کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
648795 1457199 2009 10 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
The effect of start-up cycle in ceramic coating used as thermal barrier for a gas turbine bucket
موضوعات مرتبط
مهندسی و علوم پایه مهندسی شیمی جریان سیال و فرایندهای انتقال
پیش نمایش صفحه اول مقاله
The effect of start-up cycle in ceramic coating used as thermal barrier for a gas turbine bucket
چکیده انگلیسی
The role of thermal barrier coatings (TBC) is, as their name suggests, to provide thermal insulation of the blade. A coating of about 100-400 μm can reduce the temperature by up to 200 °C. A TBC can be used either to reduce the need for blade cooling (by about 36%) increasing the turbine efficiency, while maintaining identical creep life of the substrate; or to increase considerably the creep life of the blade while maintaining level of blade cooling (and therefore allowing the blade to operate at a lower temperature for an identical turbine inlet temperature).
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Applied Thermal Engineering - Volume 29, Issues 14–15, October 2009, Pages 3056-3065
نویسندگان
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