发明名称 TURBINE BLADE TIP FINISHING APPARATUS AND METHOD
摘要 Improved apparatus and method for finishing the tips of turbine blades and the like. The invention is especially useful on worn turbine blades which have been repaired by adding weld material. An abrasive (42) first removes excess weld material (30') with a reciprocating motion and constant force. A sensor (62) indicates when the abrasive is a predetermined distance above the intended finish contour surface (C) and thereafter there is a predetermined fixed time in which the material removal continues. During the predetermined time period the motion of the abrasive is converted to one along a guided path corresponding to the path of the finished surface contour by means such as a cam (36) and cam follower (50). Thus, the time of refinishing is reduced and labor productivity is increased.
申请公布号 WO8102403(A1) 申请公布日期 1981.09.03
申请号 WO1981US00289 申请日期 1981.02.12
申请人 UNITED TECHN CORP 发明人 ARRIGONI J
分类号 B24B21/16;B24B19/14;B24B21/00;(IPC1-7):24B21/16;24B1/00 主分类号 B24B21/16
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