|国家预印本平台
首页|孔径对第三代镍基单晶高温合金DD33板式试样室温拉伸性能的影响

孔径对第三代镍基单晶高温合金DD33板式试样室温拉伸性能的影响

Effect of Hole Diameter on Tensile Behavior of a Ni-base Single Crystal Superalloy DD33

中文摘要英文摘要

本文研究了孔径(F=0.5、0.7及0.9mm)对第三代镍基单晶高温合金DD33板式试样室温拉伸性能的影响。采用ARAMIS-光学动态应变测量系统原位观测了拉伸过程中不同孔径孔周围的应变分布,并利用扫描电镜观察了拉伸试样的断口形貌。结果表明:随着孔径的增大,试样的屈服强度和抗拉强度均降低。拉伸过程中孔周围产生应变集中,而且只在孔边很小的范围。弹性变形阶段,孔边应变增长缓慢;一旦发生塑性变形,应变快速增长。孔径越大,孔周围的应变集中越严重,应变梯度越大。上述研究结果对理解含冷却孔单晶叶片的变形行为,优化叶片结构,从而提高叶片寿命具有重要意义。

Plate tensile specimens were machined from a Ni- base single crystal (SC) superalloy DD33, holes with various diameters were electrochemically machined (ECM) in the middle of the specimens. The strain fields around the holes during room temperature tensile tests were in-situ observed by an ARAMIS - optical deformation analysis system based on the digital image correlation (DIC) technique and the fracture surface was observed by scanning electron microscope (SEM). It was demonstrated that the yield strength and ultimate tensile strength decreased with the increase of hole diameter from 0.5 mm to 0.9 mm. Strain concentrated in the vicinity of the hole. The maximum strain increased slightly during elastic deformation. However, once plastic deformation began, it increased rapidly above its elastic value. In addition, the maximum strain and strain gradients adjacent to the holes increased with the increase of the hole diameter from 0.5 mm to 0.9 mm. This work is critical for understanding the crack initiation around the cooling holes with different diameters in the SC blade.

王莉、张功、楼琅洪、刘涛、周忠娇

材料科学航空航天技术

金属材料材料的组织结构缺陷与性能室温拉伸RAMIS系统镍基单晶高温合金孔径应变

王莉,张功,楼琅洪,刘涛,周忠娇.孔径对第三代镍基单晶高温合金DD33板式试样室温拉伸性能的影响[EB/OL].(2023-03-31)[2025-08-02].https://chinaxiv.org/abs/202303.10763.点此复制

评论