Device and method for producing a structural thermoplastic part
AssigneeStelia Aerospace
InventorPierre Magnin
Life of this patent
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Abstract
Structural thermoplastic part production device, intended to be integrated to a primary structure of an aeroplane, said structural part being formed from a draft part comprising reinforcing fibres embedded in a thermoplastic matrix, production device comprising a member for supporting a draft part, at least one heating member, at least one cooling member, at least one main compression member configured to compress the local portion of the draft part against the support member so as to decrease the porosity thereof and a system for moving the heating member, the compression member and the cooling member so as to stiffen each local portion of the draft part successively.
Claims12
A production device configured to be integrated to a primary structure of an aeroplane, said production device comprising a structural part being formed from a draft part comprising reinforcing fibres embedded in a thermoplastic matrix, the production device comprising:
- a member for supporting a draft part, the support member extending along a longitudinal axis,
- at least one heating member configured to heat a local portion of the draft part at a temperature making it possible to make the thermoplastic matrix of the draft part malleable,
- at least one cooling member configured to cool the local portion of the draft part at a temperature making it possible to solidify the thermoplastic matrix of the draft part,
- at least one main compression member configured to compress the local portion of the draft part against the support member so as to decrease the porosity thereof, the main compression member being situated between the heating member and the cooling member, and
- a system for moving from upstream to downstream along the longitudinal axis of the heating member, of the compression member and of the cooling member relative to the support member so as to consolidate each local portion of the draft part successively.
A method for producing a structural thermoplastic part, intended to be integrated to a primary structure of an aeroplane, from a draft part comprising reinforcing fibres embedded in a thermoplastic matrix, the draft part being supported on a support member extending along a longitudinal axis, the method comprises:
- a step of heating a local portion of the draft part at a temperature making it possible to make the thermoplastic matrix of the draft part melt, then
- a step of compressing the local portion of the draft part against the support member so as to increase the density thereof, then
- a step of cooling said local portion of the draft part at a temperature making it possible to solidify the thermoplastic matrix of the draft part.
Dependencies are inferred from the claim text.