The invention relates to a component for a turbomachine, in particular for an aircraft propulsion
system, wherein the component (1, 2, 3) is made of
alloy powder and has a first region (11) and at least one second region (12, 13, 14), a material for a component (1, 2, 3) for a turbomachine, in particular for an aircraft propulsion
system, and a manufacturing method for such a component.