Fiber-bound engineered materials formed using foundation scrims
US-2024415230-A1 · Dec 19, 2024 · US
US9713913B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9713913-B2 |
| Application number | US-201113260690-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 4, 2011 |
| Priority date | Feb 4, 2010 |
| Publication date | Jul 25, 2017 |
| Grant date | Jul 25, 2017 |
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A composite core includes a plurality of tubes, each the plurality of tubes comprising a plurality of fibers disposed in a polymeric matrix. Adjacent tubes of the plurality of tubes are adhesively bonded to one another along sides of the adjacent tubes. A method of making a composite core includes the steps of providing a plurality of tubes, each of the plurality of tubes including a plurality of fibers disposed in a polymeric matrix, and adhesively bonding adjacent tubes of the plurality of tubes along sides of the adjacent tubes. A method of making a composite core such that a removable band is included in the core, the removable band being configured to be removable through a procedure subsequent to the cure of the composite core, thereby producing gaps in the core.
Opening claim text (preview).
The invention claimed is: 1. A composite core, comprising: a first tube and a second tube, the first tube and the second tube having a plurality of fibers woven with a plurality of removable bands and disposed in a polymeric matrix, wherein at least some of the plurality of removable bands are woven with others of the plurality of removable bands to produce a weave pattern; and a first end portion of each of the first tube and the second tube being configured to support a first face sheet and a second end portion of each of the first tube and the second tube being configured to support a second face sheet; wherein the plurality of fibers of each of the first tube and the second tube are in contact with each other to form a cross-linked pattern, which in turn secures the first tube to the second tube via the plurality of fibers; and wherein the plurality of fibers of each tube are arranged in a uniaxial configuration so as to be arranged in a single direction, such that the plurality of fibers of each tube crosslink with fibers of adjacent tubes, the crosslinking being generated even though each tube has a plurality of fibers only in a single direction. 2. The composite core, according to claim 1 , wherein the plurality of fibers of the first tube and the second tube have been wound in a single helical direction to form each tube. 3. The composite core, according to claim 1 , wherein the first tube has an octagonal cross section, and the second tube has a square cross section. 4. The composite core, according to claim 1 , wherein the plurality of fibers of the first tube comprises: a first set of fibers extending in a first direction; and a second set of fibers extending in a second direction, the second set of fibers woven about the first set of fibers. 5. The composite core, according to claim 1 , wherein the plurality of fibers of the first tube comprises: a first set of fibers extending in a first direction; and a second set of fibers extending in a second direction, the second set of fibers overlaying the first set of fibers. 6. The composite core, according to claim 1 , wherein the plurality of fibers of the first tube comprises: a first set of fibers of a first material; and a second set of fibers of a second material. 7. The composite core, according to claim 1 , wherein the plurality of fibers of the first tube comprises: a first set of fibers exhibiting a first size; and a second set of fibers exhibiting a second size. 8. The composite core, according to claim 1 , further comprising: an adhesive layer disposed between the first tube and the second tube. 9. The composite core, according to claim 1 , wherein the removable bands are configured to be removed during a post-operation thereby producing gaps in the weave pattern between the first tube and the second tube. 10. A composite sandwich structure, comprising: a first skin; a core comprising: a first tube and a second tube, the first tube and a the second tube having a plurality of fibers woven with a plurality of removable bands and disposed in a polymeric matrix, the removable bands being configured to dissolve during a post cure operation, wherein at least some of the plurality of removable bands are woven with others of the plurality of removable bands in a weave pattern; wherein the plurality of fibers of each of the first tube and the second tube are in contact with each other to form a cross-linked pattern, which in turn secures the first tube to the second tube via the plurality of fibers; wherein the plurality of fibers of each tube are arranged in a uniaxial configuration so as to be arranged in a single direction, such that the plurality of fibers of each tube crosslink with fibers of adjacent tubes, the crosslinking being generated even though each tube has a plurality of fibers only in a single direction; and wherein the first skin is adhesively bonded to a first end face of the core. 11. The composite sandwich structure, according to claim 10 , further comprising: a second skin adhesively bonded to a second end face of the core.
characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure · CPC title
having particular mechanical properties · CPC title
on fibrous or filamentary layer · CPC title
Polymeric coating · CPC title
Auxiliary devices · CPC title
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