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Oxidation Assisted Crack Growth of Ni-based Superalloys

机译:氧化辅助镍基高温合金的裂纹扩展

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摘要

Ni-based superalloys are used in some of the most demanding applications, such as gas turbines for military and commercial aircraft, and industrial power plants. At elevated temperature, these materials can suffer damage from surface oxidation, creep deformation, oxidation induced grain boundary embrittlement, and microstructural evolution. These four damage processes can operate in a synergistic fashion and cause catastrophic failure of Ni-based alloys. The interaction of oxidation and creep deformation is not fully understood. This paper reviews the oxidation-assisted damage mechanisms that operate in the presence of creep deformation in the crack tip region. The emphasis will be on quantitative descriptions of the kinetics of these various time-dependent mechanisms. The paper will attempt to link the various mechanisms and their kinetics with time-dependent crack tip stress fields and model time-dependent crack growth due to dwell time in these materials. Directions for future research in this area will also be explored.
机译:镍基高温合金用于一些最苛刻的应用中,例如军用和商用飞机的燃气轮机以及工业发电厂。在高温下,这些材料可能会受到表面氧化,蠕变变形,氧化引起的晶界脆化和微观结构演变的损害。这四个破坏过程可以协同作用,并导致镍基合金的灾难性破坏。氧化和蠕变变形的相互作用尚不完全清楚。本文回顾了在裂纹尖端区域中存在蠕变变形的情况下起作用的氧化辅助损伤机理。重点将放在对这些各种时间依赖机制的动力学的定量描述上。本文将尝试将各种机制及其动力学与时间相关的裂纹尖端应力场联系起来,并模拟由于这些材料中的停留时间而导致的时间相关的裂纹扩展。还将探索该领域未来研究的方向。

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