US Patent 9982684 Hybrid metal compressor blades

A hybrid compressor blade having an airfoil portion and a root portion that includes an outer shell comprised of one or multiple types of material that are each located at a predesignated section on the compressor blade, having at least one transition region between two different sections. The transition region is comprised of one or multiple layers with a compositional gradient based upon materials in the neighboring sections to provide a gradual transition from one section to another.