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公开(公告)号:US07204019B2
公开(公告)日:2007-04-17
申请号:US09935896
申请日:2001-08-23
CPC分类号: B23P6/002 , B23H9/10 , B23H9/14 , B23P2700/06 , C23C4/02 , C23C4/18 , C23C28/32 , C23C28/345 , C23C28/3455 , F01D5/005 , F05D2230/12 , F05D2230/90 , F05D2250/232 , F05D2260/202 , Y10T29/49318 , Y10T29/49339 , Y10T29/49341 , Y10T29/49721 , Y10T29/49726 , Y10T29/4973 , Y10T29/49746
摘要: A method for repairing defects in a gas turbine component that comprises a substrate and an existing coating on the substrate. The article includes cooling holes having a predetermined air flow requirement and an outer shaped portion and an inner metering portion. The method comprises removing the existing coating and recoating the surface of the article with a nonoriginal coating. After the nonoriginal coating is applied onto the component, the cooling holes that meet a predetermined inspection criteria are reworked to remove the excess nonoriginal coating deposited in the outer shaped portion of the cooling holes. The reworking is done by receiving an electrode, having only a shaped portion with a preselected shape, in the outer shaped portion of the cooling holes thus restoring the cooling holes to the predetermined air flow requirement.
摘要翻译: 一种用于修复燃气轮机部件中的缺陷的方法,所述方法包括基板和所述基板上的现有涂层。 该制品包括具有预定空气流量要求的冷却孔和外部形状部分和内部计量部分。 该方法包括用非原始涂层去除现有涂层并重新涂覆制品的表面。 在将非原始涂层施加到部件上之后,再次加工满足预定检查标准的冷却孔,以去除沉积在冷却孔外形部分中的多余非原始涂层。 通过在冷却孔的外形部分中容纳仅具有预定形状的成形部分的电极,从而将冷却孔恢复到预定的空气流量要求,从而进行返工。