EXPERIMENTAL ANALYSIS OF WELD PARAMETERS FOR FRICTION STIR WELDING OF ALUMINIUM 6082

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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056

Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072

EXPERIMENTAL ANALYSIS OF WELD PARAMETERS FOR FRICTION STIR WELDING OF ALUMINIUM 6082

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Abstract - In this work welding of two aluminum plates willbedonewitharootgapof0.25mmalongwithaspeedof 1400and1800rpm.Afterthiswehave changedrootgapto 0.5mm and 0.75 mm along with the same speeds. After weldingattheserootgaps,theworkpiecesareinvestigated for different weld parameters. Here we will be doing HardnesstestusingBrinellHardnessTestingMachineand Vickers Hardness Testing Machine . After that weld parameters are tested for tensile strength using universal testing machine. We will examine the Microstructure behavior of Friction Stir Welded Aluminum 6082 with differentrootgapsandtoolspeeds

Key Words: Friction Stir Welding, Al 6082, Vickers Hardness Test, Brinell Hardness Test, Micro Structure Analysis.

1.INTRODUCTION

Frictionstirweldingisasolidstateweldingprocess,isthe newest addition to friction welding, a solid state welding process. Solid state welding, as the term implies, is the formation of joints n the solid state, without fusion. Solid state welding includes processes such as cold welding, explosion welding, ultrasonic welding, roll welding, forge welding.

Therearedifferenttypesoffrictionweldingsuchas Rotary Friction Welding, Inertia Friction Welding, spin welding, friction surfacing,Friction Stud Welding, , Linear Friction Welding

1.2

Chromium:0.25%max

Copper:0.1%max

Iron:0.5%max

Magnesium:0.6to1.2%

Manganese:0.4%to1.0%

Silicon:0.7to1.3%and Titanium:0.1%max

Properties of Aluminum 6082

PhysicalProperties

Density : 2700kg/m^3

MeltingPoint : 555°C

ModulusOfElasticity : 70GPa

ElectricalResistivity : 0.038x10-6 Ω.m

ThermalConductivity : 180W/m.K

ThermalExpansion : 24x10-6 /K

Fig 1. Friction Stir Welding

1. FRICTION STIR WELDING OF ALUMINUM 6082

1.1.

Composition Of Aluminum 6082

Thealloycompositionof6082aluminumis

Aluminum:95.2to98.3%

Fig 1.1. Aluminum 6082 Plates Ready For Friction Stir Welding.

Fig 1.2. Shoulder Shaped tool used For Friction Stir Welding.

2. FRICTION STIR WELDING METHODOLOGY

Friction stir welding is done on the 6 specimens of Aluminum 6082 by the following root gaps with different rpm’s.

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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056

Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072

Fig 2.1. Friction Stir Welded Aluminum 6082 With 0.25mm root gap at 1400 rpm

Fig.2.5. Friction Stir Welded Aluminum 6082 With 0.5mm root gap at 1800 rpm

Fig.2.2. Friction Stir Welded Aluminum 6082 With 0.5mm root gap at 1400 rpm

Fig 2.6. Friction Stir Welded Aluminum 6082 With 0.75mm root gap at 1800 rpm

3. EXPERIMENTAL TESTS

ON FSW 6082

Inthisworkvariousweldparametersoffrictionstirwelded Aluminum6082areexaminedbyconductingthefollowing tests.

Hardness Test with Vickers Hardness Testing MachineandBrinellHardnessTestingMachine  MicroStructureAnalysis

3.1 Brinell Hardness Test

Fig.2.3. Friction Stir Welded Aluminum 6082 With 0.75mm root gap at 1400 rpm

TheBrinell hardness test methodas used to determine Brinellhardness,isdefinedinASTME10.Mostcommonlyit is used to test materials that have a structure that is too coarseorthathaveasurfacethatistooroughtobetested usinganothertestmethod,e.g.,castingsandforgings.Brinell testing often use a very high test load (3000 kgf) and a 10mm wide indenter so that the resulting indentation averagesoutmostsurfaceandsub-surfaceinconsistencies

Fig.2.4. Friction Stir Welded Aluminum 6082 With 0.25mm root gap at 1800 rpm

Anironball oftemperedsteel ora hardmetal ball witha knowndiameterispressedverticallywithatestforceFinan isolated testing surface. Test force is exerted during a definedtime(from2to8seconds);incidencetimemustbe from10to15seconds.Brinellhardnessiscalculatedbythe pressure diameter and the test force. The hardness measurement developed by Brinell is used for soft and mediumhardmetals,non-alloyedconstructiongradesteel, aluminium, wood and work materials with irregular structuressuchascastiron.Anironballoronemadeofa hardmetalisstruckwithadefinedforceformeasurement againstthesurfaceofthematerial.

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2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page380

International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056

Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072

Hardnesstestwillbecarriedoutonthefollowingsamples.

1. Friction Stir Welded aluminum 6082 with root gap of 0.25mmattoolspeed1400

2. Friction Stir Welded aluminum 6082 with root gap of 0.5mmattoolspeed1400

3. Friction Stir Welded aluminum 6082 with root gap of 0.75mmattoolspeed1400

Fig.3.1. Brinell Hardness Testing

4. Friction Stir Welded aluminum 6082 with root gap of 0.25mmattoolspeed1800

5. Friction Stir Welded aluminum 6082 with root gap of 0.5mmattoolspeed1800

6. Friction Stir Welded aluminum 6082 with root gap of 0.75mmattoolspeed1800

4. TENSILE TEST

Fig.3.2. Hardness test indentations on work piece

3.2 Vickers Hardness Test

TheVickershardnesstestmethodconsistsofindentingthe testmaterialwithadiamondindenter,intheformofaright pyramid with a square base and an angle of 136 degrees betweenoppositefacessubjectedtoaloadof1to100kgf. Thefullloadisnormallyappliedfor10to15seconds.The two diagonals of the indentation left in the surface of the material after removal of the load are measured using a microscopeandtheiraveragecalculated.

The area of the sloping surface of the indentation is calculated.TheVickershardnessisthequotientobtainedby dividing the kgf load by the square mm area of indentation.TheVickershardnesstestmeasureshardwork materialsbutalsothehardnessofmaterialsandthinwallsor marginalareas.

Tensile Test is done with Universal Testing machine for examining the Variation of Ultimate Tensile Strength of Friction Stir Welded Aluminum 6082 with different root gaps and at different tool speeds. i.e., Tensile test will be carriedoutonthefollowingsamples.

1. Friction Stir Welded aluminum 6082 with root gap of 0.25mmattoolspeed1400

2. Friction Stir Welded aluminum 6082 with root gap of 0.5mmattoolspeed1400

3. Friction Stir Welded aluminum 6082 with root gap of 0.75mmattoolspeed1400

4. Friction Stir Welded aluminum 6082 with root gap of 0.25mmattoolspeed1800

5. Friction Stir Welded aluminum 6082 with root gap of 0.5mmattoolspeed1800

6. Friction Stir Welded aluminum 6082 with root gap of 0.75mmattoolspeed1800

Fig.3.3. Vickers Hardness Testing Machine

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TheMicrostructureanalysisisdonetofindthevariationin the microstructure of Aluminum 6082 with Friction Stir weldingwithdifferentrootgapsandatdifferenttoolspeeds. Analysiswillbeconductedonthefollowingsamples.

1. Friction Stir Welded aluminum 6082 with root gap of 0.25mmattoolspeed1400

2. Friction Stir Welded aluminum 6082 with root gap of 0.5mmattoolspeed1400

3. Friction Stir Welded aluminum 6082 with root gap of 0.75mmattoolspeed1400

4. Friction Stir Welded aluminum 6082 with root gap of 0.25mmattoolspeed1800

5. Friction Stir Welded aluminum 6082 with root gap of 0.5mmattoolspeed1800

Fig.4.2. Tensile Test Specimens

5. MICRO STRUCTURE ANALYSIS

Microstructureanalysisisthestructureofmaterialisstudied undermagnification.

Microstructure is the small scale structure of a material, definedasthestructureofapreparedsurfaceofmaterialas revealed by a microscope above 25× magnificationThe microstructureofamaterialcanstronglyinfluencephysical propertiessuchasstrength,toughness,ductility,hardness, corrosion resistance, high/low temperature behavior or wear resistance. These properties in turn govern the application of these materials in industrial practice. Microstructure at scales smaller than can be viewed withopticalmicroscope.

6. Friction Stir Welded aluminum 6082 with root gap of 0.75mmattoolspeed1800 Fig.5.2.

Fig.5.1. optical microscope

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Fig. 4.1. Universal Testing Machine
5.RESULTS AND DISCUSSIONS 5.1 Brinell Hardness Test Values Hardness Testing Parameters Type of Hardness test : BHN Type of Material : AL6082 Dimensions : 100*60*5 Size of Intender : 5mm Load applied : 250KgS
Microstructure observation of specimen under optical microscope

International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056

SPEED ROOT

GAP BRINELL HARDNESS

IMP 1 IMP 2 IMP3 IMP 4

1400 0.25 62.4 61.8 61.2 61.80

0.5 60.4 60.1 59.5 60.00

0.75 57.3 57.9 58.4 57.87

1800 0.25 63.0 63.6 64.2 63.60 0.5 62.4 61.8 61.2 61.80 0.75 59.5 60.1 60.6 60.07

Table:5.1 Brinell Hardness Test Values

5.2 Vickers Hardness Test Values

Hardness Testing Parameters

Type of Hardness test : VHN

Type of Material : AL6082 Dimensions : 100*60*5

Type of Intender : Diamond Load applied : 5Kgs

SPEED ROOT GAP VICKERS HARDNESS

IMP 1 IMP 2 IMP3 IMP 4

1400 0.25 67.0 66.6 66.3 66.63 0.5 58.0 60.0 58.3 58.77 0.75 52.1 53.3 52.8 52.73 1800 0.25 63.2 62.6 61.9 62.57 0.5 61.6 62.3 62.6 62.17 0.75 58.0 57.7 57.1 57.60

Table:5.2 Vickers Hardness Test Values

Graph 5.2 Variation of hardness with root gap at 1800 rpm 5.3.Tensile Test Values

SPEED ROOT GAP TENSILETESTREADINGS UTL UTS N/MM2 YIELD (%) YIELD LOAD Kn

YIELD STRENGT H N/MM2

1400 0.25 8.240 109.18 2 3.540 4.960 65.721 0.5 7.080 97.346 2.500 5.680 78.097 0.75 4.120 61.028 1.160 3.120 46.215

1800 0.25 3.120 42.804 3.780 2.200 30.187 0.5 1.920 30.573 3.640 1.880 29.936 0.75 1.840 26.320 1.760 1.400 20.026

Table 5.3. Overall Tensile Test Readings with different root gaps at different speeds

Graph 5.1 Variation of hardness with root gap at 1400 rpm

Graph 5.3: variation of ultimate tensile strength values with root gap at 1400 rpm

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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056

Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072

Fig.:5.5 Grain size of 0.5 root gap specimen at 1400 rpm

Graph 5.4: variation of ultimate tensile strength values with root gap at 1800 rpm

5.4 Microscope Test report

Fig.:5.6 Heat affected zone of 0.5 root gap specimen at 1400 rpm

Fig.:5.3 Grain Size of 0.25 root gap specimen at 1400 rpm

Fig.:5.7 Grain Size of 0.75 root gap specimen at 1400 rpm

Fig.:5.4 Heat affected zone of 0.25 root gap specimen at 1400 rpm

Fig.:5.8 Heat affected zone of 0.75 root gap specimen at 1400 rpm

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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056

Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072

Fig.:5.9 Grain Size of 0.25 root gap specimen at 1800 rpm

Fig.:5.12 Heat affected zone of 0.5 root gap specimen at 1800 rpm

Fig.:5.10 Heat affected zone of 0.25 root gap specimen at 1800 rpm

Fig.:5.13 Grain Size of 0.75 root gap specimen at 1800 rpm

Fig.:5.11 Grain Size of 0.5 root gap specimen at 1800 rpm

Fig.:5.14 Heat affected zone of 0.75 root gap specimen at 1800 rpm

6. CONCLUSIONS

Fromthepreviouschapterresultsfollowingconclusionscan bemadeforFSWAL6082.

1. TheHardnessoftheFrictionstirweldedAL6082 willdecreasewiththe incrementinrootgapfrom0.25mmto0.75mm.

2. TheHardnessoftheFrictionstirweldedAL6082 willdecreasewiththe incrementinspinningtoolspeedfrom1400rpmto 1800rpm.

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| Page385
2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal

International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056

Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072

Sowecanconcludethatitcanbesuggestedtoopt frictionstirweldingofAL6082withlessrootgaps and welding should be done at low spinning tool speedtogetrequiredweldqualitywithimproved weld properties like Hardness, Ultimate tensile strength,Microstructureetc.

3. The Ultimate tensile strength of the Friction stir welded AL6082 will decrease with the incrementinrootgapfrom0.25mmto0.75mm.

4. The Ultimate tensile strength of the Friction stir weldedAL6082willdecreasewiththeincrementin spinningtoolspeedfrom1400rpmto1800rpm.

5. The Microstructure variation is more with more heat affected zones(HAZs) of the Friction stir weldedAL6082withtheincrementrootgapfrom 0.25to0.75mm.

6. The Microstructure variation is more with more heat affected zones(HAZs) of the Friction stir weldedAL6082withtheincrementinspinningtool speedfrom1400rpmto1800rpm.

So,wecanconcludethatitcanbesuggestedtoopt frictionstirweldingofAL6082withlessrootgaps and welding should be done at low spinning tool speedtogetrequiredweldqualitywithimproved weld properties like Hardness, Ultimate tensile strength,Microstructureetc.

6.1.FUTURE SCOPE:

Futureworkon Frictionstirweldingcanbecarriedoutand weld parameters can be investigated for similar (or) dissimilar metals by considering the influence of various other parameters like Deformation characteristics of the metal,Angleoftool,Pressureappliedbythespintooletc.

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