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微型发动机温度限制保护闭环控制设计方法
引用本文:缪柯强,王曦. 微型发动机温度限制保护闭环控制设计方法[J]. 航空发动机, 2017, 43(3): 50-55
作者姓名:缪柯强  王曦
作者单位:1. 北京航空航天大学能源与动力工程学院,2.先进航空发动机协同创新中心:北京100191
基金项目:航空动力基础研究项目资助
摘    要:针对微型涡喷发动机转子转速闭环设计的控制结构中涡轮出口温度对燃油供给率变化敏感的问题,尤其在快速推油门杆时可能会超温,提出了1种带涡轮出口温度限制保护的闭环限制控制器的设计方法。该方法采用了双回路的闭环结构方式,并采用控制参数相似变换的增益调度增量式PI控制方法,实现了稳态/过渡态的发动机转速、温度闭环控制,所述算法在Simulink环境下进行了地面和高空的仿真验证。结果表明:控制系统在保证转子转速伺服跟踪性能的要求下还具有温度保护功能。

关 键 词:微型涡喷发动机;超温保护;增益调度;伺服跟踪

Design Method of Close Loop Controller with Temperature Limitation Protection forMicro Gas Turbine Engines
MIAO Ke-qiang,WANG Xi. Design Method of Close Loop Controller with Temperature Limitation Protection forMicro Gas Turbine Engines[J]. Aeroengine, 2017, 43(3): 50-55
Authors:MIAO Ke-qiang  WANG Xi
Affiliation:1.School of Energy and Power Engineering,Beihang University,2. Collaborative Innovation Center for AdvancedAero-Engine;Beijing 100191,China
Abstract:In order to solve the problem that the turbine outlet temperature is sensitive to the change of fuel flow in the close-loopdesigned rotor speed control structure of micro gas turbine engines, especially pushing the throttle lever quickly, a method in designing theclose-loop controller with turbine outlet temperature protection was presented. Dual circuit close-loop structure was adopted in this method.The gain-scheduled incremental PI control law with corrected control parameters was used. Set-point and transient close-loop control wasrealized in the rotor speed and temperature protection loop. The algorithm above was simulated in the standard sea level and high altitudeenvironment in the Simulink platform. The result proves that the designed control system has the ability of rotor speed servo tracking andtemperature protection at the same time
Keywords:micro gas turbine engine  over-temperature protection  gain-schedule  servo tracking
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