interface engineering of the tungsten-fiber-reinforced tungsten … · 2014. 2. 19. · interface...

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Interface Engineering of the Tungsten-Fiber-Reinforced Tungsten Composites J. Du*, T. Höschen, J-H. You, Max-Planck-Institut für Plasmaphysik, EURATOM Association, Boltzmannstr.2, 85748 Garching, Germany * corresponding author: [email protected] (address since 1st Mai 2011 : Forschungszentrum Jülich GmbH, EURATOM Association, 52425 Jülich, Germany) A toughening method for tungsten is proposed based on the reinforcement of tungsten fibers (W f /W m composites) and engineered interfaces. The interfacial parameter determination results show that selected interfaces satisfy to the interfacial debonding criterion. The interfacial debonding and fiber sliding were demonstrated by micro-mechanical 3-point bending test. The predicted stress-strain curve of the W f /W m composites with multiple fibers agree with the theoretical one, supporting the primary motivation of the thesis. Motivation: Tungsten/Tungsten composite A novel toughening method for tungsten (W), was proposed and developed based on the reinforcement of tungsten fibers (W f /W m composite) and engineered interfaces. The underlying toughening mechanism is analogous to that of a fiber-reinforced ceramic matrix composite (CMC). This work opened a new pathway to improve the toughness of tungsten as a structural material. composite stress composite strain pseudo-toughness CMC composite toughening mechanism • crack deflection • Interface debonding • fiber sliding • energy dissipation W f /W m composite concept W matrix W wire Analysis system: Single filament (fiber) composite 2 f r l f m z i s 2 f r l f m z i s =150m :2~3mm H:~0.3mm W f with interface magnetron sputtering chemical vapor deposition W f W f /W m cut & polished Fiber push-out test Experiment Specimen preparation Carbon 600 nm Cu 170 nm Cu 480 nm Cu/W m ZrO x /Zr m ZrO x /W m ErO x /W m Er/W m ErO x 600 nm 1000 nm ZrO x 150 nm 260 nm 450 nm 950 nm Lubricating coating Ductile coating Multiple-layer coating Oxide coating Designed interfaces 20.7 23 20.5 17.3 15.6 16.7 18.3 21.9 16 16.8 13.1 15.8 17.2 9.8 0 5 10 15 20 25 ZrOx 150 ZrOx 450 ZrOx 950 ZrOx&W 260 ErOx 600 ErOx 1000 ZrOx/Zr m ZrOx/W m ErOx/W m Er/W m Cu/W m Cu 170 Cu 480 carbon Average enrgy absorption (kJ/m^2 fiber fiber Result-Push-out test curve The area below the curve corresponds to the total amount of work done by the applied load—average energy absorption Δ, kJ/m 2 Result-Interfacial fracture energy ( i ) calibration and debonding criterion verification P H R R L 0.00 0.02 0.04 0.06 0.08 0.10 0.12 0 10 20 30 40 50 Load (N) Displacement (mm) A, P d B C, P fr Interface: ZrOx 450 Specimen thickness: 0.226 mm 0.05 0.10 0.15 0.20 0.25 0 500 1000 1500 2000 2500 3000 3500 Stress p (MPa) Specimen thickness H(mm) 2 3 0.6 J/m i Interface: ZrOx 450 1 1 2 2 2 1 2 ( 1) f f BH BH R R i f R f E p e e BR B H : Specimen thickness 2 d f P p R (Liang,1993) i Mode 2 fracture energy for the debonding event 9.61 5.86 2.89 3 2.99 2.03 1.23 3.5 3.46 2.01 7.66 12.34 7.41 0 2 4 6 8 10 12 14 16 ZrOx 150 ZrOx 450 ZrOx 950 ZrOx&W 260 ErOx 600 ErOx 1000 ZrOx/Zr m ZrOx/W m Er/W m ErOx/W m Cu/W m Cu170 Carbon Fracture energy (J/m^2) Fiber fracture Interfacial debonding Elastic mismatch i f 0 5 . 0 1 5 . 0 1 0 5 . 1 5 . 0 1 Fracture mechanism He,1989 Debonding criterion 0.25 0.25 Interface fracture energy i Fiber fracture energy f (320 J/m 2 ) f f f f c f i f c f 1 3 2 2 / S f f f f c f l f c f t s f s f f t The stress-strain curves is typical for a toughened composite, supporting the motivation of this work. 0 200 400 600 800 1000 1200 1400 1600 1800 0 0.5 1 1.5 2 2.5 3 3.5 Strain (%) Stress (MPa) mc sat y u Fiber pull out Interface: ZrOx450 Fiber volume: cf=0.6 Budiansky 1995 3 2 2 2 3 ( 2 ) (2 3 ) 3 f mc D D S D D S m m mc A r c mc f f m mc m cE cE 2 f c D f m mf i E E c cEr 2 f A m m R c f cE E cE 1 3 2 2 (1 ) / S f f f m f R c m f l r c EE c Er ( / ) (1 ) f c S f t R s f a m cE l r c E / sat s f a f t cE Evans 1994 A toughening method for tungsten is proposed based on the reinforcement of tungsten fibers (W f /W m composites) and engineered interfaces. The interfacial parameter determination results show that selected interfaces satisfy to the interfacial debonding criterion. The interfacial debonding and fiber sliding were demonstrated by micro-mechanical 3-point bending test. The predicted stress-strain curve of the W f /W m composites with multiple fibers agree with the theoretical one, supporting the primary motivation of the work. Interfacial fracture energy i of investigated interfaces The main focus of this work lies in the investigation of the interfacial fracture behavior of W f /W m composites with various engineered interfaces to demonstrate the feasibility of synthesizing a toughened W f /W m composite using the CMC toughening mechanism. Goal and focus of this work W matrix W wire W matrix W wire • W fiber, u > 2.5 GPa, u > 2% • Interface thickness m The fracture properties of the engineered interface are the key factors controlling the overall composite toughness. Micro-mechanical 3-point bending test (ZrO x 260) 2 m W fiber top W C Interface delamination c a) oxide interface: ZrO x 450 b) ductile interface: Cu 480 c) lubricating interface: C 600 Interface deformation and delamination can cause higher interfacial fracture energy. 1 m matrix typical W wire surface structure fiber ZrO x 450 a Conclusion Result-Crack deflection demonstration Result-Behavior prediction of W f /W m composite with multiple fibers The calculated ratios lie between 0.003 and 0.034. satisfying the 0.25 criterion. The debonding criterion is satisfied ! specimen thickness: 0.226mm y f f yield R c / y f yield f E u f f u c 2.1% u

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  • Interface Engineering of the Tungsten-Fiber-Reinforced Tungsten Composites

    J. Du*, T. Höschen, J-H. You, Max-Planck-Institut für Plasmaphysik, EURATOM Association, Boltzmannstr.2, 85748 Garching, Germany

    * corresponding author: [email protected] (address since 1st Mai 2011 : Forschungszentrum Jülich GmbH, EURATOM Association, 52425 Jülich, Germany)

    A toughening method for tungsten is proposed based on the reinforcement of tungsten fibers (Wf/Wm composites) and engineered interfaces.

    The interfacial parameter determination results show that selected interfaces satisfy to the interfacial debonding criterion.

    The interfacial debonding and fiber sliding were demonstrated by micro-mechanical 3-point bending test.

    The predicted stress-strain curve of the Wf/Wmcomposites with multiple fibers agree with the theoretical one, supporting the primary motivation of the thesis.

    Motivation: Tungsten/Tungsten composite

    A novel toughening method for tungsten (W), was proposed and developed based on the reinforcement of tungsten fibers (Wf/Wm composite) and engineered interfaces. The underlying toughening mechanism is analogous to that of a fiber-reinforced ceramic matrix composite (CMC). This work opened a new pathway to improve the toughness of tungsten as a structural material.

    com

    posi

    te s

    tress

    composite strain

    pseudo-toughnessCMC composite toughening mechanism

    • crack deflection• Interface debonding• fiber sliding• energy dissipation

    Wf/Wm composite concept

    W matrix

    W wire

    Analysis system:

    Single filament (fiber) composite

    2 fr

    l

    f

    m

    zi s

    2 fr

    l

    f

    m

    zi s

    =150m

    :2~3mmH:~0.3mm

    Wf with interface

    magnetronsputtering

    chemical vapor

    depositionWf Wf/Wm

    cut &polished

    Fiber push-out testExperiment Specimen preparation

    Carbon600 nm

    Cu 170 nmCu 480 nm

    Cu/W m

    ZrOx/Zr mZrOx/W mErOx/W mEr/W m

    ErOx600 nm1000 nm

    ZrOx150 nm260 nm450 nm950 nm

    Lubricating coatingDuctile coatingMultiple-layer coatingOxide coating

    Designed interfaces

    20.7

    23

    20.5

    17.315.6

    16.718.3

    21.9

    1616.8

    13.1

    15.817.2

    9.8

    0

    5

    10

    15

    20

    25

    ZrOx 150 ZrOx 450 ZrOx 950 ZrOx&W260

    ErOx600

    ErOx1000

    ZrOx/Zrm

    ZrOx/Wm

    ErOx/Wm

    Er/W m Cu/W m Cu 170 Cu 480 carbon

    Aver

    age

    enrg

    y ab

    sorp

    tion

    (kJ/

    m^2

    fiberfiber

    Result-Push-out test curve The area below the curve corresponds to the total amount of workdone by the applied load—average energy absorption Δ, kJ/m2

    Result-Interfacial fracture energy (i) calibration and debonding criterion verification P

    HR

    RL

    0.00 0.02 0.04 0.06 0.08 0.10 0.120

    10

    20

    30

    40

    50

    Load

    (N)

    Displacement (mm)

    A, Pd

    B

    C, Pfr

    Interface: ZrOx 450Specimen thickness: 0.226 mm

    0.05 0.10 0.15 0.20 0.250

    500

    1000

    1500

    2000

    2500

    3000

    3500

    Stre

    ss p

    (MPa

    )

    Specimen thickness H (mm)

    23 0.6 J/mi Interface: ZrOx 450

    1 12 2

    2 1

    2 ( 1)f fB H B HR Ri f R

    f

    Ep e e

    B R B

    H : Specimen thickness2d

    f

    PpR

    (Liang,1993)

    i Mode 2 fracture energy for the debonding event 9.61

    5.86

    2.89 3 2.992.03

    1.23

    3.5 3.462.01

    7.66

    12.34

    7.41

    0

    2

    4

    6

    8

    10

    12

    14

    16

    ZrOx 150 ZrOx450

    ZrOx950

    ZrOx&W260

    ErOx600

    ErOx1000

    ZrOx/Zrm

    ZrOx/Wm

    Er/W m

    ErOx/Wm

    Cu/W m Cu170 Carbon

    Frac

    ture

    ene

    rgy

    (J/m

    ^2)

    9.61

    5.86

    2.89 3 2.992.03

    1.23

    3.5 3.462.01

    7.66

    12.34

    7.41

    0

    2

    4

    6

    8

    10

    12

    14

    16

    ZrOx 150 ZrOx450

    ZrOx950

    ZrOx&W260

    ErOx600

    ErOx1000

    ZrOx/Zrm

    ZrOx/Wm

    Er/W m

    ErOx/Wm

    Cu/W m Cu170 Carbon

    Frac

    ture

    ene

    rgy

    (J/m

    ^2)

    Fiber fracture

    Interfacial debonding

    Elastic mismatch

    i

    f

    0

    5.0

    1

    5.0 10

    5.1

    5.01

    Fracture mechanism

    He,1989

    Debonding criterion

    ≤≤0.250.25Interface fracture energy i

    Fiber fracture energy f (≈ 320 J/m2)

    Budiansky 1995

    3 22

    23 ( 2 ) (2 3 )

    3f

    mc D D S D D S m mmcA

    rc

    mc

    f f mmc

    mc E c E

    2 f cD fm m f

    iE Ecc E r

    2 f

    Am m

    Rc fc E Ec E

    132 2(1 ) /S f f f m f R cm fl r c E E c E r

    ( / )(1 )f c S f

    tR

    sf

    am

    c E l rc E

    /sats fa ft c E

    Evans 1994

    The stress-strain curves is typical for a toughened composite, supporting the motivation of this work.

    0

    200

    400

    600

    800

    1000

    1200

    1400

    1600

    1800

    0 0.5 1 1.5 2 2.5 3 3.5

    Strain (%)

    Stre

    ss (M

    Pa)

    mc

    sat

    y

    uFiber pull out

    Interface: ZrOx 450Fiber volume: cf=0.6

    Budiansky 1995

    3 22

    23 ( 2 ) (2 3 )

    3f

    mc D D S D D S m mmcA

    rc

    mc

    f f mmc

    mc E c E

    2 f cD fm m f

    iE Ecc E r

    2 f

    Am m

    Rc fc E Ec E

    132 2(1 ) /S f f f m f R cm fl r c E E c E r

    ( / )(1 )f c S f

    tR

    sf

    am

    c E l rc E

    /sats fa ft c E

    Evans 1994

    A toughening method for tungsten is proposed based on the reinforcement of tungsten fibers (Wf/Wm composites) and engineered interfaces.

    The interfacial parameter determination results show that selected interfaces satisfy to the interfacial debonding criterion.

    The interfacial debonding and fiber sliding were demonstrated by micro-mechanical 3-point bending test.

    The predicted stress-strain curve of the Wf/Wmcomposites with multiple fibers agree with the theoretical one, supporting the primary motivation of the work.

    Interfacial fracture energy i of investigated interfaces

    The main focus of this work lies in the investigation of the interfacial fracture behavior of Wf/Wm composites with various engineered interfaces to demonstrate the feasibility of synthesizing a toughened Wf/Wmcomposite using the CMC toughening mechanism.

    Goal and focus of this work

    W matrix

    W wire

    W matrix

    W wire

    • W fiber, u> 2.5 GPa, u> 2%• Interface thickness m

    The fracture properties of the engineered interface are the key factors controlling the overall composite toughness.

    Micro-mechanical 3-point bending test (ZrOx 260)

    2 m

    W fiber topW C

    Interface delamination

    ca) oxide interface: ZrOx 450

    b) ductile interface: Cu 480

    c) lubricating interface: C 600

    Interface deformation and delamination can cause higher interfacial fracture energy.

    1 mmatrix

    typical W wire surface

    structure

    fiber

    ZrOx 450

    a

    ConclusionResult-Crack deflection demonstration Result-Behavior prediction of Wf/Wm composite with multiple fibers

    The calculated ratios lie between 0.003 and 0.034. satisfying the 0.25 criterion.

    The debonding criterion is satisfied !

    specimen thickness: 0.226mm

    y f f yield Rc /y f yield fE u f f uc

    2.1%u

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