Acta Metallurgica Sinica (English Letters) ›› 2019, Vol. 32 ›› Issue (3): 381-390.DOI: 10.1007/s40195-018-0779-4
Special Issue: 2018-2019高温合金专辑; 高温合金 2019-2020
• Orginal Article • Previous Articles Next Articles
Liu Liu1,2, Jie Meng2(
), Jin-Lai Liu2, Hai-Feng Zhang1,3, Xu-Dong Sun1, Yi-Zhou Zhou2
Received:2018-03-27
Revised:2018-05-28
Online:2019-03-10
Published:2019-02-22
Liu Liu, Jie Meng, Jin-Lai Liu, Hai-Feng Zhang, Xu-Dong Sun, Yi-Zhou Zhou. Effects of Crystal Orientations on the Low-Cycle Fatigue of a Single-Crystal Nickel-Based Superalloy at 980 °C[J]. Acta Metallurgica Sinica (English Letters), 2019, 32(3): 381-390.
| Elements | C | Cr | Mo | Co | W | Ta | Al | Hf | Re | Ni |
|---|---|---|---|---|---|---|---|---|---|---|
| Composition | 0.07 | 7 | 1.5 | 7.8 | 5 | 6.6 | 6 | 0.15 | 3.0 | Bal. |
Table 1 Nominal composition of the alloy (wt%)
| Elements | C | Cr | Mo | Co | W | Ta | Al | Hf | Re | Ni |
|---|---|---|---|---|---|---|---|---|---|---|
| Composition | 0.07 | 7 | 1.5 | 7.8 | 5 | 6.6 | 6 | 0.15 | 3.0 | Bal. |
Fig. 1 Relationship between the fatigue life and the strain range of experimental alloy at 980 °C: a total strain range versus fatigue life of various oriented alloy, b-d total, elastic and plastic strain ranges versus the number of cycles to failure of the alloy with the [001], [011] and [111] orientations, respectively
Fig. 2 Relationship between the fatigue life and the strain range of the experimental [001], [011] and [111] alloy at 980 °C: a normalized elastic strain range versus the number of cycles, b inelastic strain range versus the number of cycles
Fig. 3 SEM images of fatigue fracture of the [001] specimens after LCF at 980 °C: a-d ?εt/2 = 0.8%, e-h ?εt/2 = 0.45%: a, e macroscopical fracture morphology, b, f high magnification of the yellow boxes in a and e indicating the crack initiation site, c, g surface oxidation cracks, d, h high magnification of the blue dashed boxes in a and e showing striations in the area of crack propagation
Fig. 5 SEM images of fatigue fracture of the [011] specimens after LCF at 980 °C: a-d ?εt/2 = 0.8%, e-h ?εt/2 = 0.25%: a, e macroscopical fracture morphology, b, f, g surface slip morphologies, c the microporosity crack, d high magnification of the blue dashed box in a showing striations and secondary cracks, h surface oxidation crack
Fig. 7 SEM images of fatigue fracture of the [111] specimens after LCF at 980 °C: a-c ?εt/2 = 1.0%, d-f ?εt/2 = 0.2%: a, d macroscopical fracture morphology, b, e crack initiation site, c surface oxidation crack, f slip bands
Fig. 9 Morphologies of secondary cracks on the longitudinal sections of the [001] specimens after LCF at 980 °C: a forked and kinked cracks, b crystallographic secondary crack, c slip bands and partial crack closure of the crack tip (high magnification of the yellow dashed box in b), d slip bands of the crack tip (high magnification of the green dashed box in b)
Fig. 10 Morphologies of secondary cracks on the longitudinal sections of the [011] specimens after LCF at 980 °C: a secondary crack deflection at interdendritic carbides and eutectics, b the secondary crack accompanied by γ and γ′ phases distortion and slip bands, c different directions of slip bands (high magnification of the yellow dashed box in b)
Fig. 11 Morphologies of secondary cracks on the longitudinal sections of the [111] specimens after LCF at 980 °C: a secondary crack generated at the junction of different slip planes, b crack propagation path altered by carbides (high magnification of the blue dashed box in a), c crack-penetrating carbides (high magnification of the purple box in a)
| Orientations | σ0.2σ0.2 (MPa) | σbσb (MPa) | Elongation (%) | Reduction in area (%) | Elastic modulus (GPa) |
|---|---|---|---|---|---|
| [ | 792 | 850 | 23.5 | 40 | 97 |
| [ | 575 | 620 | 29 | 46 | 175 |
| [ | 575 | 625 | 40 | 43 | 234 |
Table 2 Tensile properties of experimental alloy with different orientations at 980 °C
| Orientations | σ0.2σ0.2 (MPa) | σbσb (MPa) | Elongation (%) | Reduction in area (%) | Elastic modulus (GPa) |
|---|---|---|---|---|---|
| [ | 792 | 850 | 23.5 | 40 | 97 |
| [ | 575 | 620 | 29 | 46 | 175 |
| [ | 575 | 625 | 40 | 43 | 234 |
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