摘要:
The invention relates to a device (10) for additively producing at least one component region of a component (12), in particular a component (12) of a turbomachine. The device (10) can comprise at least one component platform (16), which can be lowered and which has at least one constructing and joining zone (20) for accommodating at least one powder layer of a component material, at least one heating device (24, 28) that can be moved in relation to the component platform (16), and at least one radiation source for producing at least one high-energy beam (22), by means of which high-energy beam the powder layer can be locally fused and/or sintered to form a component layer in the region of the constructing and joining zone (20), and at least one suctioning and/or gas-feeding device (36), which is arranged on the heating device (24, 28). The device (10) can, however, also comprise at least one coating apparatus (14) for applying at least one powder layer of a component material to at least one constructing and joining zone (20) of at least one component platform (16) that can be lowered, wherein the coating apparatus (14) can be moved in relation to the component platform (16), and at least one suctioning and/or gas-feeding device (36), which is arranged on the coating apparatus (14).
摘要:
The invention relates to a device (10) for additively producing at least one component region of a component (12), in particular a component (12) of a turbomachine, wherein the device (10) comprises: at least one coating apparatus (14) for applying at least one powder layer of a component material to at least one constructing and joining zone (20) of at least one component platform (16) that can be lowered, wherein the coating apparatus (14) can be moved in relation to the component platform (16); and at least one radiation source for producing at least one high-energy beam (22), by means of which the powder layer can be locally fused and/or sintered into a component layer in the region of the constructing and joining zone (20). In addition, at least one heating device (24, 28) is arranged on the coating apparatus (14). The invention further relates to a method for producing at least one component region of a component, and a coating apparatus.
摘要:
The invention relates to a method for additively manufacturing at least one component region of a component, in particular of a turbine or compressor component, said method comprising at least the following steps: applying a layer of powder (10a-c) to a component platform in the region of a building and joining area; locally melting and/or sintering the powder layer (10a-c), wherein, in the region of the building and joining area, at least one high-energy beam is moved in relation to the component platform, selectively impinging the powder layer (10a-c), at least part of which at least one high-energy beam and the component platform are moved in relation to one another, in the form of a parallel arrangement (16) arranged along a linear feed direction (12); lowering the component platform by a predetermined layer thickness in a lowering direction; and repeating the above-mentioned steps until the component region is completed. According to the invention, the at least one high-energy beam and the component platform are moved in relation to one another for at least two different powder layers (10a-c) in such a way that, in powder layer regions arranged above one another in a lowering direction, each parallel arrangement (16) of each powder layer (10a-c) is arranged at different angles to each linear feed direction (12). The invention also relates to a device for carrying out a method of this type.