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TURBOPROPELLER ENGINE CONTROL SYSTEM AND METHOD, PROVIDING OPTIMIZED EFFICIENCY
TURBOPROPELLER ENGINE CONTROL SYSTEM AND METHOD, PROVIDING OPTIMIZED EFFICIENCY
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机译:提供优化效率的涡轮螺旋桨发动机控制系统和方法
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摘要
An electronic control system (30) for a turbopropeller engine (1) having a gas turbine (2, 4, 5, 6) and a propeller (7), coupled to the gas turbine, the control system (10) having a propeller control unit (14) and a turbine control unit (15) to jointly control engine power output based on an input request (PLA), wherein the propeller control unit (14) has a first reference generator (16), to determine a reference propeller speed (Npref) based on the input request (PLA), and a first regulator (19), to regulate a propeller speed (Np). The propeller control unit (14) has a reference correction stage (31) to apply a correction to the reference propeller speed (Npref) and generate thereby a corrected reference propeller speed (I), and the first regulator (19) regulates the propeller speed (Np) based on the corrected reference propeller speed (I) to achieve optimized efficiency.
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机译:用于涡轮螺旋桨发动机(1)的电子控制系统(30),其具有燃气涡轮(2、4、5、6)和与该燃气涡轮相连的螺旋桨(7),该控制系统(10)具有螺旋桨控制装置单元(14)和涡轮控制单元(15)基于输入请求(PLA)共同控制发动机功率输出,其中螺旋桨控制单元(14)具有第一参考发电机(16),以确定参考螺旋桨速度(N pref Sub>)基于输入请求(PLA)和第一调节器(19)来调节螺旋桨速度(N p Sub>)。螺旋桨控制单元(14)具有基准校正级(31),用于对基准螺旋桨速度(N pref Sub>)进行校正,从而生成校正后的基准螺旋桨速度(I),第一个调节器(19)根据校正后的参考螺旋桨速度(I)调节螺旋桨速度(N p Sub>),以实现最佳效率。
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