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基于N-dot的涡扇发动机加速控制器设计
引用本文:黄浏,殷锴,杨文博,郭迎清.基于N-dot的涡扇发动机加速控制器设计[J].航空发动机,2017,43(5):26-30.
作者姓名:黄浏  殷锴  杨文博  郭迎清
作者单位:1. 中国航发商用航空发动机有限责任公司,上海,201108;2. 西北工业大学动力与能源学院,西安,710129
基金项目:航空动力基础研究项目资助
摘    要:针对双转子民用涡扇发动机,进行基于转子加速度的加速控制器设计研究。采用常规的PI控制器结构,针对结构中所需的转子加速度指令,给出了1种满足要求的设计方法,并将PI控制参数的求解过程转化为带约束的非线性优化问题,利用模式搜索算法求解。构建包含稳态控制器和加速控制器的涡扇发动机闭环控制回路,进行加速过程仿真测试。结果表明:所设计的加速控制器满足涡扇发动机加速过程的性能要求,对于工程设计与应用具有一定的参考价值。

关 键 词:N-dot控制  转子加速度计划  模式搜索算法  民用涡扇发动机

Design of Acceleration Controller to a Turbofan Engine Using N-dot Method
Authors:HUANG Liu  YIN Kai  YANG Wen-bo  GUO Ying-qing
Institution:1. AECC Commercial Aircraft Engine Company Limited, Shanghai 201108, China; 2. School of Power and Energy, Northwestern Polytechnical University, Xi''an 710129, China
Abstract:Research on the design of acceleration controller using N-dot method is made for a two-spool civil turbofan engine. Based on the PI controller, an N-dot design method which could fulfill the requirements was given, and a constrained nonlinear optimization problem was proposed to obtain the PI parameters using pattern search algorithm. Then a closed-loop of a turbofan engine control with setpoint controller and acceleration controller both was constructed for acceleration simulation. The results show that the acceleration controller works well in an acceleration process and is of value for engineering application.
Keywords:N-dot control  acceleration schedule  pattern search algorithm  civil engine
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