一种高性能航空涡轮盘用铸锻合金的研究进展
谷月峰1(
),崔传勇1,2(),袁勇1,3,钟志宏1,4
),崔传勇1,2(),袁勇1,3,钟志宏1,4
RESEARCH PROGRESS IN A HIGH PERFORMANCE CAST & WROUGHT SUPERALLOY FOR TURBINE DISC APPLICATIONS
Yuefeng GU1(),Chuanyong CUI1,2(),Yong YUAN1,3,Zhihong ZHONG1,4
),Chuanyong CUI1,2(),Yong YUAN1,3,Zhihong ZHONG1,4
图27. TMW-4M3合金中热处理温度对不同强化方式的影响[49]
Fig.27. Contribution of each factor to the strength of TMW-4M3 alloys[49] (DHGB—grain boundary hardening, DHTB—annealing twin boundary hardening, DHg'I —primary γ’ hardening, DHg'II—secondary γ’ hardening, DHg'III—tertiary γ’ hardening, DHsol— solid solution hardening, DHNi—Vickers hardness of pure Ni single crystal (001))
