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{{#Wiki_filter:Joint EPRI/NRC
{{#Wiki_filter:Module III - Fire Analysis Fire Fundamentals: Fires in the Open and Fully Ventilated Fires Joint EPRI/NRC-RES Fire PRA Workshop August 6-10, 2018 A Collaboration of the Electric Power Research Institute (EPRI) & U.S. NRC Office of Nuclear Regulatory Research (RES)
-RES Fire PRA WorkshopAugust 6-10, 2018Module III
 
-Fire AnalysisFire Fundamentals: Fires in the Open and Fully Ventilated FiresA Collaboration of the Electric Power Research Institute (EPRI) & U.S. NRC Office of Nuclear Regulatory Research (RES) 2Recall: Fuel limited firesA fire where the fuel burning rate is limited only by the surface burning rate of the material. Sufficient air is always available for the fire (plenty of oxygen to support burning)Fire generates hot gases (convective fraction) and emits radiative heat (radiative fraction)Generally applies to fires in the open or fires in large compartments
Recall: Fuel limited fires A fire where the fuel burning rate is limited only by the surface burning rate of the material.
-A nuclear power plant has lots of large compartments-3Heat Release Rate (HRR)For a simple fire, the HRR can be estimated using the following equation:
Sufficient air is always available for the fire (plenty of oxygen to support burning)
-2)-H cis the net*heat of combustion (kJ/kg)
Fire generates hot gases (convective fraction) and emits radiative heat (radiative fraction)
-Ais the burning area (m 2)So HRR ends up as kJ/s or kW* "net" heat of combustion implies that a burnefficiency has been included  
Generally applies to fires in the open or fires in large compartments
-fuels don't burnat 100% efficiency in real fires c H A m Q&&m&EnergyReleased RateFuel m&q&
    - A nuclear power plant has lots of large compartments 2
4Heat Release RateHRR can be estimated experimentally using oxygen consumption calorimetrywhere:~ 13.1 MJ/kg O2for many common fuels
 
)/(2 2 O c OkgkJ H m Q&&c H 5FlamesLaminar -very small firesTurbulent
Heat Release Rate (HRR)
-most real firesFuel OxygenReaction Zone 6Ignition of GasesWith aspark orsmallflame (pilot)present,ignitionisbased onwhetherthegaseousfuelconcentrationisbetweentheupper(rich)andlower(lean)flammabilitylimits.-Thefuel-air(oxidizer)mixture issaid to beflammable if aflamewillpropagate inthismixture.With nopilotpresent, agaseousfuelinaircanstilligniteifthemixtureis at orabovetheauto-ignitiontemperature
For a simple fire, the HRR can be estimated using the following equation:
.-Theauto-ignitiontemperature isusuallymeasuredfor astoichiometricmixture-justtherightmix sothat nofuel oroxygenremainsafterthereaction.
Q&= m      &  A  H c
7Ignition of LiquidsFor a liquid to ignite, it must first evaporatesufficiently to form a flammable mixture of gaseous fuel and oxygen-This occurs at a liquid temperature called a flash-pointtemperature.
      - m  & is the burning mass flux (kg/sm2)
-In general, this temperature can be called the piloted ignition temperatureand the same term carries over to solids. -The flash-point is the temperature at which the amount of liquid evaporated from the surface achieves the lower flammable limit.If no pilot is present, the mixture must be heated to the auto-ignition temperature in order to ignite. The auto-ignition temperature of a gas will be higher than the boiling point of the liquid.LiquidsEvaporatingfuel*Spark 8Ignition of SolidsSolids do not evaporate like liquids when heated. Solids form gaseous decomposition compounds, generally leaving behind char, in a process called pyrolysis. At some point, the gases reach the lower flammability limit and may ignite by piloted ignition or, if hot enough, auto-ignition.Typically, piloted ignition temperatures for solids range from 250°C (~480°F)to 450°C(~840°F).Auto-ignition temperatures can exceed 500
      - Hc is the net* heat of combustion (kJ/kg)
°C (~930°F). -For a given material, these temperatures are not constants and can change with the nature of heating.
      - A is the burning area (m2)
-For practical purposes, a (piloted) ignition temperature (T ig) may be treated as a property of a combustible solid.We shall consider thin (less than  
So HRR ends up as kJ/s or kW
~1 mm) and thick solids to have different time responses to ignition when exposed to impinging heat fluxHot SurfaceSolidsRadiantHeatPyrolysis products*Spark 9Flame SpreadMotion of vaporization front at the ignition temperature for solids and liquids-The surface is heated by the existing flames
* net heat of combustion implies that a burn efficiency has been included - fuels dont burn at 100% efficiency in real fires                                 Energy Released Rate m&
-More material pyrolyzes(or evaporates) ahead of the flame front-The existing flame acts as the pilot-The flame (fire) spreads-Cable trayFire x p z f 10Typical Flame Spread RatesIt is very difficult to compute flame spread rates because formulas are not completely available, rates may not be steady, and fundamental fuel properties are not generally available.Nevertheless, we can estimate approximate magnitudes for spread rates for various cases.Spread caseSpread Rate (cm/s)Smoldering solids0.001 to 0.01Lateral or downward spread on thick solids0.1Upward spread on thick solids1.0 to 100. (0.022 to 2.2 mph)Horizontal spread on liquids1.0 to 100.Premixed flames (gaseous)10. to 100.(laminar)10 5(detonations) 11Zone of InfluenceRegions near the fire where damage or fire propagation is expected.For fires in the open we consider:
Fuel q&
-Flame Radiation
3
-Convection, especially inside the fire plume xTarget q&Target 12Buoyant FlowTemperature rise causes a decrease in gas densityPotential energy converted into kinetic energy  
 
-gasses flow upwards Z V DBuoyant plumeUnit volume at plume gas at density and temperature TUnit volume of air at density aand temperature T a 13Turbulent EntrainmentEntrainmentis air drawn into the fire plume by upward movement of the buoyant plume
Heat Release Rate HRR can be estimated experimentally using oxygen consumption calorimetry Q&= m&O2  H c (kJ / kg O2 )
-Engulfing air from the surroundings into the fire plumeEddies: fluctuating and rotating balls of fluid, large scale rolling fluid motion on the edge of the plume.Buoyant forceFlameEddies 14Turbulent Fire PlumeVery low initial fuel velocityEntrainment and flame height controlled by buoyancy 15Fire Plume Temperature Along the Centerline 16Example Case  
where:
-Zone-of-Influence CalculationFlame Height and Plume TemperatureHeskdestad'sFlame Height Correlation Input D -Fire diameter [m]
H c ~ 13.1 MJ/kgO2 for many common fuels 4
0.6 Q f-HRR [kW]250Result L -Flame height [m]
 
1.5where:Heskestad'sPlume Temperature Correlation Input Tamb-Ambient temp. [C]
Flames Laminar - very small fires Turbulent - most real fires Fuel              Oxygen Reaction Zone 5
20 Q f-HRR [kW]250 F e-Fire elevation [m]
 
0 H p-Target Elevation [m]
Ignition of Gases With a spark or small flame (pilot) present, ignition is based on whether the gaseous fuel concentration is between the upper (rich) and lower (lean) flammability limits.
3.7 D-Fire Diameter [m]
    - The fuel-air (oxidizer) mixture is said to be flammable if a flame will propagate in this mixture.
1 k f-Location factor 1 (-2 or 4)
With no pilot present, a gaseous fuel in air can still ignite if the mixture is at or above the auto-ignition temperature.
X r-Radiative Fraction 0.4Result Tpl-Plume Temp [C]
    - The auto-ignition temperature is usually measured for a stoichiometric mixture - just the right mix so that no fuel or oxygen remains after the reaction.
328 D Q L f 02.1 235.0 5 2&3 5 5 2 1 25o e p r f famb pl z F H Q k T T&D Q z f o 02.1 083.0 5 2&
6
17Example Case  
 
-Zone-of-Influence CalculationRadiation Heat FluxFlame Radiation: Point Source Model 2 4 R Q q r f irr&&Input Parameters: Q f: Fire heat release rate (kW) R: Distance from flames (m) X r: Radiative fraction (FIVE recommends 0.4)D: Fire diameter (m) 18Example Case  
Ignition of Liquids For a liquid to ignite, it must first evaporate sufficiently to form a flammable mixture of gaseous fuel and oxygen
-Zone-of-Influence CalculationRadiation Heat Flux 2 4 R Q q r f irr&&Point Source Flame Radiation ModelInputsFire heat release rate [kW]
      - This occurs at a liquid temperature called a flash-point temperature.
317Radiation fraction0.40Distance from flames [m]1.5ResultsHeat flux [kW/m2]4.5}}
Evaporating
                                                                            *
      - In general, this temperature can be called the piloted ignition temperature and the same term carries over to       fuel    Spark solids.
      - The flash-point is the temperature at which the amount of liquid evaporated from the surface achieves the lower flammable limit.
If no pilot is present, the mixture must be heated to the auto-ignition temperature in order to ignite.
The auto-ignition temperature of a gas will be higher than the boiling point of the liquid.
Liquids 7
 
Ignition of Solids Solids do not evaporate like liquids when heated. Solids form gaseous decomposition compounds, generally leaving behind char, in a process called pyrolysis.
Hot Surface At some point, the gases reach the lower flammability limit and may ignite by piloted ignition or, if hot enough, auto-ignition.
Pyrolysis Typically, piloted ignition temperatures for solids range from 250°C (~480°F) to 450°C(~840°F).                           products Auto-ignition temperatures can exceed 500°C (~930°F).
      - For a given material, these temperatures are not constants and can change with the nature of heating.
* Spark Radiant Heat
      - For practical purposes, a (piloted) ignition temperature (Tig) may be treated as a property of a combustible solid.
We shall consider thin (less than ~1 mm) and thick solids to have different time responses to ignition when exposed to impinging heat flux                                          Solids 8
 
Flame Spread Motion of vaporization front at the ignition temperature for solids and liquids                                 Cable tray
      - The surface is heated by the existing flames
      - More material pyrolyzes (or                     zf evaporates) ahead of the flame front
      - The existing flame acts as the pilot
      - The flame (fire) spreads                       xp Fire 9
 
Typical Flame Spread Rates It is very difficult to compute flame spread rates because formulas are not completely available, rates may not be steady, and fundamental fuel properties are not generally available.
Nevertheless, we can estimate approximate magnitudes for spread rates for various cases.
Spread case                        Spread Rate (cm/s)
Smoldering solids                  0.001 to 0.01 Lateral or downward spread on thick solids                      0.1 Upward spread on thick solids      1.0 to 100. (0.022 to 2.2 mph)
Horizontal spread on liquids      1.0 to 100.
Premixed flames (gaseous)         10. to 100.(laminar) 105 (detonations) 10
 
Zone of Influence Regions near the fire where damage or fire propagation is expected.
For fires in the open we consider:
Target
      - Flame Radiation
      - Convection, especially inside the         q& Target fire plume x
11
 
Buoyant Flow Temperature rise causes a decrease in gas density Potential energy converted into kinetic energy - gasses flow upwards Buoyant plume V
Unit volume at plume gas at density and temperature T Z                            Unit volume of air at density a and temperature Ta D
12
 
Turbulent Entrainment Entrainment is air drawn into the fire plume by upward movement of the buoyant plume
      - Engulfing air from the surroundings into the fire plume Eddies: fluctuating and rotating balls of fluid, large scale rolling fluid motion on the edge of the plume.
Buoyant force Eddies Flame 13
 
Turbulent Fire Plume Very low initial fuel velocity Entrainment and flame height controlled by buoyancy 14
 
Fire Plume Temperature Along the Centerline 15
 
Example Case - Zone-of-Influence Calculation Flame Height and Plume Temperature
(              )
53 k Q& (1  ) 2 5 T pl = Tamb + 25 f  f      r Heskdestad's Flame Height Correlation                     ((H p  Fe )  zo )
 
where:
                      & 2 L = 0.235Q f 5  1.02 D              z o = 0.083Q&f 5  1.02 D 2
Input D - Fire diameter [m]       0.6     Heskestad's Plume Temperature Qf - HRR [kW]               250        Correlation Input Result                                Tamb - Ambient temp. [C]           20 L - Flame height [m]        1.5      Qf - HRR [kW]                     250 Fe - Fire elevation [m]             0 Hp - Target Elevation [m]         3.7 D - Fire Diameter [m]               1 kf - Location factor                 1 (2 or 4)
Xr - Radiative Fraction           0.4 Result Tpl - Plume Temp [C]             328 16
 
Example Case - Zone-of-Influence Calculation Radiation Heat Flux Flame Radiation: Point Source Model Q&f  r
                                  =
q&irr 4R  2 Input Parameters:
Qf: Fire heat release rate (kW)
R: Distance from flames (m)
Xr: Radiative fraction (FIVE recommends 0.4)
D: Fire diameter (m) 17
 
Example Case - Zone-of-Influence Calculation Radiation Heat Flux Q&f  r
                              =
q&irr 4R 2 Point Source Flame Radiation Model Inputs Fire heat release rate [kW]     317 Radiation fraction            0.40 Distance from flames [m]       1.5 Results Heat flux [kW/m2]               4.5 18}}

Revision as of 19:23, 20 October 2019

Joint EPRI/NRC-RES Fire PRA Workshop - Module III - Fire Analysis -Fire Fundamentals: Fires in the Open and Fully Ventilated Fires
ML18213A076
Person / Time
Issue date: 07/31/2018
From: Tammie Rivera
NRC/RES/DRA/FRB, Electric Power Research Institute
To:
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References
Download: ML18213A076 (18)


Text

Module III - Fire Analysis Fire Fundamentals: Fires in the Open and Fully Ventilated Fires Joint EPRI/NRC-RES Fire PRA Workshop August 6-10, 2018 A Collaboration of the Electric Power Research Institute (EPRI) & U.S. NRC Office of Nuclear Regulatory Research (RES)

Recall: Fuel limited fires A fire where the fuel burning rate is limited only by the surface burning rate of the material.

Sufficient air is always available for the fire (plenty of oxygen to support burning)

Fire generates hot gases (convective fraction) and emits radiative heat (radiative fraction)

Generally applies to fires in the open or fires in large compartments

- A nuclear power plant has lots of large compartments 2

Heat Release Rate (HRR)

For a simple fire, the HRR can be estimated using the following equation:

Q&= m & A H c

- m & is the burning mass flux (kg/sm2)

- Hc is the net* heat of combustion (kJ/kg)

- A is the burning area (m2)

So HRR ends up as kJ/s or kW

  • net heat of combustion implies that a burn efficiency has been included - fuels dont burn at 100% efficiency in real fires Energy Released Rate m&

Fuel q&

3

Heat Release Rate HRR can be estimated experimentally using oxygen consumption calorimetry Q&= m&O2 H c (kJ / kg O2 )

where:

H c ~ 13.1 MJ/kgO2 for many common fuels 4

Flames Laminar - very small fires Turbulent - most real fires Fuel Oxygen Reaction Zone 5

Ignition of Gases With a spark or small flame (pilot) present, ignition is based on whether the gaseous fuel concentration is between the upper (rich) and lower (lean) flammability limits.

- The fuel-air (oxidizer) mixture is said to be flammable if a flame will propagate in this mixture.

With no pilot present, a gaseous fuel in air can still ignite if the mixture is at or above the auto-ignition temperature.

- The auto-ignition temperature is usually measured for a stoichiometric mixture - just the right mix so that no fuel or oxygen remains after the reaction.

6

Ignition of Liquids For a liquid to ignite, it must first evaporate sufficiently to form a flammable mixture of gaseous fuel and oxygen

- This occurs at a liquid temperature called a flash-point temperature.

Evaporating

- In general, this temperature can be called the piloted ignition temperature and the same term carries over to fuel Spark solids.

- The flash-point is the temperature at which the amount of liquid evaporated from the surface achieves the lower flammable limit.

If no pilot is present, the mixture must be heated to the auto-ignition temperature in order to ignite.

The auto-ignition temperature of a gas will be higher than the boiling point of the liquid.

Liquids 7

Ignition of Solids Solids do not evaporate like liquids when heated. Solids form gaseous decomposition compounds, generally leaving behind char, in a process called pyrolysis.

Hot Surface At some point, the gases reach the lower flammability limit and may ignite by piloted ignition or, if hot enough, auto-ignition.

Pyrolysis Typically, piloted ignition temperatures for solids range from 250°C (~480°F) to 450°C(~840°F). products Auto-ignition temperatures can exceed 500°C (~930°F).

- For a given material, these temperatures are not constants and can change with the nature of heating.

  • Spark Radiant Heat

- For practical purposes, a (piloted) ignition temperature (Tig) may be treated as a property of a combustible solid.

We shall consider thin (less than ~1 mm) and thick solids to have different time responses to ignition when exposed to impinging heat flux Solids 8

Flame Spread Motion of vaporization front at the ignition temperature for solids and liquids Cable tray

- The surface is heated by the existing flames

- More material pyrolyzes (or zf evaporates) ahead of the flame front

- The existing flame acts as the pilot

- The flame (fire) spreads xp Fire 9

Typical Flame Spread Rates It is very difficult to compute flame spread rates because formulas are not completely available, rates may not be steady, and fundamental fuel properties are not generally available.

Nevertheless, we can estimate approximate magnitudes for spread rates for various cases.

Spread case Spread Rate (cm/s)

Smoldering solids 0.001 to 0.01 Lateral or downward spread on thick solids 0.1 Upward spread on thick solids 1.0 to 100. (0.022 to 2.2 mph)

Horizontal spread on liquids 1.0 to 100.

Premixed flames (gaseous) 10. to 100.(laminar) 105 (detonations) 10

Zone of Influence Regions near the fire where damage or fire propagation is expected.

For fires in the open we consider:

Target

- Flame Radiation

- Convection, especially inside the q& Target fire plume x

11

Buoyant Flow Temperature rise causes a decrease in gas density Potential energy converted into kinetic energy - gasses flow upwards Buoyant plume V

Unit volume at plume gas at density and temperature T Z Unit volume of air at density a and temperature Ta D

12

Turbulent Entrainment Entrainment is air drawn into the fire plume by upward movement of the buoyant plume

- Engulfing air from the surroundings into the fire plume Eddies: fluctuating and rotating balls of fluid, large scale rolling fluid motion on the edge of the plume.

Buoyant force Eddies Flame 13

Turbulent Fire Plume Very low initial fuel velocity Entrainment and flame height controlled by buoyancy 14

Fire Plume Temperature Along the Centerline 15

Example Case - Zone-of-Influence Calculation Flame Height and Plume Temperature

( )

53 k Q& (1 ) 2 5 T pl = Tamb + 25 f f r Heskdestad's Flame Height Correlation ((H p Fe ) zo )

where:

& 2 L = 0.235Q f 5 1.02 D z o = 0.083Q&f 5 1.02 D 2

Input D - Fire diameter [m] 0.6 Heskestad's Plume Temperature Qf - HRR [kW] 250 Correlation Input Result Tamb - Ambient temp. [C] 20 L - Flame height [m] 1.5 Qf - HRR [kW] 250 Fe - Fire elevation [m] 0 Hp - Target Elevation [m] 3.7 D - Fire Diameter [m] 1 kf - Location factor 1 (2 or 4)

Xr - Radiative Fraction 0.4 Result Tpl - Plume Temp [C] 328 16

Example Case - Zone-of-Influence Calculation Radiation Heat Flux Flame Radiation: Point Source Model Q&f r

=

q&irr 4R 2 Input Parameters:

Qf: Fire heat release rate (kW)

R: Distance from flames (m)

Xr: Radiative fraction (FIVE recommends 0.4)

D: Fire diameter (m) 17

Example Case - Zone-of-Influence Calculation Radiation Heat Flux Q&f r

=

q&irr 4R 2 Point Source Flame Radiation Model Inputs Fire heat release rate [kW] 317 Radiation fraction 0.40 Distance from flames [m] 1.5 Results Heat flux [kW/m2] 4.5 18