发明申请
US20140090392A1 MODEL BASED FUEL-AIR RATIO CONTROL 审中-公开
基于模型的燃油比控制

MODEL BASED FUEL-AIR RATIO CONTROL
摘要:
A gas turbine engine comprises a compressor, a combustor, a turbine, and an electronic engine control system. The compressor, combustor, and turbine are arranged in flow series. The electronic engine control system is configured to estimate combustor fuel-air ratio based on a realtime model-based estimate of combustor airflow, and commands engine actuators to correct for a difference between the estimated combustor fuel-air ratio and a limit fuel-air ratio selected to avoid lean blowout.
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