طراحی کنترل کنندهMIN-MAX برای مدل ترمودینامیکی موتور توربوفن دومحوره غیر مخلوط شونده

نویسندگان

1 علم و صنعت ایران

2 علم و صنعت

چکیده

در این مقاله طراحی کنترلر Min-Max به‌منظور کنترل مدل ترمودینامیکی موتور توربوفن دومحوره غیر مخلوط شونده در نقطه طراحی ارائه شده است. برای این منظور، در ابتدا محدودیت‌های موجود برای عملکرد مطمئن و ایمن موتور توربوفن و همچنین شرایط عملکردی بحرانی موتور مورد نظر، از کاتالوگ‌ها و منابع موجود بدست آمده‌اند و به‌عنوان محدودیت‌های کنترلر در روند طراحی در نظر گرفته شده‌اند. مدل‌سازی ترمودینامیکی موتور توربوفن به همراه طراحی کنترلر در محیط سیمولینک نرم‌افزار MATLAB انجام شده است. نتایج بدست آمده از شبیه‌سازی نشان می‌دهند که کنترلر به‌خوبی تراست مورد درخواست خلبان را تأمین کرده و قیدهای تعریف شده همچون محدودیت سرعت و شتاب محور فشار بالا، محدودیت فشار خروجی از کمپرسور فشار بالا و محدودیت دمای خروجی از محفظه احتراق را رعایت می‌کند و همچنین از وقوع پدیده‌های سرج، استال، خاموشی شعله در محفظه احتراق و ... جلوگیری می‌کند.

کلیدواژه‌ها


عنوان مقاله [English]

Min-Max Controller Design for Double Shaft Unmixed Turbofan Engine’s Thermodynamic Model

نویسندگان [English]

  • morteza montazeri 1
  • morteza hoseini 2
  • amin emani 2
1 elm o sanAt
2 elm o sanAt
چکیده [English]

In this paper, a Min-Max controller design is presented for a doubleshaft unmixed turbofan engine’s thermodynamic model at design point. For this objective, first, the safe operation’s limitations for turbofan engine are determined from the related catalogues and references and used in controller design process. Thermodynamic Modelling and controller design are conducted in Simulink environment of MATLAB software. Simulation results show that the controller effectively provides the thrust command and the limitations of high pressure spool speed and acceleration, output pressure of high pressure compressor and output temperature of combustion chamber are satisfied and surge, stall and flameout events are prevented.

کلیدواژه‌ها [English]

  • Min-Max controller
  • thermodynamic model of turbofan engine
  • performance limitation
  • surge and stall phenomena
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