发明申请
US20090241510A1 Pressure control method and system to reduce gas turbine fuel supply pressure requirements 有权
压力控制方法和系统降低燃气轮机燃油供应压力要求

Pressure control method and system to reduce gas turbine fuel supply pressure requirements
摘要:
A system and method to reduce the gas fuel supply pressure requirements of a gas turbine, which results in an increased operability range and a reduction in gas turbine trips. According to the method, the gas turbine is allowed to start and operate at supply pressures determined as a function of ambient conditions and gas turbine compressor pressure ratio. This increases the operability window, and reduces or eliminates the need for gas fuel compressors.
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