TY - JOUR
T1 - Numerical simulation on the creep damage evolution of nickel-based single crystal specimens with slant-angled film cooling holes
AU - Liang, Jianwei
AU - Wen, Zhixun
AU - Yue, Zhufeng
N1 - Publisher Copyright:
Copyright © 2015, Northwest Institute for Nonferrous Metal Research. Published by Elsevier BV. All rights reserved.
PY - 2015/11/1
Y1 - 2015/11/1
N2 - Numerical calculations have been performed to study the creep damage evolution of nickel-based single crystal specimens with slant-angled film cooling holes. The emphasis is the effect of different slant angles on creep properties. The slant angles are 0°, 15°, 30° and 45°. The results show that the distributions of the resolved shear stress around film holes are different under different slant angles. The directions of crack propagation are θ=±54° when α=0°, 15°, 30°; however when α=45° the crack propagation directions are along θ=±46°. The specimen with α=30° has the longest failure life. In the higher stress region near the cooling hole, the phenomenon of stress relaxation will appear, such as resolved shear stress, Mises equivalent stress and stress σ11. And with the time increasing, they reach stable values. Different specimens have different damage distributions. The maximum damage points appear at locations 0°, 0°, 13° and 26° from horizontal direction when the slant angles are 0°, 15°, 30° and 45°, respectively. And thickness has influence on the distribution of resolved shear stress along the holes.
AB - Numerical calculations have been performed to study the creep damage evolution of nickel-based single crystal specimens with slant-angled film cooling holes. The emphasis is the effect of different slant angles on creep properties. The slant angles are 0°, 15°, 30° and 45°. The results show that the distributions of the resolved shear stress around film holes are different under different slant angles. The directions of crack propagation are θ=±54° when α=0°, 15°, 30°; however when α=45° the crack propagation directions are along θ=±46°. The specimen with α=30° has the longest failure life. In the higher stress region near the cooling hole, the phenomenon of stress relaxation will appear, such as resolved shear stress, Mises equivalent stress and stress σ11. And with the time increasing, they reach stable values. Different specimens have different damage distributions. The maximum damage points appear at locations 0°, 0°, 13° and 26° from horizontal direction when the slant angles are 0°, 15°, 30° and 45°, respectively. And thickness has influence on the distribution of resolved shear stress along the holes.
KW - Cooling hole
KW - Creep damage
KW - Single crystal superalloy
KW - Slant angle
UR - http://www.scopus.com/inward/record.url?scp=84951801763&partnerID=8YFLogxK
M3 - 文章
AN - SCOPUS:84951801763
SN - 1002-185X
VL - 44
SP - 2656
EP - 2660
JO - Xiyou Jinshu Cailiao Yu Gongcheng/Rare Metal Materials and Engineering
JF - Xiyou Jinshu Cailiao Yu Gongcheng/Rare Metal Materials and Engineering
IS - 11
ER -