Reinforced stringer and method of manufacture thereof

US9440725B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9440725-B2
Application numberUS-201314139147-A
CountryUS
Kind codeB2
Filing dateDec 23, 2013
Priority dateDec 26, 2012
Publication dateSep 13, 2016
Grant dateSep 13, 2016

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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

Official abstract text for this publication.

The present invention relates to a stringer, particularly to a stiffening and structural longitudinal element for skin of aircraft airfoil surfaces, characterized in that it incorporates two separate and independent reinforcement areas, one in the foot and the other at the end of the web (head) of the stringer, where the reinforcement areas are obtained by a widening of the section of the stringer, the widening being formed by a localized stack of reinforcing plies of composite material which are embedded within the stringer. The invention also relates to the method of manufacture and is particularly applicable to stringers having an L-shaped or T-shaped section.

First claim

Opening claim text (preview).

The invention claimed is: 1. A T-shaped reinforced stringer comprising a plurality of superimposed plies of composite material, wherein a foot is defined for attachment to an aircraft skin panel, and a web attached to the foot by one of its longitudinal edges, such that both elements together form a profile with an L-shaped or T-shaped section, where the plies of composite material are continuous and extend over a majority surface of the foot and of the web of the stringer, wherein the stringer incorporates at least one widening of the section of the stringer, where the widening is formed by a localized stack of reinforcing plies of composite material, and the reinforcing plies being embedded within the stringer and arranged parallel to the continuous plies on which they are superimposed, where the widening of the section extends from a free edge of the stringer to an internal termination edge in the stringer; wherein the T-shaped reinforced stringer is symmetric about an axis bisecting the web. 2. The T-shaped reinforced stringer according to claim 1 , wherein the reinforcing plies are intercalated with continuous plies, and the reinforcing plies and the continuous plies are co-cured. 3. The T-shaped reinforced stringer according to claim 1 , wherein the reinforcing plies are superimposed directly on top of one another forming a compact block, and said compact block is embedded within the stringer. 4. The T-shaped reinforced stringer according to claim 1 , comprising a widening in the web of the stringer which extends from the free edge of the web to a termination edge spaced from said free edge, and wherein a width of that widening is constant in a majority segment of the section thereof. 5. The T-shaped reinforced stringer according to claim 1 , comprising at least one widening in the foot of the stringer which extends from a free edge of the foot to an elbow for connecting with the web, and wherein a width of that widening is constant in a majority segment of the section thereof. 6. The T-shaped reinforced stringer according to claim 4 , wherein the stringer has a T-shaped section, and comprising a widening in the web and a widening in each part the foot. 7. The T-shaped reinforced stringer according to claim 1 , wherein the web has a central segment having a constant section formed only by continuous plies, which extends from an elbow of the section of the stringer to the termination edge of the widening of the web, and wherein a width of this central segment is less than that of the widening of the web. 8. The T-shaped reinforced stringer according to claim 1 , wherein an end of the widening of the web and of the widening of the foot inside the stringer end with a progressive reduction of their width. 9. The T-shaped reinforced stringer according to claim 1 , wherein the at least one widening extends along all or a majority part of a length of the stringer. 10. The T-shaped reinforced stringer according to claim 1 , wherein the at least one widening extends in one or more segments located in a longitudinal direction of the stringer. 11. The T-shaped reinforced stringer according to claim 1 , comprising segments in which a height and/or a width of reinforcements of the web and/or foot are different.

Assignees

Inventors

Classifications

  • and shaping or impregnating by compression {, i.e. combined with compressing after the lay-up operation} · CPC title

  • Subsequent to assembly · CPC title

  • B64C1/064Primary

    Stringers; Longerons · CPC title

  • Producing profiled members, e.g. beams · CPC title

  • Cross-Sectional Technologies · mapped topic

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Frequently asked questions

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What does patent US9440725B2 cover?
The present invention relates to a stringer, particularly to a stiffening and structural longitudinal element for skin of aircraft airfoil surfaces, characterized in that it incorporates two separate and independent reinforcement areas, one in the foot and the other at the end of the web (head) of the stringer, where the reinforcement areas are obtained by a widening of the section of the strin…
Who is the assignee on this patent?
Airbus Operations Sl, Airbus Operations Sl
What technology area does this patent fall under?
Primary CPC classification B64C1/064. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Sep 13 2016 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).