Yarn take-up system for weaving and a method of weaving a reinforcing fiber structure for composite material parts
US-2016376734-A1 · Dec 29, 2016 · US
US10801136B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10801136-B2 |
| Application number | US-201716089948-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 29, 2017 |
| Priority date | Apr 1, 2016 |
| Publication date | Oct 13, 2020 |
| Grant date | Oct 13, 2020 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A woven fiber structure presenting over at least one of its outside faces a satin weave formed by interlinking a first set of yarns with a second set of yarns; wherein the first set of yarns is in the majority over the outside face, the first set of yarns being formed by a mixture of yarns having an S-twist and of yarns having a Z-twist.
Opening claim text (preview).
The invention claimed is: 1. A method of treating a woven fiber structure that includes yarns made of a carbon precursor and presenting over at least one of its outside faces a satin weave formed by interlinking a first set of yarns with a second set of yarns; wherein the first set of yarns is in the majority over the outside face, said first set of yarns being formed by a mixture of yarns having an S-twist and of yarns having a Z-twist; and wherein the structure includes over its outside face: a first yarn of the second set of yarns forming a first set of satin points; a second yarn of the second set of yarns, adjacent to the first yarn of the second set of yarns, and forming a second set of satin points, the satin points of the second set being offset from the satin points of the first set by a first spacing, wherein the first spacing is the minimal distance between all the satin points of the second set and all the satin points of the first set; and a third yarn of the second set of yarns, adjacent to the second yarn of the second set of yarns, and forming a third set of satin points, the satin points of the third set being offset from the satin points of the second set by a second spacing different from the first spacing, wherein the second spacing is the minimal distance between all the satin points of the third set and all the satin points of the second set, and wherein the first, second and third yarns are consecutive yarns in this order along a direction that is transverse to a longitudinal direction of said first, second and third yarns, the method comprising: moving said woven fiber structure in an enclosure, wherein said fiber structure is moved along a direction of the yarns of the first set of yarns and wherein, during said moving, at least a portion of the outside face rubs against a wall of the enclosure. 2. A method according to claim 1 , wherein the enclosure is a heating enclosure. 3. A method of treating a woven fiber structure that includes yarns made of carbon and presenting over at least one of its outside faces a satin weave formed by interlinking a first set of yarns with a second set of yarns; wherein the first set of yarns is in the majority over the outside face, said first set of yarns being formed by a mixture of yarns having an S-twist and of yarns having a Z-twist; and wherein the structure includes over its outside face: a first yarn of the second set of yarns forming a first set of satin points; a second yarn of the second set of yarns, adjacent to the first yarn of the second set of yarns, and forming a second set of satin points, the satin points of the second set being offset from the satin points of the first set by a first spacing; wherein the first spacing is the minimal distance between all the satin points of the second set and all the satin points of the first set; and a third yarn of the second set of yarns, adjacent to the second yarn of the second set of yarns, and forming a third set of satin points, the satin points of the third set being offset from the satin points of the second set by a second spacing different from the first spacing, wherein the second spacing is the minimal distance between all the satin points of the third set and all the satin points of the second set, and wherein the first, second and third yarns are consecutive yarns in this order along a direction that is transverse to a longitudinal direction of said first, second and third yarns, the method comprising: moving said woven fiber structure in an enclosure, wherein said fiber structure is moved along a direction of the yarns of the first set of yarns and wherein, during said moving, at least a portion of the outside face rubs against a wall of the enclosure. 4. A method according to claim 3 , wherein the enclosure is a heating enclosure. 5. A method according to claim 1 , wherein the ratio of [the number of S-twist yarns in the first set of yarns] divided by [the number of Z-twist yarns in the first set of yarns] lies in the range 0.75 to 1.25. 6. A method according to claim 1 , wherein the fiber structure is a satin weave two-dimensionally woven structure. 7. A method according to claim 1 , wherein the fiber structure is formed by three-dimensional weaving. 8. A method according to claim 1 , wherein the fiber structure is a multi-satin woven fabric. 9. A method according to claim 3 , wherein the enclosure is a heating enclosure and wherein the fiber structure is subjected to pyrolysis in the heating enclosure. 10. A method of fabricating a composite material part comprising at least the following steps: forming a fiber preform from one or more woven fiber structures treated according to the method of claim 1 , and forming a matrix within the pores of the fiber preform in order to obtain the composite material part. 11. A method according to claim 10 , wherein the matrix that is formed is an organic matrix, a ceramic matrix, or a carbon matrix. 12. A method of fabricating a composite material part comprising at least the following steps: forming a fiber preform from one or more woven fiber structures treated according to the method of claim 3 , and forming a matrix within the pores of the fiber preform in order to obtain the composite material part. 13. A method according to claim 12 , wherein the matrix that is formed is an organic matrix, a ceramic matrix, or a carbon matrix.
Double or multi-ply fabrics not otherwise provided for · CPC title
with specific twist · CPC title
Woven fabrics designed to make specified articles · CPC title
Viscose · CPC title
polymers of unsaturated nitriles, e.g. polyacrylonitrile, polyvinylidene cyanide · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.