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

عظیمی, امیرحسین; عیدی عطارزاده, مسعود; تابع جماعت, صادق; عونی, عباس; ذهاب, صالحه; بال‌زده, محمدمهدی; کنکاش‌ور, بنیامین; آقایاری, مجید

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

نوع مقاله : مقاله پژوهشی

نویسندگان

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

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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