Method for making a structural part of a composite material having a calibrated thickness and structural part thus obtained
AssigneeAirbus France
InventorsMathieu Normand, Jean-Claude Lacombe
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AssigneeAirbus France
InventorsMathieu Normand, Jean-Claude Lacombe
Estimating the term…
The disclosed embodiments offer a solution for controlling the thickness of a finished structural composite part when precise tolerances must be complied with for the quality of the assembly and in order to ease the assembly operations of this part. In order to implement the method according to the disclosed embodiments, an additional layer of plies made out of a non-structural composite material, called calibrating plies, is applied onto the structural plies of the structural part, at least in an area where the thickness must be maintained within close tolerances and, after the composite material has been cured, the calibrating plies are machined in order to obtain the thickness required for the finished part. The thickness of the calibrating plies applied is determined according to the possible thicknesses of structural plies, taking into account the manufacturing spreads so that the machining operation for the calibrating plies does not affect the structural plies.
A method for producing a structural part made out of composite material including structural plies made out of fibres in a cured resin, said structural plies being capable of resisting strains likely to be applied to the part in use, said structural part having, in at least one area, a predetermined thickness Enom, defined with production tolerances, said method comprising:
A structural part made out of composite material, at least in part, said composite material including fibres in a cured resin, said structural part having in at least one area, a thickness Enom, defined with a manufacturing tolerance, wherein said structural part includes in at least one Enom thickness area:
Dependencies are inferred from the claim text.