Form-fitting housing component combination and method for the manufacture thereof

Abstract

A component combination for a shell of a flow channel (10) of a turbomachine, in particular for a housing of a gas turbine or an aircraft engine, including at least two components, a first component (1) forming a closed ring. The closed ring is axially and/or radially held in a form-fitting manner against at least one second component (2) in relation to the flow channel and is able to be removed from or placed into this position only by elastically deforming the ring without changing the second component; the present invention also includes a method for manufacturing a component combination of this type and a corresponding turbomachine having a component combination of this type.

Dependencies are inferred from the claim text.