US 12,697,655 B2

要約

Method for machining an aircraft structural component using a machining system, the machining system having a drilling unit and a riveting unit, a manufacturing process controller for actuating the components of the machining system, an optical sensor and a projection unit. The method comprising the steps of: projecting a pattern by the projection unit onto a machining point with a rivet element inserted into a drill hole of the machining point, detecting the machining point including the projection of the pattern by the sensor and generating corresponding detection data by the sensor, evaluat…

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