Decoating for rotationally symmetric components, in particular of aircraft engines

Decoating (1) for rotationally symmetric components, in particular of aircraft engines, the removal is performed by means of a removal fluid ($), which is locally attached to the to be stripped part into contact with an at least one axis of rotation (5) rotating receptacle (6) for receiving the removal fluid (4) is provided, and the Entschichtungsflussigkeitsoberflache (7) formed by the rotation of a paraboloid of revolution, wherein the one or more locally to be stripped components are accommodated in a container and immerse radially outwardly in the removal fluid (4). Characterized a decoating device (1) is created, which allows for easy stripping of radially symmetrical components in the radially outward-side region.