Method for checking the position of a preform in a mould
AssigneeSafran Aircraft Engines
InventorsMarc-Emmanuel Techer, Nicolas Ashtari
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AssigneeSafran Aircraft Engines
InventorsMarc-Emmanuel Techer, Nicolas Ashtari
Estimating the term…
The invention relates to a method for manufacturing a turbine engine blade from a preform (10) of composite material polymerised in a mould comprising a lower part (16) and an upper part, comprising at least one closure step, during which the upper part of said mould is placed on the lower part (16) of the mould containing the preform (10). The method comprises, prior to said closure step, at least one sub-step of inserting a position marker (28) into the preform (10), at least one sub-step of compacting the preform using an insert (34) intended to be received in the upper part of the mould (18), and at least one sub-step of checking the position of the marker (28) relative to a reference mark (30) of said insert (34).
A method for manufacturing a turbine engine blade from composite material comprising:
A blade preform obtained by weaving a single piece, said weave being a three-dimensional yarn weave, said preform comprising a blade root part and a blade vane part, wherein it comprises a position marker inserted into the weave of said preform and wherein the blade root part of the preform comprises a zone configured to undergo a cutting operation to obtain a finished blade, and in that said position marker of said preform is inserted into said zone.
An impregnation mould for manufacturing a blade from composite material for a turbine engine, comprising a lower mould part having a recess of substantially longitudinal orientation that substantially matches a lower part of a blade preform, and an upper part having a recess of substantially longitudinal orientation that substantially matches an upper part of the blade preform, said upper part being able to be placed on said lower part, wherein it comprises an insert, which is intended to be fixed by a first end in a clear position relative to the lower part of the mould,
Dependencies are inferred from the claim text.