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Nanocomposite coating materials offer strength toughness based on a combination of:

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D.O.F x,y = 0. N C S TATE U N I V ERS I TY. Background. Objectives. Results. Conclusions ... Nanocomposite coating materials offer strength toughness based on ... – PowerPoint PPT presentation

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Title: Nanocomposite coating materials offer strength toughness based on a combination of:


1
RVE (Representative Volume Element)
N C S TATE U N I V ERS I TY
Micromechanical Modeling of Nanotribological
Failure of Crystalline-Amorphous Nanocomposites
in Extreme Environments J. D. Pearson, W. M.
Ashmawi, and M.A. Zikry North Carolina State
University
Results
Computational Approach
Background
Case II 40 Au
Case III 40 DLC
  • Nanocomposite coating materials offer strength
    toughness based on a combination of
  • Crystalline phases
  • Amorphous phases
  • Extreme changes in
  • Temperature
  • Strain Rate
  • Environment
  • Require one system over ranges
  • Optimal Coating design
  • - Low coefficient of friction - Low wear rate
  • Finite Element Thermal and Mechanical model
    commensurate with prediction of failure
  • Brittle
  • Ductile
  • Material wear and failure criterion in Au and
    MoS2 phases
  • Gold material treated as J2 plasticity with
    kinematic hardening
  • YSZ, DLC, MoS2 elastic
  • Quasi-static, Contact elements, Periodic B.C.,
    Thermal and Mechanical loadings
  • Homogenized modulus, Aggregate model
  • Random material distributions
  • Equal size of each material in each distribution

Uniform Pressure
Case I 25 All Materials
ROM (Rule of Mixtures)
Uniform Pressure
Challenge
Horizontal Displacement
For an optimal coating How and What to combine?
6.8E-7
5.3E-7
3.8E-7
2.3E-7
0.8E-7
6.1E-7
4.6E-7
3.0E-7
1.5E-7
0
Element Wear and Failure
  • D.O.F x,y 0
  • Periodic BC

DLC
YSZ
GOLD
MoS2
  • Plastic deformation in Au and MoS2 at free
    surface based on above criterion after indentor
    travel across and return
  • Grain Size
  • Grain Spacing
  • Concentration Gradients
  • Residual Stress Effects
  • Thermal Annealing
  • Deposition conditions
  • Crystalline
  • Amorphous
  • Constituent Elements (Gold, Carbon, MoS2,
    ZrO2-Y2O3)
  • Tungsten, Titanium
  • Carbides, Nitrides, Oxides
  • HDLC

COATING MODEL - MECHANICAL
Case III 40 DLC
Case II 40 Au
Formation of Transfer film from
elements exceeding yield criterion
Steel
Case i Aggregate
MoS2
Case IIIi
Case IIi
YSZ
Case iiDistributed
GOLD
Case Ii
Case Iii
Case IIIii
Case IIii
DLC
  • Sliding indentation of Rigid indentor
  • Travel across and return over surface at 1m/s
    with linear increase until final indentation of
    .0012 m
  • Random distribution of material into identical
    grain size and spacing (i) or varying grain size
    and spacing (ii)
  • Large gradientsbetween grains
  • Maximum stressdependant upon material beneath
    indentor

Objectives
-.51E6
-.141E9
-.11E9
-.71E8
-.36E8
-.12E9
-.89E8
-.53E8
-.18E8
.17E8
  • Major Goal
  • Determine metal alloy coating response with known
    composition and microstructure under
  • ? Temperature ? Atmosphere/Humidity
  • ? Pressure ? Strain Rate
  • Understand wear mechanisms and failure modes
    inherent to each coating based on composition and
    loading
  • Simulate and predict wear and friction
    coefficients
  • Model both microstructure composition
    corresponding changes (chameleon adaptive
    behavior) with environment
  • At Low Temp, In Vacuum or Dry Air, MoS2 changes
    from amorphous to hexagonal
  • At Low Temp, In Humid Air, Diamond Like Carbon
    (DLC matrix, sp3) changes from Graphite Like
    (sp2)
  • At High Temp, Amorphous/poorly crystalline gold
    on the surface

Conclusions
  • Crystalline and ductile phases needed for
    toughness
  • Distributions can be optimized by grading the
    material through determining effective local
    properties
  • Design guidelines can be tailored for optimized
    coating behavior
  • ROM consistently estimates a higher homogenized
    modulus compared to FEA RVE
  • Large gradients in stress between different
    materials
  • Thermal strains and residual stresses have a
    significant role on coating behavior under
    loading
  • GB sliding and GB deformations need to be
    delineated for ductile phases

-.33E9
-.26E9
-.18E9
-.10E9
-.27E8
-.30E9
-.22E9
-.14E9
-.65E8
.11E8
COATING MODEL - THERMAL
Effective Stress, ?Eff , under 0.0006 m final
indentation
Case I i
Case II i
Case III i
Case III ii
Case I ii
Case II ii
0 lt ? lt .5 Mpa
5 lt ? lt 10
60 lt ? lt 119
263 lt ? lt 307
.5 lt ? lt 5
10 lt ? lt 60
119 lt ? lt 263
307 lt ? lt 351
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