چکیده مقاله
Health monitoring and life prediction of gas turbine units issignificant for the purpose of preventing component failureand catastrophic engine outage Along this, it is essential toestimate remaining life of the engine considering differentdamage mechanisms formed in the hot section components Thermal barrier coatings TBCs are commonly used toincrease temperature and corrosion resistance in hot sectioncomponents in order to improve the efficiency of the gasturbine units as well as the life extension of components Thispaper aims to estimate TBC life of combustion chamber of agas turbine unit considering the influence of oxide layergrowth and thermo mechanical fatigue effect Then,considering various in service conditions for the gas turbineunit, prediction models were developed for different zoneswith the aim to online life calculation and health monitoringof the combustion chamber
کلیدواژهها
نویسندگان
Pedram Zamani
Mechanical Design Expert, Mechanical Integration Department, Turbotec Company, Tehran, Iran
Hamid Arab Qomi
Mechanical Design Expert, Mechanical Integration Department, Turbotec Company, Tehran, Iran
Hossein Veisi
Head of Mechanical Design section, Mechanical Integration Department, Turbotec Company, Tehran, Iran
Mahdi Bonyadi
Head of Mechanical Integration Department, Turbotec Company, Tehran, Iran
Mohammad Alizadeh
Head of Engineering Deputy, Turbotec Company, Tehran, Iran
شیوه ارجاع
Zamani, Pedram and Arab Qomi, Hamid and Veisi, Hossein and Bonyadi, Mahdi and Alizadeh, Mohammad,1401,Coating life prediction and health monitoring of a gas turbine combustion chamberbased on performance-based prediction functions,The 19th National Conference and the 8th International Conference on Construction and Production Engineering of Iran,Mashhad
ارائهشده در
مجموعه مقالات نوزدهمین همایش ملی و هشتمین کنفرانس بین المللی مهندسی ساخت و تولید ایران18 اسفند 1401 · مشهد