بهبود شبیه‌ساز یک‌بعدی موتور ملی با در نظر گرفتن اثرات انتقال حرارت و افت مکانیکی در توربوشارژر

نوع مقاله : مقاله پژوهشی

نویسندگان

1 دانشکده مهندسی مکانیک، دانشگاه صنعتی امیرکبیر، تهران، ایران

2 شرکت تحقیق، طراحی و تولید موتور ایران خودرو (ایپکو)، تهران، ایران

چکیده

امروزه توربوشارژر‌ها (پرخوران‌ها) نقش مهمی در بهبود بازده، کوچک‌سازی و کاهش آلاینده‌های موتور احتراق داخلی ایفا می‌کنند. به دلیل جریان گاز داغ در توربین و هوای محیط در کمپرسور، اختلاف دما در دو سمت توربوشارژر زیاد است و این اختلاف دمای زیاد، باعث انتقال حرارت از توربین به دیگر اجزا توربوشارژر می‌شود. انتقال حرارت سبب کاهش عملکرد توربوشارژر می‌گردد، زیرا قسمتی از انرژی گاز داغ از طریق انتقال حرارت دفع شده است. نیاز به تخمین دقیق دمای گازهای خروجی توربین جهت طراحی مسیر گازهای خروجی یا تعیین شرایط مرزی توربوشارژر دوم در موتورهای دارای توربوشارژر‏های دومرحله‌ای،  همچنین نیاز به تخمین دمای خروجی کمپرسور به‌عنوان شرایط مرزی برای خنک‌کن میانی و محفظه احتراق در صورت نبود خنک‌کن میانی وجود دارد. در این پژوهش، الگوی انتقال حرارت یک‌بعدی توربوشارژر، به شبیه‌ساز یک‌بعدی موتور درگیر می‌شود. نتایج نشان‌دهنده‌ی بهبود (حداکثر تا 50 درجه سانتی‌گراد) در پیش‌بینی دمای خروجی توربین است و همچنین بر روی دیگر مشخصه‌های شبیه‌سازی موتور از جمله دمای خروجی کمپرسور، سرعت توربوشارژر، توان ترمزی موتور، فشار خروجی توربین و غیره، تأثیر نمی‌گذارد.

کلیدواژه‌ها

موضوعات


عنوان مقاله [English]

Improvement of one-dimensional simulation of national engine with consideration of heat transfer and mechanical loss effects in the turbocharger

نویسندگان [English]

  • masoud kahnooji 1
  • S.Mostafa Agha Mirsalim 1
  • Seyed Shahaboddin Alaviyoun 2
1 Energy conversion, Mechanical engineering, Amirkabir university, Tehran, Iran
2 Irankhodro Powertrain Company, Tehran, Iran
چکیده [English]

Nowadays, Turbochargers play an important role in improving the efficiency,
downsizing and pollutant reduction of internal combustion engine. Due to
the existence of hot gas flow in the turbine and surrounding air flow in the compressor,
the temperature difference between two sides of turbocharger is high and this high
temperature difference causes heat transfer from the turbine to the other
turbocharger components. The heat transfer reduces the turbocharger performance
because some of the hot gas energy has been removed through heat transfer. There is a need to accurate estimation of the temperature of the turbine exhaust gases to determine the path of the exhaust gases or to determine the boundary conditions of the second turbocharger in engines containing (two-stage turbochargers), and also a need to estimate the compressor outlet temperature as a boundary condition for intercooler and combustion chamber in the absence of an intercooler. In this study, turbocharger one-dimensional heat transfer model is coupled to one-dimensional engine simulation. The results show an improvement (up to 50 °C) in prediction of turbine outlet temperature and also does not affect other characteristics of the engine simulation such as compressor outlet temperature, turbocharger speed, engine brake power, turbine outlet pressure and etc.

کلیدواژه‌ها [English]

  • Turbocharger
  • mechanical loss
  • heat transfer
  • one dimensional simulation
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