Patent ID: 9599017
Date: 2017-03-21
CPC Classifications: F01K,F02C,F05D,F23R,Y02E

Claim:
1. A turbine system, comprising: a compressor configured to generate a compressed air stream; a combustor configured to receive the compressed air stream from the compressor and to combust a fuel stream to generate a post combustion gas stream; a turbine for receiving the post combustion gas stream from the combustor to generate power and an exhaust gas stream containing a NO a heat recovery system configured to receive the exhaust gas stream exiting the turbine for generation of a cooled gas stream exiting the heat recovery system; a carbon dioxide (CO an auxiliary compressor configured to receive the cooled gas stream exiting the carbon dioxide (CO wherein a first portion of the cooled and compressed gas stream exiting the auxiliary compressor is input to the combustor to generate a film on exposed portions of the combustor, and wherein a second portion of the cooled and compressed gas stream is input to the turbine to provide a cooling flow.