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© 2010, University of Delaware, all rights reserved INTRO TEMPERATURE MEASURMENT PROCESS DESCRIPTION ROLE OF FRICTION IN THE THERMAL DEVELOPMENT OF ULTRASONICALLY CONSOLIDATED CONTINUOUS FIBER REINFORCED METAL MATRIX COMPOSITE TAPE S. Koellhoffer (MSME), S. G. Advani, J. W. Gillespie, T. A. Bogetti (ARL) University of Delaware . Center for Composite Materials . Department of Mechanical Engineering THERMAL MODEL RESULTS & CONCLUSIONS MODEL VALIDATION ACKNOWLEDGEMENTS This work is supported by the army research laboratory through the composite materials research program Process Components Sonotrode Foils/Tapes Anvil Bonding Mechanisms Plastic Deformation Diffusion Clamping Force, F a Seats knurl pattern Brings material in contact Sonotrode Rotation, s Sonotrode Oscillation, λ Friction Removes asperities Oxide dispersal Heat generation Plastic deformation Ultrasonic consolidation has the ability to make metal matrix composite parts MMC’s offer exceptionally high stiffness and strength Low temperature welding process (10-30% T melt ) Underlying science is not well understood Lack of process maturity Bonding mechanisms are temperature dependent Need to quantify thermal development Infrared Camera Front mounted, 6° angle Temperature dependent ε Sampling Rate, 4 Hz Temp across width at nip point recorded Temperature contours can then be averaged Vertically avg T across width Horizontally avg T along length Temperature Variations Across Tape Width for each IR Image Friction coefficient determined empirically and validated experimentally Constant μ–μ constant , less accurate, easier to obtain Variable μ–μ RSM , depends on welder parameters Average Temperature Variation Across Tape Width IR FEA-μ RSM FEA-μ constant Ti-6Al-4V Horn MMC Tape AA 6061-T6 Substrate c wl f F q 2 T h, T T Fixed T at top and bottom boundaries Free convection on all edge boundaries Frictional heat flux applied at slip interface Temperatures measured across tape width at horn-tape nip point Temperature Predictions via FE model Constant µ → 15% Average Error Empirical, parameter dependent μ → 7% Average Error Trends in parameter dependent μ correlate to trends in literature Typical Experimental & Simulation Results horn IR image overlay Contour lines in red 3 2 1 3 2 1 F, λ, # of Cycles Friction Coefficient Experimental MMC Tape Trends Experimental Literature Trends

Role of Friction in the Thermal Development of Ultrasonically Consolidated Continuous Fiber Reinforced Metal Matrix Composite Tape

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Page 1: Role of Friction in the Thermal Development of Ultrasonically Consolidated Continuous Fiber Reinforced Metal Matrix Composite Tape

© 2010, University of Delaware, all rights reserved

INTRO TEMPERATURE MEASURMENTPROCESS DESCRIPTION

ROLE OF FRICTION IN THE THERMAL DEVELOPMENT OF ULTRASONICALLY

CONSOLIDATED CONTINUOUS FIBER REINFORCED METAL MATRIX COMPOSITE TAPE

S. Koellhoffer (MSME), S. G. Advani, J. W. Gillespie, T. A. Bogetti (ARL)

University of Delaware . Center for Composite Materials . Department of Mechanical Engineering

THERMAL MODEL RESULTS & CONCLUSIONSMODEL VALIDATION

ACKNOWLEDGEMENTS

This work is supported by the army

research laboratory through the

composite materials research program

Process Components

Sonotrode

Foils/Tapes

Anvil

Bonding Mechanisms

Plastic Deformation

Diffusion

Clamping Force, Fa

Seats knurl pattern

Brings material in contact

Sonotrode Rotation, s

Sonotrode Oscillation, λ Friction

Removes asperities

Oxide dispersal

Heat generation

Plastic deformation

Ultrasonic consolidation has the ability to make

metal matrix composite parts

MMC’s offer exceptionally high stiffness and

strength

Low temperature welding process (10-30% Tmelt)

Underlying science is not well understood

Lack of process maturity

Bonding mechanisms are temperature dependent

Need to quantify thermal development

Infrared Camera Front mounted, 6° angle

Temperature dependent ε

Sampling Rate, 4 Hz Temp across width at nip point

recorded Temperature contours can then

be averaged Vertically – avg T across width

Horizontally – avg T along length

Temperature Variations Across

Tape Width for each IR Image

Friction coefficient determined empirically and validated experimentally Constant μ – μconstant, less accurate, easier to obtain

Variable μ – μRSM, depends on welder parameters

Average Temperature Variation

Across Tape Width

IR FEA-µRSM FEA-µconstant

Ti-6Al-4V Horn

MMC Tape

AA 6061-T6 Substratecwl

fFq

2

Th,

T

T

Fixed T at top and bottom boundaries

Free convection on all edge boundaries

Frictional heat flux applied at slip interface

Temperatures measured across tape width at horn-tape nip point

Temperature Predictions via FE modelConstant µ → 15% Average Error

Empirical, parameter dependent µ

→ 7% Average Error

Trends in parameter dependent µ correlate to trends in literature

Typical Experimental & Simulation Results

horn

IR image overlay

Contour lines in red

3

2

1321

F, λ, # of Cycles

Fri

cti

on

Co

eff

icie

nt

Experim

enta

l M

MC

Tape T

rends

Experim

enta

l

Litera

ture

Tre

nds