On liquid film migration in aluminium–copper alloys

1998 ◽  
Vol 46 (2) ◽  
pp. 511-524 ◽  
Author(s):  
S.W. Barker ◽  
G.R. Purdy
1997 ◽  
Vol 76 (4) ◽  
pp. 729-741 ◽  
Author(s):  
P. Skeldon ◽  
G. E. Thompson ◽  
G. C. Wood ◽  
X. Zhou ◽  
H. Habazaki ◽  
...  

2006 ◽  
Vol 519-521 ◽  
pp. 1151-1156 ◽  
Author(s):  
A. Wittebrood ◽  
S. Desikan ◽  
R. Boom ◽  
Laurens Katgerman

From literature and own observations it is known that the clad and core alloys that make up aluminium brazing sheet can show severe interaction during the brazing cycle. This interaction leads to a complete re-distribution of elements, changing essential properties like strength and corrosion resistance. This interaction has been reported many times but up to present time no clear explanation is given why this interaction is actually occurring. There are a number of publications addressing the circumstances under which the interaction is more severe. Chemistry and low levels of strain applied before brazing have a significant influence on the severity of the interaction. As a yet possible mechanism behind the interaction Liquid Film Migration is mentioned. The observations done so far are in line with this described mechanism but no ultimate proof has been given so far. The question why the interaction takes place cannot be answered yet, clearly a change of free energy of the system is involved but the mechanism or mechanisms behind the change is unclear.


Author(s):  
David Viano ◽  
David StJohn ◽  
John Grandfield ◽  
Carlos Cáceres

1982 ◽  
Vol 15 (1) ◽  
pp. 13-25 ◽  
Author(s):  
A. Datta ◽  
R. A. Pethrick ◽  
S. Affrossman

1956 ◽  
Vol 9 (8) ◽  
pp. 680-680 ◽  
Author(s):  
J. M. Silcock ◽  
T. J. Heal

1962 ◽  
Vol 13 (3) ◽  
pp. 271-274 ◽  
Author(s):  
K. W. Gunn ◽  
A. R. Woodward

SummaryThe fatigue properties of unmachined extrusions of high-strength aluminium-copper alloys are known to be lower than those of conventional fully-machined test pieces. Work described in this note has shown that the removal of a layer of metal 0·025 in. thick from the surface of B.S. L65-type extrusions results in an increase in fatigue properties to values approaching those obtained from the conventional laboratory test pieces. Because the removal of material from the surface is not always a practical proposition, other methods of improving strength have been examined and the effect of surface compressive stresses has been shown to be beneficial. Sufficient compressive stress can be induced by surface-rolling to increase the fatigue properties to those of conventional specimens, but this method can only be easily applied to round sections and it is suggested that shot-peening or vapour-blasting could be used for more complicated sections.


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