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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