Coligan_XX_XX_P

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Examination of Material Flow in

    FSW of Aluminum Using Stop-Action Techniques

    Kevin Colligan

    Concurrent Technologies Corporation

    Johnstown, PA - USA

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Acknowledgements

    This work was funded by:

    The Boeing Company [1,2],

    andConcurrent Technologies Corporation (CTC )

    and the National Center for Excellence in

    Metalworking Technologies (NCEMT),

    operated by CTC [3].

    1 - Colligan, K. “Dynamic Material Deformation During Friction Stir Welding of 

     Aluminum,” 1st International Symposium on Friction Stir Welding, Thousand Oaks,

    California, June 1999.

    2 - Colligan, K, “Material Flow Behavior During Friction Stir Welding of Aluminum,”

    Welding Journal, July 1999.

    3 - Colligan, K. and Chopra, S., “Examination of Material Flow in Friction Stir Welding of 

     Aluminum Using a Stop Action Technique,” 5th International Symposium on Friction Stir 

    Welding, Metz, France, September 2004.

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    3

    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Agenda

    Introduction

    Stop Action for Cylindrical, Threaded Pins [1,2]

    Stop Action for Frustum Pins with Reentrant

    Features [3]

    Conclusions

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Introduction -

    Motivation for Material Flow Studies

    Knowledge of material flow is useful for:

     – understanding weld formation

     – diagnosing defects

     – predicting the effect of tool design changes

    Modeling has given good insight, but

    model verification can be difficult Experimental methods must be

    developed to verify models

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Introduction

    Flow visualization in FSW based on:

     – Stop Action (Colligan, Guerra, McClure, Dickerson)

     – Embedded Tracers (Colligan, Reynolds, Seidel,London, Ouyang)

    Must be repeated as tool designs evolve

    New methods needed for new tools & materials

     – tools with reentrant features

     – high-temperature FSW of steel, titanium, etc.

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Stop Action Technique - Rapid Retraction

    Welds made on Mazak 3-axis mill

     – Rigid frame

     – Rapid axis acceleration

     – 6.4mm 6061-T6 workpiece mounted at 3° tilt angle

     – Threaded pin with no reentrant features

    At end of weld, tool retracted at rate to “unscrew”

    tool from keyhole, leaving keyhole intactShoulder Profile 7° cup, smooth

    Shoulder Diameter, mm 5

    Shoulder Material H13Pin Profile threaded, cylindrical

    Pin Diameter, mm 6.4

    Pin Length, mm 6.4Pin Material WC

    Number of Flats 0

    Spindle Speed, rev/min 1,540

    Travel Speed, mm/min 216

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Pin Design - Conventional Threaded Pin

    WC pin, ground with thread forms

    1mm pitch, 6.4mm diameter, 6mm long

    Shank ground concentric to pin

    Collet used to hold tool

    Shank ground

    concentric to pin

    Surrogate pin used

    to hold tool during

    grinding

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Post-Weld Procedures

    Photograph intact keyhole using light microscope

    Section keyhole and inspect interior wall using SEM

    Section keyhole and inspect section surface using

    light microscope

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    LT Section View of Keyhole

    Upper leading edge - material curling into thread spaces

    Lower leading edge - material in filled thread spaces rotates with

    pin Upper trailing edge - void behind pin

    Lower trailing edge - material in filled thread spaces smeared

    against keyhole wall

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Section View of Keyhole - rear wall LT section

    Rear wall section shows

    origin of “onion ring”

    pattern Material in filled threads

    smeared against lower 

    rear portion of keyhole

    Material deposited at

    bottom of keyhole causes

    material from above to

    rise to fill void from upper portion of the keyhole

    Tool Motion

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Section View of Rear Keyhole -

    higher magnification view

    Thread-formed material shows

    accumulation in thread space

    on successive rotations?

     – Etching contrast based on

    variations in base plate chemistry?

     – More inhomogeneity in lower 

    threads than in upper 

     – Etch contrast preserved in stir 

    zone macrostructure

     – Change in vertical velocity

    (rotation speed) of material in

    thread spaces?

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Intact Keyhole -

    view looking down into keyhole

    Partially filled thread space

    Filled thread rotates with

    pin at some intermediate

    speed

    Leading edge of 

    keyhole, LT

    section view Welded at 1540 rev/min, 610 mm/min

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Keyhole Interior Rear Wall -

    SEM image of material from thread space

    Suggests deposition of 

    material on keyhole

    wall by smearing

    action Suggests vertical

    motion caused by

    intermediate rotation

    speed

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Plastic Deformation Processes -

    Cylindrical Threaded Pin

    Curling of material into thread spaces (upper leading edge of keyhole)

    Rotation of material in filled thread spaces at intermediate

    speed, combined with vertical motion (lower leading edge of 

    keyhole) Deposition of material by “smearing” action (rear of keyhole)

    Deposition of material at bottom of pin, causing bulk of SZ

    material to rise as shoulder passes

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Stop-Action Technique -

    Frustum Pin w/ Reentrant Features - Rapid Stop

    Perform bead-on-plate weld, 25.4mm 2195 Al-Li

    Engage emergency stop control

    Pour tap water on plate until cool

    Remove shoulder piece Section through pin

    Shoulder Profile flat shoulder with scrolls

    Shoulder Diameter, mm 30.5Shoulder Material H13

    Pin Profile threaded frustum with flats

    Pin Root/Tip Diameters,mm

    15.2/8.9

    Pin Length, mm 24.6

    Pin Material MP159

    Number of Flats 3

    Spindle Speed, rev/min 220

    Travel Speed, mm/min 102

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for 

    public release; distribution is unlimited.

    Sectioning Procedure

    End of weld was cut to 50mmsquare sample

    Sample was then sectioned using

    wire-EDM

    SEM and light microscopes usedto study the keyhole wall

    G-1G-2

    G-3

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for public release; distribution is unlimited.

    Keyhole Interior Inspection

    Inspection by light microscope

    Inspection by SEM

    Optical micrograph, specimen G3

    Pin rotation

    Trailing edge of flat

    Leading edge of flat

    G-1G-2

    G-3

    G3

    Optical micrograph, specimen F2

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for public release; distribution is unlimited.

    SEM Micrographs from G1 & G2

    Generally replicates pin surface

    Small voids observed between thread-shaped

    features

    G-1G-2

    G-3

    G2 G1

    Specimen G1

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for public release; distribution is unlimited.

    SEM Micrograph from G3

    Less material carried in flat space than in G1 or G2 Thread-shaped material retains shape further into

    flat space

    Tool motionG-1G-2

    G-3

    G3

    Arrows indicate edge of tool flat

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for public release; distribution is unlimited.

    Plastic Deformation Processes -

    Frustum Pins with Reentrant Features

    4 plastic deformation processes proposed for 

    this type of tool:

     – crushing and consolidation of thread-shaped material in

    the flat space

     – extrusion of material from flat space into next thread

    space

     – downward shear of material in thread spaces relative to

    surrounding material

     – shear of material in flat space relative to surrounding

    material

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    This work was prepared by the National Center for Excellence in Metalworking Technology,

    operated by Concurrent Technologies Corporation (CTC), under Contract No. N00014-00-C-0544 to the Office of Naval Research as part of the Navy ManTech Program. Approved for public release; distribution is unlimited.

    Conclusions

    Threaded tools with reentrant features produce

    different stir zone appearance, implying different

    material flow

    Stop-action techniques can yield insight into the

    inner-workings of the FSW process

    Different plastic deformation processes proposedfor two tool design classes