What is claimed is:
1 . A process of producing a near-net shape component, the process comprising:
forming a consolidation shell by additive manufacturing, the consolidation shell defining an interior space having a geometry corresponding to a component; providing a metallic powder to the interior space; removing gas from the interior space; and consolidating the metallic powder in the consolidation shell under sufficient heat and pressure to form the near-net shape component.
2 . The process of claim 1 , wherein the consolidating includes hot isostatic pressing.
3 . The process of claim 1 , wherein the metallic powder includes metals selected from the group consisting of nickel, cobalt, titanium, iron, alloys thereof and combinations thereof.
4 . The process of claim 1 , wherein the geometry corresponding to the component includes a geometry that forms the near-net shape component after consolidation.
5 . The process of claim 1 , further comprising removing the consolidation shell.
6 . The process of claim 5 , wherein removing the consolidation shell includes a removal process selected from the group consisting of machining, electrical removal or chemical removal.
7 . The process of claim 1 , wherein the consolidation shell includes a second, removable material to form channels in the component.
8 . The process of claim 1 , wherein the near-net shape component is a compressor blade.
9 . The process of claim 1 , wherein the providing a metallic powder to the interior space includes providing a first metallic powder and a second metallic powder.
10 . The process of claim 9 , wherein the first metallic powder and the second metallic powder have dissimilar compositions.
11 . The process of claim 9 , wherein the first metallic powder and the second metallic powder have dissimilar properties.
12 . The process of claim 1 , wherein the consolidation shell forms a coating material on the component.
13 . A consolidation shell comprising:
an interior space having a geometry corresponding to a component; and a conduit extending from the interior space; wherein metallic powder is present in the interior space.
14 . The consolidation shell of claim 13 , wherein the component is a compressor blade.
15 . The consolidation shell of claim 13 , wherein the metallic powder is a metal selected from the group consisting of nickel, cobalt, titanium, iron, alloys thereof and combinations thereof.
16 . The consolidation shell of claim 13 , wherein the metallic powder includes a first metallic powder and a second metallic powder.
17 . A component comprising:
a consolidation shell formed by additive manufacturing, the consolidation shell defining an interior space having a geometry corresponding to the component, the interior space being at least partially filled with a consolidated powder.
18 . The component of claim 17 , wherein the component is selected from the group consisting of a turbine bucket, a compressor blade, a compressor vane, an airfoil segment, a nozzle, a shroud, and a combustion component.
19 . The component of claim 17 , wherein the component is a compressor blade.
20 . The component of claim 17 , wherein the consolidation shell forms a coating on the component.