سوخت و احتراق

سوخت و احتراق

طراحی آزمونگر محفظه احتراق توربین گاز و آزمایش محفظه نمونه در شرایط اتمسفریک

نوع مقاله : مقاله پژوهشی

نویسندگان
امیرحسین عظیمی 1
مسعود عیدی عطارزاده 2
صادق تابع جماعت 3
عباس عونی 4
صالحه ذهاب 4
محمدمهدی بال‌زده 5
بنیامین کنکاش‌ور 6
مجید آقایاری 2
1 کارشناس، مهندسی هوافضا، دانشگاه صنعتی امیرکبیر، تهران
2 دانشجوی دکتری، مهندسی هوافضا، دانشگاه صنعتی امیرکبیر، تهران
3 استاد، مهندسی هوافضا، دانشگاه صنعتی امیرکبیر، تهران
4 کارشناس ارشد، مهندسی هوافضا، دانشگاه صنعتی امیرکبیر، تهران
5 کارشناس، مهندسی هوافضا، ، دانشگاه صنعتی امیرکبیر،
6 دانشجوی کارشناسی ارشد، مهندسی هوافضا، دانشگاه صنعتی امیرکبیر، تهران
چکیده
در این مقاله، به طراحی و ساخت آزمونگر محفظه احتراق توربین گاز و آزمایش محفظه نمونه در شرایط اتمسفریک پرداخته شده است. از این آزمونگر می‌توان به­منظور بررسی اثر تغییرات هندسی بر روی عملکرد محفظه احتراق، استخراج نقشه‌ اشتعال‌پذیری و پایداری، بررسی ترکیب گازهای خروجی، توزیع دمای گازهای خروجی و دمای جداره‌ محفظه‌ استفاده کرد. آزمونگر ساخته­شده، قادر به آزمایش محفظه احتراق تا حداکثر دبی هوا 800 مترمکعب بر ساعت بوده و قابلیت پیش‌گرم­کردن هوای ورودی به محفظه تا حداکثر دمای 1000 کلوین را دارد. این آزمونگر قادر به انجام آزمایش با انواع سوخت‌های مایع، گاز طبیعی و LPG است. یک قطاع تک­انژکتوره محفظه احتراق حلقوی در مقطع آزمون نصب شده است. محفظه در شرایط اتمسفریک و دبی هوا و دبی سوخت مختلف آزمایش شده است. نتایج بیانگر آن است که دمای گازهای خروجی از محفظه احتراق به­صورت غیرخطی با افزایش نسبت سوخت به هوا افزایش می‌یابد. با استفاده از مدل یک­بعدی، دمای خروجی از محفظه احتراق پیش­بینی شده و با نتایج تجربی مقایسه شده است. مدل مذکور روند تغییر دمای خروجی از محفظه احتراق را به­خوبی پیش‌بینی می‌کند.
کلیدواژه‌ها
توربین گاز
محفظه احتراق
آزمونگر
مقطع آزمون
اتمسفریک

عنوان مقاله English

Designing a Gas Turbine Combustor Test Rig and Testing a Sample Combustor at Atmospheric Conditions

نویسندگان English

AmirHossein Azimi 1
Masoud EidiAttarZade 2
Sadegh Tabejamaat 3
Abbas Oni 4
Salehe Zahab 4
MohammadMahdi BalZade 5
Benyamin Kankashvar 6
Majid Aghayari 2
1 Amirkabir University of Technology
2 Department of Aerospace Engineering, Amirkabir University of Technology, Tehran, Iran
3 Department of Aerospace Engineering, Amirkabir University of Technology, Tehran, Iran
4 Department of Aerospace Engineering, Amirkabir University of Technology, Tehran, Iran
5 Department of Aerospace Engineering, Amirkabir University of Technology, Tehran, Iran
6 Department of Aerospace Engineering, Amirkabir University of Technology, Tehran, Iran

کلیدواژه‌ها English

Gas turbine
Combustion chamber
Test rig
Test section
atmospheric
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