Prediction of type IV cracking behaviour of 2.25Cr-1Mo steel weld joint based on finite element analysis

2010 ◽  
Vol 63 (2-3) ◽  
pp. 461-466 ◽  
Author(s):  
Sunil Goyal ◽  
K. Laha ◽  
K. S. Chandravathi ◽  
K. Bhanu Sankara Rao
2018 ◽  
Vol 36 (3) ◽  
pp. 265-274
Author(s):  
T. Sakthivel ◽  
K. S. Chandravathi ◽  
K. Laha ◽  
M. D. Mathew

Author(s):  
Warren Brown

In previous papers, practical limits on the maximum applied load for standard ASME B16.5 and B16.47 carbon steel, weld neck pipe flanges were examined. A new code equation for the tangential (hoop) stress at the small end of the hub for a weld neck flange was developed to facilitate calculation of the limits using elastic analysis. The results were verified against elastic-plastic Finite Element Analysis (FEA). In this paper, the work is extended to include other flange configurations, including loose ring flanges, slip-on flanges and flat plate flanges. This paper is a continuation of the papers presented during PVP 2006 and PVP 2007 (Brown [1, 2]) and it extends the scope of the proposed methodology for determining flange stress limits in determining the maximum allowable bolt load for any given flange size and configuration.


2014 ◽  
Vol 578-579 ◽  
pp. 1276-1280
Author(s):  
Jian Suo Ma ◽  
Run Shan Bai ◽  
Min Feng Li ◽  
Yuan Qing Wang ◽  
Lei Wang ◽  
...  

The combined connection with welds and bolds mainly refers to Interaction of weld and high-strength bolts. Both bolts and welds show influence on the performance of the combined connection. In practical engineering, because of limited joint size, only welds’ performence can increase bolts number or load. Therefore, it need to explore the influences of weld on joint performance. Moreover, for given determined bolt connection, it is necessary to discuss the influences of weld size, weld length and weld height, on the performance of a certain weld joint.


2014 ◽  
Vol 24 (1) ◽  
pp. 1407-1415 ◽  
Author(s):  
You-Min Huang ◽  
I-Chiang Chou ◽  
Cho-Pei Jiang ◽  
Yi-Syun Wu ◽  
Shyh-Yuan Lee

2007 ◽  
Vol 2007 (0) ◽  
pp. 252-253
Author(s):  
Yutaka Toi ◽  
Masakazu Takagaki ◽  
Satoshi Hirose ◽  
Yukio Takahashi

Author(s):  
Warren Brown

In previous papers, practical limits on the maximum applied load for standard ASME B16.5 and B16.47 carbon steel, weld neck and slip-on pipe flanges were examined. A new code equation for the tangential (hoop) stress at the small end of the hub for a weld neck flange and new flange factors for a slip-on flanges were developed to facilitate calculation of the limits using elastic analysis. The results were verified against elastic-plastic Finite Element Analysis (FEA). In this paper, the work is extended to include other flange materials and verification is once again performed against elastic-plastic FEA. This paper is a continuation of the papers presented during PVP 2006, PVP 2007 and PVP 2008 (Brown [1–3]) and it extends the scope of the proposed methodology for determining flange stress limits in to any given flange material, size and configuration.


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