US2022298969A1PendingUtilityA1
Method and system for power production with improved efficiency
Est. expiryJul 8, 2034(~7.9 yrs left)· nominal 20-yr term from priority
F02C 3/34F05D 2270/20F05D 2240/35F25J 2260/80F02C 7/143F05D 2260/213F25J 3/04533F02C 7/10F25J 3/04618F25J 3/04018F25J 2230/06F02C 3/04F25J 2240/70F05D 2220/32Y02E20/32
71
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Claims
Abstract
The present disclosure relates to systems and methods that provide power generation using predominantly CO 2 as a working fluid. In particular, the present disclosure provides for the use of a portion of the heat of compression from a CO 2 compressor as the additive heating necessary to increase the overall efficiency of a power production system and method.
Claims
exact text as granted — not AI-modified1 . A method for heating a recirculating gas stream comprising:
passing a gas stream G at a pressure P 1 and a temperature T 1 through a recuperative heat exchanger such that the gas stream is cooled to a temperature T 2 that is less than T 1 ; separating the gas stream G into a first fraction G 1 and a second fraction G 2 ; compressing the gas stream fraction G 1 to a pressure P 2 that is greater than P 1 ; compressing the gas stream fraction G 2 to a pressure P 3 that is greater than P 1 so as to heat the gas stream fraction G 2 to a temperature T 3 that is greater than T 2 ; withdrawing the heat from the compressed gas stream fraction G 2 ; combining the gas stream fraction G 1 and the gas stream fraction G 2 to form a combined recirculating gas stream G C ; pumping the recirculating gas stream G C to a pressure P 4 that is greater than P 2 and greater than P 3 ; and passing the recirculating gas stream G C to the recuperative heat exchanger such that the gas stream G C is heated by the cooling gas stream G; wherein the heat withdrawn from the compressed gas stream fraction G 2 is added to the recirculating gas stream G C after pumping to pressure P 4 .
2 . The method according to claim 1 , wherein the temperature T 3 is about 100° C. to about 400° C.
3 . The method according to claim 1 , wherein the pressure P 2 of gas stream fraction G 1 and the pressure P 3 of gas stream fraction G 2 are each separately about 40 bar (4 MPa) to about 100 bar (10 MPa).
4 . The method according to claim 1 , wherein the pressure P 4 of the recirculating gas stream G C is about 100 bar (10 MPa) to about 500 bar (50 MPa).
5 . The method according to claim 1 , wherein the mass ratio of gas fraction G 1 to gas fraction G 2 based on the total mass of gas stream G is about 50:50 to about 99:1.
6 . The method according to claim 1 , wherein the recirculating gas stream G C after passing through the recuperative heat exchanger and receiving the heat from the compressed gas fraction G 2 has a temperature T 4 that is within 50° C. of T 1 .
7 . The method according to claim 1 , wherein gas stream fraction G 2 is compressed with multi-stage compression with no intercooling.
8 . The method according to claim 1 , wherein after withdrawing heat from gas stream fraction G 2 , the gas stream fraction G 2 is further compressed before combining with gas stream fraction G 1 .
9 . The method according to claim 1 , wherein the recuperative heat exchanger comprises three heat exchangers or three heat exchange sections in series, such that heat is transferred in a first heat exchanger or heat exchange section operating in temperature range R 1 , a second heat exchanger or heat exchange section operating in temperature range R 2 , and a third heat exchanger or heat exchange section operating in temperature range R 3 with the temperature relationship of R 1 >R 2 >R 3 .
10 . The method according to claim 9 , wherein the gas stream G is separated between the first heat exchanger or heat exchange section and the second heat exchanger or heat exchange section.
11 . The method according to claim 9 , wherein the gas stream G is separated between the second heat exchanger or heat exchange section and the third heat exchanger or heat exchange section.
12 . The method according to claim 9 , wherein the heat withdrawn from the compressed gas stream fraction G 2 is added to the recirculating gas stream G C in one or both of the third heat exchanger or heat exchange section and the second heat exchanger or heat exchange section.
13 . The method according to claim 1 , further comprising adding heat to the recirculating gas stream G C after pumping to pressure P 4 , wherein the added heat is derived from one or both of an air separation unit and a gas turbine.
14 . The method according to claim 1 , further comprising passing the heated recirculating gas stream G C from the recuperative heat exchanger to a combustor that combusts a fuel with oxygen to form a combustion product stream.
15 . The method according to claim 1 , wherein the gas stream G is a turbine exhaust stream.
16 . A method of generating power, the method comprising:
combusting a fuel with oxygen in the combustor in the presence of a recycle CO 2 stream to produce a CO 2 containing combustion stream; passing the CO 2 containing combustion stream through a turbine to expand the CO 2 containing combustion stream, generate power, and form a turbine exhaust stream; withdrawing heat from the turbine exhaust stream; dividing the turbine exhaust stream to form a first turbine exhaust portion and second turbine exhaust portion; separating water from the first turbine exhaust portion to form a main recycle CO 2 stream; compressing the main recycle CO 2 stream; compressing the second turbine exhaust portion to form a heated, compressed second turbine exhaust portion; withdrawing heat from the heated, compressed second turbine exhaust portion; separating water from the cooled, compressed second turbine exhaust portion to form a secondary recycle CO 2 stream; combining the main recycle CO 2 stream and the secondary recycle CO 2 stream to form a combined recycle CO 2 stream; compressing the combined recycle CO 2 stream; heating the combined recycle CO 2 stream with heat withdrawn from the turbine exhaust stream; and further heating the combined recycle CO 2 stream with heat withdrawn from the heated, compressed second turbine exhaust portion.
17 - 25 . (canceled)
26 . A power generating system comprising:
a combustor configured to exhaust a combustion stream; a power production turbine configured to receive and expand the combustion stream and form a turbine exhaust stream; a recuperative heat exchanger configured to receive the turbine exhaust stream; a flow separator configured to separate the cooled turbine exhaust stream into a first gas stream and a second gas stream; a first compressor configured to receive and compress the first gas stream; a second compressor configured to receive and compress the second gas stream; a pump configured to pressurize the first gas stream and the second gas stream in combination, the pump positioned downstream from the first compressor and the second compressor; a first flow path through the recuperative heat exchanger configured for passage of the turbine exhaust stream; a second flow path through the recuperative heat exchanger configured for passage of the pressurized first gas stream and second gas stream in combination; a third flow path through the recuperative heat exchanger configured for passage of the compressed second gas stream; wherein the first flow path and the third flow path are configured for heating the second flow path.
27 . The power generating system according to claim 26 , wherein the recuperative heat exchanger comprises a series of three or more heat exchangers or a series of three or more heating sections.
28 . (canceled)
29 . The power generating system according to claim 26 , wherein the first compressor comprises a multi-stage, intercooled compressor.
30 . The power generating system according to claim 26 , wherein the second compressor comprises an adiabatic, multi-stage compressor with no intercooling between compressor stages.Join the waitlist — get patent alerts
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