Effect of Lattice Structures in the Stress–Strain State for an Impeller Turbine

The stress level of a rotating component is of vital importance in order to ensure its safe operation. The primary source of stress for this type of component is the induced centrifugal stress, which depends on the material, rotational speed, and the distribution of the mass. The reduction of stress has been a topic of study for some time; however, the advent of additive technologies has prompted a new wave of research into the design and manufacture of centrifugal impellers for gas turbine engines, incorporating internal lattice structures (LSs). These structures offer benefits in terms of material savings and load reduction by decreasing the centrifugal force. The present work analyzes the stress–strain state of a turbine centrifugal impeller for six different designs, distinguished by the presence or absence of LSs of various geometries, achievable only through additive technologies. The analysis was conducted on a turbine impeller, which serves as an example of a promising small-scale gas turbine engine (SSGTE). The effectiveness of LSs was assessed through their unloading effect; furthermore, an approach to identify their optimal location within the impeller was demonstrated.