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AssigneeSafran Aircraft Engines
InventorsMickael Rancic, Jérôme Salmon, Pierre Marcel Emilien Navar
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A method for deburring an aeronautical part with an articulated tooling including a plurality of axes of rotation, the aeronautical part including at least one edge to be deburred, the articulated tooling including a tool holder, holding a calibration tool and a machining tool, the calibration tool and the machining tool being fixed to the tool holder and being immovable relative to one another, the method including steps of calibrating the calibration tool and the machining tool, of parameterizing the aeronautical part, of deburring the at least one edge to be deburred with the machining tool moving along a predetermined trajectory, on the basis of the parameters obtained during the parameterization step.
A method for deburring a turbomachine disk comprising a plurality of slots with an articulated tooling, the articulated tooling comprising a plurality of axes of rotation, the turbomachine disk comprising at least one edge to be deburred, the at least one edge to be deburred being a bottom edge of a slot of the plurality of slots of the disk, the articulated tooling comprising a tool holder, the tool holder holding a calibration tool and a machining tool, the calibration tool and the machining tool being attached to the tool holder and being immovable relative to one another, the method comprising steps of:
Dependencies are inferred from the claim text.