Method for testing a batch of material used for obtaining layers of fibres intended for manufacturing a composite material component

Patent metadata

Field	Value
Publication number	US-9417167-B2
Application number	US-201414494670-A
Country	US
Kind code	B2
Filing date	Sep 24, 2014
Priority date	Sep 27, 2013
Publication date	Aug 16, 2016
Grant date	Aug 16, 2016

Abstract

A method for testing a batch of material used to obtain layers of fibers includes taking a specimen from the batch of material, exerting a tensile force on the specimen, heating the specimen so as to relax the fibers if the specimen contains stresses, after a predetermined period of time, no longer heating and no longer exerting the tensile force on the specimen, measuring a residual extension of the specimen which corresponds to a variation in length of at least a part of the specimen in the direction of the tensile force, before and after the tensile force, and considering the batch of material not to be compliant if the residual extension exceeds a given threshold.

First claim

The invention claimed is:

1. A method for testing a batch of material used to obtain layers of fibres, the method comprising:
taking a specimen comprising fibres from the batch of material;
exerting a tensile force on the specimen for a predetermined period of time;
heating the specimen for the predetermined period of time by moving a heat source along a length of the specimen; and
measuring a residual extension of the specimen, the residual extension corresponding to a variation in length of at least a part of the specimen in the direction of the tensile force, before and after the exertion of the tensile force.

2. The method according to claim 1 , further comprising determining the batch of material to be non-compliant if the residual extension exceeds a given threshold.

3. The method according to claim 1 , wherein the tensile force is greater than or equal to 4 daN/mm 2 of cross-sectional area of the specimen.

4. The method according to claim 1 , wherein the specimen is tautened and kept taut before and after the tensile force during the measurement of the residual extension.

5. The method according to claim 4 , wherein a force of around 0.16 daN/mm 2 of cross-sectional area of the specimen is applied to tauten the specimen.

6. The method according to claim 1 , wherein the specimen is heated to a temperature of around 100° C.

7. The method according to claim 1 , wherein the specimen is in the form of a strip having a length of around 10 m, the tensile force being exerted along the length of the specimen.

8. The method according to claim 1 , wherein the fibres of the specimen are oriented in the direction of the tensile force.

9. The method according to claim 1 , wherein the specimen comprises a fixed first end connected to a fixed point of a reference element, and a movable second end at which a force is exerted.

10. The method according to claim 9 , further comprising:
providing a first mark on the specimen in the vicinity of the second end; and
providing a second mark on the reference element, the first mark and the second mark being disposed in a direction intersecting the direction of the tensile force, the residual extension corresponding to the variation in length before and after the exertion of the tensile force between the first mark and the second mark.

11. The method according to claim 1 , wherein, for a specimen having a length of 10 m and a width of around 6 mm, the threshold is around 0.8 mm for a batch of material having a density of 270 g/m 2 of pre-impregnated fibres.

12. The method according to claim 1 , wherein, for a specimen having a length of 10 m and a width of around 6 mm, the threshold is around 1 mm for a batch of material having a density of 198 g/m 2 of pre-impregnated fibres.

13. The method according to claim 1 , wherein, for a specimen having a length of 10 m and a width of around 6 mm, the threshold is around 1.2 mm for a batch of material having a density of 135 g/m 2 of pre-impregnated fibres.

14. A method for manufacturing a composite material component, comprising testing a batch of material of layers of fibres prior to use of said layers of fibres, the method for testing comprising:
taking a specimen comprising fibres from the batch of material;
exerting a tensile force on the specimen for a predetermined period of time;
heating the specimen for the predetermined period of time by moving a heat source along a length of the specimen so as to relax the fibres if the specimen contains stresses; and
measuring a residual extension of the specimen, the residual extension corresponding to a variation in length of at least a part of the specimen in the direction of the tensile force, before and after the exertion of the tensile force.

Assignees

• Airbus Operations Sas

Inventors

• De Mattia Denis

Classifications

• G01B21/32

  for measuring the deformation in a solid · CPC title

• B29C70/20

  oriented in a single direction, e.g. roofing or other parallel fibres {(B29C70/083, B29C70/226 take precedence)} · CPC title

• B29C70/54 Primary

  Component parts, details or accessories; Auxiliary operations {, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing} · CPC title

• G01N2203/0017

  Tensile · CPC title

• G01N3/18 Primary

  Performing tests at high or low temperatures · CPC title