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METHOD OF RESTORATION OF MECHANICAL PROPERTIES OF CAST INCONEL 718 FOR SERVICED AIRCRAFT COMPONENTS

机译:用于维修飞机零部件的铸型INCONEL 718的力学性能恢复方法

摘要

METHOD FOR RESTORATION OF MECHANICAL PROPERTIES OFCAST INCONEL 718 FOR SERVICED AIRCRAFT COMPONENTSABSTRACTA heat treatment process that will restore the mechanical properties of an aircraft engine article that includes a cast Inconel 718 portion welded to a wrought portion. The heat treatment process includes placing an article that includes the Inconel 718 cast portion into a heat treatment chamber, evacuating the chamber to a suitable atmosphere, heating the chamber in a manner that minimizes distortion of the cast portion to a temperature in the range of 1950[err]F to 2050[err]F ( 1060 – 1120[err]C), holding the temperature in that range for a period of time sufficient to solution a11 the delta phase precipitates, and then cooling the article to room temperature in a manner that minimizes distortion of the article. After solution heat treatment, the wrought portion of the engine part can be removed and replaced and the engine article can be reprocessed.Fig. 1
机译:恢复力学性能的方法。CAST INCONEL 718,用于维修飞机组件抽象将恢复飞机发动机制品的机械性能的热处理工艺,该飞机发动机制品包括焊接到锻造部分的铸造Inconel 718部分。热处理过程包括将包含Inconel 718铸件的制品放入热处理室中,将其抽空至合适的气氛,以将铸件的变形最小化到1950范围内的温度的方式加热室。 [erF]至2050 [F](1060 – 1120 [C]),将温度保持在该温度范围内足以溶解δ相沉淀的一段时间,然后在室温下将制品冷却至室温使制品变形最小化的方式。在固溶热处理之后,可以去除并更换发动机部件的变形部分,并且可以对发动机产品进行后处理。图。1

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