Method for manufacturing a part made of composite material for an aircraft structure by pultrusion and cocuring
US-2015321429-A1 · Nov 12, 2015 · US
US10105939B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10105939-B2 |
| Application number | US-201514823003-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 11, 2015 |
| Priority date | Aug 14, 2014 |
| Publication date | Oct 23, 2018 |
| Grant date | Oct 23, 2018 |
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 support mandrel for producing curved composite components includes a prismatoid mandrel body formed from a flexible material, the mandrel body having two polygonal bases and an upper support surface extending between the two polygonal bases of the mandrel body, and a reinforcement bar enclosed within the mandrel body and extending between the two polygonal bases of the mandrel body substantially parallel and near to the upper support surface of the mandrel body.
Opening claim text (preview).
The invention claimed is: 1. A support mandrel for producing curved composite components, comprising: a prismatoid mandrel body formed from a flexible material, the mandrel body having two polygonal bases and an upper support surface extending between the two polygonal bases of the mandrel body; a reinforcement bar enclosed within the mandrel body and extending between the two polygonal bases of the mandrel body substantially parallel and near to the upper support surface of the mandrel body; and a plurality of reinforcement pillars connected to the reinforcement bar and extending substantially perpendicular to the reinforcement bar and the upper support surface within the mandrel body. 2. The support mandrel according to claim 1 , wherein the stiffness of at least one of the reinforcement bar and the reinforcement pillars is higher than a stiffness of the prismatoid mandrel body. 3. The support mandrel according to claim 1 , wherein the reinforcement bar comprises a tubular or rectangular rod. 4. The support mandrel according to claim 1 , further comprising a plurality of spread slots cut into a surface of the mandrel body opposite to the upper support surface. 5. The support mandrel according to claim 1 , wherein the flexible material comprises an elastomers or a rubber. 6. The support mandrel according to claim 1 , wherein the two polygonal bases of the mandrel body have one of a T-shape, I-shape, Z-shape, C-shape, L-shape, Ω-shape, hat shape and trapezoid shape. 7. A system for producing curved composite components, comprising: a support mandrel, comprising: a prismatoid mandrel body formed from a flexible material, the mandrel body having two polygonal bases and an upper support surface extending between the two polygonal bases of the mandrel body; a reinforcement bar enclosed within the mandrel body and extending between the two polygonal bases of the mandrel body substantially parallel and near to the upper support surface of the mandrel body; and a plurality of reinforcement pillars connected to the reinforcement bar and extending substantially perpendicular to the reinforcement bar and the upper support surface within the mandrel body; a layup forming assembly configured to form a prepreg layup from prepreg strips on a flat surface and to transfer the prepreg layup to the upper support surface of the mandrel body of the support mandrel; and a forming wheel configured to bend the support mandrel and a prepreg layup formed on the upper support surface to a curved shape. 8. The system according to claim 7 , wherein the support mandrel is joined at its two polygonal bases of the mandrel body to form an endless loop which is wound around the forming wheel. 9. The system according to claim 7 , wherein the forming wheel comprises an outer rim formed as a mold complementary to the shape of the upper support surface of the mandrel body of the support mandrel. 10. The system according to claim 7 , wherein the layup forming assembly comprises: a plurality of prepreg storages configured to store the prepreg strips; a layup support configured to support the prepreg layup in flat form; a layup cross-forming tool configured to cross-form the prepreg layup to the two-dimensional shape of the upper support surface of the mandrel body. 11. The system according to claim 10 , wherein the layup forming assembly further comprises: a layup forming tool configured to place the prepreg layup in flat form from the layup support onto the upper support surface of the mandrel body; and a heating device configured to heat the prepreg layup on the upper support surface of the mandrel body prior to cross-forming by the layup cross-forming tool. 12. The system according to claim 7 , further comprising: a cutting assembly configured to cut the prepreg layup bent by the forming wheel in curved sections to obtain the curved composite components. 13. A method for producing curved composite components, the method comprising: laying up a prepreg layup from prepreg strips; cross-forming the prepreg layup on an upper support surface of a support mandrel, the support mandrel comprising a prismatoid mandrel body formed from a flexible material, the mandrel body having two polygonal bases and an upper support surface extending between the two polygonal bases of the mandrel body, a reinforcement bar enclosed within the mandrel body and extending between the two polygonal bases of the mandrel body substantially parallel and near to the upper support surface of the mandrel body, and a plurality of reinforcement pillars connected to the reinforcement bar and extending substantially perpendicular to the reinforcement bar and the upper support surface within the mandrel body; and bending the support mandrel and the prepreg layup on the upper support surface with a forming wheel. 14. The method according to claim 13 , the method further comprising cutting the prepreg layup bent by the forming wheel in curved sections to obtain the curved composite components.
Profiled members, e.g. beams, sections · CPC title
Curved shaped · CPC title
Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core · CPC title
Prepregs · CPC title
Producing profiled members, e.g. beams · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.