CARBON FIBERS FROM MESOPHASE PITCH: … FIBERS FROM MESOPHASE PITCH: Processing and Properties C A E...
Transcript of CARBON FIBERS FROM MESOPHASE PITCH: … FIBERS FROM MESOPHASE PITCH: Processing and Properties C A E...
C A E F F
Dr. Amod Ogale
Dow Professor of Chemical Engineering
Director, Center for Adv. Eng. Fibers and Films
2013 Graffin Lecturer of American Carbon Society
Clemson University
CARBON FIBERS FROM
MESOPHASE PITCH:
Processing and Properties
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Potential Applications
Ultra High Thermal Conductivity Composites
Ten years from now, chips will run at 30 GHz
and churn a trillion operations per sec.
Unfortunately, with today’s technology, that
would lead to chips putting out the same
amount of heat, proportionally, as a nuclear
power plant … Intel CTO Pat Gelsinger
Gen IV Nuclear Reactor: Structural materials needed to build
the advanced reactor; structural carbon-carbon composites
needed for High Temperature Internals (>1200°C) … Dr. Bill
Corwin, Natl Tech Director for Matls, ORNL
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BARRIERS TO HIGH VOLUME APPLICATIONS
• Current price of carbon fibers ranges from
~$1000/pound for high thermal conductivity carbon fibers to $15/lb for low modulus fibers.
• For electronic applications the cost of high thermal conductivity fibers must be reduced to $100/pound.
• Mesophase pitch precursors for carbon fibers with controllable molecular properties
• Process models for control and the optimization of molecular structure within fiber during processing for balance of properties
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Barriers
Carbon fibers made from mesophase pitch
• Excellent tensile modulus 800 GPa • Outstanding thermal conductivity 1100 W/m-K
• Moderate tensile strength (2000 MPa) • Poor compressive strength (700 MPa) and • Poor transverse properties (10 W/m.K)
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Topical Outline
• Molecular Structure • Flow Behavior and Processing
• Microstructure and Texture • Mechanical and Transport Properties
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Precursors: Mesophase Pitch
MW 500
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Mitsubishi AR-HP: Synthesized from Naphthalene using
BF3/HF catalysts
MALDI Analysis
Kundu,…
Ogale, Carbon,
2008
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MALDI Analysis
Petroleum Pitch-derived Experimental
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Molecular Structure: AR-HP Mesophase Pitch
5 10 15 20 25 30 35
0.00
0.02
0.04
0.06
0.08
0.10
0.12
steady-sheared at 1s-1
steady-sheared at 10s-1
as-spun fibers
graphitized fibers
au
2
normalized
intensity/4
Detector X-ray
gun
Rigaku 2-D diffractometer (Rigaku/ MSC) Cu-Kα 45
KV and 0.67 mA.
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Azimuthal Scans
0 20 40 60 80 100 120 140 160 180
0.002
0.004
0.006
0.008
0.010
0.012
0.014
0.016
0.018
0.0020
0.0025
0.0030
0.0035
0.0040
0.0045
0.0050
0.0055
no
rmal
ized
azi
mu
thal
in
tesi
ty
, deg
Peak at 25°
Peak at 7°
Kundu, Naskar, Ogale, Anderson, Arnold, CARBON 2008
Azimuthal profiles of 25and 7 peaks display off-set by 90
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Liquid
crystalline
pitch
precursor
Pitch
precursor
fiber
Melt-
spinning
Stabilized
fiber
Oxidative
stabilization
200-300°C
1-24 h
Graphitization
2000-3000°C
inert atmosphere
Carbon fiber
Processing of Mesophase Pitch-Based Carbon Fibers
“Carbon-Carbon Materials and Composites”
NASA Reference Publication 1254, Buckely and Edie,
Eds. , 1992
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0.01 0.1 1 10 100
20
40
60
80
100
305°C
297°C
vis
co
sity
, P
a.s
strain
290°C
Transient Rheo-structural Evolution
• The local maximum in shear stress is a consequence of yielding of initial texture
300 mm
flow
direction
radial
direction
300 mm
flow direction
300 mm
flow direction
300 mm
Kundu, Grecov, Rey,
and Ogale, J.
Rheology, 2009
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Flow-Microstructure Relationship: Converging Section
• Vortex formation was observed in the contraction region.
• Vortex formation typically associated with viscoelasticity of the material.
• Dynamic rheology for this material indicated low elasticity2.
Kundu and Ogale, Rheologica Acta 2010
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Melt-Spinning
Single-shot batch extruder
12 capillary hole spinneret
Capillary diameter = 150 mm,
L/D = 5 Spinning temp ~ 200-220°C Winding speed ~ 100-600 m / min
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Ultra High Temperature Heat Treatment
Graphitization furnace:
2700C Ultrahigh temperature press:
10 Tons and 2100C
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Carbonization under tension
Tungsten weight
Fiber tows
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EM images of AR-MP carbon fiber
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SEM and TEM images of ARMP carbon fibers heat treated at (a) 2600, (b) 2100, (c)
1500, & (d) 1200C.
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Figure 1 Stress-strain response of AR-MP pitch based carbon fibers heat
treated at various temperatures
Carbon fibers: Stress-strain plots
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Carbon fibers
Diameter [mm]
Force [N]
Stress [GPa]
Apparent Modulus
[GPa]
Strain-to-Failure [%]
2600C 8.5 0.7 0.110.04 1.90.7 482.1 94.1 0.42 0.2
2100C 8.9 1.0 0.160.05 2.70.5 412.0 54.6 0.70 0.1
1500C 9.1 0.5 0.150.05 2.30.6 205.7 29.4 1.10 0.2
1200C 9.1 0.7 0.130.04 2.00.7 173.8 19.7 1.10 0.3
Table 1 Tensile properties of AR-MP fibers
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Electrical Conductivity
Precursor Diameter, mm Resistivity
m-m
K1100 12 1.4 0.2
P100 12 3.2 0.3
AR-HP based 13 3.5 0.6
T300 7 18.1 5.3
Terpolymer 17 31.7 11.1
Rayon-based 12 55.5 2.3
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Carbon fibers: electrical properties
Diameter [mm]
Area [m2]
R []
Electrical resistivity
[mm]
Predicted* Thermal
conductivity [W/mK]
2600C 9.0 1.1 7.1 10-11 475.5 138 3.2 0.6 466
2100C 9.3 0.8 6.9 10-11 1,200.3 266 8.0 1.2 120
1500C 9.3 0.5 7.2 10-11 1,356.2 228 9.6 1.2 66
1200C 9.6 0.7 7.3 10-11 1,524.0 313 10.9 1.8 31
Table 2 Electrical resistivities of AR-MP fibers
*Lavin-Issi Correlation
where k[W/mK] and r[mcm] 295
)258(
000,440-
rk
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HT at 2400C Diameter
[mm]
R
[]
ER
[mm]
Predicted
Thermal
conductivity
[W/mK]
thin fibers
AR 11.7 ± 0.8 541 ± 306 3.4 438
Ex2 9.8 ± 0.8 725 ± 265 4.4 338
Ex3 11.9 ± 0.7 316 ± 88 2.8 520
thick fibers
AR 16.0 ± 0.8 164 ± 27 2.8 521
Ex2 17.6 ± 1.3 180 ± 126 2.9 502
Ex3 15.9 ± 0.7 172 ± 26 2.3 603
ER properties of 2400 C HT fibers
Carbon fibers based on experimental mesophase pitch showed smaller ER (th
us higher thermal conductivity)
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DEFICIENCIES OF CURRENT CARBON FIBERS
Stresses created by high-temperature heat treatment causes splitting,
reducing the mechanical and thermal properties of the fibers.
(S. Kumar, SAMPE Qtr, 1989)
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Ongoing Clemson Studies …
Introduction of multi-walled nanotubes of high aspect ratio disrupts the otherwise highly ordered, radial structure of carbonized fiber derived from mesophase pitch
0% Nanotubes 0.1% Nanotubes 0.3% Nanotubes
Ogale, Edie, and Rao, 2006, US Patent 7,153,452
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Recoil Test: Large stress – compressive failure
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Fiber Properties: Mechanical
Fiber Type
Diameter
(μm)
Tensile Strength
(GPa)
Compressive Strength
(GPa)
Compressive/
Tensile
(%)
0% MWNTs in
MP
8.4 2.6 ± 0.4 0.77 ± 0.04 30
0.1% MWNTs in
MP
8.0 1.8 ± 0.5 0.94 ± 0.06 53
0.3% MWNTs in
MP
11.6 1.8 ± 0.3 1.13 ± 0.04 63
• Compressive strength as a ratio of tensile strength was improved for nanocomposite carbon fibers, suggesting a decrease in the anisotropic nature of the pitch-based carbon fiber
Ahn, Lee, Ogale, Park, Fibers and Polymers, 2006
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SEM images of the fractured cross section of (a) 0 wt% and (b) CB modified
carbon fibers. White boxes correspond to the positions at which the high
resolution images were obtained.
R. Alway-Cooper, D. P. Anderson, and A. A. Ogale, CARBON 2013
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Two theta x-ray diffraction spectra of milled 0 wt% and CB modified
experimental carbon fibers, as well as the highly graphitic, commercial
grade K1100 (a) from 25 to 29˚ and (b) from 75 to 90˚.
R. Alway-Cooper, D. P. Anderson, and A. A. Ogale, CARBON 2013
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• MWCNT and carbon black was shown to modify the structure of mesophase
pitch-based carbon fibers when added in dilute concentration of about 0.3
wt%. A decrease was observed in the number of fibers that exhibited “pac-
man” splitting.
• Despite the cross-sectional textural changes, no significant reduction was
observed in the d002 spacing or La indicating that the nano-modified carbon
fibers retained a high degree of graphitic crystallinity.
• These mesophase-pitch based carbon fibers showed a strong graphitic
development and excellent transport properties, which makes them suitable
for high electrical and thermal conductivity industrial applications
Conclusions
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PROs: MULTI-FUNCTIONALITY
Excellent Strength and Stiffness = high performance
Light-weight = fuel-efficient
Outstanding Electrical and thermal conductivity
Fire-retardant
Con: COST
• Expensive on per pound basis ($ 10 to $ 1800/lb)
Carbon Fibers: Next Steps …
Current research directions: alternative precursors and novel processing routes for
reducing costs (at current fiber properties) OR
improve properties (at current cost)
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Y-P. Jeon, R, Alway-Cooper, M. Morales, and A. A. Ogale*, “Carbon Fibers”, Chapter 2.8, pp. 143-54,
Handbook of Advanced Ceramics, 2nd Edition, Elsevier, Eds. S. Somiya and M. Kaneno, 2013.
R. Alway-Cooper, D. P. Anderson, and A. A. Ogale*, “Carbon Black Modification of Mesophase Pitch-
Based Carbon Fibers”, in press, Carbon available online 3 March 2013
R. Alway-Cooper, M. Theodore, D. P. Anderson, A. A. Ogale*, “Finite Element Modeling of Transient
Heat Flow in Unidirectional Fiber-Polymer Composites During a Laser Flash Analysis”, J. Composite
Materials, Published online before print September 4, 2012, doi: 10.1177/0021998312458130
Santanu Kundu, Dana Grecov, Amod A. Ogale*, and Alejandro D. Rey*, Shear flow induced
microstructure of a synthetic mesophase pitch, Journal of Rheology, 53(10), 85-113, 2009
Santanu Kundu, Amit K. Naskar, Amod A. Ogale*, David P. Anderson and Jonahira R. Arnold,
”Observations on a low-angle x-ray diffraction peak for AR-HP mesophase pitch”, Carbon, 46(8), 1166-
69, 2008
T. Cho, Y. S. Lee, R. Rao, A.M. Rao, D. D. Edie, and A. A. Ogale*, “Structure of carbon fiber obtained
from nanotube-reinforced mesophase pitch”, Carbon, 41(7), 1419-24, 2003
A. A. Ogale*, D. P. Anderson, C. Lin, and K. Kearns, “Orientation and dimensional changes in meophase
pitch-based carbon fibers”, Carbon, 40(8), 1309-19, 2002
References
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Acknowledgments
Collaborators: Dan Edie, Mark Thies, and Dave Anderson (UDRI/AFRL)
Graduate Students: Santanu Kundu, Becky Alway-Cooper
Post-Doctoral Research Associate: Dr. Sungho Lee, Dr. Young-pyo Jeon
Sponsors:
Department of Energy
Air Force Research Lab
Army Research Lab
National Science Foundation EEC-9731680
Various industrial members thru CAEFF
Center for Advanced Engineering
Fibers and Films (CAEFF)
CAEFF Mission: To provide an integrated research and education
environment for the study of high performance fibers, films, and
composites for applications ranging from military to medical uses
• A Graduated NSF-ERC that secured over $ 30 million from
NSF and other sponsors
• Interdisciplinary faculty team
• Served over 65 industrial members
Acknowledgments