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首页> 外文期刊>The Paton Welding Journal >REPAIR WELDING OF INTERMEDIATE CASES OF AIRCRAFT ENGINES FROM HIGH-TEMPERATURE MAGNESIUM ALLOY ML10 WITH APPLICATION OF ELECTRODYNAMIC TREATMENT
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REPAIR WELDING OF INTERMEDIATE CASES OF AIRCRAFT ENGINES FROM HIGH-TEMPERATURE MAGNESIUM ALLOY ML10 WITH APPLICATION OF ELECTRODYNAMIC TREATMENT

机译:高温镁合金ML10对飞机发动机中间壳体的修复及电热处理

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摘要

Technology was developed for repair welding of damages in aircraft engine intermediate cases from magnesium alloy ML10, The technology comprises electrodynamic treatment of welds aimed at reducing the level of residual welding stresses,, It was experimentally proved that treatment practically eliminates residual stresses in the weld. At charging voltage of up to 200 V electrodynamic treatment operator can perform maximum 1100 electrodynamic impact operations per shift, and at 500 V voltage - not more than 100 operations, that fully meets the requirements of production cycle of repair welding of aircraft intermediate case.
机译:开发了一种镁合金ML10飞机发动机中间壳体损伤修复焊接技术,该技术包括对焊缝进行电动力处理以降低残余焊接应力的水平,并通过实验证明该处理实际上消除了焊缝中的残余应力。在最高200 V的充电电压下,电动操作员每班最多可以执行1100次电动冲击操作,而在500 V的电压下-不超过100次操作,完全可以满足飞机中间箱维修焊接的生产周期要求。

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