[특허]Composite structure having reinforced core and method of making the same

The Boeing Company

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특허 상세정보

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내보내기 페이스북 공유 트위터 공유 카카오톡 공유

Composite structure having reinforced core and method of making the same

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B32B-007/08 E04C-002/34 B21D-049/00
미국특허분류(USC)	428/223; 052/790.1; 029/897.34
출원번호	US-0866518 (2013-04-19)
등록번호	US-8642168 (2014-02-04)
발명자 / 주소	Chakrabarti, Buddhadev
출원인 / 주소	The Boeing Company
대리인 / 주소	Yee & Associates, P.C.
인용정보	피인용 횟수 : 3 인용 특허 : 51

초록

A polymer-based composite sandwich includes a reinforced core bonded between a pair of composite facesheets. The core includes a truss formed by groups of composite pins held in place by a layer of structural foam. The pins in the groups are radially arranged around nodes. The ends of the pins are splayed and sandwiched between the foam layer and the facesheets.

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1. A method of fabricating comprising: inserting a plurality of pins into a core, the plurality of pins arranged in groups forming a truss, the plurality of pins including medial portions within the core and distal portions respectively extending through a first surface of the core and a second surface of the core, the second surface opposite the first surface, the plurality of pins further comprising first ends and second ends; andarranging, as part of inserting, the plurality of pins such that the groups comprise subsets of three or more pins of the plurality of pins that are arranged in a crossing pattern at about corresponding first ends, are spaced apart at about the corresponding first ends, are substantially circumferentially spaced equally from each other at about the corresponding first ends, and each pin of the three or more pins overlaps at least one first other pin of the three or more pins and is overlapped by at least one second other pin of the three or more pins. 2. The method of claim 1 further comprising: forming core into a curved shape. 3. The method of claim 1 further comprising: bending the first ends to be about parallel to the first surface;bending the second ends to be about parallel to the second surface; andapplying a first composite facesheet to the first surface such that the first ends are bonded to the first composite facesheet and substantially parallel to the first composite facesheet; andapplying a second composite facesheet to the second surface such that the second ends are bonded to the second composite facesheet and substantially parallel to the second composite face sheet. 4. The method of claim 3 further comprising: curing the core together with the first composite facesheet and the second composite face sheet. 5. The method of claim 1, wherein the core comprises a foam core. 6. The method of claim 5, wherein the foam core comprises a closed cell carrier foam, and wherein the method further comprises: sealing porosity in the closed cell carrier foam created by insertion of the plurality of pins. 7. The method of claim 6, wherein sealing comprises applying a first plurality of layers of solid film adhesive on the first surface and a second plurality of layers of solid film adhesive on the second surface. 8. The method of claim 1 further comprising: flaying the first ends; andflaying the second ends. 9. The method of claim 1, wherein arranging further includes placing the subsets of three or more pins such that they radiate outwardly from a corresponding node. 10. A method of fabricating comprising: forming a core comprising a closed cell, uncured structural foam having a density between approximately 6.9 and 12 pounds per cubic foot;inserting a plurality of pins into the core, the plurality of pins arranged in groups forming a truss, the plurality of pins including medial portions within the core and distal portions respectively extending through a first surface of the core and a second surface of the core, the second surface opposite the first surface, the plurality of pins further comprising first ends and second ends, the plurality of pins comprising an uncured composite material;arranging, as part of inserting, the plurality of pins such that the groups comprise subsets of three or more pins of the plurality of pins that are arranged in a crossing pattern at about corresponding first ends, are spaced apart at about the corresponding first ends, are substantially circumferentially spaced equally from each other at about the corresponding first ends, and each pin of the three or more pins overlaps at least one first other pin of the three or more pins and is overlapped by at least one second other pin of the three or more pins;splaying the first ends;splaying the second ends;bending the first ends until the first ends are about parallel to the first surface;bending the second ends until the second ends are about parallel to the second surface;bonding a first uncured composite facesheet to the first ends and the first surface;bonding a second uncured composite facesheet to the second ends and the second surface; andco-curing the core, the pins, the first facesheet, and the second facesheet. 11. The method of claim 10 further comprising: after arranging, and prior to bonding the first uncured composite facesheet and the second uncured composite facesheet, bending the core into a curved shape. 12. An article of manufacture comprising: a core; anda plurality of pins inserted into the core, the plurality of pins arranged in groups forming a truss, the plurality of pins including medial portions within the core and distal portions respectively extending through a first surface of the core and a second surface of the core, the second surface opposite the first surface, the plurality of pins further comprising first ends and second ends, the plurality of pins further arranged such that the groups comprise subsets of three or more pins of the plurality of pins that are arranged in a crossing pattern at about corresponding first ends, are spaced apart at about the corresponding first ends, are substantially circumferentially spaced equally from each other at about the corresponding first ends, and each pin of the three or more pins overlaps at least one first other pin of the three or more pins and is overlapped by at least one second other pin of the three or more pins. 13. The article of claim 12, wherein the first ends are bent to be about parallel to the first surface, wherein the second ends are bent to be about parallel to the second surface, and wherein the article further comprises: a first composite facesheet applied to the first surface such that the first ends are bonded to the first composite facesheet and substantially parallel to the first composite facesheet; anda second composite facesheet applied to the second surface such that the second ends are bonded to the second composite facesheet and substantially parallel to the second composite face sheet. 14. The article of claim 12, wherein the plurality of pins comprises a composite material and wherein the core comprises a foam. 15. The article of claim 14, wherein the foam comprises a closed cell carrier foam, and wherein the article further comprises: a first plurality of layers of solid film adhesive on the first surface; anda second plurality of layers of solid film adhesive on the second surface. 16. The article of claim 15, wherein the first plurality of layers and the second plurality of layers are configured to seal porosity in the closed cell carrier foam created by insertion of the plurality of pins. 17. The article of claim 12 wherein the first ends and the second ends are flayed. 18. The article of claim 12, wherein the subsets of three or more pins radiate outwardly from corresponding a node. 19. The article of claim 12, wherein the core comprises a closed cell, uncured structural foam having a density between approximately 6.9 and 12 pounds per cubic foot. 20. The article of claim 12, wherein the article is part of an aircraft.

이 특허에 인용된 특허 (51)

이 특허를 인용한 특허 피인용횟수: 3

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특허 상세정보

Composite structure having reinforced core and method of making the same

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Composite structure having reinforced core and method of making the same

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이 특허에 인용된 특허 (51)

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