Gas turbine fuel nozzle with integrated flame ionization sensor and gas turbine engine
摘要:
A gas turbine fuel nozzle for a combustor of a gas turbine engine comprises a sleeve with an internal duct for premixed fuel gas flow; it further comprises a flame ionization sensor located on the sleeve externally to the duct; typically, the combustor has a single annular-shaped chamber.
信息查询
0/0