Process for manufacturing a stiffener of composite material

US8985995B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-8985995-B2
Application numberUS-201113253300-A
CountryUS
Kind codeB2
Filing dateOct 5, 2011
Priority dateOct 8, 2010
Publication dateMar 24, 2015
Grant dateMar 24, 2015

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  1. Title

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  2. Abstract

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  4. Key dates

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  5. First independent claim

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Abstract

Official abstract text for this publication.

A process for manufacturing a stiffener made of composite material with an inside surface of a concave shape, includes producing a flat strip ( 18 ) that includes at least one layer of fibers; heating it to be able to deform it; connecting one of the lateral edges of the strip ( 18 ) to a rotary mandrel ( 36 ) in such a way as to cause a winding of the strip on the mandrel ( 36 ) during its rotation, whereby the mandrel ( 36 ) has an outside surface ( 46 ) of which at least one part corresponds to the inside surface of the stiffener to be produced; and exerting tension at the other lateral edge of the strip ( 18 ) in a direction that is opposite to the direction of the movement of the strip ( 18 ) caused by the winding on the rotary mandrel ( 36 ).

First claim

Opening claim text (preview).

The invention claimed is: 1. A device for manufacturing a composite material stiffener having an inside concave surface from a flat strip comprising at least one layer of fibers, the device comprising: a table on which the flat strip rests across, the table comprising a means for heating the strip; a rotary mandrel arranged close and parallel to an edge of the table and having an outside surface of which at least one part corresponds to an inside surface of the stiffener to be p…

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What does patent US8985995B2 cover?
A process for manufacturing a stiffener made of composite material with an inside surface of a concave shape, includes producing a flat strip ( 18 ) that includes at least one layer of fibers; heating it to be able to deform it; connecting one of the lateral edges of the strip ( 18 ) to a rotary mandrel ( 36 ) in such a way as to cause a winding of the strip on the mandrel ( 36 ) during its rot…
Who is the assignee on this patent?
De Mattia Denis, Guillemot Olivier, Airbus Operations Sas
What technology area does this patent fall under?
Primary CPC classification B29C70/56. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Mar 24 2015 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).