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Fatigue resistance of the grain size transition zone in a dual microstructure superalloy disk

机译:双组织超合金圆盘中晶粒尺寸过渡区的抗疲劳性

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摘要

Mechanical property requirements vary with location in nickel-based superalloy disks. In order to maximize the associated mechanical properties, heat treatment methods have been developed for producing tailored microstructures. In this study, a specialized heat treatment method was applied to produce varying grain microstructures from the bore to the rim portions of a powder metallurgy processed nickel-based superalloy disk. The bore of the contoured disk consisted of fine grains to maximize strength and fatigue resistance at lower temperatures. The rim microstructure of the disk consisted of coarse grains for maximum resistance to creep and dwell crack growth at high temperatures up to 704 ℃. However, the fatigue resistance of the grain size transition zone was unclear, and needed to be evaluated. This zone was located as a band in the disk web between the bore and rim. Specimens were extracted parallel and transverse to the transition zone, and multiple fatigue tests were performed at 427 and 704 ℃. Mean fatigue lives were lower at 427 ℃ than 704 ℃. Specimen failures often initiated at relatively large grains, which failed on crystallographic facets. Grain size distributions were characterized in the specimens, and related to the grains initiating failures as well as location within the transition zone. Fatigue life decreased with increasing maximum grain size. Correspondingly, mean fatigue resistance of the transition zone was slightly higher than that of the rim, but lower than that of the bore. The scatter in limited tests of replicates was comparable for all transition zone locations examined.
机译:机械性能要求随镍基高温合金盘中位置的不同而变化。为了最大化相关的机械性能,已经开发了用于生产定制的微结构的热处理方法。在这项研究中,采用了一种专门的热处理方法来生产从粉末冶金处理的镍基高温合金圆盘的孔到边缘部分的各种晶粒微观结构。异形盘的孔由细晶粒组成,可在较低温度下最大程度地提高强度和抗疲劳性。圆盘的边缘微观结构由粗大晶粒组成,可以最大程度地抵抗高达704℃的高温下的蠕变和驻留裂纹增长。但是,晶粒尺寸过渡区的抗疲劳性尚不清楚,需要进行评估。该区域作为孔和轮辋之间的圆盘网中的带位于。沿平行于过渡区的方向抽取试样,并在427和704℃下进行多次疲劳测试。在427℃时,平均疲劳寿命低于704℃。样品失效通常始于相对较大的晶粒,而晶粒较大时则失败。在样品中表征了晶粒尺寸的分布,并且与晶粒的初始破坏以及过渡区域内的位置有关。疲劳寿命随着最大晶粒尺寸的增加而降低。相应地,过渡区的平均疲劳强度略高于轮辋,但低于孔的疲劳强度。对于所有检查的过渡区位置,在重复试验的有限测试中的散布可比。

著录项

  • 来源
    《International Journal of Fatigue》 |2011年第3期|p.414-426|共13页
  • 作者单位

    NASA Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135, United States;

    Honeywell Engine Systems, 111 South 34th St., Phoenix, AZ 85034, United States;

    NASA Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135, United States;

    NASA Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135, United States;

    NASA Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135, United States;

    McGraw-Hill Companies, Inc., 3073 Neil Ave., Columbus, OH 43202, United States;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    superalloy; disk; dual microstructure; transition zone; fatigue;

    机译:高温合金盘双重显微组织过渡区疲劳;

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