Microstructure and Mechanical Properties Determined in Compressive Tests of Quasi-Rapidly Solidified NiAl-Cr(Mo)-Hf Eutectic Alloy After Hot Isostatic Pressure and High Temperature Treatments

2009 ◽  
Vol 19 (5) ◽  
pp. 732-736 ◽  
Author(s):  
L. Y. Sheng ◽  
L. Nan ◽  
W. Zhang ◽  
J. T. Guo ◽  
H. Q. Ye
Keyword(s):  
Mechanical Properties ◽  
High Temperature ◽  
Eutectic Alloy ◽  
Microstructure And Mechanical Properties ◽  
Rapidly Solidified ◽  
Compressive Tests

scholarly journals Microstructure and mechanical properties of a novel rapidly solidified, high-temperature Al-alloy

2016 ◽  
Vol 112 ◽  
pp. 142-148 ◽  
Author(s):  
N.R. Overman ◽  
S.N. Mathaudhu ◽  
J.P. Choi ◽  
T.J. Roosendaal ◽  
S. Pitman
Keyword(s):  
Mechanical Properties ◽  
High Temperature ◽  
Al Alloy ◽  
Microstructure And Mechanical Properties ◽  
Rapidly Solidified

scholarly journals Mo Addition to the A354 (Al–Si–Cu–Mg) Casting Alloy: Effects on Microstructure and Mechanical Properties at Room and High Temperature

Metals ◽  
2018 ◽  
Vol 8 (6) ◽  
pp. 393 ◽  
Author(s):  
Alessandro Morri ◽  
Lorella Ceschini ◽  
Simone Messieri ◽  
Emanuela Cerri ◽  
Stefania Toschi
Keyword(s):  
Mechanical Properties ◽  
High Temperature ◽  
Casting Alloy ◽  
Microstructure And Mechanical Properties

Effect of Hot Processing on Mircrostructure and Properties of Flat Billets of TA15 Titanium Alloy

2021 ◽  
Vol 1016 ◽  
pp. 906-910
Author(s):  
Xin Hua Min ◽  
Cheng Jin
Keyword(s):  
Mechanical Properties ◽  
Heat Treatment ◽  
Titanium Alloy ◽  
High Temperature ◽  
Room Temperature ◽  
High Strength ◽  
Slow Cooling ◽  
Microstructure And Mechanical Properties ◽  
Ta15 Titanium Alloy ◽  
The Ideal

In this paper,effect of the different forging processes on the microstructure and mechanical properties of the flat flat billets of TA15 titanium alloy was investigated.The flat billiets of 80 mm×150 mm×L sizes of TA15 titanium alloy are produced by four different forging processes.Then the different microstrure and properties of the flat billiets were obtained by heat treatment of 800 °C~850 °C×1 h~4h.The results show that, adopting the first forging temperature at T1 °C、slow cooling and the second forging temperature at T2°C 、quick cooling, the primary αphases content is just 10%, and there are lots of thin aciculate phases on the base. This microstructure has both high strength at room temperature and high temperature, while the properties between the cross and lengthwise directions are just the same. So the hot processing of the first forging temperature at T1 °C、slow cooling and the second forging temperature at T2°C 、quick cooling is choosed as the ideal processing for production of aircraft frame parts.

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