Method for producing a profile that has a re-entrant angle in a composite material from a stack of layers of fibres

Patent metadata

Field	Value
Publication number	US-9840063-B2
Application number	US-201314013872-A
Country	US
Kind code	B2
Filing date	Aug 29, 2013
Priority date	Sep 7, 2012
Publication date	Dec 12, 2017
Grant date	Dec 12, 2017

Abstract

A method for producing, in a composite material, a component that has a re-entrant angle, includes stacking layers of fibers which have been pre-impregnated with a resin so as to obtain a preform and placing the preform in a tooling fixture in order to subject it to a polymerization cycle including a temperature cycle, with a temperature-increase phase and at least one soak at which the temperature is maintained, and a pressure cycle on the outside of the tooling fixture with a pressure-increase phase and a pressure-hold phase, with the layers of pre-impregnated fibers being able to slip against one another when the temperature of the temperature cycle is equal to or higher than a threshold temperature Tf dependent on the resin. The temperature-increase phase includes a soak at a temperature higher than or equal to Tf, the soak beginning before the end of the pressure-increase phase.

First claim

The invention claimed is:

1. A method for producing, in a composite material, a component that has a re-entrant angle, the said method comprising:
stacking, in a mold of a tooling fixture, layers of fibres which have been pre-impregnated with a resin so as to obtain a preform having said re-entrant angle, the stack of layers of pre-impregnated fibres comprising a defect of the bridging type at the re-entrant angle;
subjecting the preform disposed in the tooling fixture to a polymerization cycle comprising a temperature cycle including a temperature-increase phase and a first soak at which temperature is maintained, a second soak at which temperature is maintained and a third soak at which temperature is maintained, and a pressure cycle which includes subjecting the preform to a pressure at a location outside of the tooling fixture, the pressure cycle including a pressure-increase phase and a pressure-hold phase;
determining a threshold temperature Tf of the resin wherein, during the temperature-increase phase, when the temperature is equal to or higher than said threshold temperature Tf, the layers of fibres are able to slip against one another without wrinkling;
subjecting the preform to a vacuum-pulling cycle in which a vacuum is pulled on the inside of the tooling fixture, the vacuum-pulling cycle beginning before the start of the pressure cycle and at the same time as the start of the temperature cycle so that the fibres are subjected to tensile loadings before the layers of pre-impregnated fibres are compressed, the defect of the bridging type allowing the fibres in the preform to be stretched out; and
causing, during the polymerization cycle, the layers of pre-impregnated fibres to slip against one another when the temperature of the temperature cycle is equal to or higher than the threshold temperature Tf which is dependent on the resin,
characterized in that at least one of said first soak, said second soak and said third soak is at a temperature higher than or equal to the threshold temperature Tf, and at least one of said first soak, said second soak and said third soak beginning after the start of the pressure-increase phase,
characterized in that the temperature cycle includes subjecting the preform to a temperature decrease phase after said first soak, said second soak and said third soak to bring the temperature to a lower temperature than the temperature of the start of polymerization and ending the pressure-hold phase after start of said temperature decrease phase, and
characterized in that the method comprises using a forming tool interposed between the preform and a bag at the re-entrant angle.

2. The method according to claim 1 , characterized in that said first soak begins before the end of the pressure-increase phase and said second soak begins after the start of the pressure-increase phase.

3. The method according to claim 2 , characterized in that the duration of the first soak prior to the start of the pressure cycle is long enough to obtain a uniform temperature throughout the preform that is higher than or equal to the threshold temperature Tf.

4. The method according to claim 3 , characterized in that the duration of the first soak prior to the start of the pressure cycle is greater than or equal to 30 min.

5. The method according to claim 1 , characterized in that both the second soak and the third soak are performed during the pressure-hold phase.

6. The method according to claim 5 , characterized in that both the second soak and the third soak are performed during the pressure-hold phase.

7. The method according to claim 1 , characterized in that said first soak is at a temperature higher than or equal to the threshold temperature Tf.

8. The method according to claim 1 , characterized in that said second soak is at a temperature higher than or equal to the threshold temperature Tf.

9. The method according to claim 1 , characterized in that said third soak is at a temperature higher than or equal to the threshold temperature Tf.

Assignees

• Airbus Operations Sas

Inventors

• De Mattia Denis

Classifications

• B29C70/34 Primary

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

• Y10T156/10

  Methods of surface bonding and/or assembly therefor · CPC title

• Y10T428/24636

  Embodying mechanically interengaged strand[s], strand-portion[s] or strand-like strip[s] [e.g., weave, knit, etc.] · CPC title

• B29D99/0003

  Producing profiled members, e.g. beams · CPC title

• Y02T50/433

  Cross-Sectional Technologies · mapped topic