69. Another part 72 can be obtained as liquid oxygen product (LOX) via the subcooling countercurrent heat exchanger 42, pump 73 and line 74.
A liquid intermediate fraction 75 which occurs at the bottom end of the second low-pressure column section 26 is transported by means of a pump 76 into the evaporation chamber of the low-pressure column intermediate evaporator 27 and there in part evaporated. Steam generated in this process is passed together with steam produced at the top of the first low-pressure column section 25, via the lines 77 and 79 to the second low-pressure column section 26, optionally together with circulating purge liquid 78. The remainder of the intermediate fraction remaining liquid serves as reflux liquid in the first low-pressure column section 25.
At the top of the low-pressure column 26, nitrogen-rich residual gas 80 is taken off at a pressure of 1.26 bar and, after warming in the subcooling countercurrent heat exchanger 42 and main heat exchanger 20 is fed via line 81 virtually unpressurized as dry gas into the evaporative cooler 8 and there utilized for cooling down cooling water 82.
Number | Date | Country | Kind |
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102011113666.9 | Sep 2011 | DE | national |
11008618.8 | Oct 2011 | EP | regional |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2012/003945 | 9/20/2012 | WO | 00 | 3/19/2014 |