| 摘要 |
PROBLEM TO BE SOLVED: To provide a component, a turbine component, and a method of forming them.SOLUTION: A component (100) includes a first component section (102) and a second component section (104) that are joined to form a hollow structure (106) defining a plenum (108) having an interior surface (110). The component sections each include mating ridges (120, 122, 124, 126) joined together along a length (114) of the plenum, and a corrosion-resistant cladding layer (128) including a corrosion-resistant material (130) overlaying the interior surface of the plenum. In one embodiment, the component is a gas turbine combustor fuel manifold. A method of forming the component includes applying corrosion-resistant segments including a corrosion-resistant material to each of the surfaces of the component sections, and joining the component sections to form the component, where the joining step includes fusing the corrosion-resistant segments into the corrosion-resistant cladding layer, and joining the mating ridges of the component sections.SELECTED DRAWING: Figure 1 |
