Process for manufacturing a panel made of a thermoplastic composite
View Patent ↗A method of manufacturing a panel made of a composite material using a tool having a support on which a lay-up is performed, the lay-up producing a stack of plies of fiber prepregs, followed by consolidating the stack aiming to obtain the panel using a compacting plate arranged above the stack. The method is implemented such that a first set of polyimide films partially covering each other is located in contact with the stack of plies, between the latter and the compacting plate.
1. A method for manufacturing a panel in a composite material using a tooling including a support, comprising:
performing a lay-up on the support of the tooling so as to produce a stack of plies of fiber prepregs;
consolidating the stack of plies to obtain the panel using a compacting plate arranged above the stack of plies;
arranging a first set of polyimide films in contact with the stack of plies, between the stack of plies and the compacting plate, such that adjacent polyimide films partially overlap along adjacent edges thereof forming overlapping zones between the adjacent polyimide films;
arranging a second set of polyimide films in contact with the stack of plies, between the stack and the support of the tooling, such that adjacent polyimide films of the second set of polyimide films partially overlap along adjacent edges thereof forming overlapping zones between the adjacent polyimide films of the second set of polyimide films; and
creating a vacuum via a plurality of through orifices disposed within the support across the arranged polyimide films, so as to equalize air evacuation through a plurality of the overlapping zones between the adjacent polyimide films,
wherein a width of the overlapping zones is approximately 15 mm.
2. The manufacturing method according to claim 1 , further comprising:
placing on the compacting plate a first drainage fabric, such that the first fabric is located in contact with the compacting plate and separated from the first set of polyimide films by the compacting plate; and
placing on the support of the tooling a second drainage fabric, such that the second drainage fabric is located in contact with the support of the tooling, between the support and the second set of polyimide films.
3. The manufacturing method according to claim 1 , further comprising placing at least one wedge so as to limit edge effects, which are likely to occur during the step of consolidating the stack, each wedge being arranged along an edge of the stack.
4. The manufacturing method according to claim 3 , wherein each wedge limiting the edge effects has a thickness approximately equal to that of the panel to be obtained from the stack, upon completion of the step of consolidating the stack.
5. The manufacturing method according to claim 3 , wherein each wedge limiting the edge effects has at least one surface including a plurality of drainage grooves.
6. The manufacturing method according to claim 3 , wherein each wedge limiting the edge effects has an initial thickness greater than that of the panel to be obtained from the stack, upon completion of the step of consolidating the stack, each wedge being designed and arranged so as to be deformed by compression by the compacting plate, during the step of consolidating the stack.
7. The manufacturing method according to claim 1 , wherein the step of consolidating the stack is performed by applying negative pressure within a sealing chamber partially defined by the support and in which the stack of plies and the compacting plate are located, and by performing heating of the stack of plies of fiber prepregs.
8. The manufacturing method according to claim 7 , wherein the tooling further includes a negative pressure application mechanism for the sealing chamber, connected to through orifices disposed within the support.
9. The manufacturing method according to claim 8 , wherein the support is a marble plate.
10. The manufacturing method according to claim 7 , wherein the tooling further includes a heating mechanism for the stack of plies of fiber prepregs, the heating mechanism being integrated with the support.
11. The manufacturing method according to claim 1 , wherein upon completion of the step of consolidating the stack, a substantially flat panel is obtained.
12. The manufacturing method according to claim 1 , wherein upon completion of the step of consolidating the stack, a panel having a single curvature is obtained.
13. The manufacturing method according to claim 1 , wherein upon completion of the step of consolidating the stack, a panel having a double curvature is obtained.
14. The manufacturing method according to claim 12 , wherein the lay-up is performed such that following placement of a given ply of fiber prepregs on other already-stacked plies, the given ply is secured to at least one of the plies of already-stacked fiber prepregs, using at least one weld point.
15. The manufacturing method according to claim 1 , wherein an aircraft fuselage panel is manufactured.
16. The manufacturing method according to claim 1 , wherein each overlapping zone between the adjacent polyimide films includes no more than two polyimide films.
17. The manufacturing method according to claim 1 , wherein the second set of polyimide films is arranged such that adjacent polyimide films of the second set of polyimide films partially overlap along adjacent edges thereof forming overlapping zones between the adjacent polyimide films of the second set of polyimide films.
18. The manufacturing method according to claim 17 , wherein each overlapping zone between the adjacent polyimide films of the second set of polyimide films includes no more than two polyimide films of the second set of polyimide films.