|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02C-009/16 F02C-009/00 F23R-003/40 F23R-003/00|
|미국특허분류(USC)||060/723; 060/726; 060/795|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 4 인용 특허 : 18|
A catalytic gas turbine includes a compressor, a catalytic combustor, a turbine, and a flow path conducting a bypass portion of the compressed air around the combustor and turbine. A method of operating the catalytic gas turbine to activate a catalyst in the catalytic combustor includes opening an inlet guide vane upstream of the compressor to a position to produce an increased volume of compressed air. The increased volume exceeds a volume of compressed air needed to support combustion. A bypass portion of the compressed air is extracted and directed ar...
We claim as our invention: 1. A catalytic gas turbine comprising: a compressor receiving an inlet air and producing compressed air, a catalytic combustor receiving a combustion portion of the compressed air and producing a hot combustion gas; a turbine receiving the combustion gas; a flow path conducting a bypass portion of the compressed air around the combustor and turbine; and further comprising a recirculation flow path receiving a recirculation portion of the compressed air and conducting the recirculation portion into the inlet air. 2. The cata...