초록 ▼

A method is provided for manufacturing a component. The method includes forming a diffusion coating on a first intermediate article formed by an additive manufacturing process. The diffusion coating is removed from the first intermediate article forming a second intermediate article having at least

A method is provided for manufacturing a component. The method includes forming a diffusion coating on a first intermediate article formed by an additive manufacturing process. The diffusion coating is removed from the first intermediate article forming a second intermediate article having at least one enhanced surface. The diffusion coating is formed by applying a layer of coating material on at least one surface of the first intermediate article and diffusion heat treating the first intermediate article and the layer. The diffusion coating comprises a surface additive layer and a diffusion layer below the surface additive layer. The formation of the diffusion coating and removal thereof may be repeated at least once.

대표청구항 ▼

1. A method for manufacturing a component, the method comprising the steps of: forming a diffusion coating on a first intermediate article formed by an additive manufacturing process; andremoving the diffusion coating from the first intermediate article forming a second intermediate article having a

1. A method for manufacturing a component, the method comprising the steps of: forming a diffusion coating on a first intermediate article formed by an additive manufacturing process; andremoving the diffusion coating from the first intermediate article forming a second intermediate article having at least one enhanced surface. 2. The method of claim 1, wherein the step of forming a diffusion coating comprises: applying a layer of coating material on at least one surface of the first intermediate article;diffusion heat treating the first intermediate article and the layer, the diffusion coating comprising a surface additive layer and a diffusion layer below the surface additive layer. 3. The method of claim 1, further comprising the step of: repeating the forming and removing steps at least once. 4. The method of claim 2, wherein applying the layer of coating material on the at least one surface comprises applying the layer of coating material on an internal passage surface, an external surface, or both the internal passage surface and the external surface of the first intermediate article. 5. The method of claim 2, further comprising the step of consolidating the first intermediate article by a hot isostatic pressing (HIP) process concurrently with the step of diffusion heat treating. 6. The method of claim 2, wherein the step of forming a diffusion coating on a first intermediate article provides an encapsulation layer on the first intermediate article, the encapsulation layer comprising the surface additive layer, the diffusion layer, or both the surface additive layer and the diffusion layer. 7. The method of claim 6, further comprising the step of consolidating the first intermediate article by a hot isostatic pressing (HIP) process concurrently with the step of diffusion heat treating or the second intermediate article by the hot isostatic pressing (HIP) process. 8. The method of claim 1, further comprising the step of consolidating the second intermediate article by a hot isostatic pressing (HIP) process. 9. The method of claim 8, further comprising the steps of: encapsulating the second intermediate article with an encapsulation layer to form an encapsulated article prior to the step of consolidating the second intermediate article; andoptionally removing the encapsulation layer after the consolidating step. 10. The method of claim 2, wherein the diffusion layer includes an upper portion of a substrate of the first intermediate article and wherein the step of removing a diffusion coating additionally removes the upper portion of the substrate to a coating diffusion boundary defining the at least one enhanced surface of the second intermediate article. 11. A method for manufacturing a component from a first intermediate article formed by an additive manufacturing process, the method comprising: applying a coating material layer on at least one surface of the first intermediate article;diffusion heat treating the first intermediate article and the coating material layer to form a diffusion coating on the first intermediate article, the diffusion coating comprising a surface additive layer and a diffusion layer below the surface additive layer, the diffusion layer including an upper portion of a substrate of the first intermediate article;removing the diffusion coating including the upper portion of the substrate from the first intermediate article forming a second intermediate article having at least one enhanced surface; andoptionally repeating the applying, diffusion heat treating, and removing steps at least once. 12. The method of claim 11, wherein the step of applying a coating material layer on at least one surface of the first intermediate article comprises applying the coating material layer on an internal passage surface, an external surface, or on both the internal passage surface and the external surface. 13. The method of claim 11, wherein the step of optionally repeating the applying, diffusion heat treating, and removing steps is performed to reduce residual surface roughness of the second intermediate article, to reduce residual surface-connected cracks with diffusion bond failures in the second intermediate article, or both. 14. The method of claim 11, further comprising the step of consolidating the first intermediate article by a hot isostatic pressing (HIP) process concurrently with the step of diffusion heat treating. 15. The method of claim 11, wherein the steps of applying and diffusion heat treating provide an encapsulation layer on the first intermediate article, the encapsulation layer comprising the surface additive layer, the diffusion layer, or both the surface additive layer and the diffusion layer, the method further comprising the step of consolidating the first intermediate article by a hot isostatic pressing (HIP) process concurrently with the step of diffusion heat treating or the second intermediate article by the hot isostatic pressing (HIP) process. 16. The method of claim 11, further comprising the step of consolidating the second intermediate article by a hot isostatic pressing (HIP) process. 17. The method of claim 16, further comprising the steps of: encapsulating the second intermediate article with an encapsulation layer to form an encapsulated article prior to the step of consolidating the second intermediate article; andoptionally removing the encapsulation layer after the consolidating step. 18. A method for manufacturing a component from a first intermediate article formed by an additive-manufacturing process, the first intermediate article comprised of a substrate and having at least one surface, the method comprising: applying an aluminum-containing coating material layer on the at least one surface, the substrate comprising a nickel-based superalloy;diffusion heat treating the first intermediate article and the aluminum-containing coating material layer to yield an aluminide diffusion coating on the first intermediate article, the aluminide diffusion coating comprising an aluminum-rich surface additive layer and a diffusion layer below the aluminum-rich surface additive layer, the diffusion layer including an upper portion of the substrate;removing the aluminide diffusion coating from the first intermediate article thereby forming a second intermediate article having at least one enhanced surface; andoptionally repeating the applying, diffusion heat treating, and removing steps at least once. 19. The method of claim 18, further comprising a step of finishing the second intermediate article to produce the component. 20. The method of claim 18, wherein the first intermediate article comprises a first intermediate turbine article and the at least one surface comprises an internal passage surface of at least one cooling passage of a turbine component, an external surface of the turbine component, or both.