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Process for the repair of DLC-coated components and DLC-coated aircraft components

机译:修复DLC涂层组件和DLC涂层飞机组分的方法

摘要

The invention relates to a method for repairing components (1) coated with DLC as well as an aircraft component (1) coated with DLC. The method comprises the steps: evaporation and / or conversion of the DLC layer (8) by irradiation with a laser, wherein the properties of the laser radiation and the irradiation parameters are selected so that the carrier material underneath the DLC layer (8) is not impaired; and- cleaning the carrier material by blasting with a blasting agent which does not impair the carrier material.The aircraft component (1) is a variable guide vane provided for use in an aircraft engine, comprising an aerodynamically shaped vane area (2) with the vane surface (3) and an axis of rotation (4) , bearing journals (5) being provided coaxially with the axis of rotation (4) at both ends of the blade area for rotatable mounting in coaxially arranged bearing journal receivers, the bearing journals (5) each projecting from a stop surface (6) for contact with an end face of the bearing journal receivers are. The outer surfaces of the bearing journals (5) and the stop surfaces (6) are provided with a DLC layer (8) which can be repaired using a method according to the invention.
机译:本发明涉及一种修复涂有DLC的组分(1)以及涂有DLC的飞机部件(1)的方法。该方法包括步骤:通过用激光照射蒸发和/或转换DLC层(8),其中选择激光辐射和照射参数的性质,使得DLC层(8)下面的载体材料是没有受损;通过用不损害载体材料的喷砂剂爆炸清洁载体材料。飞机部件(1)是提供用于飞机发动机的可变导向叶片,包括空气动力学形式的叶片区域(2)叶片表面(3)和旋转轴(4),轴承轴颈(5)在叶片区域的两端在叶片区域的两端同轴地设置,以便在同轴地布置的轴承轴颈接收器中,轴承期刊旋转(5)从止动表面(6)突出,用于与轴承轴颈接收器的端面接触。轴承轴颈(5)和止动表面(6)的外表面设置有DLC层(8),其可以使用根据本发明的方法进行修复。

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