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Molar group contributions

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  • Molar Group Contributions to Polymer Flammability

    Richard N. Walters,1 Richard E. Lyon2

    1Galaxy Scientific Corporation, 3120 Fire Road, Egg Harbor Township, New Jersey 082342Fire Safety Section AAR-440, Airport and Aircraft Safety Research and Development, William J. Hughes TechnicalCenter, Federal Aviation Administration, Atlantic City International Airport, New Jersey 08405

    Received 8 March 2002; accepted 26 April 2002

    ABSTRACT: The specific heat-release rate is the molecu-lar-level fire response of a burning polymer. The FederalAviation Administration obtains the specific heat-releaserate of milligram samples by analyzing the oxygen con-sumed by the complete combustion of the pyrolysis gasesduring a linear heating program. Dividing the specific heat-release rate (W/g) by the rate of the temperature rise (K/s)of a sample during a test gives a material fire parameter withthe units (J/g K) and significance of the heat (release) capac-ity. The heat-release capacity appears to be a true materialproperty that is rooted in the chemical structure of the

    polymer and is calculable from additive molar group con-tributions. Hundreds of polymers of known chemical com-positions have been tested to date, providing over 40 differ-ent empirical molar group contributions to the heat-releasecapacity. Measured and calculated heat-release capacitiesfor over 80 polymers agree to within 15%, suggesting anew capability for predicting flammability from the polymerchemical structure. 2002 Wiley Periodicals, Inc. J Appl PolymSci 87: 548563, 2003

    Key words: plastics; calculations; thermal properties

    INTRODUCTION

    The additivity of molar group contributions to the phys-ical and chemical properties of polymers is the basis ofan empirical methodology for relating the chemicalstructure to the polymer properties.13 The early work inthis area4 focused on calculating the heats of combustionfrom the individual atoms comprising small molecules.However, performing calculations for large (polymer)molecules based on the interactions of the individualatoms can be very difficult.2 A simpler approach tocorrelating the polymer chemical structure to the prop-erties is to group the atomic contributions into charac-teristic structural elements (e.g., OCH3), determine thevalue of the group contribution to the property of inter-est parametrically, and add these group contributionsaccording to their molar fractions in the polymer repeatunit. This method has been used to relate the chemicalstructures of polymers to their thermal, chemical, optical,and mechanical properties with excellent results.13 Ofparticular interest in this context is the ability to predictthe thermal stability parameters of polymers (pyrolysisactivation energy, thermal decomposition temperature,and char/fuel fraction) from additive molar group con-tributions.1

    A prerequisite for any structureproperty correla-tion is the ability to identify and reproducibly measurethe intrinsic property of interest. In the area of poly-

    mer flammability, no single material property hasbeen correlated with fire performance, nor does anytest measure fire performance unambiguously be-cause the burning rate, ignitability, flammability, andheat-release rate are not intrinsic properties. Rather,they are extrinsic quantities resulting from the reac-tion of a macroscopic polymer sample to severe ther-mal exposure. Because the sample size in a flamma-bility or fire test is orders of magnitude larger than thechemical process zone,57 heat and mass transfer dom-inate the fire response. Therefore, an intrinsic materialproperty for use by scientists in designing fire-resis-tant polymers is not obtainable from standard fire orflammability tests.

    Recently, a material fire parameter with the unitsand significance of the heat-release capacity57 hasbeen identified that appears to be a good predictor ofthe fire response and flammability of polymers. Aquantitative laboratory pyrolysiscombustion methodfor directly measuring the heat-release capacity hasbeen reported.810 This article provides empirical mo-lar group contributions to the heat-release capacitythat allow its calculation from the polymer chemicalstructure. The relationship between the measured (orcalculated) heat-release capacity of a polymer and itsfire behavior or flammability is described.

    THEORY

    The solid-state thermochemistry of flaming combus-tion57 reveals a material fire parameter that has theunits of the heat (release) capacity (J/g K):

    Correspondence to: R. N. Walters ([email protected]).

    Journal of Applied Polymer Science, Vol. 87, 548563 (2003) 2002 Wiley Periodicals, Inc.

  • c hc

    01 EaeRTp

    2 (1)

    The heat-release capacity (c) is a combination of thethermal stability and combustion properties, each ofwhich is known to be calculable from additive molargroup contributions.1 The component material prop-erties are the heat of complete combustion of the py-rolysis gases [hc

    0 (J/g)], the weight fraction of the solidresidue after pyrolysis or burning [ (g/g)], the globalactivation energy for the single-step mass-loss processor pyrolysis [Ea (J/mol)], and the temperature at thepeak mass-loss rate [Tp (K)] in a linear heating pro-gram at a constant rate [ (K/s)]. The constants in eq.(1) are the natural number (e) and the gas constant (R).Equation (1) shows the heat-release capacity to be aparticular function of the thermal stability and com-bustion properties, each of which is known to be cal-culable from additive molar group contributions.1

    Consequently, c itself is a material property andshould be calculable from the same (or similar) molargroups as the component properties as long as thereare no interactions between the chemical structuralunits. Along with this assumption of group additivity,there is the postulate that for a polymer repeat unit ofmolar mass M, there is a molar heat-release capacity[ (J/mol K)] whose functional form is eq. (1) butwhich has thermal stability and combustion propertieswritten as the molar quantities H, V, E, and Y/M inplace of hc

    0, (1 ), Ea, and Tp, respectively. If eachchemical group i in the polymer adds to the compo-nent molar properties according to its molar fraction niin the repeat unit,

    HVE

    eRY/M2

    i

    niHi i

    niVi i

    niEieR

    i

    niYi/Mi 2 (2)

    where Hi, Vi, Ei, Yi, and Mi are the molar heat ofcombustion, molar fraction of fuel, molar activationenergy, molar thermal decomposition function,1 andmolar mass of component i, respectively. Expandingthe summations in eq. (2) and retaining only the non-interacting terms for which i j k (i.e., neglectingterms containing products and quotients with mixedindices), we have the following:

    i

    niHiViEi

    eRYi/Mi2

    i

    nii (3)

    Equation (3) shows that there is a molar group contri-bution to the heat-release capacity i that adds ac-cording to its molar fraction in the repeat unit of thepolymer. If Ni and Mi are the number of moles and themolar mass, respectively, of group i in the polymerwith the repeat unit molar mass M

    ni Ni

    i

    Niand M

    i

    niMi i

    Nii

    NiMi

    then the heat-release capacity on a mass basis is

    c

    M

    i

    nii

    i

    niMi

    i

    Nii

    i

    NiMi(4)

    Equations (2)(4) provide the physical basis for anadditive heat-release capacity function, but the valuesof the molar contributions of chemical groups must bederived empirically (i.e., experimentally). To this end,the heat-release capacities of more than 200 polymerswith known chemical structures have been measuredwith the measurement technique described later, andthese experimental values have been used to generateover 40 group contributions.11,12

    Figure 1 Schematic diagram of the pyrolysiscombustion flow calorimeter.

    MOLAR GROUP CONTRIBUTIONS 549

  • EXPERIMENTAL

    Materials

    Polymer samples were unfilled, natural, or virgin-grade resins obtained from Aldrich (Milwaukee, WI)and Polysciences, Inc. (Warrington, PA), and researchuniversities or directly from the manufacturers. Theoxygen and nitrogen gases used for calibration andtesting, obtained from Matheson Gas Products(Bridgeport, NJ), were dry and greater than 99.99%pure.

    Methods

    A pyrolysiscombustion flow calorimeter810 wasused for all experiments (see Fig. 1). In this device, apyrolysis probe (Pyroprobe 2000, CDS Analytical, Ox-ford, PA) is used to thermally decompose milligram-size samples in flowing nitrogen at a controlled heat-ing rate. The samples are heated at a constant rate(typically 4.3 K/s) from a starting temperature that isseveral degrees below the onset degradation temper-ature of the polymer to a maximum temperature of1200 K (930C). The 930C final temperature ensuresthe complete thermal degradation of organic polymersso that the total capacity for heat release is measuredduring the test and eq. (1) applies. Flowing nitrogensweeps the volatile decomposition products from theconstant-temperature (heated) pyrolysis chamber, andoxygen is added to obtain a nominal composition of4:1 N2/O2 before a 900C furnace is entered for 60 s toeffect complete nonflaming combustion. The combus-tion products (carbon dioxide, water, and possiblyacid gases) are then removed from the gas stream with

    Ascarite and Drierite scrubbers. The mass flow rateand oxygen consumption of the scrubbed combustionstream are measured with a mass flowmeter and zir-conia oxygen analyzer (Panametrics model 350,Waltham, MA), respectively.

    The specific heat-release rate (Qc) in the pyrolysiscombustion flow calorimeter is determined from oxygenconsumption measurements with the assumption that13.1 kJ of heat is released per gram of diatomic oxygenconsumed by combustion.1316 Because Qc is equal to thefractional mass-loss rate multiplied by the heat of com-plete combustion of the pyrolysis products,

    Qct E

    m0O2t

    hc,v0 tm0

    dmtdt (5)

    where E 13.1 0.6 kJ/g of O2, O2 is the instan-taneous mass consumption rate of oxygen, m0 is theinitial sample mass, hc,v

    0 is the instantaneous heat ofcomplete combustion of the volatile pyrolysis prod-ucts, and dm/dt is the instantaneous mass-loss (fuel-generation) rate of the sample during the test. Theadvantage of synchronized oxygen consumption cal-orimetry for determining the specific heat-release rateis the ease and speed of the method in comparisonwith the simultaneous measurement of the mass-lossrate of the solid and the heat of combustion of thepyrolysis gases.17 At Tp, the specific heat-release ratehas an analytical form:57,18

    Qcmax

    Em0

    O2max

    hc,v0 t

    m0dmtdt

    max

    hc01Ea

    eRTp2

    (6)

    Figure 2 Specific heat-release rates for several polymers measured with the microscale calorimeter.

    550 WALTERS AND LYON

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    MOLAR GROUP CONTRIBUTIONS 551

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    552 WALTERS AND LYON

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    MOLAR GROUP CONTRIBUTIONS 553

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    554 WALTERS AND LYON

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    S)

    AB

    S,Po

    lysc

    ienc

    es[9

    003-

    56-9

    ]C

    15H

    17N

    669

    36.6

    021

    1.31

    Poly

    (1,4

    -but

    aned

    iol

    tere

    phth

    alat

    e)(P

    BT

    )Po

    lysc

    ienc

    es[2

    6062

    -94-

    2]C

    12H

    12O

    447

    420

    .31.

    522

    0.22

    Poly

    (hex

    amet

    hyle

    nead

    ipam

    ide)

    Nyl

    on6/

    6,Po

    lysc

    ienc

    es[3

    2131

    -17-

    2]C

    12H

    22O

    2N

    261

    527

    .40

    226.

    32

    Poly

    azom

    ethi

    neU

    MA

    SS[N

    A]

    C15H

    9N

    336

    8.7

    77.8

    231.

    26

    Poly

    (1,4

    -phe

    nyle

    neet

    her

    sulf

    one)

    (PE

    S)B

    ASF

    Ult

    raso

    nE

    1010

    /N

    atur

    alB

    ASF

    [256

    67-4

    2-9]

    C12H

    8O

    3S

    115

    11.2

    29.3

    232.

    26

    Poly

    (p-p

    heny

    lene

    benz

    obis

    oxaz

    ole)

    (PB

    O)

    PBO

    ,Dow

    Che

    mic

    alC

    o.[8

    52-3

    6-8]

    C14H

    6O

    2N

    242

    5.4

    69.5

    234.

    21

    Poly

    (p-p

    heny

    lene

    tere

    phth

    alam

    ide)

    Kev

    lar,

    Dup

    ont

    [308

    069-

    56-9

    ]C

    14H

    10O

    2N

    230

    214

    .836

    .123

    8.25

    Poly

    (m-p

    heny

    lene

    isop

    htha

    lam

    ide)

    Nom

    ex,D

    upon

    t[2

    4938

    -60-

    1]C

    14H

    10O

    2N

    252

    11.7

    48.4

    238.

    25

    Poly

    (eth

    ylen

    ena

    phth

    ylat

    e)(P

    EN

    )E

    astm

    anC

    hem

    ical

    Co.

    [249

    68-1

    1-4]

    C14H

    10O

    430

    916

    .818

    .224

    2.23

    Dic

    yclo

    pent

    adie

    nyl

    bisp

    heno

    lcy

    anat

    ees

    ter

    XU

    -717

    87,D

    owC

    hem

    ical

    [135

    5-71

    -0]

    C17H

    17N

    O49

    320

    .127

    .125

    1.32

    Poly

    carb

    onat

    eof

    bisp

    heno

    lA

    (PC

    )Po

    lysc

    ienc

    es(M

    W

    32,0

    003

    6,00

    0)[2

    4936

    -68-

    3]C

    16H

    14O

    335

    916

    .321

    .725

    4.28

    MOLAR GROUP CONTRIBUTIONS 555

  • TA

    BL

    EI

    Con

    tinu

    ed

    Mat

    eria

    l(a

    bbre

    viat

    edna

    me)

    Tra

    de

    nam

    e,m

    anuf

    actu

    rer/

    supp

    lier

    CA

    Snu

    mbe

    rR

    epea

    tun

    itco

    mpo

    siti

    onR

    epea

    tun

    itst

    ruct

    ure

    Hea

    tre

    leas

    eca

    paci

    ty(J

    /g

    K)

    Tot

    alhe

    atre

    leas

    e(k

    J/g)

    Cha

    r(%

    )M

    W(g

    /m

    ol)

    Poly

    phos

    phaz

    ene

    Eyp

    el-A

    ,Pen

    nSt

    ate

    [NA

    ]C

    14H

    14PN

    O3

    204

    21.9

    2025

    9.24

    Poly

    (dic

    hlor

    oeth

    yld

    iphe

    nyl

    ethe

    r)R

    ice

    Uni

    vers

    ity

    (MW

    9350

    )[N

    A]

    C14H

    8O

    Cl 2

    165.

    257

    .126

    3.12

    Cya

    no-s

    ubst

    itut

    edK

    evla

    rU

    MA

    SS[N

    A]

    C15H

    9N

    3O

    254

    9.1

    58.3

    263.

    26

    Bis

    phen

    olE

    poly

    cyan

    urat

    eA

    roC

    yL

    -10,

    Cib

    aSp

    ecia

    lty

    Che

    mic

    als

    [470

    73-9

    2-7]

    C16H

    12O

    2N

    231

    614

    .741

    .926

    4.28

    Bis

    phen

    olA

    poly

    cyan

    urat

    eA

    roC

    yB

    -10,

    Cib

    aSp

    ecia

    lty

    Che

    mic

    als

    [115

    6-51

    -0]

    C17H

    14O

    2N

    228

    317

    .636

    .327

    8.31

    Poly

    (hex

    amet

    hyle

    nese

    baca

    mid

    e)N

    ylon

    6/10

    ,Po

    lysc

    ienc

    es[9

    008-

    66-6

    ]C

    16H

    30O

    2N

    287

    835

    .70

    282.

    43

    Poly

    (eth

    eret

    her

    keto

    ne)

    (PE

    EK

    )45

    0F,V

    ictr

    exU

    SA[2

    9658

    -26-

    2]C

    19H

    12O

    315

    512

    .446

    .528

    8.3

    Poly

    (silo

    xyte

    traa

    lkyl

    biph

    enyl

    ene

    oxid

    e)(P

    SA)

    Gen

    eral

    Ele

    ctri

    c[N

    A]

    C18H

    18Si

    O2

    119

    15.7

    60.1

    294.

    42

    Poly

    (eth

    erke

    tone

    keto

    ne)

    (PE

    KK

    )G

    040

    (vir

    gin

    flak

    e),

    Dup

    ont

    [749

    70-2

    5-5]

    C20H

    12O

    396

    8.7

    60.7

    300.

    31

    Tet

    ram

    ethy

    lbi

    sphe

    nol

    Fpo

    lycy

    anur

    ate

    Aro

    Cy

    M-1

    0,C

    iba

    Spec

    ialt

    yC

    hem

    ical

    [101

    657-

    77-6

    ]C

    19H

    18O

    2N

    228

    017

    .435

    .430

    6.36

    556 WALTERS AND LYON

  • TA

    BL

    EI

    Con

    tinu

    ed

    Mat

    eria

    l(a

    bbre

    viat

    edna

    me)

    Tra

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    Snu

    mbe

    rR

    epea

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    mpo

    siti

    onR

    epea

    tun

    itst

    ruct

    ure

    Hea

    tre

    leas

    eca

    paci

    ty(J

    /g

    K)

    Tot

    alhe

    atre

    leas

    e(k

    J/g)

    Cha

    r(%

    )M

    W(g

    /m

    ol)

    Bis

    phen

    olC

    poly

    carb

    onat

    eB

    PCPC

    ,Gen

    eral

    Ele

    ctri

    c[N

    A]

    C15H

    8O

    3C

    l 229

    3.0

    50.1

    307.

    13

    Poly

    benz

    imid

    azol

    e(P

    BI)

    CE

    LA

    ZO

    LE

    PBI,

    Hoe

    chst

    Cel

    anes

    e[2

    5928

    -81-

    8]C

    20H

    12N

    436

    8.6

    67.5

    308.

    34

    Poly

    (hex

    amet

    hyle

    ned

    odec

    ane

    dia

    mid

    e)N

    ylon

    6/12

    ,Po

    lysc

    ienc

    es[2

    6098

    -55-

    5]C

    18H

    34N

    2O

    270

    730

    .80

    310.

    48

    Bis

    phen

    olC

    ,po

    lycy

    anur

    ate

    BPC

    CE

    ,Cib

    aSp

    ecia

    lty

    Che

    mic

    als

    [NA

    ]C

    16H

    8O

    2C

    l 224

    4.2

    53.3

    331.

    16

    Bis

    phen

    olA

    epox

    y,ca

    taly

    tic

    cure

    phen

    oxy

    A

    DE

    R-3

    32,D

    owC

    hem

    ical

    [001

    675-

    54-3

    ]C

    21H

    24O

    465

    726

    .03.

    934

    0.42

    Phen

    olph

    thal

    ein

    poly

    carb

    onat

    eD

    owC

    hem

    ical

    [NA

    ]C

    21H

    12O

    528

    849

    .834

    4.32

    Poly

    (am

    ide

    imid

    e)(P

    AI)

    TO

    RL

    ON

    4203

    L,

    Am

    oco

    [429

    55-0

    3-3]

    C15H

    8O

    3N

    233

    7.1

    53.6

    354.

    36

    Nov

    olac

    poly

    cyan

    urat

    ePr

    imas

    etPT

    -30,

    Alli

    edSi

    gnal

    XU

    -371

    ,Cib

    a[1

    7345

    2-35

    -2]

    [309

    44-9

    2-4]

    C23H

    15O

    3N

    312

    29.

    951

    .938

    1.39

    Poly

    imid

    e(P

    I)A

    ldri

    ch[2

    6023

    -21-

    2]C

    22H

    10O

    5N

    225

    6.6

    51.9

    382.

    33

    MOLAR GROUP CONTRIBUTIONS 557

  • TA

    BL

    EI

    Con

    tinu

    ed

    Mat

    eria

    l(a

    bbre

    viat

    edna

    me)

    Tra

    de

    nam

    e,m

    anuf

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    rer/

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    lier

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    mbe

    rR

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    tun

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    mpo

    siti

    onR

    epea

    tun

    itst

    ruct

    ure

    Hea

    tre

    leas

    eca

    paci

    ty(J

    /g

    K)

    Tot

    alhe

    atre

    leas

    e(k

    J/g)

    Cha

    r(%

    )M

    W(g

    /m

    ol)

    Hex

    afluo

    robi

    sphe

    nol

    Apo

    lycy

    anur

    ate

    Aro

    Cy

    F-10

    ,Cib

    aSp

    ecia

    lty

    Che

    mic

    als

    [327

    28-2

    7-1]

    C17H

    8O

    2N

    2F 6

    322.

    355

    .238

    6.25

    Bis

    phen

    olC

    epox

    yB

    PCE

    [NA

    ]C

    20H

    18O

    4C

    l 250

    610

    3639

    3.26

    Bis

    phen

    olM

    poly

    cyan

    urat

    eA

    roC

    yX

    U-3

    66,C

    iba

    Spec

    ialt

    yC

    hem

    ical

    s[1

    2766

    7-44

    -1]

    C26H

    24O

    2N

    223

    922

    .526

    .439

    6.49

    Poly

    (phe

    nyl

    sulf

    one)

    Rad

    elR

    5200

    ,Am

    oco

    [258

    39-8

    1-0]

    C24H

    16SO

    415

    311

    .338

    .440

    0.45

    Bis

    phen

    olC

    poly

    aryl

    ate

    BPC

    PA,U

    MA

    SS[N

    A]

    C22H

    12O

    4C

    l 221

    7.6

    42.7

    411.

    02

    Bip

    heno

    lph

    thal

    onit

    rile

    Nav

    y[N

    A]

    C28H

    14N

    4O

    215

    3.5

    78.8

    438.

    44

    Poly

    sulf

    one

    ofbi

    sphe

    nol

    APS

    FU

    del

    ,Am

    oco

    [251

    35-5

    7-7]

    C27H

    22O

    4S

    345

    19.4

    28.1

    442.

    53

    LaR

    C-1

    AN

    ASA

    Lan

    gley

    [105

    030-

    42-0

    ]C

    28H

    14N

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    638

    6.7

    5747

    4.43

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    xyN

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    ac,

    cata

    lyti

    ccu

    reph

    enox

    yN

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    N-4

    38,D

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    ical

    [028

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    ]C

    10H

    11O

    246

    18.9

    15.9

    474.

    55

    Bis

    phen

    olA

    phth

    alon

    itri

    leU

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    avy

    [NA

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    31H

    20N

    4O

    240

    5.9

    73.6

    480.

    52

    Tec

    hnor

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    [NA

    ]C

    34H

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    513

    115

    .341

    .856

    8.59

    Bis

    phen

    olA

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    thal

    onit

    rile

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    .Nav

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    C31H

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    92.

    863

    .858

    8.46

    558 WALTERS AND LYON

  • The rate-independent heat-release capacity is obtainedfrom eq. (6) by the division of the maximum specificheat-release rate by the constant sample heating rate[ (K/s)]:

    c Qc

    max

    Em0

    O2max

    hc01 Ea

    eRTp2 (7)

    The quantities measured in the test are the initial samplemass and Qc (W/g). The time integration of the specificheat-release rate gives the total heat released by thecomplete combustion of the pyrolysis gases per unit ofthe initial sample mass [hc

    0 (J/g)]. c (J/g K) is calculatedfrom the peak specific heat-release rate and the linearheating rate of the sample according to eq. (7). Weighingthe sample after the test allows for the calculation of (g/g) and the average heat of complete combustion perunit mass of volatiles.

    RESULTS

    Pyrolysiscombustion flow calorimeter data for the spe-cific heat-release rates of polyethylene (PE), polypro-pylene (PP), polystyrene (PS), an acrylonitrilebuta-dienestyrene terpolymer (ABS), poly(methyl methacry-late) (PMMA), poly(ethylene terephthalate) (PET),poly(ether ether ketone) (PEEK), and polybenz-imidazole (PBI) are shown in Figure 2, having beenhorizontally shifted for clarity. Dividing the maximumspecific heat-release rate (W/g) measured during the test(peak height in Fig. 2) by the constant sample heatingrate ( 4.3 K/s in these tests) gives the heat-releasecapacity of the polymer (J/g K) for materials that ther-mally decompose in a single step. Materials exhibitingmultiple heat-release peaks are beyond the scope of thisreport and will be addressed in the future.

    The measured heat-release capacities for more than100 polymers with known chemical structures areshown in Table I. These data have been used to gen-erate the group contributions shown in Table II. Themolar group contributions were obtained by i beingtreated as adjustable parameters in the linear systemof equations for polymers with known chemical struc-tures and measured c values. The optimization cal-culation continued until the sum of the squares of therelative error between the measured c value and thevalue calculated from group contributions was a min-imum. The calculation converged rapidly to theunique i values listed in Table II, which were inde-pendent of initial estimates.

    Figure 3 is a plot of the calculated and measuredheat-release capacities for over 80 polymers for whichoptimized i values were determined. The correlationcoefficient between the measured and predicted heat-release capacities is r 0.96, and the average relativeerror is 15%.

    TA

    BL

    EI

    Con

    tinu

    ed

    Mat

    eria

    l(a

    bbre

    viat

    edna

    me)

    Tra

    de

    nam

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    anuf

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    rer/

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    lier

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    ruct

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    tre

    leas

    eca

    paci

    ty(J

    /g

    K)

    Tot

    alhe

    atre

    leas

    e(k

    J/g)

    Cha

    r(%

    )M

    W(g

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    ol)

    Poly

    (eth

    erim

    ide)

    (PE

    I)U

    ltem

    1000

    ,G

    ener

    alE

    lect

    ric

    [611

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    C37H

    24O

    6N

    212

    111

    .849

    .259

    2.61

    Poly

    este

    rof

    hyd

    roxy

    benz

    oic

    and

    hyd

    roxy

    napt

    hoic

    acid

    s

    Vec

    tra

    CL

    CP

    (vir

    gin/

    unfi

    lled

    ),H

    oech

    stC

    elan

    ese

    [706

    79-9

    2-4]

    C39H

    22O

    10

    164

    11.1

    40.6

    650.

    6

    LaR

    C-T

    OR

    NA

    SAL

    angl

    ey[1

    9198

    5-77

    -0]

    C44H

    29N

    4O

    3P

    135

    11.7

    6369

    2.71

    LaR

    C-C

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    gley

    [790

    62-5

    5-8]

    C37H

    18N

    2O

    6F 6

    143.

    457

    700.

    55

    LaR

    C-C

    P1N

    ASA

    Lan

    gley

    [871

    86-9

    4-5]

    C46H

    22N

    2O

    6F 1

    213

    2.9

    5292

    6.66

    NA

    not

    appl

    icab

    le;M

    W

    mol

    ecul

    arw

    eigh

    t.

    MOLAR GROUP CONTRIBUTIONS 559

  • Calculation of the Heat-Release Capacity

    The following example illustrates the calculation ofthe heat-release capacity from molar group contribu-

    tions for a diglycidyl ether of bisphenol A (BPA ep-oxy) cured by anionic ring-opening polymerization.This polymer has the following repeat unit chemicalstructure:

    TABLE IIStructural Groups and Their Molar Contribution to the Heat Release Capacity

    Structural groupContribution(kJ/mol K) Structural group

    Contribution(kJ/mol K) Structural group

    Contribution(kJ/mol K)

    118a OH 8.1 OOH 19.8

    77.0 {NH}

    7.6 OBr 22.0

    69.5 OCH2OOO 4.18O

    OCO22.0

    30.6 {CF2}

    1.8 23.2a

    29.5 0.1 25.5

    28.8 8.8 OCl 34.7

    28.3 OSO 10.9a 36.4a

    26.6 OOO 11.6O

    OOOCOOOPendant: 39.5

    Backbone: 13.7

    22.5 13.8 }ON{

    43.0a

    19.0 ONH2 13.9a

    O

    OOOCOOO 49.0

    18.7 OCF3 14.8POSiOP

    53.5a

    16.7 OC'N 17.6 66.7

    15.1 18.9a 74.5

    9.7 19.2 76.7

    a Molar group contribution derived from a single polymer.

    560 WALTERS AND LYON

  • The polymer repeat unit consists of six basic chemicalgroups, and the heat-release capacity is calculatedfrom the associated Ni, Mi, and i values for thesegroups, which are listed in Table III.

    The molar heat-release capacity is obtained by thesumming of the group contributions according to theirmolar fraction in the repeat unit and division by themolar mass of the repeat unit to give the heat-releasecapacity on a mass basis (J/g K).

    c

    M

    i

    nii

    i

    niMi

    i

    Nii

    i

    NiMi

    204.5 kJ/mol K340 g/mol

    601 J/g K

    The predicted value of 601 J/g K compares reasonably wellwith the measured value of 657 J/g K for this polymer.

    Heat-Release Capacity and Fire Hazard

    The primary indicator of the fire hazard of a materialis the heat-release rate in forced flaming combustion.19

    Figure 4 is a plot of the average flaming heat-releaserate of samples (10 cm 10 cm 0.64 cm, 80 g) ofpure polymer measured in a fire calorimeter at anexternal heat flux qext 50 kW/m

    2) according to stan-dard methods2022 versus the measured heat-releasecapacity. Proportionality is observed between the av-erage flaming heat-release rate of kilogram-size sam-ples and the heat-release capacity of milligram-sizesamples of the same polymer with a slope of 1.0 (kg/s)/m2/K, which is in general agreement with predic-tions for steady burning at this external heat flux.57

    Figure 3 Calculated and measured heat-release capacities for 80 pure polymers.

    TABLE IIIGroup Contributions Used in the Calculation of the Heat Release Capacity of Bisphenol A Epoxy

    Chemical group (i) N Mi (g/mol)

    (kJ/mol K)NiMi

    (g/mol)Ni

    (kJ/mol K)

    C

    1 12 28.3 12 28.3

    CH

    CH22 13 26.6 26 53.2

    4 14 16.7 56 66.8

    CH3 2 15 22.5 30 45.0

    2 76 28.8 152 57.6

    OOO 4 16 11.6 64 46.4Total 340 204.5

    MOLAR GROUP CONTRIBUTIONS 561

  • Consequently, c is a reasonable predictor of the firehazard with an empirical correlation (e.g., Fig. 4) orphysically based calculations.57

    Heat-Release Capacity and Flammability

    Flammability is taken here to mean the tendency of athin sample of a material ignited by a small flame tocontinue burning in the absence of external radiantheat after the removal of the ignition source. Self-extinguishing behavior in these tests implies a certainresistance to ignition and/or flame propagation, andstandard methods have been developed to measurethis characteristic. These flame tests are widely used torank the burning propensity of combustible solids, butthey do not yield any material property information.Two common flammability test methods are the Un-derwriters Laboratories UL 94 test for upward vertical(V) and horizontal burning (HB)23 and the criticaloxygen concentration for flame extinguishment or lim-iting oxygen index (LOI) in downward burning.24

    In flammability tests, the flame heat flux at thesample tip must provide all of the heat energy tocontinue the burning process after the removal of theBunsen burner (UL 94) or methane diffusion flame(LOI) used to cause ignition. If the heat flux from thesample surface flame is constant (UL 94 test) or in-creases in a known way with oxygen concentration(LOI), the criterion for self-extinguishing behavior inthese tests can be formulated in terms of a criticalheat-release capacity if it is assumed that a minimumheat-release rate of about 100 kW/m2 25 is needed tosustain flaming combustion. Such an analysis for theUL 94 test6 indicates that polymers with c valueslower than about 300 J/g K should self-extinguishbecause they do not release heat at a high enough rateto overcome heat losses and so the flame cannot prop-agate. Therefore, for pure polymers with c 300 J/gK, self-extinguishing behavior in the UL 94 vertical

    test (a V rating) is expected. Figure 5 contains UL 94data26 and measured heat-release capacities for sev-eral pure polymers. A transition from a self-propagat-ing (HB) flame behavior to a self-extinguishing (V-0)flame behavior occurs in the vicinity of c 300 J/g K,as predicted from the critical heat-release-rate crite-rion.

    The criterion for self-extinguishing behavior in theLOI test must take into account the fact that an in-crease in the oxygen concentration of the flowing gasstream in the test chamber increases the temperature(radiant heat flux) of the sample diffusion flame and,therefore, the amount of thermal energy deposited inthe polymer. Because the heat-release rate of the sam-ple increases with the flame heat flux, which in turnincreases with oxygen concentration, an inverse rela-tionship between c and the limiting oxygen concen-tration is expected and observed, as shown in the LOIdata1,27,28 plotted versus c in Figure 6.

    Figure 5 UL-94 ratings versus the measured heat-releasecapacities of pure polymers.

    Figure 4 Average flaming heat-release rate (HRR) versusthe heat-release capacity for several polymers. Figure 6 LOI versus the measured heat-release capacity.

    562 WALTERS AND LYON

  • Comparing Figures 5 and 6 shows that self-extin-guishing behavior in the UL 94 vertical test occurs at alower heat-release capacity (c 300 100 J/g K)than in the LOI test (c 550 100 J/g K) underam-bient conditions (298 K, LOI 21% O2). The reason forthis is that the upward burning UL 94 test is moresevere than the downward burning LOI test becauseof convective and radiative preheating of the sampleby its flame and so requires more material fire resis-tance (lower heat-release capacity) for self-extinguish-ing behavior under ambient conditions.

    CONCLUSIONS

    The heat-release capacity is a physically based mate-rial property that is a good predictor of the fire behav-ior and flammability of pure polymers. The heat-re-lease capacity is simply calculated for pure polymersfrom their chemical structures with additive molargroup contributions that have been determined em-pirically with a high level of confidence (15%). Theproposed methodology for predicting the fire behav-ior and flammability of polymers from their chemicalstructures allows for the molecular-level design ofultra-fire-resistant polymers without the expense ofsynthesizing and testing new materials.

    The authors are indebted to Stanislav I. Stoliarov of theUniversity of Massachusetts (Amherst, MA) for performingthe optimization calculations for the molar group contribu-tions to the heat-release capacity. Certain commercial equip-ment, instruments, materials, or companies are identified inthis report to adequately specify the experimental proce-dure. This in no way implies endorsement or recommenda-tion by the Federal Aviation Administration.

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    MOLAR GROUP CONTRIBUTIONS 563