Issue 61
V. Shlyannikov et alii, Frattura ed Integrità Strutturale, 61 (2022) 46-58; DOI: 10.3221/IGF-ESIS.61.03
C
Cr
Mo
Al
Ti
Nb
Ni
0.03-0.07
13.0-16.0
2.8-3.2
1.45-1.8
2.35-2.75
1.9-2.2
basis
Table 1: Chemical composition for XH73M alloy.
B [1/(MPa*n ⋅ hr)] - 2.5*10 -11
T [ ˚ C]
σ u [MPa] 1298.25 1229.53 1205.93 1079.30
σ 0 [MPa]
E [GPa]
δ [%] 34.94 32.31 27.73 10.67
ψ [%] 54.19 50.88 30.12 18.35 17.90
n
23
904.04 830.50 836.42 866.05 705.46
215.77 192.87 206.18 192.76 161.39
-
400 550 650 750
2.50 3.53 4.80 8.85
4.0*10 -12 2.1*10 -16 4.0*10 -26
839.85
8.27
Table 2: Main mechanical static properties for XH73M alloy.
In the present study, the interpretation of experimental results on the CGR in C(T) specimens of nickel-based alloy at high temperatures are presented in terms of the fracture mechanics characteristics for the conditions of elasticity and creep. Traditionally, the experimental data are presented through the creep C-integral and the elastic SIF which for C(T) specimens is given by the ASTM standard [14] as
1 1 K P f a w b w
(3)
2
3
4
a w
2
a w
a w
a w
a w
0.866 4.64
f a w
(4)
13.32
14.72
5.6
1
a w
1.5
1
where a is the crack length, w is the length of the working area of the specimen, b is the specimen thickness, and P is the applied load. To interpret the data on crack propagation at high temperatures creep-fatigue interaction loading conditions, the method for determining the C* -integral can be used, which is based on the experimentally measured load-line deflection V FL in the C(T) specimen. The compliance method [14] has been applied in order to determine the force-line displacement rate ∂ V FL / ∂ t . The relationship between compliance and normalized crack size for experimentally measurements made at the load-line for a specimen with a crack subject to constant force, P , are given by the following equation:
FL
FL C V P
(5)
2
2
3
4
5
a w
a w
a w
a w
a w
a w
1 1
12.163 12.219
20.065
0.9925
20.609
9.9314
a w
Eb
1
The expression for extending the C* -integral concept to small-scale creep conditions in the form of the C(t) -parameter is described by the equation [14]:
f
FL P V t
(6)
C t
1 f
bw
df
1
f
f
f
f
'
(7)
2
3
4
( d a w
)
2
3
4
a w
a w
a w
a w
1
0.866 4.64
f a w
13.32
14.72
5.6
(8)
2
1.5
a w
1
50
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