Method of Forming Laminar Composite Charge

US2016185030A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016185030-A1
Application numberUS-201514975344-A
CountryUS
Kind codeA1
Filing dateDec 18, 2015
Priority dateDec 19, 2014
Publication dateJun 30, 2016
Grant date

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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.

A method of forming a charge. A first part of the charge is clamped with a free part of the charge protruding from the clamp to a free edge of the charge. The free part of the charge comprises an inner layer, an outer layer and a plurality of internal layers. The outer layer is contacted with a forming roller and the inner layer is contacted with a guide roller. The free part of the charge is bent over a convex corner of a die with the forming roller to form a first bend with the outer layer on an outside of the first bend. The free part of the charge is also bent away from a mould surface of the die with the guiding roller to form a second bend with the inner layer on an outside of the second bend. The rollers are simultaneously moved across the mould surface so that they progressively draw the charge across the mould surface, the forming roller presses the inner layer of the charge against the mould surface, and the second bend moves towards the free edge of the charge.

First claim

Opening claim text (preview).

1 . A method of forming a charge, the charge comprising a plurality of layers of fibre-reinforced composite material, the method comprising: clamping a first part of the charge with a clamp, a free part of the charge protruding from the clamp to a free edge; contacting the free part of the charge with a forming roller; and advancing the forming roller across a die so that it bends the free part of the charge over a convex corner of the die, wherein as the forming roller advances across the die it rotates about an axis of rotation which also advances across the die. 2 . The method of claim 1 , wherein the charge comprises an outer layer and an inner layer, the plurality of layers of fibre-reinforced material are positioned between the inner and outer layers, and the forming roller forms a first bend with the outer layer on the outside of the first bend as it bends the free part of the charge over the convex corner of the die. 3 . The method of claim 1 , wherein as the forming roller advances across the die it presses the free part of the charge against a mould surface of the die. 4 . The method of claim 3 , wherein the charge comprises an outer layer and an inner layer, the plurality of layers of fibre-reinforced material are positioned between the inner and outer layers, and the forming roller forms a first bend with the outer layer on the outside of the first bend as it bends the free part of the charge over the convex corner of the die, and the method further comprises: contacting the inner layer with a guide; bending the free part of the charge away from the mould surface of the die to form a second bend with the inner layer on an outside of the second bend; and simultaneously advancing the forming roller and the guide across the die so that they progressively draw the free part of the charge across the mould surface, the forming roller presses the inner layer of the charge against the mould surface, and the second bend moves towards the free edge. 5 . The method of claim 4 , wherein the guide comprises a guiding roller, and as the guiding roller advances across the die it rotates about an axis of rotation which also advances across the die. 6 . The method of claim 3 , wherein as the forming roller advances across the die it presses the free part of the charge against the mould surface of the die from the convex corner of the die to the free edge of the charge. 7 . The method of claim 3 , wherein the method comprises: contacting the free part of the charge with a plurality of forming rollers; and simultaneously advancing the forming rollers so that they bend the free part of the charge over the convex corner of a die and press the free part of the charge against the mould surface of the die, wherein as each forming roller advances across the die it rotates about an axis of rotation which also advances across the die, and wherein at least one of the forming rollers moves relative to the other forming rollers as they press the free part of the charge against the mould surface of the die. 8 . The method of claim 7 , wherein the one of the forming rollers rotates about its axis of rotation at a different rate to the other forming rollers as they press the free part of the charge against the mould surface of the die. 9 . The method of claim 7 , wherein the axis of rotation of the one of the forming rollers moves relative to the axes of rotation of the other forming rollers as they press the free part of the charge against the mould surface of the die. 10 . The method of claim 3 , wherein the charge is heated as the forming roller advances across the die by a heating element which is integrated into the mould surface of the die. 11 . The method of claim 1 , wherein the first part of the charge does not move relative to the die as the free part of the charge is bent over the convex corner of the die. 12 . The method of claim 1 , further comprising heating the charge as the forming roller advances across the die. 13 . The method of claim 1 , wherein the charge is heated as the forming roller advances across the die by a heating element which is integrated into the forming roller. 14 . The method of claim 1 , further comprising pre-heating the free part of the charge before it is bent across the convex corner of the die. 15 . The method of claim 1 , wherein the plurality of layers of fibre-reinforced composite material comprise four or more layers of fibre-reinforced composite material. 16 . The method of claim 1 , further comprising heating the charge to a curing temperature after the free part of the charge has been bent over the convex corner of the die, so that the fibre-reinforced composite material cures. 17 . A method of forming a charge, the method comprising: clamping a first part of the charge with a clamp, a free part of the charge protruding from the clamp to a free edge of the charge, wherein the free part of the charge comprises an inner layer, an outer layer and a plurality of internal layers of fibre-reinforced composite material between the inner and outer layers; contacting the outer layer with a forming roller; contacting the inner layer with a guide; bending the free part of the charge over a convex corner of a die with the forming roller to form a first bend with the outer layer on an outside of the first bend; bending the free part of the charge away from a mould surface of the die with the guide to form a second bend with the inner layer on an outside of the second bend; and simultaneously advancing the forming roller and the guide across the mould surface so that they progressively draw the charge across the mould surface, the forming roller presses the inner layer of the charge against the mould surface, and the second bend moves towards the free edge of the charge, wherein as the forming roller advances across the die it rotates about an axis of rotation which also advances across the die. 18 . Apparatus for forming a charge by the method of claim 4 , the apparatus comprising: a clamp for clamping the first part of the charge; a support; a forming roller carried by the support; a forming roller actuator arranged to move the forming roller relative to the support to bring the forming roller into contact with an outer layer of the charge; a guide carried by the support; a guide actuator arranged to move the guide relative to the support to bring the guide into contact with an inner layer of the charge, a die with a convex corner and a mould surface; and a support actuator arranged to move the support across the die to form the charge. 19 . The apparatus of claim 18 , comprising a plurality of forming rollers carried by the support. 20 . The apparatus of claim 19 , wherein the plurality of forming rollers are mounted to a roller carrier which is carried by the support, and the forming roller actuator is arranged to move the roller carrier relative to the support to bring the forming rollers into contact with the outer layer of the charge. 21 . The apparatus of claim 20 , wherein each forming roller is mounted to the roller carrier by a flexible mount which enables an axis of rotation of the forming roller to move relative to the roller carrier and relative to the other forming rollers. 22 . The apparatus of claim 19 , wherein each forming roller can rotate independently of the other forming rollers.

Assignees

Inventors

Classifications

  • of plates or sheets {(B29C63/04 takes precedence; bending or folding paper B31F1/0003; folding films B65H45/00)} · CPC title

  • of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns · CPC title

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

  • B29C70/30Primary

    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

  • Sheets, plates, blanks or films · CPC title

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What does patent US2016185030A1 cover?
A method of forming a charge. A first part of the charge is clamped with a free part of the charge protruding from the clamp to a free edge of the charge. The free part of the charge comprises an inner layer, an outer layer and a plurality of internal layers. The outer layer is contacted with a forming roller and the inner layer is contacted with a guide roller. The free part of the charge is b…
Who is the assignee on this patent?
Airbus Operations Ltd
What technology area does this patent fall under?
Primary CPC classification B29C70/30. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Jun 30 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).