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REPAIR METHOD OF GAS TURBINE HIGH TEMPERATURE PART AND GAS TURBINE HIGH TEMPERATURE PART

机译:燃气轮机高温部分和燃气轮机高温部分的维修方法

摘要

PPROBLEM TO BE SOLVED: To provide a repair part of excellent strength and environment resistance by efficiently and surely uniforming a crystal growing direction of a building-up part, appropriately penetrating in and preventing recrystallization due to crack and residual stress on welding, when conducting building-up repair of the gas turbine high temperature part by a half overlap method. PSOLUTION: In the repair method of the gas turbine high temperature part for repairing a part to be repaired of the gas turbine high temperature part using a directional solidification member by build up welding of single crystal with the half overlap method, output density of a heating source of build up welding is 1 10SP4/SPto 10 10SP4/SPW/cmSP2/SPand thickness of a unit layer of build up welding is equal to or thinner than 300 m and one or more layers are formed. PCOPYRIGHT: (C)2008,JPO&INPIT
机译:

要解决的问题:通过有效并可靠地均匀化堆焊部件的晶体生长方向,适当地渗透并防止由于裂纹和焊接时的残余应力而导致的再结晶,从而提供一种具有出色强度和耐环境性的维修部件,当通过半重叠法进行燃气轮机高温部件的积层修复时。

解决方案:在燃气轮机高温部件的修复方法中,使用定向凝固构件通过半重叠法堆焊单晶来修复燃气轮机高温部件的待修复部件,输出密度堆焊热源的厚度为1 10 4 至10 10 4 W / cm 2 ,堆焊单位层的厚度焊接等于或小于300 m,并形成一层或多层。

版权:(C)2008,日本特许厅&INPIT

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