发明申请
US20110016871A1 GAS TURBINE PREMIXING SYSTEMS 失效
气体涡轮增压系统

GAS TURBINE PREMIXING SYSTEMS
摘要:
Methods and systems are provided for premixing combustion fuel and air within gas turbines. In one embodiment, a combustor includes an upstream mixing panel configured to direct compressed air and combustion fuel through a premixing zone to form a fuel-air mixture. The combustor also includes a downstream mixing panel configured to mix additional combustion fuel with the fuel-air mixture to form a combustion mixture.
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