Fatigue crack growth behavior of a new single crystal nickel-based superalloy (CMSX-4) at 650 C

Journal Article · Mon Aug 01 00:00:00 EDT 1994 · Journal of Materials Engineering and Performance; (United States)

DOI:https://doi.org/10.1007/BF02645320· OSTI ID:7038256

Sengupta, A; Putatunda, S K ^[1]; Balogh, M ^[2]

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1. Wayne State Univ., Detroit, MI (United States). Dept. of Materials Science and Engineering
2. General Motors Technical Center, Warren, MI (United States)

CMSX-4 is a recently developed rhenium containing single crystal nickel-based superalloy. This alloy has potential applications in many critical high-temperature applications such as turbine blades, rotors, nuclear reactors, etc. The fatigue crack growth rate and the fatigue threshold data of this material is extremely important for accurate life prediction, as well as failure safe design, at elevated temperatures. In this paper, the fatigue crack growth behavior of CMSX-4 has been studied at 650 C. The investigation also examined the influence of [gamma][prime] precipitates (size and distribution) on the near-threshold fatigue crack growth rate and the fatigue threshold. The influence of load ratio on the fatigue crack growth rate and the fatigue threshold was also examined. Detailed fractographic studies were carried out to determine the crack growth mechanism in fatigue in the threshold region. Compact tension specimens were prepared from the single crystal nickel-based superalloy CMSX-4 with [001] orientation as the tensile loading axis direction. These specimens were given three different heat treatments to produce three different [gamma][prime] precipitate sizes and distributions. Fatigue crack growth behavior of these specimens was studied at 650 C in air. The results of the present investigation indicate that the near-threshold fatigue crack growth rate decreases and that the fatigue threshold increases with an increase in the [gamma][prime] precipitate size at 650 C. The fatigue threshold decreased linearly with an increase in load ratio. Fractographs at 650 C show a stage 2 type of crack growth along [l brace]100[r brace] type of crystal planes in the threshold region, and along [l brace]111[r brace] type of crystal planes in the high [Delta]K region.

• OSTI ID: 7038256
• Journal Information: Journal of Materials Engineering and Performance; (United States), Journal Name: Journal of Materials Engineering and Performance; (United States) Vol. 3:4; ISSN 1059-9495; ISSN JMEPEG
• Country of Publication: United States
• Language: English

Related Subjects

36 MATERIALS SCIENCE
360103* -- Metals & Alloys-- Mechanical Properties
ALLOYS
CRACK PROPAGATION
CRYSTALS
DATA
EXPERIMENTAL DATA
FATIGUE
HEAT RESISTANT MATERIALS
HEAT RESISTING ALLOYS
INFORMATION
LIFETIME
MATERIALS
MECHANICAL PROPERTIES
MICROSTRUCTURE
MONOCRYSTALS
NICKEL ALLOYS
NICKEL BASE ALLOYS
NUMERICAL DATA
REACTOR MATERIALS
RHENIUM ALLOYS
SERVICE LIFE
STRESS INTENSITY FACTORS
TEMPERATURE RANGE
TEMPERATURE RANGE 0400-1000 K
USES