Blade
The invention relates to a method for verifying the positioning of a fibrous preform in a blade, the blade having been obtained by injecting a resin into a mould having the shape of a blade and in which a preform has been placed, the blade extending in an orthonormal blade frame of reference X, Y, Z, the blade comprising a blade root extending longitudinally along an axis X, a vane extending from the blade root along an axis Z, the blade having a thickness defined along an axis Y, the preform comprising glass tracers positioned at the surface of the preform, the centre of the tracers defining a neutral axis located at a height along the axis Z in the direction defined by the axis X, the method comprising the following steps: the acquisition (E 31 ) of tomographic 2D projections of the blade using an imaging system comprising an X-ray source, each projection being acquired at a given orientation of the X-ray source with respect to the blade; the combining (E 32 , E 32 a , E 32 b ) of the 2D projections in the direction of the axis Y so as to obtain a cumulative 2D image in the directions X and Z; the determining (E 33 ), for each pixel column defined in the direction of the axis Z, of a greyscale profile; the processing (E 34 ) of each of the profiles obtained so as to locate the position, in Z, of the neutral axis in the direction of the axis X.
1. A method for checking the positioning of a fibrous preform in a blade, the method comprising:
acquiring two-dimensional (2D) tomographic projections of a blade by an imaging system comprising an X-ray source, each projection being acquired at a given orientation of the X-ray source relative to the blade, the blade having been obtained by injection of a resin into a mold having the shape of a blade and in which a preform has been placed, the blade extending in an orthonormal blade reference frame X, Y, Z, the blade comprising a blade root extending longitudinally along an axis X, an airfoil extending from the blade root along an axis Z, the blade having a thickness defined along an axis Y, the preform comprising glass tracers positioned on the surface of the preform, the center of the tracers defining a neutral fiber located at a height along the axis Z along the direction defined by the axis X;
accumulating the 2D projections along the direction of the axis Y so as to obtain a 2D image accumulated along the directions X and Z;
determining, for each pixel column defined along the direction of the axis Z, a profile of grayscales;
processing each of the profiles obtained so as to locate the position in Z of the neutral fiber along the direction of the axis X.
2. The method according to claim 1 , wherein the accumulating comprises obtaining an accumulated 2D image made up of pixels having the maximum grayscale among a stack of pixels of the different sections stacked along the direction of the axis Y.
3. The method according to claim 1 , wherein in the accumulating the 2D projections, the accumulated 2D image is made up of pixels whose grayscale is the sum of the pixels of the different sections stacked along the direction of the axis Y.
4. The method according to claim 1 , wherein the profile of grayscales is a Gaussian, the location of the neutral fiber being the center (X 1 ) of the Gaussian.
5. The method according to claim 1 , wherein the profile of grayscales is a double Gaussian, the location of the neutral fiber being the center of the two Gaussians.
6. The method according to claim 1 , comprising filtering the location along the direction Z of the neutral fiber along the direction of the axis X.
7. The method according to claim 1 , comprising comparing the location of the thus obtained neutral fiber with a theoretical location of the neutral fiber.
8. The method for manufacturing a turbomachine blade made of composite material, the method comprising:
placing a fibrous preform in a mold having the shape of a blade;
injecting under vacuum a resin into the mold comprising the preform so as to obtain a blade called an injected blade;
checking the positioning of the fibrous preform in the injected blade by the method according to claim 1 .