发明名称 REPAIRING METHOD OF TURBINE ENGINE PART
摘要 PROBLEM TO BE SOLVED: To provide a repairing method of a turbine engine part. SOLUTION: This repairing method of the turbine engine part such as a vane and a blade having air foil comprises to remove an oxide deposit from respective parts of a part indicating damage by crushing or oxidation of heat insulating coating, to remove a ceramic heat insulating layer from the part, and to blend a surface of the part generating nicks, dents and cracks. When the part has a deteriorated aluminum area, the deteriorated area is removed or replenished. A tip part of the part is also recovered when the part is damaged, and cutting capacity of the part is restored by applying polishing to the tip part. Afterwards, ceramic coating is applied to the part. COPYRIGHT: (C)2003,JPO
申请公布号 JP2003269190(A) 申请公布日期 2003.09.25
申请号 JP20030063986 申请日期 2003.03.10
申请人 UNITED TECHNOL CORP <UTC> 发明人 BOSE SUDHANGSHU;CETEL ALAN D;DRAGHI PETER J;PIETRUSKA NORMAN
分类号 F01D5/14;B23P6/00;C23C10/02;C23G1/20;F01D5/28;F01D25/00;F02C7/00;(IPC1-7):F02C7/00 主分类号 F01D5/14
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