| Literature DB >> 31137496 |
Noor Zaman Khan1, Dhruv Bajaj2, Arshad Noor Siddiquee3, Zahid A Khan4, Mustufa Haider Abidi5, Usama Umer6, Hisham Alkhalefah7.
Abstract
The emergence of the aerospace sector requires efficient joining of aerospace grade aluminium alloys. For large-scale industrial practices, achievement of optimum friction stir welding (FSW) parameters is chiefly aimed at obtaining maximum strain rate in deforming material with least application of traverse force on the tool pin. Exact computation of strain rate is not possible due to complex and unexposed material flow kinematics. Estimation using micro-structural evolution serves as one of the very few methods applicable to analyze the yet unmapped interdependence of strain rate and traverse force. Therefore, the present work assessed strain rate in the stir zone using Zener Holloman parameter. The maximum and minimum strain rates of 6.95 and 0.31 s-1 were obtained for highest and least traverse force, respectively.Entities:
Keywords: aluminium alloys; friction stir welding; strain rate; traverse force
Year: 2019 PMID: 31137496 PMCID: PMC6566269 DOI: 10.3390/ma12101641
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.623
Chemical composition of AA2219-O.
| Elements | Al | Cu | Sn | Mn | Fe | Si | Ti | Zn | Ni | Zr | V |
|---|---|---|---|---|---|---|---|---|---|---|---|
|
| 91.97 | 6.8 | 0.02 | 0.315 | 0.16 | 0.06 | 0.04 | 0.06 | 0.023 | 0.203 | 0.165 |
Chemical composition of AA7475-T761.
| Elements | Al | Cu | Mg | Mn | Fe | Si | Ti | Zn | Ni | Zr | Cr |
|---|---|---|---|---|---|---|---|---|---|---|---|
|
| 90.99 | 1.34 | 1.93 | 0.006 | 0.101 | 0.06 | 0.023 | 5.36 | 0.002 | 0.0076 | 0.155 |
Mechanical and thermal properties of AA2219-O and AA7475-T761 alloys.
| Aluminium Alloy | UTS (MPa) | Yield Strength (MPa) | Specific Heat Capacity (J/g°C) | Thermal Conductivity (W/mK) | Incipient Melting-Liquidus Temperature (°C) |
|---|---|---|---|---|---|
|
| 468 | 430 | 0.88 | 163 | 538-635 |
|
| 256 | 210 | 0.864 | 120 | 543–643 |
Experimental plan.
| Experiment No. | Tool Rotational Speed (rpm) | Tool Traverse Speed (mm/min) |
|---|---|---|
| 1 | 710 | 250 |
| 2 | 1120 | 250 |
| 3 | 710 | 160 |
| 4 | 1120 | 160 |
Figure 1Experimental setup used for performing friction stir welding.
Figure 2Optical Micro-graphs at region A for grain size measurement of (a) Experiment 1, (b) Experiment 2, (c) Experiment 3, (d) Experiment 4.
Figure 3Schematic diagram showing the region A where optical micro-graphs are analyzed and local strain rate is computed.
Estimated local strain rates and sub-grain diameter.
| Experiment |
| |||
|---|---|---|---|---|
| 1 | 2.5 | 426 | 3.16 × 1012 | 6.95 |
| 2 | 3.1 | 448 | 3.41 × 1011 | 1.69 |
| 3 | 3.4 | 462 | 1.50 × 1011 | 1.23 |
| 4 | 4.8 | 495 | 1.27 × 1010 | 0.31 |
Peak values of traverse force for different welding parameters.
| Experiment Number | Tool Rotational Speed (rpm) | Traverse Speed (mm/min) | Peak Value of Traverse Force (N) | Average Values of Traverse Force (N) |
|---|---|---|---|---|
| 1 | 710 | 250 | 1078 | 999 |
| 2 | 1120 | 250 | 830 | 737 |
| 3 | 710 | 160 | 764 | 729 |
| 4 | 1120 | 160 | 705 | 678 |
Figure 4Traverse force exerted on the tool pin vs. distance travelled by the friction stir welding (FSW) tool for Experiments 1–4.
Experimental values for ANOVA.
| Experiment Number | Tool Rotational Speed (rpm) | Traverse Speed (mm/min) | Peak Traverse Force (N) |
|---|---|---|---|
| 1 | 710 | 250 | 1078 |
| 2 | 1120 | 250 | 830 |
| 3 | 710 | 160 | 764 |
| 4 | 1120 | 160 | 705 |
Analysis of variance.
| Source | Sum of Squares | DF | Mean Square | F Value | % Contribution |
|---|---|---|---|---|---|
|
| 2.2036 | 1 | 2.2036 | 3.56 | 28.69 |
|
| 4.8582 | 1 | 4.8582 | 7.86 | 63.26 |
|
| 0.6184 | 1 | 0.6184 | 8.05 | |
|
| 7.6802 | 3 |
Figure 5Micro-structural characterization for Experiments 1–4.
Grain size of thermo-mechanically affected zone (TMAZ) and heat affected zone (HAZ) for Experiments 1–4.
| Exp. No. | Grain Size (µm) | |
|---|---|---|
| TMAZ | HAZ | |
| 1 | 31.6 | 43.8 |
| 2 | 32.5 | 48.4 |
| 3 | 32.8 | 55.8 |
| 4 | 36.6 | 61.0 |