TY - JOUR
T1 - Investigation on the Size Effect in Large-Scale Beta-Processed Ti-17 Disks Based on Quantitative Metallography
AU - Zhang, Saifei
AU - Zeng, Weidong
AU - Gao, Xiongxiong
AU - Zhao, Xingdong
AU - Li, Siqing
N1 - Publisher Copyright:
© 2017, ASM International.
PY - 2017/10/1
Y1 - 2017/10/1
N2 - The present study investigates the mechanical properties of large-scale beta-processed Ti-17 forgings because of the increasing interest in beta thermal-mechanical processing method for fabricating compressor disks or blisks in aero-engines due to its advantage in damage tolerance performance. Three Ti-17 disks with different weights of 57, 250 and 400 kg were prepared by beta processing techniques firstly for comparative study. The results reveal a significant ‘size effect’ in beta-processed Ti-17 disks, i.e., dependences of high cycle fatigue, tensile properties and fracture toughness of beta-processed Ti-17 disks on disk size (or weight). With increasing disk weight from 57 to 400 kg, the fatigue limit (fatigue strength at 107 cycles, R = −1) was reduced from 583 to 495 MPa, tensile yield strength dropped from 1073 to 1030 MPa, while fracture toughness (KIC) rose from 70.9 to 95.5 MPa⋅m1/2. Quantitative metallography analysis shows that the ‘size effect’ of mechanical properties can be attributed to evident differences between microstructures of the three disk forgings. With increasing disk size, nearly all microstructural components in the basket-weave microstructure, including prior β grain, α layers at β grain boundaries (GB-α) and α lamellas at the interior of the grains, get coarsened to different degrees. Further, the microstructural difference between the beta-processed disks is proved to be the consequence of longer pre-forging soaking time and lower post-forging cooling rate for large disks than small ones. Finally, suggestions are made from the perspective of microstructural control on how to improve mechanical properties of large-scale beta-processed Ti-17 forgings.
AB - The present study investigates the mechanical properties of large-scale beta-processed Ti-17 forgings because of the increasing interest in beta thermal-mechanical processing method for fabricating compressor disks or blisks in aero-engines due to its advantage in damage tolerance performance. Three Ti-17 disks with different weights of 57, 250 and 400 kg were prepared by beta processing techniques firstly for comparative study. The results reveal a significant ‘size effect’ in beta-processed Ti-17 disks, i.e., dependences of high cycle fatigue, tensile properties and fracture toughness of beta-processed Ti-17 disks on disk size (or weight). With increasing disk weight from 57 to 400 kg, the fatigue limit (fatigue strength at 107 cycles, R = −1) was reduced from 583 to 495 MPa, tensile yield strength dropped from 1073 to 1030 MPa, while fracture toughness (KIC) rose from 70.9 to 95.5 MPa⋅m1/2. Quantitative metallography analysis shows that the ‘size effect’ of mechanical properties can be attributed to evident differences between microstructures of the three disk forgings. With increasing disk size, nearly all microstructural components in the basket-weave microstructure, including prior β grain, α layers at β grain boundaries (GB-α) and α lamellas at the interior of the grains, get coarsened to different degrees. Further, the microstructural difference between the beta-processed disks is proved to be the consequence of longer pre-forging soaking time and lower post-forging cooling rate for large disks than small ones. Finally, suggestions are made from the perspective of microstructural control on how to improve mechanical properties of large-scale beta-processed Ti-17 forgings.
KW - beta processing
KW - high cycle fatigue
KW - size effect
KW - Ti-17
UR - http://www.scopus.com/inward/record.url?scp=85027142994&partnerID=8YFLogxK
U2 - 10.1007/s11665-017-2812-6
DO - 10.1007/s11665-017-2812-6
M3 - 文章
AN - SCOPUS:85027142994
SN - 1059-9495
VL - 26
SP - 5016
EP - 5026
JO - Journal of Materials Engineering and Performance
JF - Journal of Materials Engineering and Performance
IS - 10
ER -