|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02C-006/08 F02C-006/00 F02C-006/18 F02C-007/26|
|미국특허분류(USC)||060/786; 060/782; 060/794; 060/795|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 15 인용 특허 : 26|
A gas turbine includes a compressor, a combustor, a turbine, and a flow path diverting an excess portion of the compressed air produced by the compressor around the turbine. The flow path conducts the excess portion into a turbine exhaust gas flow producing a cooled exhaust gas. A method of operating the gas turbine includes opening an inlet guide vane of the compressor to allow the compressor to produce an increased volume of compressed air. The increased volume exceeds a volume of compressed air needed to support combustion. An excess portion of the co...
We claim as our invention: 1. A gas turbine comprising: a compressor producing compressed air; a combustor receiving a combustion portion of the compressed air and producing a hot combustion gas; a turbine receiving the hot combustion gas and producing an exhaust gas; an inlet guide vane upstream of the compressor for controlling a volume of ambient air delivered to the compressor; a controller for generating an inlet guide vane control signal to adjust a position of the inlet guide vane for providing a desired volume of ambient air delivered to the com...