Method for modular additive manufacturing of a component and a component
A method for the additive manufacturing of a component having the following steps: additively building up multiple sub-sections for the component using a powder bed-based method, arranging the sub-sections to form a composite and additively completing the component, wherein material is deposited, by a deposition welding method, along a peripheral direction around the composite of the sub-sections in such a way that the sub-sections are integrally bonded to each other.
1. A method for additive manufacturing of a component, comprising:
additively building up a multiplicity of sections for the component by a powder bed-based method, wherein the multiplicity of the sections is provided with complementary connections during the additive building up in such a way that the sections are then connectable to each other in a form-fitting manner;
arranging the sections as a composite to form a cavity of the component, wherein the complementary connections of a first section comprise a projection extending away from a planar side surface of the first section configured to engage into a complementary groove recessed into a planar side surface of a second section, so that when the sections are connected to each other in a form-fitting manner along their respective sides, the projection extends entirely between the planar side surface of the first section and into the planar side surface of the second section to space the sections apart from one another to define a cooling passage between the planar side surfaces, wherein the projection extends through a portion of the cooling passage, and wherein a multiplicity of sections is mutually fixed after, or during the arranging; and
additively finishing the component, wherein material is deposited along a circumferential direction around the composite of the sections by a deposition welding method in such a way that the sections are connected to each other in a substance-bonding manner.
2. The method as claimed in claim 1 ,
wherein the composite of the sections is completely encased by the material.
3. The method as claimed in claim 1 ,
wherein the complementary connections are designed to interact via a tongue and groove connection.
4. The method as claimed in claim 1 ,
wherein at least one of the sections forms an inner wall of the component.
5. The method as claimed in claim 1 ,
wherein the multiplicity of the sections form a multi-wall of the component.
6. The method as claimed in claim 1 ,
wherein the multiplicity of the sections is built up in such a way that they form an internal support structure of the component.
7. The method as claimed in claim 1 , wherein at least one of the sections is aftermachined after the additive building up.
8. The method as claimed in claim 7 ,
wherein the at least one of the sections is aftermachined mechanically.
9. The method as claimed in claim 1 ,
wherein the sections are arranged on a prefabricated workpiece.
10. The method as claimed in claim 1 ,
wherein the component is a turbine blade, comprising a blade root section and blade airfoil section.
11. The method as claimed in claim 10 ,
wherein the turbine blade is a rotor blade for a gas turbine.
12. The method as claimed in claim 1 ,
wherein the component is a blade airfoil for a turbine blade.
13. The method as claimed in claim 12 ,
wherein the turbine blade is a rotor blade for a gas turbine.