Mechanical properties of cast aluminium alloy 6061-albite particulate composites

Author(s):  
K H W Seah ◽  
S C Sharma ◽  
A Ramesh
Author(s):  
R Pramod ◽  
N Siva Shanmugam ◽  
CK Krishnadasan

Aluminium alloy 6061-T6 is utilized in aerospace industry for developing pressure vessel liner. Cold metal transfer is a promising welding process used in fabricating aluminium structures. The present work is focussed to achieve an optimum welding parameter for joining a 3.5-mm thick pressure vessel and to examine the mechanical properties and metallurgical nature of the weldment. The welded joint was evaluated as defect free using radiography test. The joint efficiency (66.61%) and measured microhardness of weldment (59.78 HV) exhibited promising results. The effect of grain coarsening in the heat affected zone (HAZ) and weld zone is attributed to the thermal gradients during welding. Dissipation of small amounts of strengthening elements Si and Mg during welding leads to reduction in mechanical properties. X-ray diffraction peaks revealed the presence of intermetallic Al–Si and Fe–Si in the weld zone. Fractography examination confirms the ductile type of failure in the fractured surface of the tensile samples.


1993 ◽  
Vol 9 (10) ◽  
pp. 853-862 ◽  
Author(s):  
J. W. Luster ◽  
M. Thumann ◽  
R. Baumann

2014 ◽  
Vol 906 ◽  
pp. 249-253
Author(s):  
Arnav Gupta ◽  
Aditya Eswar ◽  
G. Dinesh Babu ◽  
M. Nageswara Rao

Cast aluminium alloys are being employed increasingly in the automotive sector due to their light weight and excellent castability. This paper focuses on the strain hardening behaviour of Hipped and non-Hipped components of cast aluminium alloy 354 subjected to two-step ageing, as opposed to the routinely carried out single-step ageing. First step ageing (at 100°C) was carried out for 2 h and 5 h; ageing time at second step (at 170°C) was 1, 2 and 5 h. Mechanical properties and strain hardening behaviour were evaluated for different variants of two-step ageing treatment. Analysis of the results shows that the Hipped components have higher hardening capacity and generally higher strain hardening rate compared to the non-Hipped ones. Some of the two-step ageing treatments give mechanical properties comparable to the conventional T61 treatment, but with significantly higher strain hardening rate.


1988 ◽  
Vol 52 (6) ◽  
pp. 609-615 ◽  
Author(s):  
Than Trong Long ◽  
Takanobu Nishimura ◽  
Tatsuyoshi Aisaka ◽  
Michihiro Ose ◽  
Mikio Morita

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