Gas turbine inlet fogging system and method for inlet fogging control
摘要
The present application provides an inlet air fogging system (100) for a gas turbine engine (110). The inlet air fogging system (100) may include a fogging nozzle array (270) and a fogging control system (320) in communication with the fogging nozzle array (270). The fogging control system (320) may include a droplet size measurement system (340) and a humidity level measurement system (390).
申请公布号
EP2570631(A3)
申请公布日期
2014.04.16
申请号
EP20120184194
申请日期
2012.09.13
申请人
GENERAL ELECTRIC COMPANY
发明人
CHILLAR, RAHUL J.;MITRA, CHAYAN;MESTRONI, JULIO ENRIQUE;MAITY, SANDIP;SHARMA, RACHIT