Determination of Superplastic Material Properties for Parent Material and Friction Stir Welded Joint of Al-Alloy AA6061-T6

Author(s):  
Senthil Kumar Velukkudi Santhanam ◽  
Ganesh Pasupathy ◽  
Padmanabhan Kuppuswamy Anantha

Superplastic forming (SPF) takes the advantage of the metallurgical phenomenon of superplasticity (SP) to form complex and highly intricate bulk and sheet metal parts. SP refers to the extraordinary formability of certain metals and alloys, ceramics, composites (both metallic- and ceramic-based), dispersion strengthened materials, nanostructured materials and bulk metallic glasses, which allows them to suffer elongations of several hundred percent under the action of tensile forces. The superplastic forming characteristics of materials like aluminium, titanium and magnesium alloys have been clearly identified in order to produce complicated near-net shapes. These materials are used in the aeronautical manufacturing industry and automotive manufacturing industries due to the significant weight (by ∼ 30%) and cost (by ∼ 50%) saving that is possible. Some research work has proved superplastic forming of friction stir welded (FSW) joints also. The FSW joint efficiencies have been characterized by mechanical and metallurgical examination. Studies are also available on the behavior of FSW joints of similar and dissimilar metals. Information on the performance of friction stir welded joints during superplastic forming is rather limited, but it is important to achieve excellent properties in the friction stir welded joints also during superplastic forming. FSP (friction stir processing) – SPF (superplastic forming) is presently being promoted as a very viable near-net shape technology for making very large and complicated sheet metal products. To achieve this superplastic material parameters are much required in industry to develop new shapes. One has to understand the flow rule relationship and mechanics involved during sheet metal forming at high temperature to select the material and forming tool with selected process parameters. This paper deals with the determination of superplastic material properties of non-superplastic aluminum alloy AA6061-T6. The superplastic material properties like strain rate sensitivity index, flow stress and strain rate were determined for both the selected material and friction stir welded sheets at various tool rotation speeds. The superplastic free blow forming experiments were performed for various constant temperatures and pressure for the parent material. Similarly the superplastic free blow forming experiments were performed for the friction stir welded joint for various tool rotation speed at constant temperature. The methods were used to determine the material properties are straight line fit method and polynomial regression method. The superplastic forming height is significantly high in case of the FSW specimens at 2000 rpm, the initial forming rate is faster and the strain rate sensitivity index obtained is also higher when compared to the parent material properties. The strain rate sensitivity index obtained for friction stir welded specimen during superplastic forming was foundto have improved when compared to the parent material.

Author(s):  
M D Naughton ◽  
P Tiernan

In this paper, the behaviour of extra-low interstitial (ELI) grade Ti-6Al-4V wire alloy has been extensively studied at varying strain rates in the range of 10-5-102 s-1 at temperatures ranging between 750 °C and 1050 °C using processing maps and experimental data to determine the material's mechanical and superplastic forming capabilities. From the slope of a log plot of strain rate versus flow stress, the strain-rate sensitivity index, m, was determined. A plot of m versus the log of strain rate was produced in order to identify the key strain rates in which ELI grade Ti-6Al-4V exhibits its superplastic regime. It was determined that this alloy is most sensitive to superplastic forming within a narrow strain-rate band of 10-4-10-3 s-1 and has a maximum strain-rate sensitivity index, m = 0.45. At strain rates below and above this range, the material exhibited negligible levels of superplasticity. The key temperature for superplastic forming was determined to be 950 °C. The effect of temperature on flow stress and flow stability was analysed using the Zener-Holloman parameter. The experimentally determined results showed excellent agreement with Guo and Ridley's activation mathematical model.


2015 ◽  
Vol 787 ◽  
pp. 437-441
Author(s):  
S. Ramesh Babu ◽  
Vijul Shah ◽  
M.P. Shyam

Superplasticity is the ability of the material to produce neck free elongations within a material before fracture. For the past three decades superplastic forming has gained a major development in many industries to produce complex shapes. To perform the superplastic forming at elevated temperatures, the material parameters such as strain rate and strain rate sensitivity index has to be determined. These parameters affect the formability in such a way that higher the strain rate during deformation, lesser will be the percentage elongation and which in turn increases the flow stress of the material there by limiting the formability. Similarly, the strain rate sensitivity index is a measure of resistance to neck formation during deformation. Lesser the strain rate sensitivity value, more will be the neck formation thereby limiting the formability. Hence in this work, an experimental setup is designed to perform the uniaxial tensile testing at elevated temperatures to determine the flow stress, percentage elongation, strain rate and strain rate sensitivity. The determination of these parameters will be helpful in executing the forming at certain temperature and pressure to attain maximum formability. Also the SEM photographs of the fractured specimen were analysed to determine at what temperature and strain rate, the cavitation density increases.


2008 ◽  
Vol 580-582 ◽  
pp. 209-212 ◽  
Author(s):  
Feng Gao ◽  
Hiroshi Nishikawa ◽  
Tadashi Takemoto

The lead-free casting solders Sn-3.5Ag-xCo (x = 0, 0.1, 0.5 and 1.0 mass%, respectively) were subjected to isothermal aging at 150°C for 0, 1008 and 2016 h, respectively. The nanoindentation methodology was employed herein to assess the mechanical properties. In particular, the strain rate sensitivity index value was derived from the creep deformation at the dwell time of the target constant load using Mayo-Nix theory. Basically, there is no remarkable tendency of the variation of Young’s modulus after aging, while to some extent, the hardness of the alloys drops. The strain rate sensitivity index value continues to decrease with the prolonged aging time. The solder grain growth and the coarsening of the intermetallics namely, Ag3Sn and CoSn2, are responsible for the mechanical evolution of the alloys. The 1.0% (mass%) Co additive improved the hardness of the solder alloy, and caused the decrease of the strain rate sensitivity value.


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