Ganged plate stack in cast plate fin heat exchanger
US-2019277571-A1 · Sep 12, 2019 · US
US10619929B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10619929-B2 |
| Application number | US-201715830537-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 4, 2017 |
| Priority date | Dec 4, 2017 |
| Publication date | Apr 14, 2020 |
| Grant date | Apr 14, 2020 |
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This disclosure provides flow components, methods of additive manufacture, and output manifolds for heat recovery steam generators incorporating flow components. A flow component may include an annular wall that defines a flow path for a fluid. The annular wall may have a normative region and a stress region. The annular wall in the stress region may include a continuous skin to form a portion of the interior wall surface and an additive manufactured mesh adjacent to the continuous skin to the interior of the annular wall. The annular wall in the normative region may have a cross-section with a different structure than the stress region.
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What is claimed is: 1. A flow component comprising: an annular wall having an interior wall surface defining a flow path for a fluid, the annular wall having a wall circumference, a wall length, and a wall thickness; at least one stress region in the annular wall, the at least one stress region including a continuous skin having a skin thickness and defining a portion of the interior wall surface and an additive manufactured mesh adjacent the continuous skin in the direction of the wall thickness, the mesh comprised of structural material and a plurality of voids; at least one normative region in the annular wall, the at least one normative region including a normative cross-section in a direction of the wall thickness that has a different structure than the mesh of the at least one stress region; and wherein the structural material of the mesh includes a plurality of fused geometric nodes of a plurality of sizes and defining the plurality of voids. 2. The flow component of claim 1 , wherein the annular wall defines a junction opening into an adjacent flow component and the at least one stress region is adjacent the junction opening. 3. The flow component of claim 2 , wherein the annular wall has a first wall thickness and a second wall thickness along the wall length and defining a thickness transition region between the first wall thickness and the second wall thickness, the at least one stress region being adjacent to the thickness transition region. 4. The flow component of claim 1 , wherein the structural material of the mesh includes a lattice of repeating support structures defining the plurality of voids. 5. The flow component of claim 4 , wherein the lattice of repeating support structures is arranged in a plurality of concentric rings from the continuous skin outward along the wall thickness at the at least one stress region. 6. The flow component of claim 1 , wherein the structural material defines the plurality of voids to be repeating shapes surrounded by the structural material. 7. The flow component of claim 1 , wherein the normative cross-section is continuously solid structural material. 8. The flow component of claim 1 , wherein the flow component comprises a portion of a manifold for distributing fluids in a power plant. 9. An output manifold for a heat recovery steam generator comprising: an annular wall having an interior wall surface defining a flow path for a fluid, the annular wall having a wall circumference, a wall length, and a wall thickness; at least one stress region in the annular wall, the at least one stress region including a continuous skin having a skin thickness and defining a portion of the interior wall surface and an additive manufactured mesh adjacent the continuous skin in the direction of the wall thickness, the mesh comprised of structural material and a plurality of voids; at least one normative region in the annular wall, the at least one normative region including a normative cross-section in a direction of the wall thickness that has a different structure than the mesh of the at least one stress region; and wherein the structural material of the mesh includes a plurality of fused geometric nodes of a plurality of sizes and defining the plurality of voids. 10. The output manifold of claim 9 , wherein the structural material defines the plurality of voids to be repeating shapes surrounded by the structural material. 11. The output manifold of claim 9 , wherein the annular wall defines a junction opening into an adjacent flow component and the at least one stress region is adjacent the junction opening. 12. The output manifold of claim 11 , wherein the annular wall has a first wall thickness and a second wall thickness along the wall length and defining a thickness transition region between the first wall thickness and the second wall thickness, the at least one stress region being adjacent to the thickness transition region. 13. The output manifold of claim 9 , wherein the structural material of the mesh includes a lattice of repeating support structures defining the plurality of voids. 14. The output manifold of claim 13 , wherein the lattice of repeating support structures is arranged in a plurality of concentric rings from the continuous skin outward along the wall thickness at the at least one stress region. 15. An additive manufactured flow component comprising: an annular wall having an interior wall surface defining a flow path for a fluid, the annular wall having a wall circumference, a wall length, and a wall thickness, wherein the annular wall includes a sintered metal; at least one stress region in the annular wall, the at least one stress region including a continuous skin having a skin thickness and defining a portion of the interior wall surface and an additive manufactured mesh adjacent the continuous skin in the direction of the wall thickness, the mesh comprised of structural material and a plurality of voids; at least one normative region in the annular wall, the at least one normative region including a normative cross-section in a direction of the wall thickness that has a different structure than the mesh of the at least one stress region; and wherein the structural material of the mesh includes a plurality of fused geometric nodes of a plurality of sizes and defining the plurality of voids. 16. The additive manufactured flow component of claim 15 , wherein the structural material of the mesh includes a lattice of repeating support structures defining the plurality of voids. 17. The additive manufactured flow component of claim 16 , wherein the lattice of repeating support structures is arranged in a plurality of concentric rings from the continuous skin outward along the wall thickness at the at least one stress region.
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