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Mechanical Stimulation of Gasless Reaction
in Inorganic Systems: overview
Alexander S. Mukasyan
Department of Chemical and Biomolecular Engineering, University of Notre Dame, USA
Outline
• Systems under investigation
• Developed Methods and Diagnostics
 High-Energy Ball Milling (HEBM)
 3D reconstructions: S&V/X-ray Tomography
 In-situ TEM Diffusion
 High-Temperature Kinetics (ETA)
• Fundamental Results: Solid Flame
• Discovery system
 Cubic BN
 Reaction Mechanism
 Recent Results
• Fundamental Results: Mechanically induced Reactions
• Conclusions
Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM)
2
 Time-resolved X-Ray Diffraction (TRXRD)
Types of transformations in the inorganic
substance under shock compression
Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM)
3
1. Powder Compaction
2. Decomposition of
inorganic chemical compounds
3. Defects Formation
4. Phase transformation
5. Shock Reaction Synthesis (SRS)
Systems Under Investigation
• Class of non-catalytic self-sustaining chemical reactions, which does not require oxygen and any other gas-
phase reactants, so-called gasless reactive systems. It is more important that while significant heat is
released during the reactions in such a system, the main product is a valuable solid-state material.
4
Combustion
products (solid)
Combustion
Zone (solid)
Initial
reagents
(solid)
Thermal
Initiation
Mechanical
Stimulation
Solid State, Gasless Exchange Reaction
Adiabatic Combustion Temperature:
Tad = 1895 K
Tad << Tmelting (TiN, B, TiB2, BN)
TiN + 3B → BN + TiB2+ Q (85 kJ/mole)
Examples:
Ni + Al → NiAl + Q (117 kJ/mole)
Gasless Reaction
Adiabatic Combustion Temperature:
Tad = 1911 K
Tad = Tmelting (NiAl)
Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM)
Chemical Reactions and Shock Wave:
early studies
Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 5
Systems Method Conclusion Publication/Year
Ti + C, W + C, Al+ C Recovery From mixture of Ti and Carbon powders
TiC
Y. Horiguchi, and Y. Nomura, 1963
Bull. Chem. Soc. Jap., 36, 486
Cr + S; Cr + Se; Cr + Te Recovery Fabricated CrS had much lower densities
than the ordinary modification;
S. S. Batsanov, 1967
Inzh.-Fiz. Z., 12, 104-119
Al + Cu (3:1) Analysis of Shock adiabat Possible rapid massexchange in shock
wave
O.N. Breusov, 1977
Proc. IV All-Union Symp. Combust. Explos. 61–72
Al + Ni (1:3.5) Recovery XRD analysis: AlNi3 phase; reaction
initiation at hot regions
Y. Horie, R.A. Graham, I.K. Simonsen, 1985
Mater. Lett. 3 354–359
Sn + S Analysis of Shock adiabat Possible rapid mass exchange in SW due
to the difference in the mass velocities
S.S. Batsanov, et.al., 1986
Comb. Expl. Shock. Wave 22, 765–768
Nb + Liquid N2
Nb + Liquid CO2
Recovery XRD analysis: NbN; NbC G.A. Adadurov, 1986
Russ. Chem. Rev. 55 282–296
Al + Ni; Al + Ti Recovery. Modelling Yield depends on pressure : Ni3Al, NiAl,
sol-sol
R.A. Graham, et. al., 1986
Book: Shock Waves Condens. Matter, Springer. Boston, MA, 693–711
Ti + B; Nb + B Recovery. Modelling XRD and SEM: TiB2; NbB2; NbB H. A. Grebe, A. Advani, N. N. Thadhani, 1991
AIP Conference Proceedings 231, 501
Ti – Si; Nb - Si Recovery XRD: Ti5Si3; NiSI in air NOT in argon B.R. Kruger, A.H. Mutz, T. Vreeland Jr. 1992
Metall. Trans. 23A, 55–58
Al + Ni (1:2.6) Time-pressure profile.
Recovery:
EDS; AlNi3; reaction may occur in the
100 ns wide shock front
L.S. Bennett, et al., 1992
Appl. Phys. Lett. 61, 520–521
Al + Ni (1:3) Recovery. Modelling Influence of particle size and
morphology
N.N. Thadhani, et. al., 1992,
J. Mater. Res. 7, 1063–1075.
Experimental Configurations for SRS
6Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM)
Schematic diagram of the compression of a
substance in a cylindrical tube; 1)
metallic tube; 2) test substance; 3) and 4)
regions of single compression behind the
front of the incident and head SW; 5)
region of double compression behind the
front of the incident and reflected SW. The
dashed lines indicate the initial positions of
the explosive, the tube, and the specimen.
Schematic of the
Asay shear impact test
Standard shock synthesis equipment with plane
wave apparatus and the combination of different
steels for the sample recovery capsule which
avoids shock wave reflections from the top of the
sample holder piston along the release path.
Diagnostics
Hugoniot curves for various substances and
the corresponding shock-wave profiles
1) without transformations (Tr); 2) Tr with
increase in volume; 3) Tr with decrease in
volume; a) pressure profile in the shock wave
in the absence of Tr; b) Tr with increase in
volume; c) Tr with decrease in volume; d) Tr
with decrease in volume at sufficiently high
pressures.
Rankine - Hugoniot
Relationships
Schematic illustrating (a) P-V and (b) P-
Up Hugoniot curves for solid and porous
materials. Curves O'BA' and O'CA' are
for typical metal and ceramic powders
and Curve OA is for solid density
material.
Recover Capsule
Followed by product structural
characterization: XRD, SEM, TEM, EDS etc
Detecting:
(a) Phase transformation: evidence of
the reaction initiation by SW
(b) Synthesis of non-equilibrium phase:
evidence of the reaction occurring in SW
Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 7
Diagnostics
High-Speed
Micro Video Recording
Time-resolved
Temperature
Measurements
X-ray scattering (SAXS) and
Time-Resolved X-Ray diffraction
of synchrotron radiation
Time resolution 1 ns
Time resolution 1 msTime resolution 1 GHz
Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 8
Diagnostics
Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 8
Dana D. Dlott, Cite as: AIP Conference Proceedings 1793, 020001 (2017)
Shock Compression Dynamics Under a Microscope
Conceptual Mechanistic Model
The schematics of the conceptual model showing
the progress of the synthesis in three stages; the
initial configuration, the transition zone, and the
final compressed configuration, where the critical
region in the synthesis event takes place in the
transition zone
Graham
Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 9
CONMAH: CONfiguration change, Mixing, Activation, and Heating).
SRS Mechanisms
Roller Mechanism:
Shear Stress Plastic Flow
Two layers of the substance are displaced relative to
one another, the nuclei of phase A, located between
them, can be regarded as a kind of roller about which
oscillations are executed. Atoms which are passing in
the immediate vicinity of the nucleus have sufficient
time to combine with the latter forming the new
phase. Thus in contrast to the usual diffusional
growth of crystallization centers, in which each atom
must find its way to the new phase, pushing apart its
neighbors by virtue of the energy of thermal motion,
the formation of the new phase during shock
compression occurs by transport of the entire mass of
the initial phase, by plastic flow.
Supersonic martensitic (MT)
type of reaction waves
MT is a specific variant of the realization of
a polymorphic transformation associated
with a cooperative mechanism of atomic
displacements MT transition occurs upon
a significant deviation from the point of
equilibrium of the phases in an active
medium capable of liberating energy.
Nanoscale mechanisms of phase
Nucleation at plastic-strain-induced
defects.
Mechanically induced
Thermal Explosion
. The shock wave provides an ignition
source at localization centers (for
example, pore collapse). Such
phenomenon has been described as a
virtual combustion wave and is typical
of thermal explosions. The actions of
the stress wave on the material,
through pore collapse and plastic
deformation, heat and mix the material
until the requirements for reaction
initiation are met.
Ultra-fast Force
diffusion
The fluid-dynamic model of
ultrafast (forced) diffusion caused
by a difference in the particle
velocity of the components
in shock-compressed matter
Complete intermixing of particles
is achieved owing to penetration
of rapidly moving particles into
slowly moving particles.
Dremin, Breusov Batsanov Jette, Goroshin, ReevesAl'tshuler
Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 10
Chemical Reactions and Shock Wave: Ni-Al System
Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 5
Systems Method Conclusion Publication/Year
Al + Ni (1:3.5) Recovery XRD analysis: AlNi3 phase; reaction
initiation at hot regions
Horie Y., R. Graham, I.Simonsen, 1985
Mater. Lett. 3 354–359
Al + Ni (3:1) Analysis of Shock adiabat Influence of particle morphology Song, I. and N. Thadhani, 1992
Met. Trans. A, 23(1), 41-48
Al + Ni (3:1; 1:1;1:3) Recovery the chemical reactions in this system
are promoted by increased volume of Ni
Dunbar, E., N. Thadhani, R. Graham, 1993
Mater. Sci., 28, 2903-2914.
Al + Ni (1:2.6) Monitoring pressure The excess pressure is best explained as
an indicator of a fast exothermic
reaction during the shock loading.
Bennett, L., F. Sorrell, et al. 1992
Appl. Phys. Lett., 61(5), 520-521
Al + Ni (1:2.6) Monitoring pressure The excess pressure is best explained as
an indicator of a fast exothermic
reaction during the shock loading
Yang Y. et al. 1997
Appl. Phys. Lett., 70(25), 3365-3367
Al + Ni (1:1 volume) The Hugoniot
measurement
Influence of morphology; melting and
dissolution for spherical Ni; Shock
induced for Ni-flakes
Eakins, D.; Thadhani, N, 2006
J. Appl. Phys., 100, 113521
Al + Ni (1:1 volume) Recovery. Modelling Shock densification for different
morphologies
Eakins, D.; Thadhani, N., 2008
Appl. Phys. Lett. 2008, 92, 111903.
Al + Ni laminate Recovery Laser Shock Compression Wei C. et al., 2009
AIP Conference Proceedings 1195, 305
Al + Ni (1:1)
HEBM
High-speed video
recording, recovery
Asay Shaer impact test Reeves R. et al., 2010
J. Phys. Chem. C 2010, 114, 14772–14780
Chemical Reactions and Shock Wave: Ni-Al System
Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 5
Systems Method Conclusion Publication/Year
Al + Ni (1:1) Time-pressure profile.
Recovery:
Laser Shock Compression
Melting-dissolution mechanism
Wei C. et al., 2011
Acta Materialia 59 (2011) 5276–5287
Al + Ni (1:1) Recovery. Modelling Configuration effect Specht P., N. Thadhani, T. Weihs, 2012
JJOURNAL OF APPLIED PHYSICS 111, 073527
Al + Ni (1:1) Time-pressure profile.
Recovery:
Laser Shock Compression
Ni/Al laminates
Wei C. et al., 2012
Acta Materialia 60 3929–3942
Al + Ni (1:1)
HEBM
High-speed video
recording, recovery
Asay Shear impact test
Mechanically induced Explosion
Reeves R. et al., 2013
Propellants Explos. Pyrotech. 38, 611 – 621
Al + Ni (1:1) Pressure-time analysis Influence of additives, Cu, PTRE Wei. X et al., 2015
Journal of Alloys and Compounds 648, 540-549
Al + Ni (1:1) The Hugoniot
measurement and
modelling
Multilayered nano foils Kelly S. Thadhani, N, 2016
JOURNAL OF APPLIED PHYSICS 119, 095903
Al + Ni
laminate
The Hugoniot
measurement and
modelling
Shock densification for different
morphologies
Specht P., et,al 2017
JOURNAL OF APPLIED PHYSICS 121, 015110
Al + Ni (1:1) High-speed video
recording, recovery
Asay Shear impact test, role of fracture Beason M. , et al., 2017
Acta Materialia 133, 247-257
Al + Ni (2:1)
HEBM and nano foils
Time-pressure profile.
Recovery, modelling
Asay type of experiment
Influence of additives: oxides
Kerong R. et al., 2019
Metals 2019, 9, 499
SSR in Gasless Reaction in Ni + Al System:
Real time Studies
Schematic of Asay shear impact test. Figure (A)
shows the windowed sample holder Fig. (B) shows
the plunger and sample with the retaining plates
removed.
Gas gun constructed at Purdue University.
This gun has a 25.4 mm bore, 4.6 m barrel,
and has accelerated a 26 g projectile to 1 km/s
Shock Initiated Reaction: Ni + Al System
Sequence of images high speed video images from shear impact test
in nano-mixture exhibiting reaction
(impact velocity ~250m/s average combustion front velocity ~10cm/s).
Shock Induced Thermal Explosion Ni + Al System
Sequence of images high speed video images from shear impact test in nano-mixture
(the impact velocity ~1070 m/s average combustion front velocity ~1000 m/s)
Shock Induced Reaction in TiN- B System
XRD results for thermally and
mechanically initiated reactions
Mechanical InitiationThermal Initiation
(a)
(b) (c)
(a)Mechanically-induced
composite TiN/B (dark
phase – B; light phase TiN)
(b)Product of thermal initiation
of TiN/B (dark phase – BN;
light phase TiB2/TiN)
(c)Product of mechanical
initiation of TiN/B (dark
phase – B; light phase –
TiB2/TiN)
Initial Composite
Thermal Initiation Mechanical Initiation
1
TEM: c-BN Formation
(a) TEM images of typical particles formed in the
Ti-B-N system after shock. Relatively large
TiB2 and h-BN crystallites are dominant within
the field of view. The inset shows a magnified
TEM image of the surface area of the large
TiB2 crystallite (70–100 nm in diameter) that
has a layer of the c-BN phase.
(b) Magnified area of the c-BN crystal phase at
the interface with the TiB2 crystalline particle.
Intensity distribution on the magnified fragment of the HRTEM image of the c-BN phase in vertical (a) and
horizontal (b) directions showing that d-spacing in both directions are close to 0.18 nm.
1
Intensity
Intensity
Y, nm X, nm
Proposed Reaction Mechanism
TEM & SEM results revealed the formation of a nano-mixture of B and TiN surrounding unreacted B crystals.
Select Area Diffraction (SAD) patterns, EDS, and High Resolution TEM analysis of structural transformations
allow the suggestion of a simple two-step mechanism for reaction of TiN/3B. First, formation of TiB2 from the
finely mixed regions of TiN/B, followed by production of the BN phase.
1
Initial Quenched Thermally Initiated Shock Initiated
J. Physical Chemistry C, 123 (17) 11273-11283 (2019)
A mechanism for the
structural transformation
occurring at the boundary
between initially unreacted
B and TiN phases is
suggested based on
experimental observations
In the case of thermally
initiated reaction, near-
complete conversion to
product is observed. This
is likely due to prolonged
exposure to high
temperature conditions
For the shock-initiated
reaction, some micron
scale Boron crystals remain
unreacted and surrounded
by TiN. The short time
scales during which
conditions suitable for
reaction persist limit the
degree of conversion
B B
TiN/B
TiN
TiB2
BN
B
TiN/B/TiB2
TiB2
BN
Structural Transformations: HEBM TiN/3B
2
TEM TiB2 d-spacing (100) 2.62Å
B
B
Reaction
Layers
1 nm
2.60Å 2.60Å
TiB2
SEM Cross-section
Reaction
Layers
B
B
BN
TiB2
Shock-initiated - TEMQuenched Reaction -
TEM
15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90
0
200
400
600
800
1000
1200
1400
Intensity(counts)
2 Theta (degrees)
43.36o
50.53o
Shock-induced Synthesis:
B-GaN System
2
Solid Flame
Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM)
2
5
A B
AB
d
D
𝒓 =
𝟏
𝜹
𝑭(𝑻, 𝜼)
𝒊𝒇 𝜹 = 𝟎 ↔ 𝒓 = ∞
𝒓 =
𝟏
𝜹 + 𝜹 𝟎
𝑭(𝑻, 𝜼)
𝒍𝒆𝒕 𝒖𝒔 𝒎𝒂𝒌𝒆 𝚫~𝜹 𝟎
𝒘𝒆 𝒎𝒂𝒚 𝒆𝒙𝒑𝒆𝒄𝒕 𝜼 = 𝟏 𝒕𝒉𝒓𝒐𝒖𝒈𝒉 𝒓𝒂𝒑𝒊𝒅
𝒈𝒓𝒂𝒊𝒏 𝒃𝒐𝒏𝒅𝒂𝒓𝒚 𝒅𝒊𝒇𝒇𝒖𝒔𝒊𝒐𝒏
𝑫𝒍𝒊𝒒𝒖𝒊𝒅 = 𝟏𝟎−𝟓
𝒄𝒎 𝟐
𝒔
𝑫 𝒔𝒐𝒍𝒊𝒅 = 𝟏𝟎−𝟗
𝒄𝒎 𝟐
𝒔
𝑫 𝒈𝒓𝒂𝒊𝒏 𝒃𝒐𝒖𝒏𝒅𝒂𝒓𝒚 = 𝟏𝟎−𝟓 − 𝟏𝟎−𝟔
𝒄𝒎 𝟐
𝒔
Conclusions
 Ultra-fast (0.1–5 ms) shock-induced reactions occurred in
the 3B-TiN system
 The results illustrate the possibility of rapid reactions
occurring in the solid state on incredibly short timescales.
 This process may provide a unique route for the discovery
and fabrication of advanced compounds.
 Fundamental questions to be resolved :
 What is the mechanism for ultra fast solid-state reactions under
the shock wave conditions?
 Can other metastable phases be produced under unique CS
conditions?
2
Final Remarks
A long list of fundamental questions
remain re the physical nature of the
heterogeneous self-sustained reactions
Breakthrough hybrid concepts involving
self-sustained reactions make combustion
synthesis method extremely promising
specifically for fabrication of high
temperature and ultra high temperature
ceramics
2
ACKNOWLEDGMENTS
 This work was supported by the Department of Energy, National Nuclear Security Administration , under
the Award No. DE- NA0 0 02377 as part of the Predictive Science Academic Alliance Program II.
24Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM)

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Aps mukasyan final: Mechanical Stimulation of Gasless Reaction in Inorganic Systems: overview

  • 1. Mechanical Stimulation of Gasless Reaction in Inorganic Systems: overview Alexander S. Mukasyan Department of Chemical and Biomolecular Engineering, University of Notre Dame, USA
  • 2. Outline • Systems under investigation • Developed Methods and Diagnostics  High-Energy Ball Milling (HEBM)  3D reconstructions: S&V/X-ray Tomography  In-situ TEM Diffusion  High-Temperature Kinetics (ETA) • Fundamental Results: Solid Flame • Discovery system  Cubic BN  Reaction Mechanism  Recent Results • Fundamental Results: Mechanically induced Reactions • Conclusions Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 2  Time-resolved X-Ray Diffraction (TRXRD)
  • 3. Types of transformations in the inorganic substance under shock compression Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 3 1. Powder Compaction 2. Decomposition of inorganic chemical compounds 3. Defects Formation 4. Phase transformation 5. Shock Reaction Synthesis (SRS)
  • 4. Systems Under Investigation • Class of non-catalytic self-sustaining chemical reactions, which does not require oxygen and any other gas- phase reactants, so-called gasless reactive systems. It is more important that while significant heat is released during the reactions in such a system, the main product is a valuable solid-state material. 4 Combustion products (solid) Combustion Zone (solid) Initial reagents (solid) Thermal Initiation Mechanical Stimulation Solid State, Gasless Exchange Reaction Adiabatic Combustion Temperature: Tad = 1895 K Tad << Tmelting (TiN, B, TiB2, BN) TiN + 3B → BN + TiB2+ Q (85 kJ/mole) Examples: Ni + Al → NiAl + Q (117 kJ/mole) Gasless Reaction Adiabatic Combustion Temperature: Tad = 1911 K Tad = Tmelting (NiAl) Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM)
  • 5. Chemical Reactions and Shock Wave: early studies Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 5 Systems Method Conclusion Publication/Year Ti + C, W + C, Al+ C Recovery From mixture of Ti and Carbon powders TiC Y. Horiguchi, and Y. Nomura, 1963 Bull. Chem. Soc. Jap., 36, 486 Cr + S; Cr + Se; Cr + Te Recovery Fabricated CrS had much lower densities than the ordinary modification; S. S. Batsanov, 1967 Inzh.-Fiz. Z., 12, 104-119 Al + Cu (3:1) Analysis of Shock adiabat Possible rapid massexchange in shock wave O.N. Breusov, 1977 Proc. IV All-Union Symp. Combust. Explos. 61–72 Al + Ni (1:3.5) Recovery XRD analysis: AlNi3 phase; reaction initiation at hot regions Y. Horie, R.A. Graham, I.K. Simonsen, 1985 Mater. Lett. 3 354–359 Sn + S Analysis of Shock adiabat Possible rapid mass exchange in SW due to the difference in the mass velocities S.S. Batsanov, et.al., 1986 Comb. Expl. Shock. Wave 22, 765–768 Nb + Liquid N2 Nb + Liquid CO2 Recovery XRD analysis: NbN; NbC G.A. Adadurov, 1986 Russ. Chem. Rev. 55 282–296 Al + Ni; Al + Ti Recovery. Modelling Yield depends on pressure : Ni3Al, NiAl, sol-sol R.A. Graham, et. al., 1986 Book: Shock Waves Condens. Matter, Springer. Boston, MA, 693–711 Ti + B; Nb + B Recovery. Modelling XRD and SEM: TiB2; NbB2; NbB H. A. Grebe, A. Advani, N. N. Thadhani, 1991 AIP Conference Proceedings 231, 501 Ti – Si; Nb - Si Recovery XRD: Ti5Si3; NiSI in air NOT in argon B.R. Kruger, A.H. Mutz, T. Vreeland Jr. 1992 Metall. Trans. 23A, 55–58 Al + Ni (1:2.6) Time-pressure profile. Recovery: EDS; AlNi3; reaction may occur in the 100 ns wide shock front L.S. Bennett, et al., 1992 Appl. Phys. Lett. 61, 520–521 Al + Ni (1:3) Recovery. Modelling Influence of particle size and morphology N.N. Thadhani, et. al., 1992, J. Mater. Res. 7, 1063–1075.
  • 6. Experimental Configurations for SRS 6Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) Schematic diagram of the compression of a substance in a cylindrical tube; 1) metallic tube; 2) test substance; 3) and 4) regions of single compression behind the front of the incident and head SW; 5) region of double compression behind the front of the incident and reflected SW. The dashed lines indicate the initial positions of the explosive, the tube, and the specimen. Schematic of the Asay shear impact test Standard shock synthesis equipment with plane wave apparatus and the combination of different steels for the sample recovery capsule which avoids shock wave reflections from the top of the sample holder piston along the release path.
  • 7. Diagnostics Hugoniot curves for various substances and the corresponding shock-wave profiles 1) without transformations (Tr); 2) Tr with increase in volume; 3) Tr with decrease in volume; a) pressure profile in the shock wave in the absence of Tr; b) Tr with increase in volume; c) Tr with decrease in volume; d) Tr with decrease in volume at sufficiently high pressures. Rankine - Hugoniot Relationships Schematic illustrating (a) P-V and (b) P- Up Hugoniot curves for solid and porous materials. Curves O'BA' and O'CA' are for typical metal and ceramic powders and Curve OA is for solid density material. Recover Capsule Followed by product structural characterization: XRD, SEM, TEM, EDS etc Detecting: (a) Phase transformation: evidence of the reaction initiation by SW (b) Synthesis of non-equilibrium phase: evidence of the reaction occurring in SW Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 7
  • 8. Diagnostics High-Speed Micro Video Recording Time-resolved Temperature Measurements X-ray scattering (SAXS) and Time-Resolved X-Ray diffraction of synchrotron radiation Time resolution 1 ns Time resolution 1 msTime resolution 1 GHz Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 8
  • 9. Diagnostics Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 8 Dana D. Dlott, Cite as: AIP Conference Proceedings 1793, 020001 (2017) Shock Compression Dynamics Under a Microscope
  • 10. Conceptual Mechanistic Model The schematics of the conceptual model showing the progress of the synthesis in three stages; the initial configuration, the transition zone, and the final compressed configuration, where the critical region in the synthesis event takes place in the transition zone Graham Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 9 CONMAH: CONfiguration change, Mixing, Activation, and Heating).
  • 11. SRS Mechanisms Roller Mechanism: Shear Stress Plastic Flow Two layers of the substance are displaced relative to one another, the nuclei of phase A, located between them, can be regarded as a kind of roller about which oscillations are executed. Atoms which are passing in the immediate vicinity of the nucleus have sufficient time to combine with the latter forming the new phase. Thus in contrast to the usual diffusional growth of crystallization centers, in which each atom must find its way to the new phase, pushing apart its neighbors by virtue of the energy of thermal motion, the formation of the new phase during shock compression occurs by transport of the entire mass of the initial phase, by plastic flow. Supersonic martensitic (MT) type of reaction waves MT is a specific variant of the realization of a polymorphic transformation associated with a cooperative mechanism of atomic displacements MT transition occurs upon a significant deviation from the point of equilibrium of the phases in an active medium capable of liberating energy. Nanoscale mechanisms of phase Nucleation at plastic-strain-induced defects. Mechanically induced Thermal Explosion . The shock wave provides an ignition source at localization centers (for example, pore collapse). Such phenomenon has been described as a virtual combustion wave and is typical of thermal explosions. The actions of the stress wave on the material, through pore collapse and plastic deformation, heat and mix the material until the requirements for reaction initiation are met. Ultra-fast Force diffusion The fluid-dynamic model of ultrafast (forced) diffusion caused by a difference in the particle velocity of the components in shock-compressed matter Complete intermixing of particles is achieved owing to penetration of rapidly moving particles into slowly moving particles. Dremin, Breusov Batsanov Jette, Goroshin, ReevesAl'tshuler Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 10
  • 12. Chemical Reactions and Shock Wave: Ni-Al System Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 5 Systems Method Conclusion Publication/Year Al + Ni (1:3.5) Recovery XRD analysis: AlNi3 phase; reaction initiation at hot regions Horie Y., R. Graham, I.Simonsen, 1985 Mater. Lett. 3 354–359 Al + Ni (3:1) Analysis of Shock adiabat Influence of particle morphology Song, I. and N. Thadhani, 1992 Met. Trans. A, 23(1), 41-48 Al + Ni (3:1; 1:1;1:3) Recovery the chemical reactions in this system are promoted by increased volume of Ni Dunbar, E., N. Thadhani, R. Graham, 1993 Mater. Sci., 28, 2903-2914. Al + Ni (1:2.6) Monitoring pressure The excess pressure is best explained as an indicator of a fast exothermic reaction during the shock loading. Bennett, L., F. Sorrell, et al. 1992 Appl. Phys. Lett., 61(5), 520-521 Al + Ni (1:2.6) Monitoring pressure The excess pressure is best explained as an indicator of a fast exothermic reaction during the shock loading Yang Y. et al. 1997 Appl. Phys. Lett., 70(25), 3365-3367 Al + Ni (1:1 volume) The Hugoniot measurement Influence of morphology; melting and dissolution for spherical Ni; Shock induced for Ni-flakes Eakins, D.; Thadhani, N, 2006 J. Appl. Phys., 100, 113521 Al + Ni (1:1 volume) Recovery. Modelling Shock densification for different morphologies Eakins, D.; Thadhani, N., 2008 Appl. Phys. Lett. 2008, 92, 111903. Al + Ni laminate Recovery Laser Shock Compression Wei C. et al., 2009 AIP Conference Proceedings 1195, 305 Al + Ni (1:1) HEBM High-speed video recording, recovery Asay Shaer impact test Reeves R. et al., 2010 J. Phys. Chem. C 2010, 114, 14772–14780
  • 13. Chemical Reactions and Shock Wave: Ni-Al System Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 5 Systems Method Conclusion Publication/Year Al + Ni (1:1) Time-pressure profile. Recovery: Laser Shock Compression Melting-dissolution mechanism Wei C. et al., 2011 Acta Materialia 59 (2011) 5276–5287 Al + Ni (1:1) Recovery. Modelling Configuration effect Specht P., N. Thadhani, T. Weihs, 2012 JJOURNAL OF APPLIED PHYSICS 111, 073527 Al + Ni (1:1) Time-pressure profile. Recovery: Laser Shock Compression Ni/Al laminates Wei C. et al., 2012 Acta Materialia 60 3929–3942 Al + Ni (1:1) HEBM High-speed video recording, recovery Asay Shear impact test Mechanically induced Explosion Reeves R. et al., 2013 Propellants Explos. Pyrotech. 38, 611 – 621 Al + Ni (1:1) Pressure-time analysis Influence of additives, Cu, PTRE Wei. X et al., 2015 Journal of Alloys and Compounds 648, 540-549 Al + Ni (1:1) The Hugoniot measurement and modelling Multilayered nano foils Kelly S. Thadhani, N, 2016 JOURNAL OF APPLIED PHYSICS 119, 095903 Al + Ni laminate The Hugoniot measurement and modelling Shock densification for different morphologies Specht P., et,al 2017 JOURNAL OF APPLIED PHYSICS 121, 015110 Al + Ni (1:1) High-speed video recording, recovery Asay Shear impact test, role of fracture Beason M. , et al., 2017 Acta Materialia 133, 247-257 Al + Ni (2:1) HEBM and nano foils Time-pressure profile. Recovery, modelling Asay type of experiment Influence of additives: oxides Kerong R. et al., 2019 Metals 2019, 9, 499
  • 14. SSR in Gasless Reaction in Ni + Al System: Real time Studies Schematic of Asay shear impact test. Figure (A) shows the windowed sample holder Fig. (B) shows the plunger and sample with the retaining plates removed. Gas gun constructed at Purdue University. This gun has a 25.4 mm bore, 4.6 m barrel, and has accelerated a 26 g projectile to 1 km/s
  • 15. Shock Initiated Reaction: Ni + Al System Sequence of images high speed video images from shear impact test in nano-mixture exhibiting reaction (impact velocity ~250m/s average combustion front velocity ~10cm/s).
  • 16. Shock Induced Thermal Explosion Ni + Al System Sequence of images high speed video images from shear impact test in nano-mixture (the impact velocity ~1070 m/s average combustion front velocity ~1000 m/s)
  • 17. Shock Induced Reaction in TiN- B System XRD results for thermally and mechanically initiated reactions Mechanical InitiationThermal Initiation (a) (b) (c) (a)Mechanically-induced composite TiN/B (dark phase – B; light phase TiN) (b)Product of thermal initiation of TiN/B (dark phase – BN; light phase TiB2/TiN) (c)Product of mechanical initiation of TiN/B (dark phase – B; light phase – TiB2/TiN) Initial Composite Thermal Initiation Mechanical Initiation 1
  • 18. TEM: c-BN Formation (a) TEM images of typical particles formed in the Ti-B-N system after shock. Relatively large TiB2 and h-BN crystallites are dominant within the field of view. The inset shows a magnified TEM image of the surface area of the large TiB2 crystallite (70–100 nm in diameter) that has a layer of the c-BN phase. (b) Magnified area of the c-BN crystal phase at the interface with the TiB2 crystalline particle. Intensity distribution on the magnified fragment of the HRTEM image of the c-BN phase in vertical (a) and horizontal (b) directions showing that d-spacing in both directions are close to 0.18 nm. 1 Intensity Intensity Y, nm X, nm
  • 19. Proposed Reaction Mechanism TEM & SEM results revealed the formation of a nano-mixture of B and TiN surrounding unreacted B crystals. Select Area Diffraction (SAD) patterns, EDS, and High Resolution TEM analysis of structural transformations allow the suggestion of a simple two-step mechanism for reaction of TiN/3B. First, formation of TiB2 from the finely mixed regions of TiN/B, followed by production of the BN phase. 1 Initial Quenched Thermally Initiated Shock Initiated J. Physical Chemistry C, 123 (17) 11273-11283 (2019) A mechanism for the structural transformation occurring at the boundary between initially unreacted B and TiN phases is suggested based on experimental observations In the case of thermally initiated reaction, near- complete conversion to product is observed. This is likely due to prolonged exposure to high temperature conditions For the shock-initiated reaction, some micron scale Boron crystals remain unreacted and surrounded by TiN. The short time scales during which conditions suitable for reaction persist limit the degree of conversion B B TiN/B TiN TiB2 BN B TiN/B/TiB2 TiB2 BN
  • 20. Structural Transformations: HEBM TiN/3B 2 TEM TiB2 d-spacing (100) 2.62Å B B Reaction Layers 1 nm 2.60Å 2.60Å TiB2 SEM Cross-section Reaction Layers B B BN TiB2 Shock-initiated - TEMQuenched Reaction - TEM
  • 21. 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 0 200 400 600 800 1000 1200 1400 Intensity(counts) 2 Theta (degrees) 43.36o 50.53o Shock-induced Synthesis: B-GaN System 2
  • 22. Solid Flame Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM) 2 5 A B AB d D 𝒓 = 𝟏 𝜹 𝑭(𝑻, 𝜼) 𝒊𝒇 𝜹 = 𝟎 ↔ 𝒓 = ∞ 𝒓 = 𝟏 𝜹 + 𝜹 𝟎 𝑭(𝑻, 𝜼) 𝒍𝒆𝒕 𝒖𝒔 𝒎𝒂𝒌𝒆 𝚫~𝜹 𝟎 𝒘𝒆 𝒎𝒂𝒚 𝒆𝒙𝒑𝒆𝒄𝒕 𝜼 = 𝟏 𝒕𝒉𝒓𝒐𝒖𝒈𝒉 𝒓𝒂𝒑𝒊𝒅 𝒈𝒓𝒂𝒊𝒏 𝒃𝒐𝒏𝒅𝒂𝒓𝒚 𝒅𝒊𝒇𝒇𝒖𝒔𝒊𝒐𝒏 𝑫𝒍𝒊𝒒𝒖𝒊𝒅 = 𝟏𝟎−𝟓 𝒄𝒎 𝟐 𝒔 𝑫 𝒔𝒐𝒍𝒊𝒅 = 𝟏𝟎−𝟗 𝒄𝒎 𝟐 𝒔 𝑫 𝒈𝒓𝒂𝒊𝒏 𝒃𝒐𝒖𝒏𝒅𝒂𝒓𝒚 = 𝟏𝟎−𝟓 − 𝟏𝟎−𝟔 𝒄𝒎 𝟐 𝒔
  • 23. Conclusions  Ultra-fast (0.1–5 ms) shock-induced reactions occurred in the 3B-TiN system  The results illustrate the possibility of rapid reactions occurring in the solid state on incredibly short timescales.  This process may provide a unique route for the discovery and fabrication of advanced compounds.  Fundamental questions to be resolved :  What is the mechanism for ultra fast solid-state reactions under the shock wave conditions?  Can other metastable phases be produced under unique CS conditions? 2
  • 24. Final Remarks A long list of fundamental questions remain re the physical nature of the heterogeneous self-sustained reactions Breakthrough hybrid concepts involving self-sustained reactions make combustion synthesis method extremely promising specifically for fabrication of high temperature and ultra high temperature ceramics 2
  • 25. ACKNOWLEDGMENTS  This work was supported by the Department of Energy, National Nuclear Security Administration , under the Award No. DE- NA0 0 02377 as part of the Predictive Science Academic Alliance Program II. 24Center for Shock Wave-processing of Advanced Reactive Materials (C-SWARM)