期刊名称：International Journal of Innovative Research in Science, Engineering and Technology
印刷版ISSN：2347-6710
电子版ISSN：2319-8753
出版年度：2017
卷号：6
期号：7
页码：13900
DOI：10.15680/IJIRSET.2017.0607162
出版社：S&S Publications
摘要：The Optimization of various aero engine components has a very big role in effective development ofmodern aircrafts. In the current project, the rotating compressor disk is the component chosen for shape optimization.The problem of this study is that consideration of aero engine disc that works with a high rotational velocity at elevatedtemperatures. The compressor disk is analyzed in ANSYS APDL tool to get stress outputs and the results are calculatedanalytically. The FEA model of the disc is modeled in an analysis tool ANSYS and analysis is carried out to get stressoutput. Calculating the burst margin for every result output. Selecting the best optimum result by consideration ofminimum disk mass and burst margin increment obtained during the analysis.
