کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
251229 502925 2015 12 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Load mitigation of wind turbine blade by aeroelastic tailoring via unbalanced laminates composites
ترجمه فارسی عنوان
کاهش بار تیغه توربین بادی توسط خیاطی هواپیما از طریق کامپوزیت ورقه نازک
کلمات کلیدی
اتصال پیچ و تاب، عدم تعادل ضخامت کف، کاهش بار خستگی، تقاضای جمعی زمین
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی عمران و سازه
چکیده انگلیسی

The parametric study of unbalanced tri-axial non-crimp fabrics laminates, typically used in the blade skin layup, showed that the highest bend-twist coupling up to 0.56 was achieved when all three kinds of unbalances (i.e. ply-angle, ply-material and ply-thickness unbalances) were simultaneously present in the laminates. Based on aeroelastic tailoring via unbalanced laminates, the bend-twist coupling towards feather of various degrees was implanted to the skin layup of a variable-speed collective-pitch controlled 5 MW wind turbine rotor blades and fully-coupled aero-servo-elastic analyses were performed. The results showed that when the ply-thickness unbalance is added in the skin layup, in addition to already existing ply-angle and ply-material unbalances, an average increase in the coupling magnitude by approximately 51% along the blade length and a reduction in fatigue load and collective-pitch demand by approximately 1.6–2.9% and 5.5–19.9% across the range of applied stochastic winds ranging from 7 m/s to 23 m/s.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Composite Structures - Volume 128, 15 September 2015, Pages 122–133
نویسندگان
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