Method and apparatus for extracting a fiber of a wound composite part

US9511337B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9511337-B2
Application numberUS-201514730588-A
CountryUS
Kind codeB2
Filing dateJun 4, 2015
Priority dateNov 27, 2012
Publication dateDec 6, 2016
Grant dateDec 6, 2016

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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

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Disclosed is a method and an apparatus for extracting a long fiber, and in particular an endless fiber, embedded in a resin matrix forming a wound composite part, wherein the fiber is extracted as one single part by unwinding after a pyrolisis treatment for a decomposition of the matrix.

First claim

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What is claimed is: 1. A method for extracting a fibre embedded in a resin matrix forming a wound composite part having a main axis, wherein the fibre forms a multiplicity of adjacent winding turns in the direction of the main axis, comprising the steps: positioning the composite part on a retainer extending in the direction of the main axis, creating a resin free fibre structure by pyrolisis treatment, supporting the fibre structure by a supporting pressure directing from the inside to the outside of the fibre structure, locating and grabbing a free end of the fibre, and unwinding the fibre. 2. The method in accordance with claim 1 , wherein the composite part is aligned horizontally. 3. The method in accordance with claim 1 , wherein the pyrolisis is done continuously. 4. The method in accordance with claim 1 , wherein a core element for creating the supporting pressure (p) is positioned in the fibre structure along the main axis (m) before the removal of the retainer. 5. The method in accordance with claim 1 , wherein a core element for creating the supporting pressure (p) is positioned in the fibre structure along the main axis (m), wherein the removal of the retainer and the supporting of the fibre structure by the core element are done simultaneously. 6. The method in accordance with claim 1 , wherein the locating and grabbing of the free end of the fibre is done by electric charging. 7. The method in accordance with claim 1 , wherein, the locating and grabbing of the free end of the fibre is done by rotating the fibre structure around the main axis. 8. An apparatus for extracting a fibre embedded in a resin matrix forming a wound composite part having a main axis, wherein the fibre forms a multiplicity of adjacent winding turns in the direction of the main axis, in particular for performing a method according to one of the preceding claims, comprising: a retainer for receiving the composite part, a furnace for carrying out a pyrolisis treatment for creating a resin free fibre structure, an expandable core element for supporting the fibre structure, a means for locating and grabbing a free end of the fibre, and a bobbin for receiving the unwound fibre. 9. The apparatus in accordance with claim 8 , wherein the retainer has an outer fixation mechanism for fixing the composite part in a first position and an inner fixation mechanism for fixing the composite part in a second position. 10. The apparatus in accordance with claim 9 , wherein the inner fixation mechanism is incorporated in a retainer head and is expandable in the direction of the main axis. 11. The apparatus in accordance with claim 8 , wherein the retainer has a cavity for receiving the core element. 12. The apparatus in accordance with one of claim 8 , wherein the retainer head is conically shaped. 13. The apparatus in accordance with one of claim 8 , wherein the retainer head has a front opening for releasing the core element. 14. The apparatus in accordance with of claim 8 , wherein the means for locating and grabbing the free end of the fibre comprises an electrical energy source for providing direct current, a movable grabber and wiring for connecting the retainer and the grabber with the energy source. 15. The apparatus in accordance with of claim 8 , wherein the means for locating grabbing the free end of the fibre comprises a drive mechanism for rotating the core element around the main axis and a grabber positioned outside of the fibre structure. 16. A method for extraction a fibre embedded in a resin matrix forming a wound composite part having a main axis, wherein the fibre forms a multiplicity of adjacent winding turns in the direction of the main axis, comprising the steps: positioning the composite part on a retainer extending in the direction of the main axis, creating a resin free fibre structure by pyrolisis treatment, supporting the fibre structure by a supporting pressure directing from the inside to the outside of the fibre structure, locating and grabbing a free end of the fibre, and unwinding the fibre, wherein the composite part is aligned horizontally, wherein the pyrolisis is done continuously. 17. A method for extraction a fibre embedded in a resin matrix forming a wound composite part having a main axis, wherein the fibre forms a multiplicity of adjacent winding turns in the direction of the main axis, comprising the steps: positioning the composite part on a retainer extending in the direction of the main axis, creating a resin free fibre structure by pyrolisis treatment, supporting the fibre structure by a supporting pressure directing from the inside to the outside of the fibre structure, locating and grabbing a free end of the fibre, and unwinding the fibre, wherein the composite part is aligned horizontally, wherein the pyrolisis is done continuously, wherein a core element for creating the supporting pressure (p) is positioned in the fibre structure along the main axis (m) before the removal of the retainer, wherein a core element for creating the supporting pressure (p) is positioned in the fibre structure along the main axis (m), wherein the removal of the retainer and the supporting of the fibre structure by the core element are done simultaneously. 18. A method for extraction a fibre embedded in a resin matrix forming a wound composite part having a main axis, wherein the fibre forms a multiplicity of adjacent winding turns in the direction of the main axis, comprising the steps: positioning the composite part on a retainer extending in the direction of the main axis, creating a resin free fibre structure by pyrolisis treatment, supporting the fibre structure by a supporting pressure directing from the inside to the outside of the fibre structure, locating and grabbing a free end of the fibre, and unwinding the fibre, wherein the composite part is aligned horizontally, wherein the pyrolisis is done continuously, wherein a core element for creating the supporting pressure (p) is positioned in the fibre structure along the main axis (m) before the removal of the retainer, wherein a core element for creating the supporting pressure (p) is positioned in the fibre structure along the main axis (m), wherein the removal of the retainer and the supporting of the fibre structure by the core element are done simultaneously, wherein the locating and grabbing of the free end of the fibre is done by electric charging, wherein, the locating and grabbing of the free end of the fibre is done by rotating the fibre structure around the main axis.

Assignees

Inventors

Classifications

  • B29B17/02Primary

    Separating plastics from other materials · CPC title

  • containing silica · CPC title

  • Disintegrating plastics, {e.g. by milling}(B29B9/02, B29B11/02, B29B13/10, {B29B17/02} take precedence) · CPC title

  • B01J6/008Primary

    Pyrolysis reactions (of hydrocarbons C10G9/00) · CPC title

  • Chemistry & Metallurgy · mapped topic

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What does patent US9511337B2 cover?
Disclosed is a method and an apparatus for extracting a long fiber, and in particular an endless fiber, embedded in a resin matrix forming a wound composite part, wherein the fiber is extracted as one single part by unwinding after a pyrolisis treatment for a decomposition of the matrix.
Who is the assignee on this patent?
Airbus Operations Gmbh
What technology area does this patent fall under?
Primary CPC classification B29B17/02. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Dec 06 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).