Membrane technology for use in a power generation process
Disclosed herein is a power generation process in which a portion of the carbon dioxide generated by gaseous fuel combustion is recycled back to the power generation process, either pre-combustion, post-combustion, or both. The power generation process of the invention may be a combined cycle process or a traditional power generation process. The process utilizes sweep-based membrane separation.
1. A process for controlling carbon dioxide exhaust from combustion of a gaseous fuel, comprising:
(a) performing a combustion step by combusting a mixture comprising a gaseous fuel and an oxygen-containing gas in a combustor, thereby generating a combustor exhaust stream comprising carbon dioxide and nitrogen;
(b) routing the combustor exhaust stream as at least a portion of a working gas stream to a gas turbine, thereby generating electrical power and creating a turbine exhaust stream;
(c) providing a first membrane having a first feed side and a first permeate side, and being selectively permeable to carbon dioxide over nitrogen and to carbon dioxide over oxygen;
(d) passing at least a portion of the turbine exhaust stream across the first feed side;
(e) withdrawing from the first permeate side a partially concentrated carbon dioxide first permeate stream;
(f) withdrawing from the first feed side a carbon dioxide-depleted first residue stream;
(g) providing a second membrane having a second feed side and a second permeate side, and being selectively permeable to carbon dioxide over nitrogen and to carbon dioxide over oxygen;
(h) passing the first residue stream across the second feed side;
(i) passing air, oxygen-enriched air, or oxygen as a sweep stream across the second permeate side;
(j) withdrawing from the second feed side a second residue stream that is depleted in carbon dioxide compared to the first residue stream;
(k) withdrawing from the second permeate side a second permeate stream comprising oxygen and carbon dioxide; and
(l) passing at least a portion of the second permeate stream to a location between the combustor and the gas turbine as part of the working gas stream.
2. The process of claim 1 , wherein the oxygen-containing gas comprises at least 15 volume % oxygen.
3. The process of claim 1 , wherein the combustor exhaust stream comprises at least 2 volume % oxygen.
4. The process of claim 1 , wherein the process recovers at least 80 volume % of the carbon dioxide generated by the combustion step into the partially concentrated carbon dioxide first permeate stream.
5. The process of claim 1 , wherein the partially concentrated carbon dioxide first permeate stream contains at least 20 volume % carbon dioxide.
6. The process of claim 1 , wherein the first membrane and the second membrane exhibit a selectivity for carbon dioxide over oxygen of at least 10.