New Ni3Al-based directionally-solidified superalloy IC10

Hangkong Cailiao Xuebao/Journal of Aeronautical Materials

Volumn 26, Issue 3, 2006, Pages 20-24

  Zhao, Xi Hong ^a,b   Huang, Zhao Hui ^a   Tan, Yong Ning ^a   Zhang, Qiang ^a   Yu, Qian ^a   Xu, Hui Bin ^b  

^a BEIJING INSTITUTE OF AERONAUTICAL MATERIALS   (China)

^b BEIHANG UNIVERSITY   (China)

Author keywords

Castability; Fatigue; Oxidation; Stress rupture; Superalloy

Indexed keywords

AIRCRAFT ENGINES; AIRCRAFT MATERIALS; CARBIDES; FATIGUE OF MATERIALS; HEAT TREATMENT; OXIDATION RESISTANCE; X RAY DIFFRACTION ANALYSIS;

CASTABILITY; IC10 SUPERALLOY; STRESS RUPTURE;

SUPERALLOYS;

EID: 33746260186     PISSN: 10055053     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (13)

1. GOULETTE M J. The future costs less-high temperature materials form an aeroenging perspective[A]. Superalloys 1996[C]. Warrendale PA: TMS, 1996: 3.
2. SETH B B. Superalloys-the utility gas turbine perspective[A]. Superalloys 2000[C]. Warrendale PA: TMS, 2000. 3.
3. WALSTON W S, O'HARA K S, ROSS E W, POLLOCK T M, WURPHY W H. RENE'N6: third generation single superalloy[A]. Superalloys 1996[C]. Warrendale PA: TMS, 1996. 27-34.
4. DIDIER ARGENCE, CYRIL VERNAULT, YVES DESVALLEES, et al. MC-NG: A 4th generation single-crystal superalloy for future aeronautical turbine blade and vanes[A]. Superalloys 2000[C]. Warrendale PA: TMS, 2000. 829-837.
5. KOBAYASHI T, SATO M, KOIZUMI Y, et al. Development of a third generation DS superalloy[A]. Superalloys 2000[C]. Warrendale PA: TMS, 2000. 323-328.
6. LI J R, ZHONG Z G, TANG D Z, et al. A low-cost second generation single crystal superalloy DD6[A]. Superalloys 2000[C]. Warrendale PA: TMS, 2000. 777-783.
7. HARRIS K, ERIKSON G L, SCHWER R E. MAR M 247Derivations: CM247LC DS alloy CMSX Single crystal alloys properties and performance[A]. Superalloys 1984[C]. TMS, 1984. 221-230.