发明申请
US20110067377A1 GAS TURBINE COMBUSTION DYNAMICS CONTROL SYSTEM 审中-公开
气体涡轮机燃烧动力学控制系统

GAS TURBINE COMBUSTION DYNAMICS CONTROL SYSTEM
摘要:
A system comprises a gas turbine combustor having a plurality of combustor cans, crossfire tubes for connecting combustor cans, and a tubular connection system connecting the combustor cans to control combustion dynamics. The tubular connection system comprises tubes for connecting at least a pair of the combustor cans.
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