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MODEL-BASED COORDINATED AIR-FUEL CONTROL FOR A GAS TURBINE

机译:燃气轮机的基于模型的协调空气燃料控制

摘要

A coordinated air-fuel controller (13) and associated method provide a fuel controller (23), a combustion air controller (25) and a steady-state air versus fuel model (15). The fuel controller (23) generates a fuel control output signal (33) and the combustion air controller (25) generates a combustion air control output signal (47). The fuel controller (23) determines a preliminary fuel control signal (41) based on at least one of first and second loop control signals, and determines the fuel control output signal (33) based on the preliminary fuel control signal (41). The steady-state air versus fuel model (15) processes the preliminary fuel control signal (41) to determine an expected steady-state combustion air control signal (53). The combustion air controller (25) determines a preliminary combustion air control signal (51) based on at least one of a third loop control signal (37c) and a fourth loop control signal (37c), and determines the combustion air control output signal (47) based on the preliminary combustion air control signal (51) and the expected steady-state combustion air control signal (53).
机译:协调的空燃控制器(13)和相关方法提供了燃料控制器(23),燃烧空气控制器(25)以及稳态空气对燃料模型(15)。燃料控制器(23)产生燃料控制输出信号(33),燃烧空气控制器(25)产生燃烧空气控制输出信号(47)。燃料控制器(23)基于第一回路控制信号和第二回路控制信号中的至少一个确定初步燃料控制信号(41),并基于初步燃料控制信号(41)确定燃料控制输出信号(33)。稳态空气对燃料模型(15)处理初步燃料控制信号(41)以确定预期的稳态燃烧空气控制信号(53)。燃烧空气控制器(25)基于第三回路控制信号(37c)和第四回路控制信号(37c)中的至少一个来确定预备燃烧空气控制信号(51),并确定燃烧空气控制输出信号( 47)基于初步燃烧空气控制信号(51)和期望稳态燃烧空气控制信号(53)。

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