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Effect of Shoulder Geometry on Joint Morphology and
Mechanical Properties of Friction Stir Lap Welded 2024
Aluminum Alloy
Name: Amish Singh
Supervisor: Yue Yu Mei
Shenyang Aerospace University
1
Introduction
FSW
Process
Advantages and disadvantages
2
FSW
Solid State Welding
Thermo-mechanical action
Non-consumable tool
Can be applied on
Magnesium, Copper, Zinc,
steel, Titanium and it’s
alloys.
Best application on
aluminum dude to
thermo-mechanical
properties
Types of joints
Butt
Lap
T-joint
Spot joint
3
Advantages
• Environment friendly
• Energy efficient
• Great mechanical properties
• Low cost
• Less distortion
Disadvantages
• Welding speeds slower for some welding processes
• Requires a backing bar
• Workpieces must be rigidly clamped
• Keyhole in the end
4
Friction Stir Lap Welding
• Joint between two overlapping plates
• Tool plunged into the top surface and partially
into the bottom surface
• Widely used in transportation industries like
shipbuilding, train and automobile.
5
Defects
Hook
Cold
lap
Voids
Kissing
bond
6
RotationalTools
 Three rotational tools have been used
 All pin-less and non-consumable
 Different number of grooves on each tool
7
Material and it’s composition
Name of
element Cu Mn Mg Si Zn Ni Cr Pb Bi Al
Compos-
ition
4.3-
4.5
0.5-
0.6
1.3-
1.5
<0.5 <0.5 <0.5 <0.5 <0.5 <0.5 Remainder
Metal: Al2024
Dimensions: 300mm*150mm*1.5mm
Overlap region: 50mm
8
Two-pointer Four-pointer Six-pointer
Change in tool shoulders after the FSLW process
9
Experiment Process
 Research objectives:
 The main objectives of this thesis are:
 A) To join two 2024-T4 Al alloy plates using FSLW.
 B) To investigate the change occurring within the microstructure of
the welded lap joint during friction stir welding through the use of
experimental welding, constitutive modeling, and physical
simulation.
 C) To determine the effect of shoulder geometry on the mechanical
properties of the joint with the use of various kinds of pin-less tools.
10
Procedure
 Plates were cut into respective width, height and length
 Used sand paper to remove the oxide layer
 Plates were placed in an overlapping position and clamped to the FSW
table to carry out the process
 Process repeated with three pin-less tools under two rotational speeds
Serial
number
Type of
tool Rotation speed
Welding
speed
Tilt
angle
Plunge
depth
1 Two-pointer 2000rpm 1500rpm 20mm 2.5° 0.2mm
2 Four-pointer 2000rpm 1500rpm 20mm 2.5° 0.2mm
3 Six-pointer 2000rpm 1500rpm 20mm 2.5° 0.2mm
11
 Obtained welds are taken to Wire Cut Electric Discharge Digital control
machine.
 Cut into two different groups of samples- metallographic and lap shear
 Lap shear taken to the tensile strength testing machine
 Metallographic samples taken to the metallographic microscope to study
microstructures.
12
Results and Discussion
 Grooves work as pins in the case
of a pin-less tool.
 The number of grooves on the
shoulder is equally proportional
to the fineness of the weld
material.
 The resultant force goes in the
normal direction hence helping
the material to go underneath
the pin-less tool.
13
Microstructure Classification
Different microstructural zones
 SZ
 TMAZ
 HAZ
 BM
14
Cross Section of Microstructures
SZ
SZ
Two-pointer @ 1500 rpm and 2000 rpm
SZ
SZ
TMAZ
HAZ
BM
TMAZ
HAZ
Four-pointer @ 1500 rpm and 2000 rpm
15
SZ
SZ
TMAZ
HAZ
TMAZ
HAZ
BM
Six-pointer @ 1500 rpm and 2000 rpm
16
Magnified images of Microstructures
2 pointer @ 1500 and
2000 rpm
4 pointer @ 1500 and
2000 rpm
6 pointer @ 1500 and
2000 rpm
17
Microstructure
HAZ
HAZ
TMAZ
2 pointer @ 1500 and 2000
rpm
4 pointer @ 1500 and 2000
rpm
18
HAZ
TMAZ
SZ
SZ
TMAZ
6 pointer @ 1500 rpm 6 pointer @ 2000 rpm 6 pointer and BM
19
Lap Shear Failure Load
Tool Name
Rotational
Speed r/min
Transverse
Speed
mm/min
Average
Tensile
Strength N
Average Lap
Shear Failure
Load N/mm
2-pointer
1500 20 1351 45
2000 20 1746 58.2
4-pointer
1500 20 1964 65.5
2000 20 2136 71.2
6-pointer
1500 20 2245 74.8
2000 20 2364 78.8
 Calculated using the tensile strength testing machine
 Weld specimen elongated to the point of fracture to calculate the max lap shear failure load
 Weld sample cut to 30 mm in diameter
20
Fracture Morphology
2 pointer @ 1500 and
2000 rpm
4 pointer @ 1500 and
2000 rpm
6 pointer @ 1500 and
2000 rpm
21
Conclusion
The following conclusions are obtained through this experiment:
 (1) The 2024-T4 aluminum alloy FSLW joints have been successful obtained with three
different tools.
 (2)By the analysis of the cross section, it is found that with the increase of the number of
pointer, the area of the SZ increases, and the depth of SZ is increased.
 (3) There was no traditional Hook defect and cold lap on cross section, but the lap
interface was obviously deformed at high rotational speed.
 (4)With the increase of rotational speed when 2, 6 pointer tool was used grain
refinement on SZ or TMAZ, but by 2 pointer tool grains on HAZ did not refinement as
rotational speed increases.
 (5) The best lap shear failure load was got when the 6 pointer tool was used and the
rotational speed was 2000r/min, and the value was 78.8N/mm.
 (6) The crack propagation along the alcad, all joints showed shear fracture mode;
 (7) In the fracture morphology analysis, a large number of dimples were found, which
indicating ductile fracture.
22

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Effect of shoulder geometry on joint morphology and mechanical properties of Friction Stir Lap Welded 2024 Aluminum alloy

  • 1. Effect of Shoulder Geometry on Joint Morphology and Mechanical Properties of Friction Stir Lap Welded 2024 Aluminum Alloy Name: Amish Singh Supervisor: Yue Yu Mei Shenyang Aerospace University 1
  • 3. FSW Solid State Welding Thermo-mechanical action Non-consumable tool Can be applied on Magnesium, Copper, Zinc, steel, Titanium and it’s alloys. Best application on aluminum dude to thermo-mechanical properties Types of joints Butt Lap T-joint Spot joint 3
  • 4. Advantages • Environment friendly • Energy efficient • Great mechanical properties • Low cost • Less distortion Disadvantages • Welding speeds slower for some welding processes • Requires a backing bar • Workpieces must be rigidly clamped • Keyhole in the end 4
  • 5. Friction Stir Lap Welding • Joint between two overlapping plates • Tool plunged into the top surface and partially into the bottom surface • Widely used in transportation industries like shipbuilding, train and automobile. 5
  • 7. RotationalTools  Three rotational tools have been used  All pin-less and non-consumable  Different number of grooves on each tool 7
  • 8. Material and it’s composition Name of element Cu Mn Mg Si Zn Ni Cr Pb Bi Al Compos- ition 4.3- 4.5 0.5- 0.6 1.3- 1.5 <0.5 <0.5 <0.5 <0.5 <0.5 <0.5 Remainder Metal: Al2024 Dimensions: 300mm*150mm*1.5mm Overlap region: 50mm 8
  • 9. Two-pointer Four-pointer Six-pointer Change in tool shoulders after the FSLW process 9
  • 10. Experiment Process  Research objectives:  The main objectives of this thesis are:  A) To join two 2024-T4 Al alloy plates using FSLW.  B) To investigate the change occurring within the microstructure of the welded lap joint during friction stir welding through the use of experimental welding, constitutive modeling, and physical simulation.  C) To determine the effect of shoulder geometry on the mechanical properties of the joint with the use of various kinds of pin-less tools. 10
  • 11. Procedure  Plates were cut into respective width, height and length  Used sand paper to remove the oxide layer  Plates were placed in an overlapping position and clamped to the FSW table to carry out the process  Process repeated with three pin-less tools under two rotational speeds Serial number Type of tool Rotation speed Welding speed Tilt angle Plunge depth 1 Two-pointer 2000rpm 1500rpm 20mm 2.5° 0.2mm 2 Four-pointer 2000rpm 1500rpm 20mm 2.5° 0.2mm 3 Six-pointer 2000rpm 1500rpm 20mm 2.5° 0.2mm 11
  • 12.  Obtained welds are taken to Wire Cut Electric Discharge Digital control machine.  Cut into two different groups of samples- metallographic and lap shear  Lap shear taken to the tensile strength testing machine  Metallographic samples taken to the metallographic microscope to study microstructures. 12
  • 13. Results and Discussion  Grooves work as pins in the case of a pin-less tool.  The number of grooves on the shoulder is equally proportional to the fineness of the weld material.  The resultant force goes in the normal direction hence helping the material to go underneath the pin-less tool. 13
  • 14. Microstructure Classification Different microstructural zones  SZ  TMAZ  HAZ  BM 14
  • 15. Cross Section of Microstructures SZ SZ Two-pointer @ 1500 rpm and 2000 rpm SZ SZ TMAZ HAZ BM TMAZ HAZ Four-pointer @ 1500 rpm and 2000 rpm 15
  • 17. Magnified images of Microstructures 2 pointer @ 1500 and 2000 rpm 4 pointer @ 1500 and 2000 rpm 6 pointer @ 1500 and 2000 rpm 17
  • 18. Microstructure HAZ HAZ TMAZ 2 pointer @ 1500 and 2000 rpm 4 pointer @ 1500 and 2000 rpm 18
  • 19. HAZ TMAZ SZ SZ TMAZ 6 pointer @ 1500 rpm 6 pointer @ 2000 rpm 6 pointer and BM 19
  • 20. Lap Shear Failure Load Tool Name Rotational Speed r/min Transverse Speed mm/min Average Tensile Strength N Average Lap Shear Failure Load N/mm 2-pointer 1500 20 1351 45 2000 20 1746 58.2 4-pointer 1500 20 1964 65.5 2000 20 2136 71.2 6-pointer 1500 20 2245 74.8 2000 20 2364 78.8  Calculated using the tensile strength testing machine  Weld specimen elongated to the point of fracture to calculate the max lap shear failure load  Weld sample cut to 30 mm in diameter 20
  • 21. Fracture Morphology 2 pointer @ 1500 and 2000 rpm 4 pointer @ 1500 and 2000 rpm 6 pointer @ 1500 and 2000 rpm 21
  • 22. Conclusion The following conclusions are obtained through this experiment:  (1) The 2024-T4 aluminum alloy FSLW joints have been successful obtained with three different tools.  (2)By the analysis of the cross section, it is found that with the increase of the number of pointer, the area of the SZ increases, and the depth of SZ is increased.  (3) There was no traditional Hook defect and cold lap on cross section, but the lap interface was obviously deformed at high rotational speed.  (4)With the increase of rotational speed when 2, 6 pointer tool was used grain refinement on SZ or TMAZ, but by 2 pointer tool grains on HAZ did not refinement as rotational speed increases.  (5) The best lap shear failure load was got when the 6 pointer tool was used and the rotational speed was 2000r/min, and the value was 78.8N/mm.  (6) The crack propagation along the alcad, all joints showed shear fracture mode;  (7) In the fracture morphology analysis, a large number of dimples were found, which indicating ductile fracture. 22