کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
299784 512445 2016 19 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Effect of nozzle and combustion chamber geometry on the performance of a diesel engine operated on dual fuel mode using renewable fuels
ترجمه فارسی عنوان
تاثیر نازل و هندسه محفظه احتراق بر عملکرد یک موتور دیزل که در حالت سوخت دوگانه با استفاده از سوخت های تجدید پذیر عمل می کند
کلمات کلیدی
گاز تولید کننده، موتور سوخت دوگانه سیستم گازسفجر، محفظه احتراق، کارایی، احتراق و انتشار
موضوعات مرتبط
مهندسی و علوم پایه مهندسی انرژی انرژی های تجدید پذیر، توسعه پایدار و محیط زیست
چکیده انگلیسی


• Gasifier-engine system with optimum engine parameters makes the system completely independent from fossil fuels.
• HOME – producer gas combination under a dual-fuel mode does not require any major engine modifications.
• This work presents the effect of engine parameters on the performance of HOME-producer gas fueled diesel engine.
• Gasifier-engine system with renewable fuels favored a high injection pressure of 230 bar and re-entrant combustion chamber.

Renewable and alternative fuels have numerous advantages compared to fossil fuels as they are biodegradable, providing energy security and foreign exchange saving and addressing environmental concerns, and socio-economic issues as well. Therefore renewable fuels can be predominantly used as fuel for transportation and power generation applications. In view of this background, effect of nozzle and combustion chamber geometry on the performance, combustion and emission characteristics have been investigated in a single cylinder, four stroke water cooled direct injection (DI) compression ignition (CI) engine operated on dual fuel mode using Honge methyl ester (HOME) and producer gas induction. In the present experimental investigation, an effort has been made to enhance the performance of a dual fuel engine utilizing different nozzle orifice and combustion chamber configurations. In the first phase of the work, injector nozzle (3, 4 and 5 hole injector nozzle, each having 0.2, 0.25 and 0.3 mm hole diameter and injection pressure (varied from 210 to 240 bar in steps of 10 bar) was optimized. Subsequently in the next phase of the work, combustion chamber for optimum performance was investigated. In order to match proper combustion chamber for optimum nozzle geometry, two types of combustion chambers such as hemispherical and re-entrant configurations were used. Re-entrant type combustion chamber and 230 bar injection pressure, 4 hole and 0.25 mm nozzle orifice have shown maximum performance. Results of investigation on HOME-producer gas operation showed 4–5% increased brake thermal efficiency with reduced emission levels. However, more research and development of technology should be devoted to this field to further enhance the performance and feasibility of these fuels for dual fuel operation and future exploitations.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Renewable Energy - Volume 93, August 2016, Pages 483–501
نویسندگان
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