Wall component for a combustion chamber and method for manufacturing a wall component

Abstract

A wall component for a combustion chamber, in particular of an engine of an aircraft, is manufactured by an additive manufacturing method, with at least one part of an inner and/or an outer combustion chamber wall, wherein there is at least one mixed air opening arranged with respect to a central axis, having a bordered opening and a circumferential wall surrounding the bordered opening, within the combustion chamber wall. Efficient production can be achieved by the fact that a plurality of flow guide webs extending radially inwards are arranged on the circumferential wall.

Dependencies are inferred from the claim text.