REVERSE ENGINEERING TERHADAP ANALISIS FATIGUE BILAH KIPAS MESIN TURBOFAN MENGGUNAKAN METODE ELEMEN HINGGA
Abstract
Faktor Intensitas Tegangan (K) akibat adanya perambatan retak pada model bilah kipas mesin turbofan TAY 650-15 yang diperbaiki dengan teknik scallop dikaji secara komputasional. Perubahan harga K terhadap panjang retak diamati untuk memprediksi umur sisa dari bilah kipas. Dari hasil simulasi diperoleh bahwa bilah kipas yang diperbaiki dengan teknik scallop yang melebihi kedalaman dalam SRM akan memiliki umur sisa yang jauh lebih pendek dari umur yang ditentukan oleh pabrik.
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