METHOD FOR CORRECTING THE RADIAL MOMENT WEIGHT OF A VANE FOR AN AIRCRAFT TURBINE ENGINE

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United States of America Patent

APP PUB NO 20250100673A1
SERIAL NO

18690459

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Abstract

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A method for correcting the radial moment weight of a vane includes the step of providing a vane extending along an axis of elongation (Z) between a free end and an opposite root, the vane having a blade made of composite material and having a leading edge. The method further includes the steps of measuring the radial moment weight of the vane and comparing the measured radial moment weight to a reference value and adjusting the radial moment weight of the vane according to the result of the comparison. The vane has at least one adjustment cavity extending along the leading edge and opening into the free end of the vane. The adjustment is carried out by inserting a first material into the adjustment cavity.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AIRCRAFT ENGINES2 BOULEVARD DU GÉNÉRAL MARTIAL VALIN 75015 PARIS

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
LAUWICK, Lucas Antoine Christophe MOISSY-CRAMAYEL, FR 6 0
MOUROT, Maxime Mathieu MOISSY-CRAMAYEL, FR 2 0
QUEANT, Didier MOISSY-CRAMAYEL, FR 5 23

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