文章摘要
张少华,卢玉章,郑伟,彭建强,谢光,张功,申健.一次枝晶间距对DD26单晶高温合金持久各向异性的影响[J].材料导报,2016,30(14):6-9
一次枝晶间距对DD26单晶高温合金持久各向异性的影响
Effect of Primary Dendrite Arm Spacing on the Anisotropic Stress Rupture Properties in a Nickel-base Single Crystal Superalloy DD26
  
DOI:10.11896/j.issn.1005-023X.2016.14.002
中文关键词: DD26 单晶高温合金 各向异性 一次枝晶间距 持久性能 位错形貌
英文关键词: DD26, single crystal superalloy, anisotropy, primary dendrite arm spacing, stress rupture properties, dislocation morphology
基金项目:国家自然科学基金(51401216);国家重大科学仪器设备开发专项资助项目(2012YQ22023304)
作者单位E-mail
张少华 中国科学院金属研究所, 沈阳 110016 zhangshaohua@imr.ac.cn 
卢玉章 中国科学院金属研究所, 沈阳 110016  
郑伟 中国科学院金属研究所, 沈阳 110016  
彭建强 哈尔滨汽轮机厂有限责任公司, 哈尔滨 150046  
谢光 中国科学院金属研究所, 沈阳 110016  
张功 中国科学院金属研究所, 沈阳 110016  
申健 中国科学院金属研究所, 沈阳 110016  
摘要点击次数: 2584
全文下载次数: 1351
中文摘要:
      研究了取向对高速冷却法(DD26-HRS)和液态金属冷却法(DD26-LMC)制备的DD26单晶高温合金760 ℃/670 MPa条件下持久性能的影响。结果表明,DD26-HRS合金一次枝晶间距明显大于DD26-LMC合金,而且DD26-HRS合金持久各向异性更为严重。位错形貌显示靠近[001]-[012]边界试样变形以基体内多滑移为主。由于DD26-HRS合金γ′相尺寸较大,抑制了层错带剪切γ′相的变形机制,从而使得DD26-HRS合金持久寿命高于LMC合金。然而,靠近[001]-[112]边界试样变形以单方向层错剪切γ′相为主,基体内开动的位错较少,DD26-HRS合金枝晶间粗大的碳化物相周围易于位错的堆积,从而萌生裂纹并沿碳化物界面迅速开裂,造成DD26-HRS合金持久寿命低于DD26-LMC合金。
英文摘要:
      The orientation dependence of stress rupture behavior in a single crystal superalloy DD26 processed by high rate solidification (DD26-HRS) and liquid metal cooling (DD26-LMC) was investigated under the condition of 760 ℃/670 MPa. The results demonstrated that the primary dendrite arm spacing (PDAS) of DD26-HRS alloy was much larger than that of DD26-LMC alloy, and the creep anisotropy of DD26-HRS alloy was more serious than DD26-LMC alloy. The dislocation morphology showed that the deformation was dominated by multiple slipping when the orientation of specimen was near the [001]-[012] boundary in the standard stereographic triangle. Due to the larger size of γ′ particles in DD26-HRS alloy, the deformation mechanism of stacking fault shear was inhibited. Therefore, the stress rupture life of DD26-HRS alloy was longer than DD26-LMC alloy. However, the deformation of specimen, whose orientation was near the [001]-[112] boundary, was predominated by single 1/3〈112〉 dislocations shearing γ′ particles, and little type of dislocations slipping in γ matrix. Around the larger script carbide in DD26-HRS alloy, it was easy to pile up with dislocations and initiate cracks. As a result, the stress rupture life of DD26-HRS alloy is much shorter than DD26-LMC alloy.
查看全文   查看/发表评论  下载PDF阅读器
关闭