Composite structure and methods of assembling same

US9950480B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9950480-B2
Application numberUS-201213416851-A
CountryUS
Kind codeB2
Filing dateMar 9, 2012
Priority dateMar 9, 2012
Publication dateApr 24, 2018
Grant dateApr 24, 2018

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

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A composite structure and method of assembling a composite structure is provided. The composite structure includes a base member having an outer surface and an inner surface. The inner surface defines a channel therethrough. The composite structure further includes a support member coupled to the outer surface. A fabric overwrap is coupled to the support member.

First claim

Opening claim text (preview).

What is claimed is: 1. A composite structure comprising: a base member comprising an outer surface and an inner surface, said inner surface defining a channel therethrough; a plurality of unidirectional fiber tows positioned about said outer surface, wherein said plurality of unidirectional fiber tows are formed from a majority of fibers oriented in a first direction and a minority of fibers oriented in a second direction, said minority of fibers configured to hold said majority of fibers together; and a fabric overwrap comprising strands of structural fibers, said fabric overwrap coupled to said plurality of unidirectional fiber tows and to said outer surface of said base member, wherein said strands of structural fibers are interwoven to and about said base member and said plurality of unidirectional fiber tows such that said plurality of unidirectional fiber tows are coupled to said outer surface. 2. The composite structure of claim 1 wherein said base member comprises a hollow preform tube. 3. The composite structure of claim 1 wherein said base member comprises at least one of a polygonal shape and a circular shape. 4. The composite structure of claim 1 wherein said base member comprises at least one of a metallic, thermoplastic and reconfigured thermoplastic composite material. 5. The composite structure of claim 1 wherein said base member comprises an electrically conductive material. 6. The composite structure of claim 1 wherein said fabric overwrap comprises a flange. 7. The composite structure of claim 1 , wherein an amount of resin is substantially infused into said fabric overwrap. 8. The composite structure of claim 7 wherein said resin is configured to encapsulate said plurality of unidirectional fiber tows. 9. A fuselage section comprising: a fuselage skin; and a composite structure coupled to said fuselage skin, said composite structure comprising: a base member comprising an outer surface and an inner surface, said inner surface defining a channel therethrough; a plurality of unidirectional fiber tows positioned about said outer surface, wherein said plurality of unidirectional fiber tows are formed from a majority of fibers oriented in a first direction and a minority of fibers oriented in a second direction, said minority of fibers configured to hold said majority of fibers together; a fabric overwrap comprising strands of structural fibers, said fabric overwrap coupled to said plurality of unidirectional fiber tows and to said outer surface of said base member, wherein said strands of structural fibers are interwoven to and about said base member and said plurality of unidirectional fiber tows such that said plurality of unidirectional fiber tows are coupled to said outer surface. 10. The fuselage skin of claim 9 further comprising an electrical component coupled to said inner surface. 11. The fuselage skin of claim 9 wherein said base member comprises at least one of a polygonal and a circular shape.

Assignees

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Classifications

  • by incorporating or moulding on preformed parts, e.g. inserts or layers {, e.g. foam blocks (mould constructions therefor B29C33/12; joining preformed parts by moulding B29C65/70)} · CPC title

  • Hollow or container type article [e.g., tube, vase, etc.] · CPC title

  • B29C70/542Primary

    Placing or positioning the reinforcement in a covering or packaging element before or during moulding, e.g. drawing in a sleeve · CPC title

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What does patent US9950480B2 cover?
A composite structure and method of assembling a composite structure is provided. The composite structure includes a base member having an outer surface and an inner surface. The inner surface defines a channel therethrough. The composite structure further includes a support member coupled to the outer surface. A fabric overwrap is coupled to the support member.
Who is the assignee on this patent?
Tsotsis Thomas Karl, Boeing Co
What technology area does this patent fall under?
Primary CPC classification B29C70/542. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Apr 24 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).