Materials Analysis for Aircraft Engine Aft Cooling Plates Using Estimated Low Cycle Fatigue Life

Substantial cost savings have been demonstrated by material design changes after initial product development. As more information about a product's operating environment becomes available to a designer, it is possible to consider a more costeffective material that still meets or exceeds the design intent, such as minimum low cycle fatigue life. This is especially true in the aircraft engine industry, where precise operating cycle data is not available until after the first engine is built and tested. A methodology for predicting estimated low cycle fatigue life has been developed to investigate potential material change candidates for an aft cooling plate. A twodimensional macromechanical finite element model (FEM) has been developed using ANSYS and used to determine the effects of varying material properties. It is shown that slight changes in density, coefficient of thermal expansion and modulus of elasticity have profound effects on component and effective stresses, and therefore, estimated low cycle fatigue (ELCF) life. Aerospace