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TURBINE BLADE TIP FINISHING APPARATUS AND METHOD.

机译:涡轮叶片尖端修整装置和方法。

摘要

device and method for finishing the edges of improved turbine vanes of a similar.the method is particularly useful in the case of turbine blades which have been reparees by re welding.an abrasive (42) - first of all the surplus solder (30 ') with a back and forth motion and constant force.a detector (62) indicates when the abrasive is a distance above the surface of the predeterminee (c) outline of finishing required.then the removal of material for a pre-set period of time.during this period, the movement of the abrasive is pre-set in a converted motion along a path corresponding to the path of the guide edges of the finished surface by means of a cam (36).and a roller (50). the time of finishing is reduced and productivity increased.
机译:用于修整类似的改进型涡轮叶片的边缘的装置和方法。该方法在通过重新焊接修复的涡轮叶片的情况下特别有用。磨料(42)-首先是多余的焊料(30')带有往复运动和恒定力的检测器(62)指示磨料何时达到预定范围(c)所需精加工轮廓的距离以上,然后在预设的时间内清除材料。在此期间,通过凸轮(36)和辊子(50)以沿着与精加工表面的引导边缘的路径相对应的路径的转换运动来预设磨料的运动。减少了修整时间,提高了生产率。

著录项

  • 公开/公告号EP0045794A4

    专利类型

  • 公开/公告日1984-08-08

    原文格式PDF

  • 申请/专利权人 UNITED TECHNOLOGIES CORPORATION;

    申请/专利号EP19810900704

  • 发明设计人 ARRIGONI JOHN PETER;

    申请日1981-02-12

  • 分类号B24B21/16;B24B1/00;

  • 国家 EP

  • 入库时间 2022-08-22 09:00:02

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