2012 Composites in Construction

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    Composites in construction

    Jan Wastiels

    20 April 2012

    Content

    intro composite materials

    (G)FRC and applications

    ECC and applications

    TRC and applications vubonite

    tensile modelling

    processing

    vubonite applications

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    Composite materials

    strong and stiff fibres are embedded in a matrix

    fibres are oriented following structural needs

    with polymer matrix: high fibre fractions Vfarepossible

    result: lightweight and strong materials

    aerospace > aviation > transport > building

    building applications ?

    Comparison steel - flame retardant

    polyester composite

    E E/ f f/

    Steel 205 26 250 32

    Pol 2,5 1,7 50 35

    Polc 16,5 11 270 175

    E: stiffness modulus (GPa)

    E/: specific stiffness

    f: strength (MPa)

    f/: specific strength

    Pol: flame retardant polyester

    Polc: polyester composite with 20wt% UD glass fibres

    Conclusion:

    the composite improves much when specific properties are considered:

    absolute stiffness of the composite is poor, but specific stiffness is acceptable

    absolute strength of the composite is OK, but specific strength is very good

    BUT: drawbacks of polymer matrix: use of solvents, VOCs, bad fire resistance, high cost

    price, hazardous waste

    building applications ???

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    CIF5 Newcastle July

    10 20085

    An absolute fire resistant matrix for composites:

    vubonite

    Polyester - glass composite0 sec 15 sec

    30 sec 40 sec

    CIF5 Newcastle July

    10 20086

    An absolute fire resistant matrix for composites:

    vubonite

    M1 Polyester - glass composite

    65 sec60 sec

    20 sec 40 sec

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    CIF5 Newcastle July

    10 20087

    An absolute fire resistant matrix for composites:

    vubonite

    M1 Polyester - glass composite

    65 sec60 sec

    20 sec 40 sec

    Cement matrix?

    Polyester Cement C/P

    E (GPa) 2.5 25 x 10

    fc (MPa) 40 40 =

    ft (MPa) 50 5 /10

    mu()

    20 0.2 /100

    matrix fails in tension long before fibres!

    composite stress at matrix cracking is very low!

    behaviour in cracked stage is normal

    E : stiffness modulus

    fc : compressive strength

    ft : tensile strength

    mu : matrix tensile failure

    strain

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    Minimum amount of fibres

    Vf crit = (mu / fu ).Vm

    mu = 5 MPa

    fu = 2 GPa

    Vm 1 (> 0.95)

    Vf crit = 0.25 %

    Glass fibre reinforced cement (GRC)

    Traditional production technology: short fibres

    Typical 2 to 4%

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    Fibre length effect Short fibres: critical length lc lc = (fu . r)/fu

    fu 1 MPa

    r = 7 m (fibre) lc = 14 mm

    r = 0.1 mm (bundle) 200 mm

    in practice always l < lc

    pullout occurs

    efficiency l = 0.03 to 0.5

    Fibre orientation effect

    efficiency of oriented fibres is lower than 1

    different values for uncracked and crackedmatrix

    dependent on distribution of fibres (2D-3D)

    strongly dependent for cracked matrix onbending stiffness of fibres

    values between 1/6 and 3/

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    Combined efficiency

    for 2D distribution: = 3/8 . 3/10 . l/lc

    for individual fibres: = 0.11,

    thus Vf crit = 0.25%/0.11 = 2.3%

    for fibre bundles: < 0.01,

    thus Vf crit = 25%

    since Vf< 5%, pseudo plastic behaviour intension is hardly obtainable

    Consequences of production technique

    no tensile strength increase

    limited ductility

    hardly crack opening

    control by fibres

    no load bearing

    applications

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    Use of GRC: various

    Engineered Cement Composites (ECC)

    Vf= 2 % of short,

    random PVA fibres

    self compacting

    cement Ductile and very

    flexible, due to

    tuned interaction

    cement-fibres

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    ECC: behaviour in bending high ductility compared to conventional GRC

    however limited post-cracking stiffness

    ECC: behaviour in tension

    enormous ductility (3 to 7 %) and limited crack width

    but nearly no strain hardening (post-cracking stiffness)

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    Applications of ECC

    mainly surface repair of retaining walls, bridgedecks and dams

    Structural application needs

    compressive strength: is provided by the matrix

    ductility: can be solved (ECC)

    tensile strength significantly higher than the cement itself:cu = fu Vf

    significant post-cracking stiffness: Ec = EfVf enough fibres: Vf> Vf crit = (mu / fu).Vm controlled efficiency of fibres

    strict crack width control (see later)

    many strong, stiff and aligned fibres!

    cost price: glass fibres

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    Fibre Reinforced Cement TRCFRC - ECC

    Short fibres

    Distribution & orientation not

    controlled

    Low fibre content

    Concrete processing:- Casting

    - Pressure forming (plates)

    - Shotcrete

    Textile Reinforced Cement

    24

    TRCFRC - ECC

    Short fibres Prefabricated textiles

    Distribution & orientation not

    controlled

    Low fibre content

    Concrete processing:- Casting

    - Pressure forming (plates)

    - Shotcrete

    Carefully controlled orientation

    and distribution

    High fibre content possible

    Composite processing:- Hand lay-up

    - Pultrusion

    - Calendaring

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    TRC opportunities

    25

    - Lightweight constructions

    - Freeform constructions

    - High fibre volume fraction

    - Flexible reinforcement

    -Compressive AND tensile stresses

    structural material

    durability is very important issue

    - Limited concrete cover

    1. Felix Candela, Mexico,1958

    2. Heinz Isler, UK

    Applications of TRC: sandwich elements

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    Applications of TRC: thin walled elements

    Applications of TRC: diamond-shaped grid

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    Applications of TRC: pedestrian bridge

    Which cement?

    Traditional:production technique leads to limited VfE-glass must be replaced by AR-glass ($) for

    durability reasons

    Hydration products cause embrittlement withtime, even with AR-glass

    heavy coating is needed, so bad interaction cement-fibre

    and low efficiency

    Vubonite does not present these drawbacks

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    CIF5 Newcastle July

    10 200831

    An absolute fire resistant matrix for composites:

    vubonite

    Why (or what is) vubonite ?

    Powder component: based on the calciumsilicatemineral Wollastonite (CaSiO3)

    CIF5 Newcastle July

    10 200832

    An absolute fire resistant matrix for composites:

    vubonite

    Why (or what is) vubonite ?

    Powder component: based on the calciumsilicatemineral Wollastonite (CaSiO3)

    Liquid component: proprietary metal ion modified

    phosphoric acid

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    CIF5 Newcastle July

    10 200833

    An absolute fire resistant matrix for composites:

    vubonite

    Why (or what is) vubonite ?

    Powder component: based on the calciumsilicatemineral Wollastonite (CaSiO3)

    Liquid component: proprietary metal ion modifiedphosphoric acid

    Acid-base setting reaction after mixing

    CIF5 Newcastle July

    10 200834

    An absolute fire resistant matrix for composites:

    vubonite

    Why (or what is) vubonite ?

    Powder component: based on the calciumsilicatemineral Wollastonite (CaSiO3)

    Liquid component: proprietary metal ion modified

    phosphoric acid Acid-base setting reaction after mixing

    Fresh mixture is acidic (pH=1), but neutral (pH=7)after hardening: compatible with glass fibres

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    CIF5 Newcastle July

    10 200835

    An absolute fire resistant matrix for composites:

    vubonite

    Why (or what is) vubonite ?

    Powder component: based on the calciumsilicatemineral Wollastonite (CaSiO3)

    Liquid component: proprietary metal ion modifiedphosphoric acid

    Acid-base hardening reaction after mixing

    Fresh mixture is acidic (pH=1), but neutral (pH=7)after hardening: compatible with glass fibres

    Vubonite is always used in combination with fibresand/or fillers: it is a matrixor binderfor (fibre)composites, similar to organic resins like polyester

    Tensile experimental data

    0

    20

    40

    60

    80

    100

    120

    0 0,4 0,8 1,2 1,6

    strain(%)

    stress(MPa)

    0

    10

    20

    30

    40

    0,0 0,4 0,8 1,2 1,6 2,0

    strain (%)

    stress(MPa)

    0,0

    0,5

    1,0

    1,5

    2,0

    2,5

    3,0

    3,5

    4,0

    4,5

    5,0

    5,5

    0,0 1,0 2,0 3,0 4,0 5,0 6,0 7,0 8,0 9,0 10,0 11,0 12,0

    Elongation in mm/m

    Force in kN

    E-modulus of the matrix

    first crack in the matrix

    starting point of the crack pattern

    last crack in the matrix

    E-modulus of the reinforcement

    breaking point

    Random E-glass 10% (vubonite)

    UD E-glass 10% (vubonite)

    UD AR-glass 2% (OPC)

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    0

    5

    10

    15

    20

    25

    30

    0 0.2 0.4 0.6 0.8 1

    strain (%)

    stress (MPa)

    Stress-strain behaviour

    static loading

    matrixfibre

    matrix

    fibre

    matrix-fibreinterface

    Stress-strain behaviour

    static loading

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    ACK theory (Aveston, Cooper, Kelly)

    Three stages in tensile behaviour:

    uncracked

    multiple cracking

    crack opening

    Aligned UD

    reinforcement

    ACK Stage 1

    Fibres and matrix linear elastic

    Perfect adhesion fibres-matrix

    Law of mixtures: Ec = EmVm + EfVf

    The end of stage 1 is reached when c = mu(and m = mu) : the first crack appears at a

    composite stress

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    ACK Stage 2

    At crack location: all load taken up by fibresVfmust be larger than Vf crit to avoid failure:

    Deterministic material properties: not onlyone crack appears at mc , but all possible

    cracksmultiple cracking stage

    ACK Stage 2

    Local high shear stress at interfacedebonding of fibre and matrix over length 0

    diameter 2r

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    ACK Stage 2 Constant frictional shear stress 0 at debonded

    interface stress transfer from fibres to matrix

    starting at crack after debonding length 0 the

    matrix stress again reaches mu

    In the debonded length no new crack can appear

    ACK Stage 2

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    ACK Stage 2

    In the end, the crack spacing x is everywherebetween 0 and 20

    mean crack spacing: x = 1.3370 the deformation increases due to the multiple

    cracking:

    with

    ACK Stage 3

    Fibres and matrix debonded over the wholelength everywhere frictional slip

    stress in matrix remains unchanged during

    loading all the extra load is taken up bythe fibres

    stiffness : EfVf (adapted law of mixtures)

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    0

    5

    10

    15

    20

    25

    30

    0 0.2 0.4 0.6 0.8 1strain (%)

    stress(MPa)

    experimental

    theory ACK

    ACK-Theory versus experiment

    mu1

    mu2

    mu3

    EfVf

    Stress-strain behaviour

    static loading

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    Weibull distribution function for matrix tensile strength (Curtin 1998)

    c

    c

    1

    exp1:

    =

    0

    m

    R

    cXxngcrackspaci

    +=

    xEc

    cc

    0

    1

    1

    =

    104

    1

    cff

    ccE

    x

    VE

    Stochastic Cracking Model

    0

    5

    10

    15

    20

    25

    30

    0 0.2 0.4 0.6 0.8 1strain (%)

    stress(MP

    a)

    experimentaltheory stochastic crackingtheory ACK

    Stochastic cracking model vs. experiment

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    Example: glass fibre chopped mat 2%

    0

    5

    10

    15

    20

    25

    30

    0 0,5 1 1,5 2strain (%)

    stress(MPa)

    Vf= 2%

    0

    1

    2

    3

    4

    5

    6

    0 5 10 15 20 25

    Vf (%)

    X(mm)

    ductility: no

    strength: 7 MPa

    post-cracking stiffness: 0.5 GPa

    Example: glass fibre chopped mat 5%

    0

    5

    10

    15

    20

    25

    30

    0 0,5 1 1,5 2strain (%)

    stress(MPa)

    Vf= 5%

    0

    1

    2

    3

    45

    6

    0 5 10 15 20 25

    Vf (%)

    X(mm)

    ductility: yes

    strength: 16 MPa

    post-cracking stiffness: 1.2 GPa

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    Example: glass fibre chopped mat 10%

    0

    5

    10

    15

    20

    25

    30

    0 0,5 1 1,5 2strain (%)

    stress(MPa)

    Vf= 10%

    0

    1

    2

    3

    4

    5

    6

    0 5 10 15 20 25

    Vf (%)

    X(mm)

    ductility: yes

    strength: 33 MPa

    post-cracking stiffness: 2.4 GPa

    Example: glass fibre chopped mat 20%

    0

    5

    10

    15

    20

    25

    30

    0 0,5 1 1,5 2strain (%)

    stress(MPa)

    Vf= 20%

    0

    1

    2

    3

    45

    6

    0 5 10 15 20 25

    Vf (%)

    X(mm)

    Conclusion: Vf has an important effect on the stress-strain curve

    ductility: yes

    strength: 67 MPa

    post-cracking stiffness: 4.8 GPa

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    Low Vf leads to large crack spacing and crack opening. For V f higher than 5%,crack spacing is dense, and average crack width is limited for all stress levels

    vubonite composite: crack width and spacing

    0

    10

    20

    30

    40

    50

    60

    70

    0 10 20 30stress (MPa)

    crackwidth(m) Vf = 2%

    Vf = 5%

    Vf = 10%

    Vf = 20%

    0

    10

    20

    30

    40

    50

    0 10 20 30

    stress (MPa)

    x(mm)

    Vf = 20%

    Vf = 10%

    Vf = 5%

    Vf = 2%

    1

    m

    m

    no load 15% 30% max load

    1mm

    T

    Textile fibre structures for

    vubonite

    Biaxial

    Multiaxial Knitted

    Leno-woven

    Spacer with

    varyingdistances

    Spacer

    Circular

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    Composite processing

    Cement composite processing

    30 to 50% particles: non-Newtonian viscous

    fluid with non-zero yield stress separation

    and filtering

    58

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    CIF5 Newcastle July

    10 200859

    An absolute fire resistant matrix for composites:

    vubonite

    Processing: hand lay-up

    1 4

    2 3

    CIF5 Newcastle July

    10 200860

    An absolute fire resistant matrix for composites:

    vubonite

    Processing: vacuum bagging

    1 3

    2

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    CIF5 Newcastle July

    10 200861

    An absolute fire resistant matrix for composites:

    vubonite

    Processing: pultrusion

    CIF5 Newcastle July

    10 200862

    An absolute fire resistant matrix for composites:

    vubonite

    Processing: pultrusion

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    CIF5 Newcastle July

    10 200863

    An absolute fire resistant matrix for composites:

    vubonite

    Processing: spray-up

    Self compacting impregnator

    Translation of the hand lay-up processing intoa mechanised and automatic process: well

    controlled wetting and impregnation with

    precise fibre volume

    64

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    Self compacting impregnator

    Translation of the hand lay-up processing intoa mechanised and automatic process: well

    controlled wetting and impregnation with

    precise fibre volume

    65

    Self compacting impregnator

    Feeding of textile fibre

    structure (2 to 4 textiles)

    66

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    Self compacting impregnator

    Continuously refreshed

    matrix material

    67

    Self compacting impregnator

    Grooves for controlled wetting

    and impregnation of fibres

    68

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    Self compacting impregnator

    Adjustable calendar pressure for

    controlled impregnation

    (pneumatic muscles up to 12 kN)

    69

    Self compacting impregnator

    Adjustable pressure for

    compaction (self weight 600N,

    eventually increased to 3kN)

    70

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    Self compacting impregnator

    Continuous process 300m/hour

    through movable support

    (thickness buildup)

    71

    1 min 5 min400C

    14 min

    After 120 min

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    CIF5 Newcastle July

    10 200873

    An absolute fire resistant matrix for composites:

    vubonite

    Applications

    Intelli Fire Wall , used to separate high power transformers in case of calamity.

    Each wall is composed of 24 lightweight panels and can be erected in very short time.

    The walls are designed to withstand the forces of an explosion and the heat of a

    transformer fire

    CIF5 Newcastle July

    10 200874

    An absolute fire resistant matrix for composites:

    vubonite

    Applications

    Fire protective cable duct to be used in large buildings, industry, tunnels, etc.

    This shape has been designed for pultrusion

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    CIF5 Newcastle July

    10 200875

    An absolute fire resistant matrix for composites:

    vubonite

    Applications

    Thin composite mould for the thermoforming

    of curved glass panels (size approx. 50 cm)

    CIF5 Newcastle July

    10 200876

    An absolute fire resistant matrix for composites:

    vubonite

    Applications

    Protection of electricity and data transmissionpoles against bush fires in California

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    CIF5 Newcastle July

    10 200877

    An absolute fire resistant matrix for composites:

    vubonite

    Applications

    Fire resistant piping

    CIF5 Newcastle July

    10 200878

    An absolute fire resistant matrix for composites:

    vubonite

    Applications

    Thermal insulation forConstant volumecombustion chamber(UGent)

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    CIF5 Newcastle July

    10 200879

    An absolute fire resistant matrix for composites:

    vubonite

    Applications

    Prototype bridge with sandwich panels

    CIF5 Newcastle July

    10 200880

    An absolute fire resistant matrix for composites:

    vubonite

    Applications

    Sculptures

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    CIF5 Newcastle July

    10 200881

    An absolute fire resistant matrix for composites:

    vubonite

    Applications

    Decoration of the main desk in the health center

    of luxury hotels in Slovenia and Italy. Ivan Kisovec

    CIF5 Newcastle July

    10 200882

    An absolute fire resistant matrix for composites:

    vubonite

    Applications

    Rubensplein Knokke Franz West

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    Uplifting the roof of the operahouse Unter der Linden Berlin:

    vubonite screen transparent to sound