Aircraft cabin panel and method of manufacturing the same
US-2018251205-A1 · Sep 6, 2018 · US
US2020264584A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2020264584-A1 |
| Application number | US-201916276815-A |
| Country | US |
| Kind code | A1 |
| Filing date | Feb 15, 2019 |
| Priority date | Feb 15, 2019 |
| Publication date | Aug 20, 2020 |
| Grant date | — |
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A system may include a 3D core design engine and a 3D core printing engine. The 3D core design engine may be configured to determine, in a CAD model, an under-core ply of a composite part and a core footprint on the under-core ply specified for an additive 3D core to be manufactured via additive manufacturing for insertion into the composite part, compute a bottom core surface of the additive 3D core from the under-core ply and core footprint, access core design parameters for the additive 3D core; and construct an additive 3D core design in the CAD model based on the computed bottom core surface and the core shape parameters. The 3D core printing engine may be configured to store the additive 3D core design to support subsequent manufacture of the additive 3D core via additive manufacturing.
Opening claim text (preview).
1 . A method comprising: by a computing system: determining, in a computer-aided design (CAD) model, an under-core ply of a composite part and a core footprint on the under-core ply, the under-core ply and core footprint specified for an additive 3-dimensional (3D) core to be manufactured via additive manufacturing and to be inserted into the composite part; computing a bottom core surface of the additive 3D core from the under-core ply and core footprint; accessing core design parameters for the additive 3D core, the core design parameters comprising core thickness parameters and core shape parameters that define the additive 3D core; constructing an additive 3D core design in the CAD model for the additive 3D core based on the computed bottom core surface and the core design parameters; and storing the additive 3D core design to support subsequent manufacture of the additive 3D core via additive manufacturing. 2 . The method of claim 1 , wherein computing the bottom core surface of the additive 3D core comprises: determining an uncured thickness of plies in the composite part up to the under-core ply; and setting a shape of the bottom core surface as a shape of a portion of the under-core ply as outlined by the core footprint. 3 . The method of claim 1 , wherein constructing the additive 3D core design in the CAD model comprises computing a top core surface by offsetting the computed bottom core surface according to the core thickness parameters. 4 . The method of claim 3 , wherein the core shape parameters comprises parametric or geometric parameters that define a side surfaces of the additive 3D core; and wherein constructing the additive 3D core design in the CAD model comprises computing core side surfaces by applying the core shape parameters to define the side surfaces between the computed top and bottom core surfaces of the additive 3D core. 5 . The method of claim 1 , where the additive 3D core design constructed in the CAD model is represented as a boundary representation (B-Rep), surface mesh, faceted surface, or any combination thereof. 6 . The method of claim 1 , further comprising, prior to providing the additive 3D core design to the printing hardware: defining an interior composition of the additive 3D core. 7 . The method of claim 6 , where defining the interior composition comprises: identifying a cell shape and cell size from a 3D cell library, the cell shape and cell size selected to meet a predetermined performance capability for the additive 3D core; and defining the interior composition of the additive 3D core according to the cell shape and cell size. 8 . A system comprising: a 3-dimensional (3D) core design engine configured to; determine, in a computer-aided design (CAD) model, an under-core ply of a composite part and a core footprint on the under-core ply specified for an additive 3-dimensional (3D) core to be manufactured via additive manufacturing for insertion into the composite part; compute a bottom core surface of the additive 3D core from the under-core ply and core footprint; access core design parameters for the additive 3D core, the core design parameters comprising core thickness parameters and core shape parameters that define the additive 3D core; and construct an additive 3D core design in the CAD model based on the computed bottom core surface and the core shape parameters; and a 3D core printing engine configured to store the additive 3D core design to support subsequent manufacture of the additive 3D core via additive manufacturing. 9 . The system of claim 8 , wherein the 3D core design engine is configured to compute the bottom core surface of the additive 3D core by: determining an uncured thickness of plies in the composite part up to the under-core ply; and setting a shape of the bottom core surface as a shape of a portion of the under-core ply as outlined by the core footprint. 10 . The system of claim 8 , wherein the 3D core design engine is configured to construct the additive 3D core design in the CAD model by computing a top core surface by offsetting the computed bottom core surface according to the core thickness parameters. 11 . The system of claim 10 , wherein the core shape parameters comprises parametric or geometric parameters that define a side surfaces of the additive 3D core; and wherein the 3D core design engine is configured to construct the additive 3D core design in the CAD model by: computing core side surfaces by applying the core shape parameters to define the side surfaces between the computed top and bottom core surfaces of the additive 3D core. 12 . The system of claim 8 , where the additive 3D core design constructed in the CAD model is represented as a boundary representation (B-Rep), surface mesh, faceted surface, or any combination thereof. 13 . The system of claim 8 , wherein the 3D core design engine is further configured to define an interior composition of the additive 3D core. 14 . The system of claim 13 , where the 3D core design engine is configured to define the interior composition by: identifying a cell shape and cell size from a 3D cell library, the cell shape and cell size selected to meet a predetermined performance capability for the additive 3D core; and defining the interior composition of the additive 3D core according to the cell shape and cell size. 15 . A non-transitory machine-readable medium comprising instructions that, when executed by a processor, cause a computing system to: determine, in a computer-aided design (CAD) model, an under-core ply of a composite part and a core footprint on the under-core ply, the under-core ply and core footprint specified for an additive 3-dimensional (3D) core to be manufactured via additive manufacturing and to be inserted into the composite part; compute a bottom core surface of the additive 3D core from the under-core ply and core footprint; access core design parameters for the additive 3D core, the core design parameters comprising core thickness parameters and core shape parameters that define the additive 3D core; construct an additive 3D core design in the CAD model for the additive 3D core based on the computed bottom core surface and the core shape parameters; and store the additive 3D core design to support subsequent manufacture of the additive 3D core via additive manufacturing. 16 . The non-transitory machine-readable medium of claim 15 , wherein the instructions, when executed by the processor, cause the computing system to compute the bottom core surface of the additive 3D core by: determining an uncured thickness of plies in the composite part up to the under-core ply; and setting a shape of the bottom core surface as a shape of a portion of the under-core ply as outlined by the core footprint. 17 . The non-transitory machine-readable medium of claim 15 , wherein the instructions, when executed by the processor, cause the computing system to construct the additive 3D core design in the CAD model by computing a top core surface by offsetting the computed bottom core surface according to the core thickness parameters. 18 . The non-transitory machine-readable medium of claim 17 , wherein the core shape parameters comprises parametric or geometric parameters that define a side surfaces of the additive 3D core; and wherein the instructions, when executed by the processor, cause the computing system to construct the additive 3D core design in the CAD model by computing core side surfaces by applying the core shape parameters to define the side surfac
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