High temperature compressive flow behavior of a Mo–Si–B solid solution alloy

2006 ◽  
Vol 54 (1) ◽  
pp. 13-17 ◽  
Author(s):  
P. Jain ◽  
A.P. Alur ◽  
K.S. Kumar
Alloy Digest ◽  
1970 ◽  
Vol 19 (4) ◽  

Abstract INCONEL Alloy 601 is a nickel-chromium solid-solution alloy with excellent high-temperature properties which make it attractive for many application in aerospace and process industries. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-152. Producer or source: Huntington Alloy Products Division, An INCO Company.


2016 ◽  
Vol 723 ◽  
pp. 21-26
Author(s):  
Tsutomu Ito ◽  
Takashi Mizuguchi

In this study, the superplastic behavior on a fine-grained aluminum solid solution alloy consisting of thermally unstable microstructures was investigated. In order to obtain the fine-grained microstructure, friction stir processing (FSP) was applied to a commercial 5083 aluminum alloy. An equiaxial fine-grained microstructure of 7.8 mm was obtained after FSP, but this microstructure was thermally unstable at high temperatures. Commonly, for fine-grained superplasticity to occur (or to continue grain boundary sliding (GBS)), it is necessary to keep the fine-grained microstructure to less than 10 mm during the high-temperature deformation. However, in this study, a large elongation of over 200% was observed at high temperatures in spite of the occurrence of grain growth. From the microstructural observations, it was determined that the fine-grained microstructure was maintained until the early stage of deformation, but the transgranular deformation was observed at a strain of over 100%. The microstructural feature of the abovementioned transgranular deformation is similar to the deformation microstructure of the solute drag creep occurring in "Class I"-type solid solution alloys. This indicates that the deformation mechanism transition from GBS to the solute drag creep occurred during high-temperature deformation. Here, the possibility of occurrence of the superplastic elongation through deformation mechanism transition is discussed as a model of the thermally unstable aluminum solid solution alloy.


2006 ◽  
Vol 980 ◽  
Author(s):  
Padam Jain ◽  
K. S. Kumar

AbstractMulti phase alloys at the Mo-rich end of the Mo-Si-B system have drawn recent attention because of their high temperature performance capabilities. Previous studies on two- and three-phase alloys have confirmed the central role of the Mo-rich solid solution phase in affecting creep resistance and low-temperature toughness in these multiphase alloys. Thus, it is important to understand the intrinsic mechanical response of the matrix solid solution. In this study, compression and tensile tests were conducted over a nominal strain rate regime spanning 10-4 s-1 to 10-7 s-1 and temperature ranging from 1000°C to 1300°C in vacuum on a Mo-Si-B solid solution alloy (Mo-3Si-1.3B in at.%) that contained a low fraction (~5 %) of the T2 phase. The microstructure of the deformed specimens was examined to elucidate the underlying deformation mechanisms.


Alloy Digest ◽  
1988 ◽  
Vol 37 (4) ◽  

Abstract TANTALOY 60 Metal is a vacuum-melted, solid-solution alloy of tantalum and tungsten. It retains useful strength up to 4500 F. Its corrosion resistance is similar to unalloyed tantalum and it is only slightly more difficult to fabricate. If high-temperature exposure is under conditions other than vacuum or inert atmosphere, coating protection may be required. The alloy is used in highly specialized and sophisticated aerospace system applications and in special chemical process. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ta-9. Producer or source: Fansteel Metallurgical Corporation.


Alloy Digest ◽  
1991 ◽  
Vol 40 (4) ◽  

Abstract AA 5454 is a wrought non-heat-treatable aluminum/magnesium alloy. It is a solid solution alloy of relatively high strength capable of some further strengthening by cold work. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-314. Producer or source: Various aluminum companies.


Alloy Digest ◽  
2003 ◽  
Vol 52 (12) ◽  

Abstract DuraFoil-Clad is a laminate composite form of DuraFoil (see Alloy Digest SS-892, November 2003), a heat-resistant ferritic stainless steel with excellent oxidation resistance for high-temperature applications. The material is a metallurgically bonded Al/Fe-Cr stainless steel/Al metallic composite. The material should be converted to a uniform solid-solution alloy (the single alloy form DuraFoil) by diffusion alloying before service in high-temperature applications. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as deformation. It also includes information on corrosion resistance as well as forming, heat treating, and joining. Filing Code: SS-897. Producer or source: Engineered Materials Solutions Inc.


1996 ◽  
Vol 460 ◽  
Author(s):  
P. H. Kitabjian ◽  
A. Garg ◽  
R. Noebe ◽  
W. D. Nix

ABSTRACTWe have investigated the high-temperature deformation behavior of the solid-solution strengthened alloy Ni-47.5Al-2.5Ti. Single crystals were deformed in compression in the “hard” <001> and “soft” <111> orientations, at temperatures between 900°C and 1200°C. The results show that Ti has a very powerful solute strengthening effect in NiAl. The creep rates for the solid-solution alloy were observed to be three to four orders of magnitude lower than for the stoichiometric material. We discuss our efforts to understand this solid-solution strengthening effect. We have studied high-temperature deformation transients in an effort to determine whether solute drag effects contribute to the creep resistance of this solid solution. In addition, we have examined the solute size effect of Ti as it replaces Al on the Al sub-lattice. We discuss the probable mechanism of creep of this alloy in light of TEM observations of the dislocation structures in creep-deformed crystals.


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