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Gamma Prime Precipitate Evolution During Hot Forging of a γ-γ' Ni-Based Superalloy at Subsolvus Temperatures

机译:γ-γ'Hi基超合金的热锻造γ丸沉淀出的进化温度

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Nickel superalloys are used to manufacture high temperature rotating engine parts such as high pressure discs in gas turbine engines. Alloy 720Li (720Li) is a precipitation-hardened Ni-based superalloy commonly produced by cast and wrought processes. Conventional ingot-to-billet conversion is an expensive and very complex process, requiring multiple open die forging operations and reheating steps in order to achieve a homogeneous microstructure. The present work studies the microstructural evolution of 720Li billet material with the presence of large unrecrystallized structures. The interaction of γ' precipitates with recrystallization during hot forging at subsolvus temperatures was investigated. Double truncated cones were forged at subsolvus temperatures following two forging approaches: single blow and double blow with an intermediate heat treatment. Combined EBSD-EDX analysis was employed to characterize the microstructural evolution of 720Li during hot forging operations. Primary γ' precipitates promote hetero-epitaxial recrystallization during slow cooling, whereas secondary precipitates, formed during slow cooling are not dissolved during reheating, prior to the forging operations. The presence of undissolved secondary γ' promotes strain accumulation and the occurrence of continuous dynamic recrystallization (CDRX). Intermediate heat treatment plays an instrumental role on the recrystallization behaviour for the alloy 720Li. Dissolution of the secondary γ' precipitates results in a strong preconditioning of the 720Li microstructure prior to the second blow of deformation, promoting the formation of fully recrystallized structures and removing the undesired large unrecrystallized regions. The coalescence of intragranular γ' precipitates into clusters of coalesced γ' precipitates represents a clear transition from the apparent unrecrystallized regions to the fully recrystallized structures.
机译:镍高温合金用于制造高温旋转发动机部件,例如燃气轮机发动机的高压盘。合金720LI(720LI)是一种常见的沉淀硬化的基于高超合金,通常由铸造和锻造方法产生。常规的铸锭 - 坯料转换是一种昂贵且非常复杂的过程,需要多个开放式锻造操作和再加热步骤以实现均匀的微观结构。本作者研究了720Li坯料材料的微观结构演化与大型未结晶结构的存在。研究了γ'沉淀析出在子振作温度下再结晶的沉淀物。在两种锻造方法后,双截头锥体伪造出来,单次锻造方法:单次打击和双重打击中间热处理。结合EBSD-EDX分析用于在热锻操作期间表征720LI的微观结构演进。初级γ'沉淀物在缓慢冷却过程中促进杂外延重结晶,而在锻造操作之前,在再加热期间,在缓慢的缓慢形成期间形成的次级沉淀物。未溶解的次级γ'的存在促进了应变积累和连续动态再结晶的发生(CDRX)。中间热处理在合金720li的重结晶行为上起作用的作用。次级γ'沉淀物的溶解导致在第二次变形中的720LI微观结构的强预处理,促进完全重结晶结构的形成并除去不需要的大未结晶区域。腔内γ'的聚结沉淀成聚结γ'沉淀物的簇表示从表观未结晶的区域到完全重结晶结构的透明过渡。

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