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    • 9. 发明授权
    • Repair process
    • 维修过程
    • US07377417B2
    • 2008-05-27
    • US11292505
    • 2005-12-02
    • Monika D. Kinstler
    • Monika D. Kinstler
    • B23K31/00B23P6/04
    • B23P6/007B23K35/0244B23K35/025B23K35/304B23K2101/001B23P6/045Y10T29/49318
    • In accordance with the present invention, a process for repairing metal workpieces, such as turbine engine components, is provided. The process comprises the steps of forming a braze paste containing a first nickel base alloy material containing boron and chromium and a second nickel base alloy material containing chromium and cobalt, applying the brazing paste to an area of the metal workpiece containing at least one crack, and subjecting the workpiece and the brazing paste to a brazing cycle by heating the brazing paste and the workpiece, preferably to a temperature in the range of from 2000 to 2200 degrees Fahrenheit. During the brazing cycle, the brazing paste flows into and fills the at least one crack and thus repairs the metal workpiece.
    • 根据本发明,提供了一种用于修理诸如涡轮发动机部件的金属工件的工艺。 该方法包括以下步骤:形成含有含有硼和铬的第一镍基合金材料和含有铬和钴的第二镍基合金材料的钎焊膏,将钎焊膏施加到包含至少一个裂纹的金属工件的区域中, 并且通过将钎焊膏和工件加热而使工件和钎焊膏经受钎焊循环,优选为2000-2200华氏度的温度。 在钎焊循环期间,钎焊膏流入并填充至少一个裂纹,从而修复金属工件。