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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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  • 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

  • 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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    16

    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