Solution heat treatment method for manufacturing metallic components of a turbo machine

A solution heat treatment method is disclosed for manufacturing metallic components 1 of a turbo machine, which components 1 provide a hot gas flow channel when assembled in the turbo machine after manufacturing, wherein the components 1 are subjected to a time-temperature-cycle in a furnace. The me...

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Bibliographic Details
Main Authors BALLIEL MARTIN, SCHNEIDER MARTIN
Format Patent
LanguageChinese
English
Published 30.06.2017
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Summary:A solution heat treatment method is disclosed for manufacturing metallic components 1 of a turbo machine, which components 1 provide a hot gas flow channel when assembled in the turbo machine after manufacturing, wherein the components 1 are subjected to a time-temperature-cycle in a furnace. The method includes positioning the components 1 in the furnace in a same principle as the component assembly in the turbo machine, but leaving flow areas and gaps 9 between neighbouring components; then starting the time-temperature-cycle; and applying an inert gas during the solution heat treatment process so that the inert gas flows through flow areas and gaps 9 for achieving a uniform temperature. 本发明涉及种用于制造涡轮机的金属部件(1)的固溶热处理方法,其中在制造之后当在涡轮机中组装时部件(1)提供热气体流动通道,其中部件(1)在炉中承受时间-温度-周期。所述方法的特征在于-以与涡轮机中部件组装相同的原理将部件(1)定位在炉中,而且在邻近的部件(1)之间保留流动区域和间隙(9),然后-开始时间-温度-周期并且-在固溶热处理过程期间应用惰性气体,使得惰性气体流动通过所述流动区域和间隙(9),以便实现在固溶热处理过程中在任何时刻,特别地在快速冷却和加热阶段期间的均匀温度。
Bibliography:Application Number: CN201611273083