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Friction Stir Welding of Aluminum MMC 6061-XX%
Boron Carbide

Han Zhang* and Tracy W. Nelson** T. Haynes*
*Reynolds Metals Company
**Brigham young University
Provo, UT
Aluminum metal matrix composites (MMC) offer increased stiffness, strength and wear
resistance over standard aluminum alloys. However, the weldability of these materials is greatly
compromised with the addition of non-metallic reinforcement. Powder metallurgy products of
METAMIC materials with B4C reinforcement developed at Reynolds Metals Company is being
considered for neutron shielding applications because of the ability of B10 isotope to absorb the
neutrons. Fusion welding studies have demonstrated the ability to join in this type of material
with minimal welding-related defects using carefully controlled parameters. However, the joint
strength is determined by the choice of filler material. Solid state welding method could be used
to join this type of material offering better joint mechanical properties. Friction stir welding
(FSW) was investigated as a possible means of joining this material. Preliminary results
demonstrate that FSW is a viable process for joining producing superior mechanical properties
compared to traditional fusion welding. Test results for both fusion welding and FSW will be
compared, as well as tool wear and the feasibility of joining 6061-21% B4C METAMIC neutron
shielding materials.



1. Background
Friction stir welding (FSW) is a relatively new joining process that has received
considerable attention since being patented in 1991 by The Welding institute in Cambridge
England (Ref. 1-3). The advantages of friction stir welding (FSW) over conventional fusion
welding have been recognized by many industries, especially for joining aluminum alloys (Ref.
11-17). A few of the advantages that pose significant cost reductions in the manufacturing of
aluminum aerospace structures include the elimination of cracking in both the fusion zone and
heat-affected zone, porosity, filler metals, shielding gases and costly weld preparation (Ref. 1
and 15). Despite these potential benefits and the tremendous development efforts by numerous
industries to implement this process into production, there is still a vast amount of research and
development needed in order to better understand the microstructure and long term service
integrity associated with friction stir welds (FSWs). An understanding of microstructural
evolution during FSW and how the associated microstructures affect such mechanical and
physical properties as strength, fatigue, creep and corrosion is critical. Such an understanding
will bring broader acceptance, and thus, new applications for this new innovative joining
technology.
Although FSW has gained broad acceptance in joining many aluminum and cooper
alloys, there are a number of other materials which could benefit tremendously from this process.
Aluminum metal matrix composites (MMC) are among those materials that could take advantage
of the benefits that FSW offers over traditional fusion welding techniques. MMC materials
suffer from a variety of problems when subject to traditional fusion welding processes. Welds in
alloys like 6061-Al2O3 exhibit poor mechanical properties due to loss in composite material and
porosity formation. During welding, the aluminum oxide particulate dissociates resulting in free
excess oxygen which may for porosity in the weld and a lower composite particulate count in the
matrix. Both of the above lead to reduced mechanical properties.
Likewise, aluminum alloys reinforced with SiC or B4C particulate suffer from similar
problems. SiC and B4C dissociate during fusion welding resulting in excess Si and B in the
matrix. The carbon form these phases combines with aluminum to form an adverse aluminum
carbide (Al4C3) phase which is soluble in water. Again, the loss of reinforcing particulate and the
formation of adverse aluminum carbide and porosity results in reduce mechanical properties of
these alloys when fusion welded.
Despite their problems during welding, these materials offer increased stiffness and
specific strength. Alloys strengthened with B4C also exhibit reduced density with increased wear
resistance and neutron absorption. Alloy 6061-XX%B4C can exhibit an XX% in modulus with
up to XX% B4C. This alloy also exhibits excellent neutron absorption characteristics making
this alloy particularly beneficial in the nuclear industry. ?????
2. Experimental Approach
Both gas tungsten arc welds (GTAW) and friction stir welds (FSW) were made in ??? in. thick
6061-XX%B4C. GTAW were produced using xXX amps alternating current with pure Argon
shileindg gas. ????? FSW were produced at 670 RPM and 4.5 and 5.5 IPM using a tool design
developed at BYU.
3. Results and Discussion
Although possible, it is difficult to produce quality welds in 6061-XX%B4C using GTAW.
There exist a miriad of problems associated with GTAW in this materials such as porosity,
adverse second phase formation and excess eutectic formation in the fusion zone. Optical and
SEM photomicrographs of transverse section of GTAW and FSW in 6061-XX%B4C are shown
in Figures 1-5.

2 mm
Figure 1. Transverse photomicrograph showing presence of porosity in an autogenous GTAW in
6061-XX%B4C.

10 µm
Figure ?. Transverse photomicrograph showing aluminum carbide (black needles) in an
autogenous GTAW in 6061-XX%B4C
Al4C3

Figure ?. Chemical analysis of needle phases (black) in Figure ?.

2 mm
Figure ?. Photomicrograph of GTAW with 4043 filler metal in 6061-21%B4C.
Shrinkage Porosity

Si
20 µm
a)

1 µm
b)

Figure ?. GTAW with 4043 filler in 6061-21%B4C, a) showing shrinkage porosity in weld, and
b) showing eutectic formation.

a)

b)

Figure ?. Transverse photomicrographs of the weld regions in a) GTAW and, b) FSW.

All the test results indicate that FSW is a superior joining process comparative to GTAW when
joining 6061-XX%B4C. Tensile test results are shown below in Figure ?. From
36.0

Strength (ksi) + Elongation (%)

40.0
35.0

30.4

29.4

30.0
22.9

25.0
19.5

18.0

20.0

19.8
17.4

15.0

12.0

10.0
5.0

5.0

4.0

0.0
BS

FSW-4.5

UTS
4.0

YS
Elongation

FSW-5.25

Conditions

TIG

Figiure ?. Comparison of base metal and weld metal Tensile properties in 6061-XX%B4C.

Steels

1 mm

100 µm

Figure ?. SEM backscatter of surface of FSW indicating deposits of Fe from the tool at the
advancing side of the welding.
4. Conclusions
1. METAMIC neutron shielding materials containing B4C can be welded using TIG method.

2. Standard welding procedure used to join I/M monolithic 6061 can not be used to join this
type of material due to serve hydrogen-induced porosity and formation of Al4C3 at the fusion
zone.
3. The density of hydrogen-induced porosity can be minimized by controlling heat input and
dilution.
4. No apparent heat affected zone softening was detected.
5. Fusion zone mechanical properties are determined by the choice of filler material.
6. FSW can be used to join this material with similar tensile properties as parent material.
However, the long weld can not be made due to serve tool wear.
7. References
1. Welding Institute; TWI; Thomas, WM; Nicholas, ED; Needham, JC; Murch, MG; TempleSmith, P; Dawes, CJ, “Improvements Relating to Friction Welding [Friction Stir Welding
and Friction Plunge Welding],” PCT World Patent Application WO 93/10935. Filed: 27
Nov.1992 (UK 9125978.8, 6 Dec.1991). Publ: 10 June 1993.
2. TWI; Thomas, WM; Nicholas, ED; Needham, JC; Temple-Smith, P; Kallee S, WKW;
Dawes, CJ, “Improvements Relating to Friction Welding [Friction Stir Welding and Friction
Plunge Welding],” UK Patent Application 2 306 366 A, Filed: 17 Oct.1996 (UK 9521570, 20
Oct.1995; 9523827, 22 Nov.1995; 9605864, 20 Mar.1996). Publ: 7 May 1997.
3. TWI; Thomas, WM; Murch, MG; Nicholas, ED; Temple-Smith, P; Needham, JC; Dawes,
CJ, “Improvements Relating to Friction Welding [Friction Stir Welding and Friction Plunge
Welding],” European Patent Application 653 265 A2. Filed: 27 Nov.1992 (UK 9125978, 6
Dec.1991). Publ: 17 May 1995.
4. W.M. Mahoney, C.G. Rhodes, J.G. Flintoff, R.A. Spurling, and W.H. Bingel, “Properties of
Friction-Stir-Welded 7075 T651 Aluminum”, Metallurgical and Materials Transactions,
Vol. 29A, July 1998, pp. 1955-1964.
5. C.G. Rhodes, M.W. Mahoney, and W.H. Bingel, 1997, “Effects of Friction Stir Welding on
Microstructure of 7075 Aluminum,” Scipta Metallurgia, 30(1), pp 69-75.
6. L.E. Murr, G. Liu, and J.C. McClure, 1997, “Dynamic Recrystallization in Friction Stir
Welding of Aluminum Alloy 1100,” Journal of Material Science Letters, 16(22), 1801-1803.
7. G. Liu, L.E. Murr, C-S. Niou, J.C. McClure and F.R. Vega, 1997, “Microstructural Aspects
of the Friction Stir Weleidng of 6061-T6 Aluminum,” Scripta Materialia, 37(1), pp 355-361.
8. L.E. Murr, G.Liu and J.C. McClure, 1998, “A TEM Study of Precipitation and Related
Microstructures in Friction Stir Welded 6061 Aluminum,” Journal of Materials Science,
33(5), pp1243-1251.
9. P. Ditzel and J.C. Lippold, “Microstructural Evolution During Friction Stir Welding of
Aluminum Alloy 6061-T6”, Edison Welding Institute, Cooperative Research Program,
Summary Report SR9709, Nov. 1997.
10. K.E. Knipstr(m and B. Pekkari, “Friction Stir Welding Process Goes Commercial”, Welding
Journal, Sept. 1997, pp. 55-57.
11. D.E. Spindler, “What Industry Needs to Know about Friction Welding”, Welding Journal,
March 1994, pp. 37-42.
12. C.J. Dawes and W.M. Thomas, “Friction Stir Process Welds Aluminum Alloys”, Welding
Journal, March 1996, pp. 41-45.
13. W.M. Thomas and E.D. Nicholas, “Friction stir welding for the transportation industries”,
Materials and Design, Vol. 18, Nos. 4/6, 1997, pp. 269-273.
14. M.J. Johnsen, “Friction Stir Welding Takes Off at Boeing”, Welding Journal, Feb. 1999, pp.
35-39.
15. T. Shinoda and Y. Kondo, “Friction Stir Welding of Aluminum Plate”, Welding
International, Vol. 11, No. 3, 1997, pp. 179-184.
16. O.T. Midling and H.G. Johansen, “Production of Wide Aluminum Profiles by Solid-State
Friction Stir Welding”, International Aluminum Extrusion Seminar & Exposition, Chicago,
IL, May 1996.
17. O.T. Midling, “Material Flow Behavioral and Microstructural Integrity of Friction Stir Butt
Weldments”, Presented at the 4th International Conference on Aluminum Alloys, Atlanta,
USA, ICAA4I, Sept. 15, 1994.

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Ifs welding al_mmc_b4_c

  • 1. Friction Stir Welding of Aluminum MMC 6061-XX% Boron Carbide Han Zhang* and Tracy W. Nelson** T. Haynes* *Reynolds Metals Company **Brigham young University Provo, UT Aluminum metal matrix composites (MMC) offer increased stiffness, strength and wear resistance over standard aluminum alloys. However, the weldability of these materials is greatly compromised with the addition of non-metallic reinforcement. Powder metallurgy products of METAMIC materials with B4C reinforcement developed at Reynolds Metals Company is being considered for neutron shielding applications because of the ability of B10 isotope to absorb the neutrons. Fusion welding studies have demonstrated the ability to join in this type of material with minimal welding-related defects using carefully controlled parameters. However, the joint strength is determined by the choice of filler material. Solid state welding method could be used to join this type of material offering better joint mechanical properties. Friction stir welding (FSW) was investigated as a possible means of joining this material. Preliminary results demonstrate that FSW is a viable process for joining producing superior mechanical properties compared to traditional fusion welding. Test results for both fusion welding and FSW will be compared, as well as tool wear and the feasibility of joining 6061-21% B4C METAMIC neutron shielding materials.  
  • 2. 1. Background Friction stir welding (FSW) is a relatively new joining process that has received considerable attention since being patented in 1991 by The Welding institute in Cambridge England (Ref. 1-3). The advantages of friction stir welding (FSW) over conventional fusion welding have been recognized by many industries, especially for joining aluminum alloys (Ref. 11-17). A few of the advantages that pose significant cost reductions in the manufacturing of aluminum aerospace structures include the elimination of cracking in both the fusion zone and heat-affected zone, porosity, filler metals, shielding gases and costly weld preparation (Ref. 1 and 15). Despite these potential benefits and the tremendous development efforts by numerous industries to implement this process into production, there is still a vast amount of research and development needed in order to better understand the microstructure and long term service integrity associated with friction stir welds (FSWs). An understanding of microstructural evolution during FSW and how the associated microstructures affect such mechanical and physical properties as strength, fatigue, creep and corrosion is critical. Such an understanding will bring broader acceptance, and thus, new applications for this new innovative joining technology. Although FSW has gained broad acceptance in joining many aluminum and cooper alloys, there are a number of other materials which could benefit tremendously from this process. Aluminum metal matrix composites (MMC) are among those materials that could take advantage of the benefits that FSW offers over traditional fusion welding techniques. MMC materials suffer from a variety of problems when subject to traditional fusion welding processes. Welds in alloys like 6061-Al2O3 exhibit poor mechanical properties due to loss in composite material and porosity formation. During welding, the aluminum oxide particulate dissociates resulting in free excess oxygen which may for porosity in the weld and a lower composite particulate count in the matrix. Both of the above lead to reduced mechanical properties. Likewise, aluminum alloys reinforced with SiC or B4C particulate suffer from similar problems. SiC and B4C dissociate during fusion welding resulting in excess Si and B in the matrix. The carbon form these phases combines with aluminum to form an adverse aluminum carbide (Al4C3) phase which is soluble in water. Again, the loss of reinforcing particulate and the formation of adverse aluminum carbide and porosity results in reduce mechanical properties of these alloys when fusion welded. Despite their problems during welding, these materials offer increased stiffness and specific strength. Alloys strengthened with B4C also exhibit reduced density with increased wear resistance and neutron absorption. Alloy 6061-XX%B4C can exhibit an XX% in modulus with up to XX% B4C. This alloy also exhibits excellent neutron absorption characteristics making this alloy particularly beneficial in the nuclear industry. ????? 2. Experimental Approach Both gas tungsten arc welds (GTAW) and friction stir welds (FSW) were made in ??? in. thick 6061-XX%B4C. GTAW were produced using xXX amps alternating current with pure Argon shileindg gas. ????? FSW were produced at 670 RPM and 4.5 and 5.5 IPM using a tool design developed at BYU.
  • 3. 3. Results and Discussion Although possible, it is difficult to produce quality welds in 6061-XX%B4C using GTAW. There exist a miriad of problems associated with GTAW in this materials such as porosity, adverse second phase formation and excess eutectic formation in the fusion zone. Optical and SEM photomicrographs of transverse section of GTAW and FSW in 6061-XX%B4C are shown in Figures 1-5. 2 mm Figure 1. Transverse photomicrograph showing presence of porosity in an autogenous GTAW in 6061-XX%B4C. 10 µm Figure ?. Transverse photomicrograph showing aluminum carbide (black needles) in an autogenous GTAW in 6061-XX%B4C
  • 4. Al4C3 Figure ?. Chemical analysis of needle phases (black) in Figure ?. 2 mm Figure ?. Photomicrograph of GTAW with 4043 filler metal in 6061-21%B4C.
  • 5. Shrinkage Porosity Si 20 µm a) 1 µm b) Figure ?. GTAW with 4043 filler in 6061-21%B4C, a) showing shrinkage porosity in weld, and b) showing eutectic formation. a) b) Figure ?. Transverse photomicrographs of the weld regions in a) GTAW and, b) FSW. All the test results indicate that FSW is a superior joining process comparative to GTAW when joining 6061-XX%B4C. Tensile test results are shown below in Figure ?. From
  • 6. 36.0 Strength (ksi) + Elongation (%) 40.0 35.0 30.4 29.4 30.0 22.9 25.0 19.5 18.0 20.0 19.8 17.4 15.0 12.0 10.0 5.0 5.0 4.0 0.0 BS FSW-4.5 UTS 4.0 YS Elongation FSW-5.25 Conditions TIG Figiure ?. Comparison of base metal and weld metal Tensile properties in 6061-XX%B4C. Steels 1 mm 100 µm Figure ?. SEM backscatter of surface of FSW indicating deposits of Fe from the tool at the advancing side of the welding. 4. Conclusions 1. METAMIC neutron shielding materials containing B4C can be welded using TIG method. 
  • 7. 2. Standard welding procedure used to join I/M monolithic 6061 can not be used to join this type of material due to serve hydrogen-induced porosity and formation of Al4C3 at the fusion zone. 3. The density of hydrogen-induced porosity can be minimized by controlling heat input and dilution. 4. No apparent heat affected zone softening was detected. 5. Fusion zone mechanical properties are determined by the choice of filler material. 6. FSW can be used to join this material with similar tensile properties as parent material. However, the long weld can not be made due to serve tool wear. 7. References 1. Welding Institute; TWI; Thomas, WM; Nicholas, ED; Needham, JC; Murch, MG; TempleSmith, P; Dawes, CJ, “Improvements Relating to Friction Welding [Friction Stir Welding and Friction Plunge Welding],” PCT World Patent Application WO 93/10935. Filed: 27 Nov.1992 (UK 9125978.8, 6 Dec.1991). Publ: 10 June 1993. 2. TWI; Thomas, WM; Nicholas, ED; Needham, JC; Temple-Smith, P; Kallee S, WKW; Dawes, CJ, “Improvements Relating to Friction Welding [Friction Stir Welding and Friction Plunge Welding],” UK Patent Application 2 306 366 A, Filed: 17 Oct.1996 (UK 9521570, 20 Oct.1995; 9523827, 22 Nov.1995; 9605864, 20 Mar.1996). Publ: 7 May 1997. 3. TWI; Thomas, WM; Murch, MG; Nicholas, ED; Temple-Smith, P; Needham, JC; Dawes, CJ, “Improvements Relating to Friction Welding [Friction Stir Welding and Friction Plunge Welding],” European Patent Application 653 265 A2. Filed: 27 Nov.1992 (UK 9125978, 6 Dec.1991). Publ: 17 May 1995. 4. W.M. Mahoney, C.G. Rhodes, J.G. Flintoff, R.A. Spurling, and W.H. Bingel, “Properties of Friction-Stir-Welded 7075 T651 Aluminum”, Metallurgical and Materials Transactions, Vol. 29A, July 1998, pp. 1955-1964. 5. C.G. Rhodes, M.W. Mahoney, and W.H. Bingel, 1997, “Effects of Friction Stir Welding on Microstructure of 7075 Aluminum,” Scipta Metallurgia, 30(1), pp 69-75. 6. L.E. Murr, G. Liu, and J.C. McClure, 1997, “Dynamic Recrystallization in Friction Stir Welding of Aluminum Alloy 1100,” Journal of Material Science Letters, 16(22), 1801-1803. 7. G. Liu, L.E. Murr, C-S. Niou, J.C. McClure and F.R. Vega, 1997, “Microstructural Aspects of the Friction Stir Weleidng of 6061-T6 Aluminum,” Scripta Materialia, 37(1), pp 355-361. 8. L.E. Murr, G.Liu and J.C. McClure, 1998, “A TEM Study of Precipitation and Related Microstructures in Friction Stir Welded 6061 Aluminum,” Journal of Materials Science, 33(5), pp1243-1251. 9. P. Ditzel and J.C. Lippold, “Microstructural Evolution During Friction Stir Welding of Aluminum Alloy 6061-T6”, Edison Welding Institute, Cooperative Research Program, Summary Report SR9709, Nov. 1997. 10. K.E. Knipstr(m and B. Pekkari, “Friction Stir Welding Process Goes Commercial”, Welding Journal, Sept. 1997, pp. 55-57. 11. D.E. Spindler, “What Industry Needs to Know about Friction Welding”, Welding Journal, March 1994, pp. 37-42. 12. C.J. Dawes and W.M. Thomas, “Friction Stir Process Welds Aluminum Alloys”, Welding Journal, March 1996, pp. 41-45.
  • 8. 13. W.M. Thomas and E.D. Nicholas, “Friction stir welding for the transportation industries”, Materials and Design, Vol. 18, Nos. 4/6, 1997, pp. 269-273. 14. M.J. Johnsen, “Friction Stir Welding Takes Off at Boeing”, Welding Journal, Feb. 1999, pp. 35-39. 15. T. Shinoda and Y. Kondo, “Friction Stir Welding of Aluminum Plate”, Welding International, Vol. 11, No. 3, 1997, pp. 179-184. 16. O.T. Midling and H.G. Johansen, “Production of Wide Aluminum Profiles by Solid-State Friction Stir Welding”, International Aluminum Extrusion Seminar & Exposition, Chicago, IL, May 1996. 17. O.T. Midling, “Material Flow Behavioral and Microstructural Integrity of Friction Stir Butt Weldments”, Presented at the 4th International Conference on Aluminum Alloys, Atlanta, USA, ICAA4I, Sept. 15, 1994.