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Process for producing a workpiece in titanium alloy comprising a modified hot working stage and workpiece thus produced

机译:包括改进的热加工阶段的钛合金工件的生产方法以及由此生产的工件

摘要

With this alloy having the composition (in mass %) Mo equivalent = 5 to 13 and Al equivalent = 3 to 8, Ti and impurities = the remainder, this process comprises a hot preliminary trimming of an ingot of the said alloy giving a hot blank, then a final trimming of at least a portion of this blank, preceded by a preheating above the real beta transition (2) of the said hot-trimmed alloy, the final trimming ratio (S/s) being higher than or equal to 1.5, and dissolving and then annealing treatments are then performed on the blank of an article obtained by final trimming. The process is characterised in that the said blank is cooled from its preheating temperature (8) to a temperature (9) of start of final trimming, situated between the beta transition (2) and the appearance of the alpha phase (7). …??The invention also relates to the article obtained for a selected composition. The fabricated articles are intended, for example, for compressor discs or aircraft propulsion systems.
机译:该合金的组成(质量%)为Mo当量= 5至13,Al当量= 3至8,Ti和杂质=剩余物,该工艺包括对所述合金锭进行热初步修整,得到热坯料。 ,然后对该坯料的至少一部分进行最终修整,然后在所述热修整合金的实际β转变(2)之上进行预热,最终修整比(S / s)大于或等于1.5然后,对通过最终修整获得的制品的坯料进行溶解,然后进行退火处理。该方法的特征在于,将所述坯料从其预热温度(8)冷却到开始进行最终修整的温度(9),该温度位于β转变(2)和α相(7)的出现之间。本发明还涉及针对所选组合物获得的制品。制成品旨在用于例如压缩机盘或飞机推进系统。

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