System and method for low emissions combustion
View Patent ↗A turbine system comprises a compressor for compressing air to generate a compressed flow, an air separation unit for receiving and separating at least a portion of the compressed flow into oxygen and a low-oxygen stream, a combustor for receiving and combusting at least a portion of the low-oxygen stream, a portion of the compressed flow and a fuel to generate a high temperature exhaust gas, and a turbine for receiving and expanding the high temperature exhaust gas to generate electricity and a reduced temperature low-NOx exhaust gas.
1. A turbine system comprising:
a compressor for compressing a first stream of air to generate a compressed flow;
an air separation unit for receiving and separating a second stream of air into oxygen and a low-oxygen stream;
a combustor for receiving and combusting at least a portion of said low-oxygen stream, a portion of said compressed flow and a fuel to generate a high temperature exhaust gas;
a turbine for receiving and expanding said high temperature exhaust gas to generate electricity and a reduced temperature low-NOx exhaust gas;
an Exhaust Gas Recirculation (EGR) circuit including a Heat Recovery Steam Generator (HRSG), wherein said reduced temperature low-NOx exhaust gas is directed to the HRSG for the generation of steam and a reduced temperature exhaust gas;
a flow splitter for splitting said reduced temperature exhaust gas into a first portion and a second portion that is directed to said compressor for compression along with said first stream of air;
a carbon dioxide capture system for receiving the first portion;
a water removal system for receiving and removing excess water from the second portion to produce a low-oxygen, low-water stream; and
a heat exchanger for receiving said second portion and said low-oxygen stream from said air separation unit for heat exchange therebetween.
2. A turbine system in accordance with claim 1 , wherein said steam is directed to a bottoming cycle for the generation of additional electricity.
3. A turbine system in accordance with claim 1 , wherein the first portion is between about 50% to about 80% of the reduced temperature exhaust gas.
4. A turbine system in accordance with claim 1 , wherein said low-oxygen stream has less than about 20% by volume of oxygen.
5. A turbine system in accordance with claim 1 , wherein said low-oxygen stream has less than about 15% by volume of oxygen.
6. A turbine system in accordance with claim 1 , wherein said low-NOx exhaust gas has a NOx level of less than about 30 ppm.
7. A turbine system in accordance with claim 1 , wherein said low-NOx exhaust gas has a NOx level of less than about 10 ppm.