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AssigneeSafran Aircraft Engines
InventorsPierre-Alexis Poulet, Richard Mounien, Lucas Antoine Christophe Lauwick
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A method for manufacturing a blade of a fan for an aircraft turbomachine extending around a longitudinal axis, the blade including an aerofoil made of a composite material having a leading edge and a trailing edge connected by a pressure side and a suction side, the aerofoil extending between a base and a free end, the method including each of the following steps: —pairing and bonding a metal shield to the leading edge, —obtaining a first measurement of a radial moment weight of the blade before or after the metal shield has been bonded to the leading edge and determining a machining kerf, —machining the free end and/or the trailing edge along the machining kerf so as to adjust the mass and radial moment weight of the blade, —obtaining a second measurement of the radial moment weight of the blade.
A method for manufacturing a vane for a fan of an aircraft turbomachine extending about a longitudinal axis, the vane comprising a blade made of a composite material having a leading edge and a trailing edge connected by a pressure side and a suction side, the blade extending between a root and a free end, the method comprising each of the following steps:
Dependencies are inferred from the claim text.