Abstract
When talking about ISO tolerancing of a mechanical component it generally comes along with the hypothesis that the component is rigid. Our study deals with a turbine blade on which significant constraints are exerted during operation, causing deformation of its aerodynamic part. For that reason, ISO specification of rigid parts do not apply on the entire component. Therefore, this contribution is about the proposition of a tolerancing method that permits to perform ISO tolerancing of different parts of the component while taking into account the possible deformations. On the example of a turbine blade the developed approach based on existing methodologies is explained in detail containing tolerance writing and deformation analysis.
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