Method for controlling the conformity of the profile of a curved surface of a turbomachine element
AssigneeSafran Aircraft Engines
InventorsDominique Maurice Gerard BEIGNON, Antoine BERSON
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AssigneeSafran Aircraft Engines
InventorsDominique Maurice Gerard BEIGNON, Antoine BERSON
Estimating the term…
The invention relates to a method for controlling the conformity of a profile of a section of a curved surface of a turbomachine element, comprising the following step: —(100) acquiring coordinates of a plurality of measurement points of the section in a frame of reference defined for said section; characterised in that the method comprises the following steps: —(200) calculating, based on the coordinates of these measurement points, the radius of curvature of the section at each of these points, in order to obtain a measured evolution curve of the radius of curvature according to the position of the measurement points along said section; —(300) comparing the measured evolution curve of the radius of curvature, obtained in the preceding step, with a theoretical evolution curve of the radius of curvature of the predetermined section; —(400) evaluating the conformity of the section based on the comparison carried out in the preceding step.
A control method of the conformity of a profile of a section of a curved surface of an element of a turbomachine comprising the following steps:
Dependencies are inferred from the claim text.