Friction Spot Welding and Friction Seam Welding

• US 20150360317A1
• Filed: 01/21/2014
• Published: 12/17/2015
• Est. Priority Date: 01/22/2013
• Status: Abandoned Application

• Current Assignee: University of Utah Research Foundation (State of Utah)
• Original Assignee: University of Utah Research Foundation (State of Utah)
• Inventors: Kalvala, Prasad Rao, Akram, Javed, Tshibind, Alex Ilunga, Jurovitzki, Abraham L., Minra, Manoranjan, Sarma, Biplab
• Application Number:
  US14/762,705
• Publication Number:
  US 20150360317A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B23K 20/12 the heat being generated by friction; Friction welding
• CPC Class Codes: B23K 20/1265 Non-butt welded joints, e.g. overlap-joints, T-joints or spot welds
• CPC Class Codes: B23K 20/128 making use of additional material
• CPC Class Codes: B23K 20/22 taking account of the properties of the materials to be welded
• CPC Class Codes: B23K 35/0261 Rods, electrodes, wires
• CPC Class Codes: B23K 35/402 Non-consumable electrodes; C-electrodes
• CPC Class Codes: B32B 15/01 all layers being exclusively metallic making layered metal workpieces by pressure cladding B23K20/22; making coatings with a metallic material characterised by its composition C23C30/00
• CPC Class Codes: B32B 15/011 all layers being formed of iron alloys or steels
• CPC Class Codes: B32B 15/015 the said other metal being copper or nickel or an alloy thereof
• CPC Class Codes: B32B 15/016 all layers being formed of aluminium or aluminium alloys
• CPC Class Codes: C22C 14/00 Alloys based on titanium
• CPC Class Codes: C22C 19/03 based on nickel
• CPC Class Codes: C22C 19/055 with the maximum Cr content being at least 20% but less than 30%
• CPC Class Codes: C22C 21/00 Alloys based on aluminium
• CPC Class Codes: C22C 21/08 with silicon
• CPC Class Codes: C22C 21/14 with silicon
• CPC Class Codes: C22C 21/16 with magnesium
• CPC Class Codes: C22C 23/00 Alloys based on magnesium
• CPC Class Codes: C22C 38/00 Ferrous alloys, e.g. steel alloys cast-iron alloys C22C37/00
• CPC Class Codes: C22C 38/02 containing silicon
• CPC Class Codes: C22C 38/04 : containing manganese
• CPC Class Codes: C22C 38/40 : with nickel
• CPC Class Codes: C22C 9/00 : Alloys based on copper
• CPC Class Codes: C22C 9/04 : with zinc as the next major constituent

Abstract

Systems and methods for spot welding and seam welding an upper material layer to a lower material layer using a rod. The rod can be a non-consumable rod or a consumable rod.

Claims

1. A method of spot welding an upper material layer to a lower material layer relative to a welding axis, the upper material layer being positioned in overlying relation to at least a portion of the lower material layer, the upper and lower material layers having respective top and bottom surfaces, the method comprising:

axially advancing and rotating a rod relative to the welding axis such that a distal end of the rod contacts the top surface of the upper material layer;

applying an axial force to the rotating rod such that frictional heat between the distal end of the rod and the upper material layer plasticizes a portion of the upper material layer;

with a portion of the upper material layer plasticized, applying the axial force to the rotating rod such that a portion of the bottom surface of the upper material layer and a portion of the top surface of the lower material layer are deformed, thereby forming a metallurgical bond between the upper and lower material layers; and

axially retracting the rod relative to the welding axis such that the distal end of the rod is removed from contact with the top surface of the upper material layer.

2. The method of claim 1, wherein the rod is substantially perpendicular to the top surface of the upper material layer when the distal end of the rod contacts the top surface of the upper material layer.

3. The method of claim 1, wherein the upper material layer and the lower material layer have respective thicknesses, and wherein the thickness of the upper material layer and the thickness of the lower material layer both range from about 0.5 mm to about 3.25 mm.

4. The method of claim 1, wherein the upper material layer and the lower material layer comprise a first material.

5. The method of claim 4, wherein at least the distal end of the rod comprises the first material.

6. The method of claim 4, wherein the at least the distal end of the rod comprises a second material different from the first material.

7. The method of claim 1, wherein the upper material layer comprises a first material, and wherein the lower material layer comprises a second material different from the first material.

8. The method of claim 7, wherein at least the distal end of the rod comprises the first material.

9. The method of claim 7, wherein at least the distal end of the rod comprises the second material.

10. The method of claim 7, wherein at least the distal end of the rod comprises a third material different from the first material and the second material.

11. The method of claim 1, wherein at least one intermediate material layer is positioned between the upper material layer and the lower material layer, wherein each intermediate material layer of the at least one intermediate material layer has a top surface and a bottom surface, and wherein the step of applying the axial force to the rotating rod such that the distal end of the rod penetrates through the upper material layer comprises applying the axial force to the rotating rod such that at least a portion of the top and bottom surfaces of each intermediate material layer is deformed, thereby forming a metallurgical bond between the upper material layer, the at least one intermediate material layer, and the lower material layer.

12. The method of claim 3, wherein the rod is a non-consumable rod.

13. The method of claim 3, wherein the rod is a consumable rod.

14. The method of claim 13, wherein the step of applying an axial force to the rotating rod comprises applying an axial force to the rotating rod such that frictional heat between the distal end of the rod and the upper material layer plasticizes a portion of the distal end of the rod, wherein, with a portion of the distal end of the rod and a portion of the upper material layer plasticized, the axial force is applied to the rotating rod such that the distal end of the rod penetrates through at least a portion of the upper material layer, thereby defining a cavity, and wherein, prior to axial retraction of the consumable rod, the plasticized portion of the distal end of the rod fills the cavity.

15. The method of claim 14, wherein the rod has a diameter ranging from about 5 mm to about 25 mm, wherein, prior to plasticization of the distal end of the rod, the rod has a longitudinal length ranging from about 50 mm to about 100 mm, and wherein, following filling of the cavity by the plasticized portion of the distal end of the rod, the longitudinal length of the rod ranges from about 45 mm to about 90 mm.

16. The method of claim 1, wherein the rod rotates at a rotational rate ranging from about 500 RPM to about 3,000 RPM.

17. The method of claim 1, wherein the axial force applied to the rod ranges from about 1,000 N to about 25,000 N.

18. A method of lap seam welding an upper material layer to a lower material layer relative to a vertical axis, the upper material layer being secured in overlying relation to at least a portion of the lower material layer, the upper and lower material layers having respective top and bottom surfaces and being configured for movement along a weld traverse axis, the weld traverse axis being substantially perpendicular to the vertical axis, the method comprising:

axially advancing and rotating a rod relative to the vertical axis such that a distal end of the rod contacts the top surface of the upper material layer;

applying an axial force to the rotating rod such that frictional heat between the distal end of the rod and the upper material layer plasticizes a portion of the upper material layer;

with a portion of the upper material layer plasticized, applying the axial force to the rotating rod such that a portion of the bottom surface of the upper material layer and a portion of the top surface of the lower material layer are deformed,

axially advancing the upper and lower material layers relative to the weld traverse axis by a desired length, thereby forming a metallurgical bond of the desired length between the upper and lower material layers; and

axially retracting the rod relative to the vertical axis such that the distal end of the rod is removed from contact with the top surface of the upper material layer.

19. The method of claim 18, wherein the rod is substantially perpendicular to the top surface of the upper material layer when the distal end of the rod contacts the top surface of the upper material layer.

20. The method of claim 18, wherein the upper material layer and the lower material layer have respective thicknesses, and wherein the thickness of the upper material layer and the thickness of the lower material layer both range from about 0.5 mm to about 2 mm.

21. The method of claim 18, wherein the upper material layer and the lower material layer comprise a first material.

22. The method of claim 21, wherein at least the distal end of the rod comprises the first material.

23. The method of claim 21, wherein at least the distal end of the rod comprises a second material different from the first material.

24. The method of claim 18, wherein the upper material layer comprises a first material, and wherein the lower material layer comprises a second material different from the first material.

25. The method of claim 24, wherein at least the distal end of the rod comprises the first material.

26. The method of claim 24, wherein at least the distal end of the rod comprises the second material.

27. The method of claim 24, wherein at least the distal end of the rod comprises a third material different from the first material and the second material.

28. The method of claim 18, wherein at least one intermediate material layer is secured between the upper material layer and the lower material layer, wherein each intermediate material layer of the at least one intermediate material layer has a top surface and a bottom surface,

wherein the step of applying the axial force to the rotating rod such that the distal end of the rod penetrates through the upper material layer comprises applying the axial force to the rotating rod such that at least a portion of the top and bottom surfaces of each intermediate material layer is deformed, and

wherein the step of axially advancing the upper and lower material layers relative to the weld traverse axis comprises axially advancing the upper material layer, the lower material layer, and the at least one intermediate material layer by the desired length, thereby forming a metallurgical bond of the desired length between the upper material layer, the at least one intermediate material layer, and the lower material layer.

29. The method of claim 20, wherein the rod is a non-consumable rod.

30. The method of claim 18, wherein the method is used as a cladding method.

31. The method of claim 18, wherein, following formation of the lap seam weld between the upper material layer and the lower material layer, the method further comprises lap seam welding at least one additive layer to the upper material layer.

32. The method of claim 18, wherein the rod rotates at a rotational rate ranging from about 800 RPM to about 1600 RPM.

33. The method of claim 18, wherein the axial force applied to the rod ranges from about 5000 N to about 9,000 N.

34. The method of claim 31, wherein the method is used as an additive manufacturing method.

35. A method of lap seam welding an upper material layer to a lower material layer relative to a vertical axis, the upper material layer being secured in overlying relation to at least a portion of the lower material layer, the upper and lower material layers having respective top and bottom surfaces and being configured for movement along a weld traverse axis and a transverse axis, the weld traverse axis and the transverse axis being positioned in a plane substantially perpendicular to the vertical axis, the weld traverse axis being substantially perpendicular to the transverse axis, the method comprising:

axially advancing and rotating a rod relative to the vertical axis such that a distal end of the rod contacts a first location on the top surface of the upper material layer;

applying a first axial force to the rotating rod such that frictional heat between the distal end of the rod and the upper material layer plasticizes a portion of the upper material layer;

with a portion of the upper material layer plasticized, applying the first axial force to the rotating rod such that a portion of the bottom surface of the upper material layer and a portion of the top surface of the lower material layer are deformed,

axially advancing the upper and lower material layers relative to the weld traverse axis by a first desired length, thereby forming a first seam weld between the upper and lower material layers;

axially retracting the rod relative to the vertical axis such that the distal end of the rod is removed from contact with the top surface of the upper material layer;

axially advancing and rotating the rod relative to the vertical axis such that the distal end of the rod contacts a second location on the top surface of the upper material layer, the second location on the top surface being spaced from the first location relative to the transverse axis;

applying a second axial force to the rotating rod such that frictional heat between the distal end of the rod and the upper material layer plasticizes a portion of the upper material layer;

with a portion of the upper material layer plasticized, applying the second axial force to the rotating rod such that a portion of the bottom surface of the upper material layer and a portion of the top surface of the lower material layer are deformed,

axially advancing the upper and lower material layers relative to the weld traverse axis by a second desired length, thereby forming a second seam weld between the upper and lower material layers; and

axially retracting the rod relative to the vertical axis such that the distal end of the rod is removed from contact with the top surface of the upper material layer,

wherein the first seam weld and the second seam weld overlap relative to the transverse axis.

36. The method of claim 35, wherein at least one intermediate material layer is secured between the upper material layer and the lower material layer, wherein each intermediate material layer of the at least one intermediate material layer has a top surface and a bottom surface,

wherein the steps of applying the first and second axial forces to the rotating rod such that the distal end of the rod penetrates through the upper material layer comprise applying the first and second axial forces to the rotating rod such that at least a portion of the top and bottom surfaces of each intermediate material layer is deformed, and

wherein the steps of axially advancing the upper and lower material layers relative to the weld traverse axis comprise axially advancing the upper material layer, the lower material layer, and the at least one intermediate material layer by the first and second desired lengths, thereby forming the first and second seam welds between the upper material layer, the at least one intermediate material layer, and the lower material layer.

37. The method of claim 35, wherein, prior to the step of axially advancing and rotating the rod relative to the vertical axis such that the distal end of the rod contacts the second location on the top surface of the upper material layer, the method comprises axially shifting the upper and lower material layers relative to the transverse axis such that the vertical axis is substantially aligned with the second location.

38. The method of claim 35, wherein, prior to the step of axially advancing and rotating the rod relative to the vertical axis such that the distal end of the rod contacts the second location on the top surface of the upper material layer, the method comprises axially shifting the rod relative to the transverse axis such that the vertical axis is substantially aligned with the second location.