| 摘要 |
<p>The method, according to the invention, for estimating a thickness of a ceramic thermal barrier coating that is to be physically deposited in vapour form by a target onto a hot part of a gas turbine mounted on a support tool, comprises: - a step (E10) of digitally modelling the geometric shape of the hot part and its kinematics with respect to the target; - a step (E20) of surface meshing the modelled hot part; and - a step (E50) of estimating, for at least one mesh of the hot part exposed to the target's radiation when the coating is deposited, a thickness of coating that is to be deposited onto said mesh at a given moment using a radiation model of the target and taking into account the position of said mesh at said moment with respect to the target.</p> |
