Method for producing a component using a sintering process

摘要

The present disclosure relates generally to engine technology. In particular, the present disclosure relates to the manufacture of engine components with a complex geometric structure. In particular, the present disclosure relates to a method (70) for producing a complex component (32), comprising providing (72) a first component (34a), comprising a first component thermal expansion coefficient; a first joining surface (36a); and a first bearing surface (40a, 40b, 40c); Providing (74) a second component (34b) having a second component thermal expansion coefficient; a second joining surface (36b); and a second bearing surface (42a, 42b, 42c); Providing (76) a jacket element (38) having a jacket element thermal expansion coefficient; and a jacket element bearing surface (48a, 48b, 48c, 48d); and heating (78) the first component (34a), the second component (34b) and the casing element (38) from a first temperature to a second temperature in order to carry out a joining process of the first component (34a) and the second component (34b). The present disclosure further relates to a component, in particular for a gas turbine engine for an aircraft, and to such a gas turbine engine.