بررسی عددی اثر افزودن نانو ذرات به روغن موتور بالگرد

نویسندگان

1 دانشکده مهندسی مکانیک دانشگاه فردوسی مشهد

2 مرکز توسعه علوم و فناوری مهندسی سطح و خوردگی شرکت پشتیبانی و نوسازی بالگردهای ایران (پنها)

3 تهران-انتهای اتوبان شهید بابایی-دانشگاه جامع امام حسین (ع)

چکیده

در این مقاله عملکرد نانوذرات افزوده‌‌شده به روغن با هدف بهبود انتقال حرارت مورد بررسی قرار گرفته است. در ابتدا، خصوصیات ترموفیزیکی روغن بالگرد (MIL-L-23699) با همکاری آزمایشگاه شیمی شرکت پشتیبانی و نوسازی بالگردهای ایران (پنها)، اندازه‌گیری شدند. سپس، با گرداوری سایر داده‌ها هندسه مسئله با نرم‌افزار گمبیت تولید و شبکه‌بندی شده و برای شبیه‌سازی جریان و انتقال حرارت به نرم‌افزار انسیس فلوئنت 2/17 انتقال داده شده است. از مدل تک‌فازی و روش حجم ‌محدود برای حل این مسئله استفاده شده است. نتایج نشان داد که با افزودن نانوذرات به روغن بالگرد خواص حرارتی، نظیر عدد ناسلت نسبت به روغن خالص به‌طور قابل توجهی بهبود می‌یابد و این درحالی است که بهبود فرایند انتقال حرارت برای نانوسیال طلا- روغن نسبت به نانوسیالات دیگر بیشتر می‌باشد. همچنین، مقایسه نتایج نشان داد، افزودن نانوذرات به روغن پایه سبب ایجاد تغییر فشار ناچیزی می‌شود، ولی در پمپاژ نانوسیال تاثیر خاصی ندارد. از طرفی نتایج نشان داد، با افزایش عدد رینولدز، عدد ناسلت و فشار استاتیکی افزایش و ضریب اصطکاک کاهش می‌یابد. همچنین، ملاحظه شد در یک رینولدز ثابت با افزایش دمای کاری، عدد ناسلت، ضریب اصطکاک و فشار استاتیکی کاهش و دمای بی‌بعد افزایش می‌یابد. بنابراین، افزودن نانوذرات به روغن بالگرد سبب بهبود خواص انتقال حرارت، خنک‌کاری بهتر موتور، کوچک‌سازی سیستم روان‌کاری موتور، توانایی تحمل بارگذاری‌های زیاد، توانایی پرواز در ارتفاعات بالاتر و در نهایت افزایش قدرت و بازدهی موتور خواهد شد.

کلیدواژه‌ها


عنوان مقاله [English]

Numerical Investigation of the Effect of Adding Nanoparticles to Helicopter Motor Oil

نویسندگان [English]

  • ali shakiba 1
  • omran karami zarandi 2
  • khodadad vahedi 3
1 ferdosi mashhad
2 -
3 emam hosein
چکیده [English]

In this paper, the effects of added nanoparticles to oil with the aim of improving heat transfer were investigated. At first, thermophysical characteristics of helicopter oil (MIL-L-23699) were measured by cooperation of chemical laboratory of Iran Helicopter Support and Renewal Company (PANHA). Then, by collecting other data, geometry of the problem was produced and gridded through the use of Gambit software and was transmitted to Ansys Fluent 17.2 for simulating the flow and heat transfer. The single-phase model and control volume technique have been used to solve this problem. The results reveal that by adding nanoparticles to helicopter oil, thermal properties, such as Nusselt number, considerably improve in comparison with pure oil. However, the improvement of heat transfer process for gold-oil nanofluid is more than the other nanofluids. Comparing the results also shows that adding nanoparticles to the base oil causes a slight pressure change, which has no special effect on nanofluid pumping. The results indicate that by increasing Reynolds number, Nusselt number and static pressure increase and friction coefficient decreases. It is also observed that in a constant Reynolds number, by increasing working temperature, Nusselt number, friction coefficient, and static pressure decrease and temperature increases. Therefore, adding nanoparticles to helicopter oil would lead to the improvement of heat transfer properties, better cooling of the size of engine, shrinking the engine lubrication system, the ability of tolerating high loads, the ability of flying at higher altitudes, and eventually the enhancement of power and efficiency of the engine.

کلیدواژه‌ها [English]

  • Nanofluid
  • Heat Transfer
  • Lubrication
  • Helicopter Oil
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