Issue 46
W. Song et alii, Frattura ed Integrità Strutturale, 46 (2018) 94-101; DOI: 10.3221/IGF-ESIS.46.10
T HE EXTENDED ANALYTICAL EQUATION BASED ON SIF S
Extension of analytical solutions onsidering the comprehensive effects of joints geometry on the non-dimensional parameters i analytical equations from these results via least square fitting methods. The non-dimensional parameters i k analytical solutions of NSIFs at weld toe in non-load-carrying cruciform joints under pure tension were proposed by Lazzarin et al. [5] and Atzori et al. [23], which are shown as follows: C k , we can deduce the
1.12(2 / ) 0.485( / ) b t t t
0.985(2 / ) b t
k
1.212 0.495 e
e
(12)
1.259
1
1.126(2 / ) 0.769( / ) b t t t
1.959(2 / ) b t
k
0.508 0.797 e
e
(13)
2.723
2
k mentioned above, the equations of i
k for LCWJ considering the penetration effect under
Similar to the expression of i
pure tension and bending loadings can be expressed as the following form:
2
i
i
i
k A B e
( ) h t
( ) h t
p t
(
)
C e
(19)
i
i
i
i
The numerical analysis of LCWJ under different loading conditions demonstrate local geometry imposes negligible effect on the strain energy density, as also reflects in Eqn. 6, which cancel the effect of the attachment plate thickness (L), while incorporates the effects of weld length (h) and penetration length (p). Finally, the i k equations of weld toe and weld root under different loading conditions from the Eqn. 14 becomes: For weld toe:
3.177( ) 4.707( h t
3.691( ) h t
p t
)
toe, tension
1.204 1.284
6.8
Tension:
(15)
k
e
e
1
7.763( ) 22.41( h t
4.892( ) h t
p t
1 toe,bending
)
0.8681 0.6158
2.563
(16)
Bending:
k
e
e
For weld root:
1.414( ) 0.3516( h t
1.414( ) h t
p t
)
, root tension k
0.2553 7.732
9.287
e
e
(17)
Tension:
1
4.556( ) 7.304( h t
, root bending
1.762( ) h t
p t
)
(18)
Bending:
k
e
e
0.056+0.2706
0.6201
1
Based on these extension equations, the NSIF and SED values at weld toe and weld root in LCWJ can be simply estimated without some FE analysis.
E XPERIMENTAL VERIFICATION
I
n this section, the experiments data were used to verify the proposed analytical solutions. High cycle fatigue experiments of load-carrying cruciform welded joints were performed on a 250KN electro-hydraulic servo testing system MTS 809 with a loading-control condition. Fig. 3 illustrates the procedure of specimens processing and fatigue tests. Two panels of 10CrNi3MoV steel were fabricated in Fig. 3(a). Each panel was cut up into LCWJ specimens of 35mm width by wire-electrode method, as shown in Fig. 3(b). This steel yield stress is about 693MPa. The nominal stress range of 100-200 MPa was tested with a stress ratio (R=0.1) and loading frequency between 5 and 15Hz. More test details are described in Ref. [10].
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