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Research on control law for a sub-idle engine operation

机译:亚空转发动机运行控制规律研究

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Starting is a process which an gas turbine has to experience before it operating between the idle and maximum power points, and the problem how to ensure an gas turbine succeed to rapidly and safely start is necessary to be taken seriously. Most control laws only address the operating range between the idle and maximum power points because of the lack of models which can simulate a sub-idle engine operation. The paper gives a control law for a sub-idle engine operation based on a existed starting model. A closed loop control law for the total temperature after the primary combustion chamber (TT4) was proposed in order to persistently obtain the maximum surplus power during a whole starting process of an aero-engine. Meanwhile, several limit controllers for surge margin is added to the reference command of the TT4 closed loop, taking into account prevention against surge or stall. Moreover, freezing the integral of the PT controller before the ignition of an engine is introduced to anti-windup. The result of simulation illustrates that an turbofan engine can successfully start from engine off to idle power with a persistent maximum surplus power and the protection of several limit controllers, which can guarantee adequate surge margin of 3 compression components and TT4 to not exceed the maximum value.
机译:起动是燃气轮机在怠速和最大功率点之间运行之前必须经历的过程,并且必须认真考虑如何确保燃气轮机成功快速且安全地起动的问题。由于缺乏可模拟次怠速发动机运行的模型,大多数控制定律仅针对怠速和最大功率点之间的运行范围。基于现有的起动模型,给出了副怠速发动机运行的控制规律。为了在航空发动机的整个启动过程中持续获得最大的剩余功率,提出了对主燃烧室(TT4)之后的总温度的闭环控制定律。同时,考虑到防止电涌或失速,将几个电涌裕量极限控制器添加到TT4闭环的参考命令中。此外,在引入发动机点火之前,冻结PT控制器的积分以防结垢。仿真结果表明,涡扇发动机能够以持久的最大剩余功率和几个极限控制器的保护,成功地从发动机关闭转入怠速,这可以确保3个压缩组件和TT4的足够喘振裕度不超过最大值。

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