Two-surface sandwich structure for accommodating in-plane expansion of one of the surfaces relative to the opposing surface
US-9555871-B2 · Jan 31, 2017 · US
US12303994B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12303994-B2 |
| Application number | US-202318365125-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 3, 2023 |
| Priority date | Aug 3, 2023 |
| Publication date | May 20, 2025 |
| Grant date | May 20, 2025 |
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A method of additive manufacturing a structure having integrated passages is provided. In one aspect, the method includes forming first and second parts, each part having a near net shape. The first and second parts are formed by moving a friction stir tool configured to deposit a filler material. An inner surface of each part can be machined to form a generally smooth surface. The first and the second parts are joined to form a structure. The structure is machined to form a generally smooth outer surface. The method includes machining a plurality of grooves extending into the generally smooth outer surface of the structure. A tube is placed into each of the plurality of grooves and a layer of material is deposited to secure the tubes within the plurality of grooves. The method can include machining the outer surface to a predetermined shape.
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What is claimed is: 1. A method of additive manufacturing a part comprising: forming a first part and a second part separate from the first part, each part having a near net shape, the first part and the second part formed by moving a friction stir tool configured to deposit a filler material; machining an inner surface of each part; joining the first part and the second part to form a structure, the inner surfaces of the first part and the second part configured to define an interior space of the structure; machining an outer surface of the structure; machining a plurality of grooves extending into the outer surface of the structure, the plurality of grooves sized to each receive a tube; placing a tube into each of the plurality of grooves; depositing a layer of material configured to secure the tubes within the plurality of grooves by moving the friction stir tool across the outer surface of the structure; and machining the outer surface of the structure to form a predetermined shape. 2. The method of claim 1 , wherein the first part and the second part are hemispheres. 3. The method of claim 1 , wherein the tubes are configured to transport a liquid for heat exchange. 4. The method of claim 1 , wherein the structure has a cylindrical shape. 5. The method of claim 1 , wherein the structure is a tank. 6. The method of claim 1 , wherein joining the first part and the second part comprises at least one of welding, gluing, melting, and fastening the first part and the second part to form the structure. 7. The method of claim 1 , wherein the friction stir tool comprises a spindle having a channel extending along a central axis of the spindle and configured to hold the filler material, and wherein forming a first part and a second part comprises rotating the spindle of the friction stir tool to deposit the filler material held in the channel. 8. A method of additive manufacturing a part comprising: forming a first part having a near net shape and a second part having a near net shape, by depositing layers of material using a friction stir tool, a new layer added to a surface of a previously deposited layer; joining the first part and the second part to form a structure, an inner surface of the first part and an inner surface of the second part configured to define an interior space of the structure; machining a plurality of grooves extending into an outer surface of the structure, the plurality of grooves sized to each receive a wire; positioning a wire into each of the plurality of grooves; securing the wires within the plurality of grooves with additional material deposited over the wires; and machining the outer surface of the structure to form a predetermined shape. 9. The method of claim 8 , further comprising machining the inner surface of the first part and the inner surface of the second part. 10. The method of claim 8 , wherein the first part and the second part are hemispheres. 11. The method of claim 8 , wherein the structure has a cylindrical shape. 12. The method of claim 8 , wherein the structure is a tank and the interior space is configured to hold a gas or a liquid. 13. The method of claim 8 , wherein the wires comprise hollow wires. 14. The method of claim 13 , wherein the hollow wires are configured to transport a gas or a liquid for heat exchange. 15. The method of claim 8 , wherein the wires comprise solid wires. 16. The method of claim 15 , wherein the wires comprise solid aluminum wires. 17. The method of claim 15 , further comprising removing the solid wires from the predetermined shape using a chemical or thermal process. 18. The method of claim 8 , wherein the material is a first material and the wires are formed of a second material different than the first material. 19. The method of claim 8 , wherein the material is a first material and the wires are formed of a second material that is the same as or substantially the same as the first material. 20. The method of claim 8 , wherein joining the first part and the second part comprises at least one of welding, gluing, melting, and fastening the first part and the second part to form the structure.
Tools therefor, e.g. characterised by the shape of the probe · CPC title
Products made by additive manufacturing · CPC title
Processes of additive manufacturing · CPC title
Aluminium or alloys thereof · CPC title
making use of additional material · CPC title
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