The required power of the MGT-40 gas turbine starter
عنوان مقاله: The required power of the MGT-40 gas turbine starter
شناسه ملی مقاله: JR_EES-3-2_006
منتشر شده در شماره 2 دوره 3 فصل Summer and Autumn در سال 1394
شناسه ملی مقاله: JR_EES-3-2_006
منتشر شده در شماره 2 دوره 3 فصل Summer and Autumn در سال 1394
مشخصات نویسندگان مقاله:
Saadat Zirak - Faculty of Mechanical Engineering Department Semnan University, Semnan, Iran
Hamid Ebrahimi - Aerospace Department Sharif University Of Technology Tehran, Iran
Ahmad Reza Maissamy - MapnaTurbine Company (TUGA), Karaj, Iran
خلاصه مقاله:
Saadat Zirak - Faculty of Mechanical Engineering Department Semnan University, Semnan, Iran
Hamid Ebrahimi - Aerospace Department Sharif University Of Technology Tehran, Iran
Ahmad Reza Maissamy - MapnaTurbine Company (TUGA), Karaj, Iran
Determination of the starter torque-speed diagram is a major task in the design or selection of a proper gas turbine starter. In this paper, the maximum power of the MGT-40 gas turbine starter was calculated based on the dynamics of the rotor, start-up logic, and compressor map. In a recent research, the pressure ratio was assumed as a linear function of the rotor speed and the required starter power was calculated. In this study, the value is determined from the field data. To evaluate the proposed method, the results of obtained power were compared with that of the turbine performance reports. The comparison resulted in a reasonable engineering approximation
کلمات کلیدی: Compressor Map, Gas Turbine Starter, Start-up Logic, Start-up Power, Torque-Speed Diagram
صفحه اختصاصی مقاله و دریافت فایل کامل: https://civilica.com/doc/515085/