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TRANSCRIPT
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Copyright 2013 Toray Industries, Inc. All Rights Reserved
NANOALLOY® Technology for High Performance CFRP
March 29, 2013 Workshop on Next Generation Transport Aircraft
Toray Industries, Inc. Ehime Plant Composite Materials Research Laboratories
Takayuki Fujiwara
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Target for mechanical properties
1)Relative values to conventional material :100
Flexural modulus1)
Frac
ture
toug
hnes
s(K
IC)1
)
50
80 100
100
150
Conventional epoxy
120
200
0
(2005)(1995)
Impact resistantresin
50
90
100
150
200
0100
Conventional CFRP
120
(2005)(1995)
0˚ Compression strength1)
Impact-resistantpregreg
110
Inte
rlam
inar
frac
ture
toug
hnes
s(G
Ic)
CFRP Epoxy resin
1. Introduction2
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B:Epoxy or thermoplastic (Tp)
MixingA: Epoxy(Ep) Bi-continuous structure
Sea-island structure
NANOALLOY® technology changes the compatible mixture into nano-scale phases during the cure.
CuringCompatible mixture
TEM image 100 nm
NANOALLOY® technology for epoxy1. Introduction
100 nmTEM imageTEM image 100 nmTEM image
One phase
Two phaseTem
pera
ture
A ratio0 1
One phase
Two phaseTem
pera
ture
A ratio0 1
Reaction-induced phase separation
Boundaryshifting
3
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Why “nano”?1. Introduction
273 10
6 fVn 9106 fVSA 16
23/1
fd
The interaction between matrix and domain
4
0° 90°Homogeneous dispersion between carbon fibers
Nanophase separation increases the interaction.
Carbon fiber (ϕ: 6 μm)Interlayer distance
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NANOALLOY® Map
Flexural modulus1)
Impact resistant resin applied epoxy/thermoplastic
NANOALLOY®Fr
actu
re to
ughn
ess(
KIC
)1)
100
100 115
150
200
Conventional epoxy
130
250
50
NANOALLOY® technology improves both fracture toughness and flexural modulus of epoxy resin.
1)Relative values to conventional epoxy :100
1. Introduction5
Epoxy resin
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Impact resistant prepreg applied epoxy/thermoplastic
NANOALLOY® technology
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TEM image of cured resin
500nm
Properties Conventional epoxy Impact resistant epoxy
Flexural modulus1) 100 94Flexural deflection1) 100 113
Fracture toughness (KIc)1) 100 181Glass transition temperature (°C) 115 120
•The toughness is drastically improved with keeping other major properties.
•Thermoplastic is dispersed in cured resin as nano-scale domain (White dots in TEM image).
1) Relative values to conventional epoxy :1002) Cured condition : 135°C x 2hrs.3) KIc : Crack opening mode, Fracture toughness test
Cured resin properties2. Impact resistant prepreg applied epoxy/thermoplastic NANOALLOY® technology7
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Mechanism for impact resistance
1. “Thermoplastic domain” absorbs impact energy by “cavitation” effect.
2. “Spherical thermoplastic structure” absorbs impact energy by plastic deformation.
3. “Nano-scale dispersed” thermoplastic domain stops crack propagation by blocking out its route.
Thermoplastic domain
50nm
Crack Cavitation Crack wraps around domains
Toughened epoxy resin
8 2. Impact resistant prepreg applied epoxy/thermoplastic NANOALLOY® technology
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Charpy impact strength Standard-modulus CF(T700S)- prepreg
0
50
100
150
200
ConventionalCha
rpy
impa
ct s
treng
th[k
J/m
2 ]
FAW=150gsm, Wf=63% prepregTest method : JIS (3mm-t)
Total absorbed energy (laminate)
+ 79%
0
200
400
600
800
Cha
rpy
impa
ct s
treng
th[k
J/m
2 ]
+59%
Total absorbed energy (model pipe)
Conventional Impact resistant
FAW=150gsm, Wf=63% prepregPipe inner diameter=6.3mmf [+/-45˚ 3ply, 0˚ 3ply]
Energy before the max. load
Total absorbed energy +
Energy after the max. load
Load
→
Displacement →
ConventionalImage of charpy impact test chart
Impact resistant
Load
→
Displacement →6
Impact resistant properties of CFRP9
Impact resistant
2. Impact resistant prepreg applied epoxy/thermoplastic NANOALLOY® technology
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CFRP of standard-modulus CF (T700S)
Conventional Impact resistant
0゚ Tensile1)2)Strength 100 101
Modulus 100 101
90゚ Tensile strength1) 100 104
0゚ Compression strength1) 100 93
0゚ Flexural1)2)Strength 100 98
Modulus 100 93
0゚ Interlaminar shear strength1) 100 90
Inplane shear strength1) 100 96
Interlaminar fracture toughness(GIc) 100 245
Charpy impact strength1) 100 179
1) Relative values to conventional CFRP :1002) Normalized value in Vf = 60%
10
CFRP properties2. Impact resistant prepreg applied epoxy/thermoplastic NANOALLOY® technology
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Charpy impact strength Modelate-modulus CF(T800S) - prepreg
0
50
100
150
200
+61%
0
200
400
600
800
+39%
ConventionalCha
rpy
impa
ct s
treng
th[k
J/m
2 ]
Total absorbed energy (laminate)
Cha
rpy
impa
ct s
treng
th[k
J/m
2 ]
Total absorbed energy (model pipe)
Conventional
FAW=150gsm, Wf=63% prepregTest method : JIS (3mm-t)
FAW=150gsm, Wf=63% prepregPipe inner diameter=6.3mmf [+/-45˚ 3ply, 0˚ 3ply]
7
Impact resistant properties of CFRP11
Impact resistant Impact resistant
2. Impact resistant prepreg applied epoxy/thermoplastic NANOALLOY® technology
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CFRP of intermidiate-modulus CF (T800S)
Conventional Impact Resistant
0゚ Tensile1)2)Strength 100 101
Modulus 100 101
90゚ Tensile strength1) 100 104
0゚ Compression strength1) 100 93
0゚ Flexural1)2)Strength 100 98
Modulus 100 93
0゚ Interlaminar shear strength1) 100 90
Inplane shear strength1) 100 96
Interlaminar fracture toughness(GIc) 100 270
Charpy impact strength1) 100 161
Mechanical properties of CFRP12
1) Relative values to conventional CFRP :1002) Normalized value in Vf = 60%
2. Impact resistant prepreg applied epoxy/thermoplastic NANOALLOY® technology
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Charpy impact strength High-modulus CF(M40J )- prepreg
0
50
100
150
200
Cha
rpy
impa
ct s
treng
th[k
J/m
2 ]
Total absorbed energy (laminate)
Conventional
+8%
0
200
400
600
800
ConventionalCha
rpy
impa
ct s
treng
th[k
J/m
2 ]
Total absorbed energy (model pipe)
+18%
FAW=150gsm, Wf=63% prepregTest method : JIS (3mm-t)
FAW=150gsm, Wf=63% prepregPipe inner diameter=6.3mmf [+/-45゚ 3ply, 0゚ 3ply]
8
Impact resistant properties of CFRP13
•The charpy impact strength improvement is smaller than the result of T700S or T800S.
•The fracture of fiber is predominant rather than that of resin in interlayers.
Impact resistant Impact resistant
2. Impact resistant prepreg applied epoxy/thermoplastic NANOALLOY® technology
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CFRP of Hi-Modulus CF (M40J)
Conventional Impact Resistant
0゚ Tensile1)2)Strength 100 98
Modulus 100 100
90゚ Tensile strength1) 100 100
0゚ Compression strength1) 100 97
0゚ Flexural1)2)Strength 100 103
Modulus 100 97
0゚ Interlaminar shear strength1) 100 93
Inplane shear strength1) 100 100
Interlaminar fracture toughness(GIc) 100 113
Charpy impact strength1) 100 108
Mechanical properties of CFRP14
1) Relative values to conventional CFRP :1002) Normalized value in Vf = 60%
2. Impact resistant prepreg applied epoxy/thermoplastic NANOALLOY® technology
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1.E-11
1.E-10
1.E-09
1.E-08
1.E-07
1.E-06
1.E-05
100 200 300 400 500GIIc [J/m2]
Mode-IInterlaminar fracture toughness(GIc)(Double Cantilever Beam)
1.E-10
1.E-09
1.E-08
1.E-07
1.E-06
50 100 150 200 250GIc[J/m2] C
rack
ext
entio
n ra
teda
/dN
[m/c
ycle
]
Conventional CFRPImpact resistant CFRP
Mode-II Interlaminar fracture toughness (GIIc)(End Notched Flexure)
9
Cra
ck e
xten
tion
rate
da/d
N[m
/cyc
le]
*These experimental data are not guaranteed in all case.
Fatigue resistance properties of CFRP15
The crack propagation energy of impact resistant CFRP is significantly larger than the conventional CFRP.
2. Impact resistant prepreg applied epoxy/thermoplastic NANOALLOY® technology
Conventional CFRPImpact resistant CFRP
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Summary
NANOALLOY® technology led to the invention of a novel prepreg.
Impact resistant prepreg applied epoxy/thermoplastic NANOALLOY® technology• The impact-resistant prepreg is well-suited for damage-sensitive applications. • The impact-resistant prepreg achieved higher charpy impact strength by about
80% than the conventional prepreg.
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17
Thank you for your attention