Patent Grant
6915661
The present invention relates to an integrated air separation process and apparatus. In particular, it is related to an air separation process integrated with a gas turbine process and a natural gas liquefaction process.
It is known from U.S. Pat. No. 3,731,495 to integrate an air separation unit (ASU) with a gas turbine by removing compressed air from the gas turbine compressor, sending it to the ASU and sending a nitrogen enriched gas from the ASU upstream of the expander of the gas turbine. In this case, the expander of the gas turbine is coupled to the gas turbine compressor.
It is known from U.S. Pat. No. 4,566,885 and U.S. Pat. No. 5,139,548 to couple the compressors of two gas turbines with the cycle compressors of a refrigeration cycle, using a multicomponent refrigerant (MCR), of a natural gas liquefaction process.
At certain sites, it may be desired to transform a first stream of natural gas into liquefied natural gas and a second stream of natural gas at least one product of the conversion of the natural gas, such as methanol, DME or the product of a Fischer Tropsch reaction. The conversion reaction frequently requires the supply of large amounts of gaseous oxygen. Heat generated by the reaction is commonly used to raise steam which is then expanded in a steam turbine to generate electricity.
An object of the invention is to reduce the costs of a production complex which simultaneously produces from the same natural gas source both liquefied natural gas and a product of the conversion of the natural gas, such as methanol, dimethyl ethers or a Fischer Tropsch product, by integrating an air separation unit, a gas turbine, a natural gas conversion unit and a natural gas liquefaction unit.
Typically in the prior art, the power requirements are provided by a steam turbine powering the MAC compressor of the ASU as shown in U.S. Pat. Nos. 3,868,817, 4,099,383 and 4,184,322 and two gas turbines powering the multicomponent refrigerant cycle and propane cycle of the natural gas liquefier as mentioned above.
The integrated process of the invention uses only a single gas turbine.
According to one aspect of the invention, there is provided a process for separating air in a system comprising a gas turbine, including a compressor, a combustor and an expander, said expander being coupled to the compressor, a natural gas conversion unit, a natural gas liquefaction unit and an air separation unit comprising the steps of:
a) compressing air in the compressor, sending a first part of the air to the combustor and a second part of the air to the air separation unit;
b) separating at least the second part of the air in the air separation unit to form at least an oxygen enriched gas and an nitrogen enriched gas;
c) sending a first stream of natural gas from a source of natural gas to the natural gas conversion unit and at least part of the oxygen enriched gas to the natural gas conversion unit;
d) compressing at least part of the nitrogen enriched gas and sending at least part of the compressed nitrogen enriched gas upstream of the expander; and,
e) feeding a second stream of natural gas from the source of natural gas to the natural gas liquefaction unit,
wherein work produced by the expander is used to operate a cycle compressor of a refrigeration cycle of the natural gas liquefaction unit.
The terms ‘oxygen enriched’, ‘nitrogen enriched’ and ‘argon enriched’ mean enriched with respect to air.
According to further optional aspects of the invention:
The process may also include the steps of:
The cycle compressor is a multi-component refrigeration fluid compressor or a propane cycle compressor.
According to a further aspect of the invention, there is provided an integrated apparatus comprising an air separation unit, a gas turbine having an air compressor, a combustor and an expander, a natural gas conversion unit and a natural gas liquefaction unit having
a) conduits for sending air from the air compressor to the combustor and to the air separation unit;
b) a conduit for sending a nitrogen enriched gas from the air separation unit to a point upstream the expander;
c) a conduit for sending an oxygen enriched gas from the air separation unit to the natural gas conversion unit;
d) a conduit for sending a first stream of natural gas from a natural gas source to the natural gas conversion unit;
e) a conduit for sending a second stream of natural gas from the natural gas source to the natural gas liquefaction unit; and,
f) means for transferring work from the expander to the air compressor and to a compressor of a refrigeration cycle of the natural gas liquefaction unit.
Additionally, the expander may be coupled to the air compressor. Also, The apparatus may comprise a conduit for sending natural gas to a natural gas conversion unit and a conduit for sending an oxygen enriched gas from the air separation unit to the conversion unit. Preferably the expander is coupled to the compressor of the refrigeration cycle.
The compressor 1 of a gas turbine produces a first part of compressed air 3 which is sent to a combustor 5. The combustor is also fed by fuel 4 which may be (or may include) natural gas from natural gas source 25. The rest of the compressed air 7 is mixed with compressed air 9 from a dedicated main air compressor (MAC) 11 and thereafter cooled and purified (not shown). The dedicated main air compressor is not an essential part of the apparatus. Between 10 and 30% of the air 13 may be further compressed in a booster air compressor (BAC) 14 to a pressure required to vaporize the liquid oxygen, for example. The booster is also not essential to the apparatus since certain air separation processes use a single high air pressure. The further compressed air 13 is cooled in the main heat exchange line, liquefied and sent to the columns of the ASU 20. The mixture 15 of part of air streams 7 and 9 is sent to the column of the ASU 20 operating at the highest (or higher) pressure, which is above 8 bar abs. and frequently above 12 bar abs following cooling in the main heat exchange line.
The ASU may comprise a double or triple column system as described for example in patents EP-A-0504029 and EP-A-538857.
From a column of the ASU 20 operating at a lower pressure is withdrawn a nitrogen enriched gaseous stream 16. The stream is warmed in the main heat exchange line and then compressed in nitrogen compressor 19 and sent to the gas turbine to a point upstream of the expander 17. In the example the nitrogen is sent to a point downstream the combustion chamber but it may alternatively be sent to the combustion chamber.
An oxygen enriched gas stream 21 containing at least 99% mol. oxygen is removed from a column of the ASU as a liquid, pressurized to between 25 and 50 bar abs., vaporized in the main heat exchange line and sent to a natural gas conversion unit 23, such as a Fischer Tropsch unit, wherein a first stream of natural gas 33 from a natural gas source 25 is converted to other products.
The natural gas source may be a gas field connected by pipeline to the mainland or to an offshore treatment plant or a methane tanker.
The ASU 20 may also produce liquid final products 24 or argon enriched products 26.
The expander 17 is fed by combustion gases 19 from the combustor 5 and is coupled to the compressor 1. The MAC and BAC compressors 11, 14 are each coupled to a respective motor as is the nitrogen compressor 19. To provide electricity for at least one of the motors without requiring import of electricity from an external network, steam from the unit 23 may be expanded in a steam turbine 31 which is coupled to a generator.
The expander 17 is also coupled to a compressor 22 of a multicomponent refrigerant cycle used to liquefy a second natural gas stream 35 from natural gas source 25. Another compressor of the cycle 27 is driven by an electric motor, which is preferably fed with electricity produced by the stream turbine 31. The natural gas is cooled in vessel 28 by indirect and direct contact with the compressed multicomponent refrigerant compressed in compressors 22,27 and is thereby liquefied to form liquefied natural gas 29.
In the case of
The second natural gas stream 35 is cooled using a closed propane cycle 37 and sent to the liquefier 28 to produced liquefied natural gas 29. A multicomponent refrigeration cycle 39 is used to liquefy the natural gas. One of the compressors 22 of the cycle is coupled to the gas turbine expander 17 whilst the other 27 has a motor fed by electricity generated by steam turbine 31. The compressor 41 of the propane cycle also has a motor fed by electricity generated by steam turbine 31.
It will be appreciated that in order to avoid importing electricity to what may be a remote site, it is preferable that the gas turbine expander be coupled to a compressor the natural gas liquefaction plant, such as an MCR compressor 22,27 or a propane compressor 41 where there is a propane cycle. Since air from the gas turbine compressor is sent to the ASU, the remaining compressors should be powered using electricity generated by the steam turbine.
This application claims the benefit under 35 U.S.C. § 119 (e) to provisional Application No. 60/425,860, filed Nov. 13, 2002, the entire contents of which are incorporated herein by reference.
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| Number | Date | Country | |
|---|---|---|---|
| 20040089021 A1 | May 2004 | US |
| Number | Date | Country | |
|---|---|---|---|
| 60425860 | Nov 2002 | US |
