Synthesis of Nanostructured Materials by nonequilibrium Processing
by
Jatin Bhatt Assistant Professor Department of Metallurgical & Materials Engineering, Visvesvaraya National Institute of Technology, Nagpur
Classification Discrete nano (dn) materials
0D or 1D
Classification of nanomaterials Nanoscale device (nd) materials Usually 2D some time 1D
Bulk (nc or ns) materials 3D
Problem & Solutions
Fundamental Issue Control of structure at very fine scale
To reduce local entropy density
Two direct consequences 1) Require significant amount of energy /expensive. 2) Thermodynamically unstable and revert back to high entropy state (disordered state)…. Disordered state to desired nanostructured state.
Processes “Such processes are rapid solidification from the liquid state, mechanical alloying, plasma processing , and vapor deposition.
Disordered structure
Regular Atomic structure
Figure shows the basic concept of "energize and quench" to synthesize nonequilibrium materials [Prog. In Mat. Sci., 46(2001)1]
Processes Bulk NanoMaterials by 1) Bottom Up Approach (Pure, Costly, Time consuming) 2) Top Up Approach (Not of high quality but fast & relatively inexpensive) Some process that can defy above broad categorization •
Deposition (CVD/PVD)
•
Consolidation of dn materials
•
Sever Plastic Deformation (SPD)
•
Equal Channel Angular Processing (ECAP)
•
High Pressure Torsion
•
Surface Mechanical Attrition
•
Crystallization from amorphous phase i.e from Bulk Metallic Glasses Recent report by Kumar and Schroers, APL 92(2008)031901 (NEMSs and nanoimprinting-BMG can replicate nanoscale surface feautures)
Nishiyama et al., Mater.Trans JIM 45(2004)1245
BMG prerequisite to nanostructure formation
~10 nm
Nanocrystallization on heating
The HRTEM micrograph of the vit1 BMG annealed at 623 K under 4 GPa for 4 h [Wang et al., , Appl. Phys. Lett. 75 (1999) 2770. ]
HRTEM image of As cast Bulk Metallic Glass
Experiment have demonstrated BMG has Short range ordering (SRO) but long range disordering (LRDO) [Unpublished work]
Case study 1
Zr-Pd Phase Diagram
Journal of Phase Equilibria, 15 (1994) (6)
Rapid Solidification
Argon Atmosphere
Graphite Crucible
Schematic diagram of Melt spinning technique for Rapid Solidification
XRD studies
i
*
5
- i-phase
5i
i
(a) i
*
*
Intensity (a.u)
5 i5
5 5
Zr80Pt20
*
i α− Zr 5 Zr5Pt3 ZrPt
*
(b) (c) (d)
30
40
50
60
70
2θ
XRD patterns of melt spun Zr80Pt20 alloy with various phases at different wheel velocities (a) nanocrystalline at 10m/s, (b) nanoQC at 20m/s, (c) nanoQC + amorphous at 30m/s and (d) amorphous at 40m/s
XRD studies
*
Zr75Pd25
*
*
Intensity (a.u)
*
*
- i-Phase
(a) (b) (c) (d)
30
40
50 2θ
60
70
XRD patterns of melt spun Zr75Pd25 alloy with various phases at different wheel velocities (a) and (b) nanoQC at 10m/s and 20m/s, respectively, (c) nanoQC + amorphous at 30m/s and (d) amorphous at 40m/s.
XRD studies (a)
(b)
wheel side
Zr75Pd25, 40m/s
Intensity (a.u)
Intensity (a.u)
Zr80Pt20, 40m/s
wheel side
air side
30
40
50 2θ
60
air side
70
30
40
50
60
2θ
XRD pattern of the wheel side and air side of the melt spun ribbons at 40m/s for amorphous phase (a) Zr80Pt20 (b) Zr75Pd25
70
Nanoindentation study
250
(i) nanocrystalline (10m/s) (ii) nanoQC (20m/s) 200 (iii) nanoQC + amorphous (30m/s) (iv) amorphous (40m/s) (iv)
Zr80Pt20
150
(ii) (i) 180
100
(i) nanocrystalline (10m/s) (ii) nanoQC (20m/s) 170 (iii) nanoQC + amorphous (30m/s) (iv) amorphous (40m/s)
50
0
(a) 0
200
400
600
800
1000 1200 1400 1600
Displacement into surface (nm)
Load (mN)
Load (mN)
(iii)
Zr80Pt20
160 18nm (iii)
150
140
(iv)
15nm (ii) (i)
130 1200
1240
(b) 1280
Displacement into surface (nm)
(a) Load vs. Displacement (P-h) curves for different phases in melt spun Zr80Pt20 alloy and (b) magnified figure showing small pop in and pop up events in amorphous phase (shown by dotted arrow).
1320
Nanoindentation study 250
(i) nano QC (10 m/s) (ii) nano QC (20 m/s) (iii) nano QC+ amorphous (30 m/s) (iv) amorphous (40 m/s)
Load (mN)
200
(iii)
150
Zr75Pd25
(iv)
(ii) (i) 100
180
Zr75Pd25
(i) nano QC (ii) nano QC 170 (iii) nano QC+ amorphous (iv) amorphous
50
(iii)
0
(a) 200
400
600
800
1000 1200 1400 1600
Displacement into surface (nm)
Load (mN)
0
160
150 15nm
12nm (iv)
140
(ii)
130 1200
(i) 1240
1280
Displacement into surface (nm)
(a) Load vs. Displacement (P-h) curves for different phases in melt spun Zr75Pd25 alloy and (b) magnified figure showing small pop in and pop up events in amorphous phase (shown by dotted arrow)
(b) 1320
Nanomechanical Properties Phase
Melt spun wheel velocity (m/s)
Hardness (GPa)
Elastic Modulus (GPa)
H/E Ratio
Zr80Pt20 Nanocrystalline
10
5.2
60
0.09
NanoQC
20
5.9
70
0.08
NanoQC + Amorphous
30
6.5
93
0.07
Amorphous
40
5.5
65
0.09
Zr75Pd25 NanoQC
10
5.3
66
0.08
NanoQC
20
5.5
68
0.08
NanoQC + Amorphous
30
6.2
81
0.08
Amorphous
40
5.1
62
0.08
Case study 2
Thermodynamic Model: Entropy due to Configuration n
ΔS config = − R ∑ ci ln ci i =1
B 0.00 1.00
0.25
ΔSconfig/R
1.0
0.75
0.9 0.50
0.50
0.75
1.00 A 0.00
0.25
0.25
0.50
0.75
0.00 1.00 C
Isometric contours of ΔSconfig/R
Thermodynamic Model: Enthalpy calculation c c c ΔH chem( ABC ) = ΔH AB + ΔH BC + ΔH AC
ΔH ijc = ci c j (c j ΔH mix (i
in
j)
+ ci ΔH mix ( j
-5 0.00 Zr -7.5 1.00 -10 Δ Hchem -12.5 -15 -17.5 0.25 0.75 -20 -22
0.50
0.50
0.75
0.25
-5
1.00 Cu 0.00
0.25
0.50
0.75
0.00 1.00 Ti
Isometric contours of ΔHchem for Cu-Zr-Ti system
in i
))
Topological Model: Entropy due to atomic mismatch calculation Mansoori et al., J. Chem. Phys. 54(1971)1523-1525.
0.00 Zr1.00 ΔSσ/kB
0.25
0.75
0.50 0.25 0.23 0.22 0.2 0.75 0.175 0.15 0.10 1.00 Cu 0.00
0.50
0.25
0.25
0.50
0.75
0.00 1.00 Ti
Isometric contours of ΔSσ/kB for Cu-Zr-Ti system
Composition Identification
Cu46Zr43Ti11
-5 0.00 Zr1.00 -7.5 ΔSσ/kB -10 Δ Hchem -12.5 -15 Δ Sconfig/R -17.5 0.25 0.75 -20 -22
Cu60Zr30Ti10 0.25 0.23 0.22 0.2 0.175 0.15 0.10
3
0.50
0.50 1
0.75
1.00 Cu 0.00
2
0.25
4
0.50
0.75
0.25
0.00 1.00 Ti
Superposition of isocontours of ΔHchem and ΔSσ/kB, indicating their intersections with in ΔSconfig/R range of 0.9-1.0 for Cu-Zr-Ti system
HRTEM 2Φ x 70mm
3Φx40mm
Bulk Metallic Glassy samples
Typical bright field image and corresponding SADP obtained for Cu60Zr30Ti10 showing amorphous pattern
Thermal History of as cast samples Heating Rate 20K/min
Tx1
Exothermic
Tx2 Relaxed
DSC trace of as cast Cu60Zr30Ti10 BMG 500
600
700
800
Temperature (K)
Sample Name
Condition
As cast
As cast
Relaxed
Annealed in supercooled liquid region (723K for1h)
Tx1
Annealed at the offset of first crystallization peak (795K for1h)
Tx2
Annealed at the offset of second crystallization peak (845 K for 1h)
XRD studies nd i u (a) 2 crystallization
Intensity (a.u)
uCu10Zr7 i Cu8Zr3 5 Cu3Ti2
st
(b) 1 crystallization (c) Super cooled liquid region (d) As Cast
i i u uu u 5
u
45 nm
i
u
u
(a) (b)
u
(c) (d) 20
30
40
2θ
65 nm
50
60
70
Hardness Studies
850
As cast Relaxed structure Tx1 Tx2
800
Hv (VHN)
750 700 650 600 550 500 0
100
200
300
400
500
Load (g)
Hardness (H) vs. Load (P) for as cast, Relaxed, Tx1 and Tx2 samples
Wear Studies 0.5
110
(a)
20 N 40 N
100 90
Wear rate, x10 (kg/m)
-10
0.3
0.2
0.1
80 70 60 50 40 30 20 10 0
0.0
Relaxed
Tx1
As Cast
Tx2
12
8
As Cast
Wear Resistance, x10 (kg/m)
Coefficient of friction, μ
0.4
(b)
20 N 40 N
10
(c)
20 N 40 N
8 6 4 2 0
As Cast
Relaxed
Tx1
Tx2
Relaxed
Tx1
Tx2
Wear vs. Hardeness
12
Relaxed
20N 40N
Wear Resistance
10 8
Archard Equation Q= KW/H
As cast
6
Q= Vol. removed per unit sliding distance.
4 2 Tx2
Tx1
W= Normal Load. H= Indentation hardness.
0 500
550
600
650
700
Hardness (VHN)
Wear resistance dependence on hardness at loads of 20N and 40N
SEM Studies (a) (a)
(b)
SEM micrographs of worn surface of Cu60Zr30Ti10 BMG in (a) relaxed state and (b) annealed at Tx2 at a load of 40N. The arrow marks shows the sliding direction.
SEM Studies
SEM micrographs of worn out fracture surface of Tx2 sample
Conclusions: 1. In case 1, nano composite of nano quasicrystalline and amorphous phase showed excellent combination of hardness and elastic modulus in comparison to monolithic nano crystalline or nano quasicrystalline phase. 2. In case 2, relaxed structure of BMG i.e relaxed SRO showed excellent hardness and wear performance in comparison to nano crystallized phases. 3. Crystallization process in multicomponent glassy alloys is usually quite complicated leading to a number of phases in multiple steps have different sizes/varying volume percentages in matrix of parent phase and contribute differently to the mechanical properties. 4. The nano range should be close to stability limit of crystalline phase on the amorphous matrix which reduces the crack formation and propagation and induces hardness. 5. Close control of nano structure (ns) dimension/ distribution is required to develop ns dimensions- properties relationships.