Method for relieving stresses by rotation
AssigneeSafran Aircraft Engines
InventorsElliott Archibald Breittmayer, David Gardy, Jocelyn Bastide
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AssigneeSafran Aircraft Engines
InventorsElliott Archibald Breittmayer, David Gardy, Jocelyn Bastide
Estimating the term…
A method for relieving residual stresses in a part includes increasing the rotation speed, which includes measuring, at a first given instant, values representative of the rotation speed and the radial enlargement; measuring, at a second given instant after the first instant, values representative of the rotation speed and the radial enlargement; determining a leading coefficient of a first affine function from the preceding values; determining a target radial enlargement value as a function of a value representative of the rotation speed, in the form of a second affine function, the origin of which is the value of a desired final residual enlargement and the leading coefficient of which is the leading coefficient of the first affine function; stopping the increase in rotation speed of the part from the moment that the actual enlargement of the rotating part corresponds to the target relative radial enlargement value that has been determined.
A method for relieving residual stresses in a part by rotating said part, the method for relieving stresses comprising a step of increasing a rotation speed and a step of decreasing the rotation speed, wherein the step of increasing the rotation speed comprises:
Dependencies are inferred from the claim text.