Heat treatment behavior of can-forged titanium aluminide alloy in (α+γ) region

1998 ◽  
Vol 5 (2) ◽  
pp. 86-89 ◽  
Author(s):  
Yong Liu ◽  
Baiyun Huang ◽  
Yuehui He ◽  
Zhongyong Deng
2017 ◽  
Vol 899 ◽  
pp. 418-423
Author(s):  
Rafael Paiotti Marcondes Guimarães ◽  
Juliano Soyama ◽  
Thomas Ebel ◽  
Márcio C. Fredel ◽  
Florian Pyczak

In powder metallurgical processing the sintering process, as well as heat treatments, can drastically influence microstructure formation. In the case of γ-titanium aluminides, it is critical to achieve certain microstructure parameters, such as colony size, porosity and grain boundary morphology in order to obtain appropriate mechanical properties. In this study, the effect of a heat treatment implemented after sintering with the objective of varying the colony size was investigated. Specimens of Ti-45Al-5Nb-0.2B-0.2C prepared by metal injection moulding and uniaxial pressing of feedstock were used to evaluate the tensile and creep properties. Heat treatments conducted at 1350 and 1400 °C for 3 h led to colony sizes of approximately 100 and 200 μm, respectively. Classically, there is an inverse relationship between grain size and creep resistance, nonetheless, for γ-titanium aluminides, the morphology of the colony boundaries was also found to play a role. The larger colony sizes achieved with the heat treatments did not improve the primary creep resistance, which was explained by the change in the morphology of the colony boundaries as they became larger.


2021 ◽  
Author(s):  
Igor POLOZOV ◽  
Artem KANTYUKOV ◽  
Kirill STARIKOV ◽  
Anna GRACHEVA ◽  
Vera POPOVICH ◽  
...  

1994 ◽  
Vol 364 ◽  
Author(s):  
J. Kameda ◽  
C. R. Gold ◽  
E. S. Lee ◽  
T. E. Bloomer ◽  
M. Yamaguchi

AbstractSmall punch (SP) tests on single grained titanium aluminide (Ti-48 at.%Al) specimens with 12° and 80° lamellar orientations with respect to the tensile stress axis were conducted at 1123 K in air. Brittle cracks readily extended through the thickness in the 80° lamellar structure. In a SP specimen with the 12° lamellar structure load-interrupted at the strain of 0.43%, surface cracks with the depth of 15–25 μm were formed along lamellar boundaries. Local oxidation behavior on partly sputtered surfaces in the load-interrupted 12° lamellar specimen was examined using scanning Auger microprobe (SAM). Oxygen enriched regions were observed near cracks and some lamellar layers. The mechanisms of high temperature oxygen-induced cracking are discussed in terms of the local oxidation near cracks and lamellar boundaries.


2012 ◽  
pp. 278-294
Author(s):  
Mauro Filippini ◽  
Stefano Beretta ◽  
Luca Patriarca ◽  
Giuseppe Pasquero ◽  
Silvia Sabbadini

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