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Repair of gas turbine blade tip without recoating the repaired blade tip

机译:修复燃气轮机叶片尖端,而无需重新涂覆已修复的叶片尖端

摘要

A damaged gas turbine blade (40) which has previously been in service, and which is made of a base metal, is furnished. Any damaged material is removed from the damaged blade tip (50). The damaged blade tip (50) is weld repaired with a nickel-base superalloy that is more resistant to oxidation resistance than is the base metal in the operating environment of the tip-repaired gas turbine blade (60). The method does not include any step of coating a lateral surface of the repaired blade tip with a non-ceramic coating after the step of weld repairing.
机译:提供了一种损坏的燃气轮机叶片(40),该燃气轮机叶片(40)先前已经使用过并且由贱金属制成。从损坏的刀片尖端(50)上清除所有损坏的材料。损坏的叶片尖端(50)用镍基高温合金进行焊接修复,该镍基高温合金在尖端修复后的燃气轮机叶片(60)的工作环境中比母材更具抗氧化性。该方法不包括在焊接修复步骤之后用非陶瓷涂层涂覆修复的刀片尖端的侧面的任何步骤。

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