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    • 3. 发明公开
    • TSA 코팅 리페어 방법
    • 热喷涂铝涂层修复方法
    • KR1020140028465A
    • 2014-03-10
    • KR1020120094814
    • 2012-08-29
    • 현대중공업 주식회사
    • 양병용
    • C23C4/00B05B7/20B05B7/22
    • C23C4/01C23C4/02C23C4/08C23C4/129
    • A TSA coating repairing method is disclosed. The TSA coating repairing method includes a coating separation region measuring step which measures the size of a coating separation region and determines whether the measured size exceeds a reference size or not; a surface treatment step which treats the surface of the coating separation region with one among a blasting surface treatment method or a power tool cleaning surface treatment method based on the result of the coating separation region measuring step; and a recoating step which forms an aluminum coating layer on the top of the surface-treated coating separation region again. The TSA coating repairing method reduces unnecessarily surface-treated areas by selecting the repairing method suitable for the size of the TSA coating separation region and improves the working efficiency by reducing time required for the TSA coating repair. [Reference numerals] (AA) START; (BB) END; (S210) Coating separation region measuring step; (S220) Is a reference size of the coating separation region exceeded?; (S230) Power tool cleaning surface treatment step; (S240) Blasting surface treatment step; (S250) Re-coating step
    • 公开了一种TSA涂层修复方法。 TSA涂层修复方法包括:涂布分离区域测量步骤,其测量涂层分离区域的尺寸,并确定所测量的尺寸是否超过参考尺寸; 基于涂布分离区域测量步骤的结果,在喷砂表面处理方法或电动工具清洁表面处理方法中的一种处理涂层分离区域的表面的表面处理步骤; 以及再次在表面处理的涂层分离区域的顶部上形成铝涂层的重涂步骤。 TSA涂层修复方法通过选择适合于TSA涂层分离区域的尺寸的修复方法来减少不必要的表面处理区域,并通过减少TSA涂层修复所需的时间来提高工作效率。 (附图标记)(AA)START; (BB)END; (S210)涂布分离区测定工序; (S220)涂层分离区域的参考尺寸是否超过? (S230)电动工具清洗表面处理步骤; (S240)喷砂表面处理步骤; (S250)再涂布步骤