发明名称 METHOD FOR RESTORING AIRSEAL ON TURBINE BLADE
摘要 <p>The method is for restoring airseals on gas turbine blades and vanes. A worn or damaged airseal is removed by abrasive belt grinding perpendicular to its length to create a stub. Then a piece of material is joined to the stub, as by welding. Next the airseal weldment is contoured using abrasive belting, perpendicular to the weldment length. The repair is for components having two airseals of different dimensions. A single two-position fixture is usable to remove old airseals and to refinish airseal weldments. Refinishing is accomplished with a contoured belt; the contour is chosen to be intermediate, but within the tolerance of, the contours of the first and second airseals. As a result, airseals are economically restored in short runs.</p>
申请公布号 KR840002484(B1) 申请公布日期 1984.12.31
申请号 KR19800000733 申请日期 1980.02.22
申请人 UNITED TECHNOLOGIES CORP. 发明人 ARRIGONI, JOHN PETER
分类号 F01D25/00;B23P6/00;F01D5/00;F02C7/00 主分类号 F01D25/00
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