发明名称 Repair method
摘要 <p>The method involves removing the damaged area of fiber composite component, and forming a splice (2) in the region of the removed damaged area. The Z-pins (5) formed as spring steel wires are inserted into the fiber composite component (1) in the region of the splice. A repair-fiber semi-finished material (6) is inserted to the splice such that the repair fiber semi-finished material is draped around the Z-pins and the fiber bundle of repair fiber semi-finished material is not damaged by the Z-pins. The repair fiber semi-finished material is cured.</p>
申请公布号 EP2602098(A1) 申请公布日期 2013.06.12
申请号 EP20120195841 申请日期 2012.12.06
申请人 DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V. 发明人 HOLZHUETER, DIRK;HUEHNE, CHRISTIAN;KOLESNIKOV, BORIS;STEFFEN, OLAF
分类号 B29C73/10 主分类号 B29C73/10
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