REPAIR METHOD FOR A COMPOSITE COMPONENT FOR AN AIRCRAFT, COMPOSITE COMPONENT FOR AN AIRCRAFT, AND DEVICE FOR REPAIRING A COMPOSITE COMPONENT FOR AN AIRCRAFT

摘要

The invention relates to a repair method for a composite component (1) for an aircraft, comprising a base body (2) consisting of a fibrous composite material and a metal part (3) connected to the base body (2). Measures are taken so that the temperature in the region of the connection of the metal part (3) to the base body (2) does not exceed a pre-determined value, and additional material (5) is applied to the metal part (3) using a thermal energy supply.