Effect of temperature and load during hot impression creep of Cu-Zn-Al alloy

Author(s):  
A. Sai Deepak Kumar ◽  
Mohammad Fayaz Anwar ◽  
E. Vara Prasad ◽  
P. Bharath Sreevatsava ◽  
C. Vanitha
2008 ◽  
Vol 58 (8) ◽  
pp. 643-646 ◽  
Author(s):  
Tsutomu Tanaka ◽  
Yorinobu Takigawa ◽  
Kenji Higashi

2007 ◽  
Vol 534-536 ◽  
pp. 597-600 ◽  
Author(s):  
C. Lucien Falticeanu ◽  
I.T.H. Chang ◽  
J.S. Kim ◽  
R. Cook

The increasing demand for automotive industries to reduce the weight of the vehicles has led to a growing usage of Al alloy powder metallurgy (P/M) parts such as camshaft bearing caps, shock absorber pistons and brake calipers [1,2]. In order to control the sintered microstructure and mechanical properties of the aluminium alloy powder metallurgical (P/M) parts, it is essential to establish a fundamental understanding of the microstructural development during the sintering process. Current research at Birmingham University is focussed on the investigation of the sintering behaviour of Al-Cu-Mg-Si powder blends using a combination of Scanning Electron Microscopy, Energy Dispersive Microanaylsis (SEM) and Differential Scanning Calorimetry (DSC). This paper presents a detailed study of the effect of temperature and initial starting materials on the evolution of microstructure during the sintering of Al-Cu-Mg-Si blends for PM.


2016 ◽  
Vol 877 ◽  
pp. 251-257
Author(s):  
Wei Jun He ◽  
Chun Hong Li ◽  
Zhi Qiang Li ◽  
Bai Feng Luan ◽  
Qing Liu

Carbon nanotubes reinforced aluminum alloy (CNTs/Al alloy) composite was fabricated by the method of flake powder metallurgy. With Gleeble-3500 system, hot compression tests at different temperatures and strain rates were conducted to investigate the effect of temperature and strain rate on the deformation behaviors of the CNTs/Al alloy composite. Experimental results show that the composite’s ductility is worse at higher deformation temperature within range of 300 oC-450 oC. Additionally, the composite’s ductility is better at higher strain rate, which is against general knowledge. The microstructure before and after deformation were characterized by SEM and TEM. It demonstrates that the grain size of the composite is always in the nanoscale. The abnormal effects of temperature and strain rate on the ductility may be explained by the evolution of work hardening capability at different deformation conditions.


1980 ◽  
Vol 102 (4) ◽  
pp. 350-355 ◽  
Author(s):  
V. M. Radhakrishnan ◽  
A. J. McEvily

Investigations have been carried out to study the effect of temperature on crack growth under creep condition in 6061 Al alloy. A parameter approach, connecting the three variables - crack growth rate a˙, the load point deflection rate Δ˙ and the applied load P - given in the form a˙∝Δ/˙PPoα1/θ where α, θ, and Po are constants, has been found to give good correlation with the experimental data. The exponents, α and θ, are dependent on temperature. The activation energy for the crack growth process has been found to be around 24 Kcal/mole.


Metals ◽  
2018 ◽  
Vol 8 (10) ◽  
pp. 819 ◽  
Author(s):  
Ahmed Mosleh ◽  
Anastasia Mikhaylovskaya ◽  
Anton Kotov ◽  
Waheed AbuShanab ◽  
Essam Moustafa ◽  
...  

This paper presents the effect of temperature and strain rate on the superplastic deformation behavior of Ti-3%Mo-1%V-4%Al, Ti-4%V-6%Al, and Ti-1.8%Mn-2.5%Al alloys, which have different initial microstructures. The microstructure, before and after superplastic deformation in the deformation regimes that provided the maximum elongation, was analyzed. The deformation regimes, corresponding to the minimum strain hardening/softening effect, provided a higher elongation to failure due to their low tendency toward dynamic grain growth. As the values of stress became steady (σs), the elongation to failure and strain-hardening coefficient were analyzed under various temperature–strain rate deformation regimes. The analysis of variance of these values was performed to determine the most influential control parameter. The results showed that the strain rate was a more significant parameter than the temperature, with respect to the σs, for the investigated alloys. The most influential parameter, with both the elongation to failure and strain-hardening coefficient, was the temperature of the Ti-3%Mo-1%V-4%Al and Ti-1.8%Mn-2.5%Al alloys and the strain rate of the Ti-4%V-6%Al alloy.


1982 ◽  
Vol 52 (3) ◽  
pp. 202-205 ◽  
Author(s):  
M. I. Guseva ◽  
Yu. V. Martynenko ◽  
O. I. Chelnokov ◽  
I. P. Chernov ◽  
V. N. Shadrin ◽  
...  

2020 ◽  
Vol 780 ◽  
pp. 139175
Author(s):  
Phalgun Nelaturu ◽  
Saumyadeep Jana ◽  
Rajiv S. Mishra ◽  
Glenn Grant ◽  
Blair E. Carlson

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