Correlation Between Microstructure and Properties of New Heat-Resistant Alloy SP2215
LIANG Kai, YAO Zhihao(), XIE Xishan, YAO Kaijun, DONG Jianxin
School of Materials Science and Engineering, University of Science and Technology Beijing, Beijing 100083, China
Cite this article:
LIANG Kai, YAO Zhihao, XIE Xishan, YAO Kaijun, DONG Jianxin. Correlation Between Microstructure and Properties of New Heat-Resistant Alloy SP2215. Acta Metall Sin, 2023, 59(6): 797-811.
With the improvement of the steam parameters of thermal power units, the requirements put forward for the stress rupture strength and structural stability of heat-resistant materials for boiler superheater/reheater pipes become higher. SP2215, as a new heat-resistant alloy, is an excellent candidate for 620-650°C ultra-supercritical boiler superheater/reheater. In this study, the correlation between microstructure evolution and properties of the SP2215 heat-resistant alloy aging at different temperatures and time was studied via a series of creep and impact tests. The results show that the SP2215 alloy has excellent microstructure stability in high-temperature condition. Moreover, various nanoscale precipitations such as Cu-rich, MX, NbCrN, and M23C6 phases occur during aging. In the early period of aging, with the increase in aging temperature and aging time, the precipitations increase rapidly, improving the strength of the material; however, the impact toughness of the SP2215 alloy decreases considerably, with substantial intergranular fracture caused by the continuous precipitation and growth of M23C6 at the boundary, as shown with the quantitative calculation using the JMA model. In the late period of aging, the precipitations gradually stabilize, and the grain size remains in the range of 4.5-5 grade. As a result, the 1 × 105 h stress rupture strength of the SP2215 alloy at 650 and 700oC still remain more than 120 and 70 MPa, respectively. Hence, the alloy can be used as a domestic replacement for foreign HR3C, Super304H, and other similar heat-resistant alloys.
Fig.1 Varieties of grain size of the SP2215 heat-resistant alloy aged at different temperatures and time (Insets show the microstructures of the alloy under different aging conditions, t—aging time)
Fig.2 OM image of SP2215 heat-resistant alloy aged at 650oC for 500 h
Fig.3 TEM images of Cu-rich precipitates in the SP2215 heat-resistant alloy aged at 650oC (a-d) and 700oC (e-h) for 500 h (a, e), 2000 h (b, f), 6000 h (c, g), and 10000 h (d, h)
Fig.4 EDS analyses of Cu-rich precipitates (a) and the matrix (b)
t / h
650oC
700oC
500
5.97
18.95
2000
11.51
38.36
6000
18.40
48.37
10000
20.28
53.73
Table 1 Average sizes of Cu-rich particles at different aging temperatures and time
Fig.5 SEM images of precipitates at and near the boundaries in the SP2215 heat-resistant alloy aged at 650oC (a-c) and 700oC (d-f) for 500 h (a, d), 4000 h (b, e), and 10000 h (c, f) (Insets show the higher magnification SEM images of precipitates at and near the boundaries)
Fig.6 EDS mappings of the precipitates at and near the boundaries in the SP2215 heat-resistant alloy after aging at 650oC for 6000 h
Fig.7 Volume fractions of M23C6 as a function of aging time at different aging temperatures
Fig.8 Fitting curves of lnln[1 / (1 - f)] and lnt of SP2215 heat-resistant alloy at different aging temperatures (f—conversion rate of M23C6 phase)
Fig.9 JMA kinetic curves of M23C6 of the SP2215 alloy aged at 650 and 700oC
Fig.10 SEM images of M23C6 phases precipitated at the twin boundary (a), inside the grain (b, c) and at the grain boundary (d), and the EDS mappings (e) (Arrows point to the M23C6 phase at the specific locations)
Fig.11 TEM images of MX precipitates after aging at 650oC for 500 h (a), and NbCrN precipitates after aging at 650oC (b) and 700oC (c) for 6000 h
Element
Matrix (500 h)
MX
500 h
2000 h
6000 h
10000 h
Nb
0.06
1.40
8.44
4.08
6.10
Cr
11.97
13.11
16.99
18.22
33.15
N
5.95
8.71
24.93
12.44
-
C
33.17
32.02
19.72
22.36
-
Table 2 Varieties of main compositions in MX precipitates of SP2215 alloy during the aging at 650oC
Element
Matrix (500 h)
MX
500 h
2000 h
6000 h
10000 h
Nb
0.06
2.02
6.35
7.41
11.79
Cr
11.97
18.17
18.89
22.62
41.26
N
5.95
10.88
20.50
26.10
12.61
C
33.17
21.23
27.92
18.75
-
Table 3 Varieties of main compositions in MX precipitates of SP2215 alloy during the aging at 700oC
Fig.12 EDS mappings of NbCrN precipitates in the SP2215 heat-resistant alloy after aging at 650oC for 2000 h (a) and 6000 h (b)
Fig.13 TEM image of the ellipsoid NbCrN phase (a) and the selected area electrical diffraction (SAED) pattern (b) of circle in Fig.13a
Fig.14 Linear extrapolation curves of SP2215 heat-resistant alloy at different temperatures
Fig.15 C value calculated by fitting (tr—rupture time, T—temperature)
Fig.16 Larson-Miller curves of SP2215 heat-resistant alloy (P—Larson-Miller parameter, σ—stress)
Fig.17 Variety of tensile strength (Rm) and yield strength (Rp0.2) at high temperature
Fig.18 Hardness curves of the SP2215 heat-resistant alloy after aging at 650 and 700oC
Steel
650oC
700oC
Ref.
SP2215
16.5
12.5
This work
HR3C
4.7
4
[30]
Super304H
17.5
-
[6]
Table 4 Comparison of impact energy of SP2215, HR3C[30], and Super304H[6] heat-resistant alloys after long-term aging at 650 and 700oC for 3000 h
Fig.19 Impact energy curve of the SP2215 heat-resistant alloy after aging at 700oC
Fig.20 Impact macrofractures of the SP2215 heat-resistant alloy aged at 650oC (a, b) and 700oC (c, d) for 500 h (a, c) and 6000 h (b, d) (Arrows point to the sources of cracks)
Fig.21 Impact micro fractures of the SP2215 heat-resistant alloy aged at 650oC (a-c) and 700oC (d-f) for 500 h (a, d), 4000 h (b, e), and 10000 h (c, f)
Fig.22 Effect of M23C6 content of on impact energy (ak—impact energy, V—volume fraction)
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