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The method for heat treatment after welding of configurations member welded formed from gamma prime strengthened superalloys

机译:由γ′增强的超级合金形成的构型构件的焊接后的热处理方法

摘要

The invention relates to a method of post-weld heat treatment of a without a filler material electron beam or laser welded high strength component made of a gamma prime (³') strengthened superalloy based on Ni or Co or Fe or combinations thereof. The method consists of the following steps a) providing the welded component, then b) heating the welded component by applying a rapid heating-up rate in the range of about 20 to 40°C/min during the entire temperature range from RT up to a temperature T 1 of at least 1000°C, then c) holding the welded component at T 1 and then heating the component by applying a slow heating-up rate of about 5°C/min to a final temperature T f , then d) holding the welded component at T f for a time t f , wherein isothermal dwell time t f is sufficient for at least partially dissolving the gamma prime phase in the weld and also in the base material surrounding the weld; then e) cooling the component with a cooling rate of about ‰¥ 20°C/min and f) finally optionally applying a precipitation hardening treatment according to the known state of the art
机译:本发明涉及一种无焊缝后热处理的方法,该无焊缝后处理无填充材料的电子束或由基于Ni或Co或Fe或它们的组合的γ′(Ⅲ′)增强超合金制成的激光焊接的高强度部件。该方法包括以下步骤a)提供焊接部件,然后b)在从RT到至少1000°C的整个温度T 1的整个温度范围内,通过以大约20至40°C / min的快速加热速率加热焊接部件,然后c)将焊接的零件保持在T 1处,然后通过以大约5°C / min的缓慢升温速率将零件加热到最终温度T f,然后d)将焊接部件在T f保持时间t f,其中等温停留时间t f足以至少部分地溶解焊缝中以及围绕焊缝的基材中的γ′相;然后e)以约¥20°C / min的冷却速率冷却组件,并f)最后,根据现有技术水平,可选地进行沉淀硬化处理

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