Aluminum MMC

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    FRICTION STIR WELDING OFALUMINUM MMC 6092-17.5%SiCP

    Tracy W. Nelson*, Dick Lederich**

    *Brigham Young University

    Provo, UT

    **The Boeing Company

    Phantom Works

    St. Louis, MO

    Acknowledgments: Work sponsored by the MetalsAffordability Initiative

    Scott Packer

    Advanced Metal Products Inc.

    Bountiful, Utah

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    OUTLINE

    Background

    MMCs

    Joining MMCs

    ObjectivesProcedures

    Results

    Summary

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    BackgroundAluminum MMCs offer:

    Advantages:Low density, high specific strength, and high modulus

    High fatigue strength

    Better wear resistance

    Disadvantages:

    Low fracture toughness

    Fabrication difficulty

    High cost

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    BackgroundWeldability of MMCs is greatly compromised

    reaction between second phase and Al matrix isoften detrimental

    porosity, cracking, aluminum carbides, etc.

    often limited in use because of poor weldability

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    GTAW in 6061-21%B4C

    GTAW

    Hydrogen induced porosity

    Formation of Al4C3Al4C3

    10 m2 mm

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    GTAW in 6061-21%B4C

    2 mm

    20 m

    1 m

    Shrinkage Porosity

    Si

    Two-pass weld, ER 4043 filler, Ar shielding gas

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    Objectives

    Assess the feasibility of joining 6092-

    17.5%SiCp via FSW

    Compare weld quality, mechanical properties,

    and second phase distribution

    Evaluate effects of post weld aging on tensile

    properties and failure

    Characterize tool wear

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    Procedure Base Material - alloy 6092-17.5%SiCp

    0.100 (2.54 mm) sheet; 8 X 24 (20cm X 60cm) panels

    heavily oxidized must remove before welding

    Weld Procedure Development Choose optimal spindle speed, travel speed

    Tool materials evaluated H13 tool steel

    Polycrystalline cubic boron nitride (CBN)

    Weldment Characterization

    Both as-welded and post-weld aged Tensile testing (ASTM E8)

    Optical and SEM analyses

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    Weld Parameter Evaluation Parameters evaluated for H13 tool

    RPM 202, 545 and 815

    IPM 6.4, 11, and 26 Parameters used for further testing 545 rpm and 11 ipm

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    Weld Parameter Evaluation Welds Made with CBN

    Tooling No spalling of the surface

    Less flash

    Better consolidation

    Much wider range ofparameters possible

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    Mechanical Properties As welded tensile properties for FSW 6092-17.5%SiCp

    Strengths very similar between H13 and CBN (3% difference)

    Significant difference in tensile elongation between two tool

    materials (87% difference)

    Coupon #

    0.2% Yield

    Stress(Ksi)

    Ult. Tensile

    Stress(Ksi)

    Elong. in 2

    in.(%)

    Fail. Loc.1=DXZ, 2=AS-

    TMAZ, 3=RS-

    TMAZ, 4=HAZ

    0.2% Yield

    Stress(Ksi)

    Ult. Tensile

    Stress(Ksi)

    Elong. in 2

    in.(%)

    Fail. Loc.1=DXZ, 2=AS-

    TMAZ, 3=RS-

    TMAZ, 4=HAZ

    1 33700 38020 0.85 1 34220 39406 1.63 2

    2 31526 35070 0.85 3 32000 37538 2.00 2

    3 32500 35398 0.60 1 31800 37707 1.95 2

    4 34284 39446 0.90 3 34239 38996 1.35 2

    5 31847 37302 1.15 1 32500 37617 1.33 2

    6 34000 36643 0.65 1 33400 38589 2.00 2

    7 33000 37365 1.45 1&3 33400 37662 2.20 2

    8 32800 37382 1.00 1&3 31200 36233 1.50 2

    Average 32957 37078 0.93 32845 37969 1.74

    Stand. Dev. 994 1402 0.274 1139 999 0.335

    H13 Tool CBN Tool

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    Comparison of Tensile Failures Tensile Failure locations

    H13 tool TMAZ and DXZCBN tool HAZ

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    Post weld aging to T6 w/o SHT Initial test age at 325F for various times

    Oxide mechanically removed

    Oxide chemically removed, flash machined after welding

    Effect of Post Weld Aging

    TMAZ (R side)4.545.832.0As Weld

    TMAZ (A side)3.947.934.4325F/2h

    TMAZ (A side)2.348.137.3325F/4h

    TMAZ (A side)1.848.538.2325F/6h

    TMAZ (A side)1.749.039.4325F/8h

    TMAZ (A side)0.739.434.6325F/7h

    Flash was machined away (.006)1.248.440.9325F/4h

    TMAZ (A side)1.438.430.2325F/2h

    TMAZ (A side)2.134.824.8As Weld

    Comments Failure LocationElong.

    (% )

    UTS

    (ksi)

    0.2%YS

    (ksi)

    Condition

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    Effect of SHT and Aging

    Failed in nugget1.151.541.2STA-1

    Failed in nugget0.237.0-STA-2

    Failed in nugget1.250.340.1STA-3

    Failed at root side disbond-23.1-Flash removed; 0.020

    removed from root

    Failed at root side disbond-26.4-Flash removed (0.004)Failed at root side disbond-30.1-None

    CommentsElong.

    (%)

    UTS

    (ksi)

    0.2% YS

    (ksi)

    Description of

    Machining

    SHT at 1030F for 3 hrs, T6 temper at 325F for 7-8 hours

    Rockwell B 77-79, verifying T6

    Results

    Failure at root side disbond Chemical oxide removal, flash machined after welding

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    Root Side Disbond Failures Lazy Sinterface

    Etched dye penetrant and radiograph inspections failed to detect

    Originally believed to be oxide stringers, but SEM failed todetect oxides (different etch rate)

    Need to pickle materials

    mechanical cleaning was insufficient

    As welded and Aged Failed Tensile Sample

    500 m 500 m

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    Comparison of Particulate Distribution

    SiC particulate distribution Distribution in weld is same as in base metal

    Base Metal Nugget-H13 Nugget - CBN

    15 m

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    Lack of Bonding at Surface Interleaving on top surface of weld in 6092-17.5%SiCp

    H13 Welds CBN Welds

    250 m 250 m

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    Tool Wear Tool wear after FSW 6092-17.5%SiCp

    H13 tool after 6 feet of weld

    Loss on diameter of pin (essentially no threads left) Loss of radius on shoulder

    not feasible to produce significant length of weld

    CBN tool after 20 feet of weld

    No measurable wear on any features

    H13 tool CBN tool

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    Effects of Tool Wear Degradation of weld quality

    Surface of weld spallsPin wear affects penetration and stirring action

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    Typical region

    1 mm

    Steels

    100 mLarger magnification of trailing sideClose to the end of the weld

    1 mm

    Steels

    Fe

    Effects of Tool Wear Contamination of weld from tool debris

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    Super Abrasive FSW Tools Cubic Boron Nitride (CBN) and Poly-Crystalline

    Diamond (PCD) tools

    254 cm of FSW in 6061-25%B4

    C 170 cm of FSW in 6061-25%SiC

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    Summary FSW FSW can be used to join this material

    As-welded tensile strengths are considerably lower than parent

    material. Aging at 250F increases strength 20%at expense of ductility

    STA after welding results in strengths that are marginally

    higher than direct aging, and 20% lower than parent material

    Distribution and size of reinforcement is unaffected Due to severe tool wear, traditional tool steels can only be used for

    relatively short welds.

    CBN tool materials exhibited no wear in 20 (3 m) of weld in6092-17.5%SiC

    CBN tools give better surface finish, wider range of acceptableparameters, no weldment contamination, and better properties.