Topology optimization analysis of aircraft engine turbine disks.
By considering manufacturing constraints, it leads to obtaining an even more ideal shape.
Using the general-purpose finite element analysis software AIFEM, we will conduct topology optimization analysis of an aircraft engine turbine disk. Since a typical turbine disk is designed based on the engineer's experience, knowledge, and numerous tests, it can be time-consuming and costly, and it may be difficult to achieve an ideal design effect that breaks through existing design thinking. By utilizing AIFEM's topology optimization function, we will perform structural optimization of the turbine disk, taking into account the coupling of thermal loads and centrifugal forces, to obtain a better shape. *For more detailed information, please refer to the related links. For further details, you can download the PDF or feel free to contact us.*
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