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    Explosion Hazards ofHydrogen-Air Mixtures

    Professor John H.S. LeeMcGill University, Montreal, Canada

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    Hydrogen Safety Issues

    Wide spread use of hydrogen requires significant efforts

    to resolve safety issues

    Hydrogen is already used extensively in many industrialapplications (but general public not exposed to thedangers)

    Extensive research efforts have already been devoted

    to hydrogen safety issues Post-Three Mile Island accident information notwidely disseminated

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    Hydrogen Safety Research

    BEFORE HYDROGEN CAN BE USED AS A COMMON

    ENERGY CARRIER:

    Achieve public acceptance of hydrogen-technologies

    Provide at least the same level of safety, reliability,comfort as todays fossil fuels

    No solutions are available in terms of widely acceptedstandards, methodologies, mitigation techniques andregulations)

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    Hydrogen and todays fuels

    Qualitative comparison of

    Safety profiles

    Properties of hydrogenare different from todaysfuels

    H2 is less dangerousin terms of thermal

    and fire hazards, may be responsible

    for stronger pressureeffects

    0

    20

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    Buoy

    ancy

    Deto

    nability

    Flam

    mable

    rang

    e

    Flam

    esp

    eed

    Fire

    spread

    Mole

    cular

    weig

    ht

    Fire

    emi

    ssivity

    Energy

    per

    kg

    Energy

    per

    m3

    Ignition

    ene

    rgy

    Properties

    Relativeunits

    Hydrogen

    Today's energy carriers

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    Safety Issues

    To evaluate hydrogen safety the following set of

    issues should be addressed for each of theapplications

    Hydrogen release, mixing, and distribution Thermal, pressure, and missile effects from H2 fires

    and H2-air cloud explosions

    Mitigation techniques for detection, dilution, andremoval of hydrogen

    Risk evaluation, both specific and in comparison with

    todays fossil energy carriers Standardization, and regulatory issues

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    Objectives

    To contribute to common understanding and approaches

    for addressing hydrogen safety issues To integrate experience and knowledge on hydrogensafety

    To integrate and harmonise the fragmented research base

    To provide contributions to safety requirements, standards

    and codes of practice To contribute to an improved technical culture on handlinghydrogen as an energy carrier

    To promote public acceptance of hydrogen technologies

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    Accident scenarios

    Confined Explosions

    leakage of H2 into buildings contamination of high pressure H2 storage facilities by air

    Unconfined Explosions

    major rapid release into the atmosphere

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    Hindenburg (May 6, 1937)

    Lakehurst (New Jersey)

    Fired started near tail during landing Flame spread ~ 50 m/s

    Ship was 803 ft. ~ 245 m long Destruction completed in 32 seconds

    36 lives lost

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    Crescent City, Illinois

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    Crescent City, Illinois

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    Jackass Flat (Nevada)

    January 9, 1964 Unconfined H2-air explosion

    Test to measure acoustic noise due to high flow ratehydrogen

    1000 kg H2 discharged from vertical rocket nozzle at 23 MPain 30 seconds

    Discharge rate uniformly increased to 55 kg/s, maintained for

    10 seconds then reduced to zero

    Ignition occurs 26 seconds after discharge begins

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    Jackass Flat (Nevada)

    January 9, 1964

    No pressure wave detected in near field less than 0.8 km Explosion heard 3.2 km away

    Wide spread minor damage near hydrogen discharge,but superficial

    Estimate 10 kg of H2 involved in the explosion

    TNT equivalent of 8%

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    Jackass Flat (Nevada) January 9, 1964

    P l

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    Polysar

    (April 19, 1984) Unconfined H2-air explosion

    Rapid release of H2 from a ruptured gasket of a WorthingtonCompressor at 600psi

    10-20 seconds delay before ignition

    Three fatalities

    Extensive major structural damage in the near field

    Glass and minor structural damage up to 1 km

    Detonation occurred in near field

    Damage compatible to detonation of about 0.1 kg H2-aircloud

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    Chi Li ht d P C t P k

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    China Light and Power Cast Peak

    Generating Station (August 28, 1992) Confined explosion

    Explosion in hydrogen receiver

    Production of hydrogen by electrolysis

    Low pressure compressor: 500 kPa

    High pressure compressor: 13.6 MPa

    Two hydrogen receivers: 8.68 m long x 1.12 m diameter Hydrogen plant shut down August 24 to 26

    Hydrogen plant resume to supply H2 to receivers @ 06:30

    on August 27

    China Light and Po er Cast Peak

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    China Light and Power Cast Peak

    Generating Station (August 28, 1992) Pressure at receiver: 6.9 MPa

    August 28 from 00:30 to 02:00 gas from receiver suppliedto generator

    Hydrogen purity in generator dropped to 85%

    Receiver disconnected from generator at 02:30; H2supplied from bottles

    Sampling indicated hydrogen purity in receivers about 95%

    Receiver #1 reconnected to generator to supply H2 togenerator at 09:45 on August 28

    China Light and Power Cast Peak

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    China Light and Power Cast Peak

    Generating Station (August 28, 1992) A drop in H2 purity in generators noted immediately

    Both receivers exploded at 10:05

    Two fatalities; 18 injured by fragments

    Extensive blast damage ~ 100 m radius

    TNT equivalent 275 kg

    Conclusion: all the gas supplied to the receiver over a 20hour period (from 06:30 on August 27 to 02:30 on August28) was air!

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    Blainville Quebec

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    Blainville, Quebec

    (March, 2000)

    Confined explosion Motor vehicle test center

    Tank with 350 psi natural gas filled with air to 3500 psi

    instead of nitrogen

    Explosion occur during pressure adjustment before crash

    test Extensive damage to car and building

    3 workers killed

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    C l i f A id t

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    Conclusion from Accidents

    Rapid release in open atmosphere (Jackass Flat)

    minor blast damages

    Rapid release in a congested area with equipment,

    structure etc. (Polysar)

    severe blast damages, DDT

    Contamination of high pressure storage facility by air(China Light)

    severe blast damages

    A id t i t id

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    Accident scenarios to avoid

    Rapid release in congested area (high density ofequipment)

    Air contamination of high pressure hydrogen storage

    facilities

    Leakage of hydrogen into poorly vented enclosures

    E l i ti f h d

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    Explosion properties of hydrogen

    Equilibrium thermodynamics properties for hydrogenexplosion well established

    Chemical kinetics of hydrogen oxidation sufficiently

    understood quantitatively (explosion limits, laminar flamepropagation)

    Explosion parameters are also well established

    (flammability limit, ignition energy, quenching distance, etc.)

    E l i ti f h d

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    Explosion properties of hydrogen

    Detonation states are well known (Chapman-Jouguetdetonation velocity, overpressure, etc.)

    Dynamic detonation parameters adequately known

    (initiation energy, detonability limit, critical diameter) Detonation sensitivity of high pressure H2-air mixturesdoes not increase as other hydrocarbon fuels do

    Transition and onset of detonation (i.e. quantitativedescription of turbulent flame acceleration, condition for theonset of detonation) still not understood

    Major unresolved problem

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    Major unresolved problem

    Development of turbulent combustion models todescribe high speed deflagrations with consideration ofcompressibility effects

    Quantitative theory for the onset of detonation

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    The Problem of the Transition fromDeflagration to Detonation

    Current Understandingand Outstanding Problems

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    Two Modes of Combustion

    Deflagration

    propagation via diffusion mechanism

    Detonation

    Propagation via shock ignition

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    Slowest Burning Rate

    Laminar Flame

    molecular diffusion of heat and species

    m/s1010

    10

    ~~

    1

    3

    5

    ctS

    heat

    radicals

    S

    Flame Thickness:

    mm101010~~

    135

    ct

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    Fastest Burning Rate

    CJ Detonation

    Ignition by adiabatic shock compression

    D

    m/s18005.5

    30~30

    ~

    ~

    2

    o

    oo

    cD

    ceQ

    Qec

    cD

    D

    reactionzone

    shock

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    Self-Propagating Deflagration Waves

    are unstable

    accelerate to some critical state and undergotransition to detonation waves

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    Urtiew & Oppenheim

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    (1966)

    1480 m/s

    H2 + 0.5 O2@ Po = 1 atm

    VCJ = 2837 m/s

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    initial phase of flame acceleration involves numerousinstability mechanisms

    not possible to characterize the flame accelerationphase by a single reproducible parameter like therun-up distance

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    bypass the initial phase and look at the final phase of theonset of detonation

    determine the critical deflagration speed prior to onset ofdetonation

    use obstacles to get to critical speed rapidly

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    systematic studies of DDT in rough tubes began atMcGill in the late 1970s

    tubes from 5 cm to 2.5 m were used

    obstacles were in the form of orifice plates, cylindricalrods, Shchelkin spirals, etc.

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    time

    distance

    Findings from Rough Tube

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    g g

    Experiments

    rapid acceleration to a quasi-steady velocity

    steady velocity is not too sensitive to tube diameter or

    obstacle configuration

    distinct transition from steady velocity to a higher valuewhen mixture sensitivity varies

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    Three Distinct Regimes

    turbulent deflagration < 100 m/s sonic regime

    deflagration speed ~ sound speed of

    products~ 1000 m/s (~ VCJ)

    quasi-detonation or detonation

    ~ VCJ with large velocity deficit

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    Critical Deflagration Speed for

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    Onset of Detonation

    ~ VCJ

    ~ sound speed of products

    Eder & Brehm (2001)

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    Vasilev (2006)

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    (confined) 0.33 Mcrit 0.56 MCJ (unconfined)

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    Mechanism of Onset of Detonation in

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    Rough (Obstacle-Filled) Tubes

    turbulence from obstacles

    pressure waves

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    Two Modes of

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    Onset of Detonation

    1. unstable mixture: local explosion, SWACERmechanism evidenced by formation of retonationwaves

    2. progressive wave amplification resonant coupling withturbulent reaction zone

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    180

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    0

    20

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    60

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    1.6 1.8 2 2.2 2.4 2.6 2.8 3 3.2 3.4 3.6

    Time (ms)

    Pr

    essure

    (kPa)

    theoreticalCJ detonation pressure

    incidentCJ detonation

    transition todetonation

    140

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    0

    20

    40

    60

    80

    100

    120

    1.6 2.1 2.6 3.1 3.6

    Time (ms)

    P

    ressure

    (kP

    a)

    Theoretical CJ Pressure

    incidentCJ detonation

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    detonation mechanism is resonant coupling betweentransverse pressure waves and chemical reactions

    transition means setting up the conditions for theresonant coupling to occur

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    t b l t b ti b i th d fl ti t i

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    turbulent combustion brings the deflagration to maximumspeed; Chapman-Jouguet deflagration ~ VCJ

    transition to detonation requires the resonant couplingbetween transverse pressure fluctuations and thechemical reactions

    Chapman-Jouguet deflagration speed is not governed

    b ti t (h t b l )

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    by reaction rate (hence turbulence)

    turbulent combustion rate must be fast enough topressurize reaction zone

    gasdynamic expansion drives the deflagration like a CJdetonation

    hence, sound speed energetic parameters dominate andnot turbulence

    Outstanding Problems in DDT

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    quantify the pre-detonation state

    (thermodynamic, turbulence, chemical kinetics)

    theory for the development of local explosions centers

    from hydrodynamic fluctuations

    condition for rapid amplifcation of pressure waves

    (SWACER)