Conceptual Design of Aeroderivative Industrial Gas Turbines

سال انتشار: 1399
نوع سند: مقاله ژورنالی
زبان: انگلیسی
مشاهده: 70

فایل این مقاله در 10 صفحه با فرمت PDF قابل دریافت می باشد

استخراج به نرم افزارهای پژوهشی:

لینک ثابت به این مقاله:

شناسه ملی سند علمی:

JR_JASTI-13-2_004

تاریخ نمایه سازی: 8 مرداد 1402

چکیده مقاله:

Designing and manufacturing turbine engines have many complexities and challenges that need time and cost. Therefore, reputable companies producing gas turbines have always sought to shorten the design and construction processes, one of which is to use the core of aerial gas turbines in industrial gas turbines. This category of industrial gas turbines is called aero-derivative gas turbines. Aerial gas turbines can be used as industrial gas turbines due to their particular characteristics such as lightweight, relatively small dimensional size, high efficiency, and performance. These characteristics can shorten the design and manufacturing process. In the present work, ALF ۵۰۲ aero gas turbine has been studied to convert its application to the derived industrial gas turbine. GasTurb software has been used to model this gas turbine for industrial applications. In this study, six different scenarios have been studied for converting aero engines to industrial engines, and results have been discussed. Finally, three scenarios were selected to be implemented on this engine among the studied scenarios.

نویسندگان

Rahman Amiri

Department of Aerospace Engineering Amirkabir University of Technology

Ali Madadi

Department of Aerospace Engineering Amirkabir University of Technology

Abolghasem Mesgarpour Tousi

Department of Aerospace Engineering Amirkabir University of Technology

مراجع و منابع این مقاله:

لیست زیر مراجع و منابع استفاده شده در این مقاله را نمایش می دهد. این مراجع به صورت کاملا ماشینی و بر اساس هوش مصنوعی استخراج شده اند و لذا ممکن است دارای اشکالاتی باشند که به مرور زمان دقت استخراج این محتوا افزایش می یابد. مراجعی که مقالات مربوط به آنها در سیویلیکا نمایه شده و پیدا شده اند، به خود مقاله لینک شده اند :
  • El-Sayed, Ahmed F. Aircraft Propulsion and Gas Turbine Engine. CRC ...
  • Rauch, D., Design Study of an Air Pump and Integral ...
  • Kurzke, J., GasTurb ۱۳ User's Manual, Design and Off-Design Performance ...
  • نمایش کامل مراجع