Method and assembly for bonding complex composite assemblies
US-10632687-B2 · Apr 28, 2020 · US
US11358350B1 · US · B1
| Field | Value |
|---|---|
| Publication number | US-11358350-B1 |
| Application number | US-201815967037-A |
| Country | US |
| Kind code | B1 |
| Filing date | Apr 30, 2018 |
| Priority date | Jun 30, 2017 |
| Publication date | Jun 14, 2022 |
| Grant date | Jun 14, 2022 |
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A method of forming a sandwich structure including at least partially filling an open volume of an open cellular core with a sacrificial mold material, consolidating the sacrificial mold material to form a sacrificial mold, laying up a composite facesheet on each of at least two surfaces of the open cellular core, co-curing the composite facesheets by applying a consolidation temperature and a compaction pressure to the composite facesheets to form the sandwich structure, and removing the sacrificial mold. The compaction pressure is greater than a compressive strength of the open cellular core and less than a combined compressive strength of the open cellular core and the sacrificial mold.
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What is claimed is: 1. A method of forming a sandwich structure, the method comprising: at least partially filling an open volume of an open cellular core with a sacrificial mold material; placing the open cellular core in a chamber of a mold before at least partially filling the open volume with the sacrificial mold material; pressing the at least two surfaces of the open cellular core into at least one spacer positioned between the open cellular core and inner surfaces of the chamber, the at least one spacer masking the at least two surfaces of the open cellular core from contact with the sacrificial mold material; consolidating the sacrificial mold material to form a sacrificial mold; laying up a composite facesheet on each of at least two surfaces of the open cellular core; and co-curing the composite facesheets by applying a consolidation temperature and a compaction pressure to the composite facesheets to form the sandwich structure, wherein the compaction pressure is greater than a compressive strength of the open cellular core and less than a combined compressive strength of the open cellular core and the sacrificial mold. 2. The method of claim 1 , wherein the at least one spacer comprises a material selected from the group of materials consisting of silicone, rubber, closed cell foam, a polymer film, and combinations thereof. 3. The method of claim 1 , wherein the consolidation temperature is from about 23° C. to about 180° C. 4. The method of claim 1 , wherein the compaction pressure is from about 0.1 MPa to about 12 MPa. 5. A method of forming a sandwich structure, the method comprising: at least partially filling an open volume of an open cellular core with a sacrificial mold material; applying a release agent to the open cellular core before at least partially filling of the open volume with the sacrificial mold material; masking the at least two surfaces of the open cellular core against exposure to the release agent; consolidating the sacrificial mold material to form a sacrificial mold; laying up a composite facesheet on each of at least two surfaces of the open cellular core; and co-curing the composite facesheets by applying a consolidation temperature and a compaction pressure to the composite facesheets to form the sandwich structure, wherein the compaction pressure is greater than a compressive strength of the open cellular core and less than a combined compressive strength of the open cellular core and the sacrificial mold. 6. The method of claim 1 , wherein the at least partially filling of the open volume with the sacrificial mold material is performed by a process selected from the group of processes consisting of pouring under gravity, filling under vacuum, filling under positive pressure, sifting powder, compaction of powder, and combinations thereof. 7. The method of claim 1 , wherein the sacrificial mold material is selected from the group of materials consisting of eutectic salt, plaster, polyethylene glycol (PEG), polyethylene oxide (PEO), ceramic spheres, wax, and combinations thereof. 8. The method of claim 1 , wherein each of the at least two composite facesheets comprises pre-impregnated fiber reinforced polymers. 9. The method of claim 1 , wherein each of the at least two composite facesheets comprises a dry fabric reinforcement layer and a liquid resin on the dry fabric reinforcement layer. 10. The method of claim 1 , wherein the removing of the sacrificial mold is performed by a process selected from the group of processes consisting of burning the sacrificial mold, dissolving the sacrificial mold, etching the sacrificial mold, fracturing the sacrificial mold, evaporating the sacrificial mold, melting the sacrificial mold, and combinations thereof. 11. The method of claim 1 , wherein the open cellular core comprises a plurality of struts arranged in a lattice structure. 12. The method of claim 11 , wherein each strut of the plurality of struts has a solid cross-section or a hollow cross-section. 13. The method of claim 1 , wherein each strut of the plurality of struts is a photopolymer waveguide. 14. The method of claim 1 , wherein the open cellular core comprises foam. 15. The method of claim 1 , wherein the open cellular core comprises a partially connected honeycomb structure or a grid architecture.
soluble or fusible {(in particular used in injection moulding B29C45/4457)} · CPC title
destructible (B29C33/52 takes precedence; in particular used in injection moulding B29C45/4457) · CPC title
Open cell foam · CPC title
Two or more layers · CPC title
characterised by features of a layer {of} foamed material · CPC title
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