ML18213A076: Difference between revisions

From kanterella
Jump to navigation Jump to search
(Created page by program invented by StriderTol)
(StriderTol Bot change)
 
(One intermediate revision by the same user not shown)
Line 16: Line 16:


=Text=
=Text=
{{#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)
{{#Wiki_filter:Joint EPRI/NRC-RES Fire PRA Workshop August 6-10, 2018 Module III - Fire Analysis Fire Fundamentals: Fires in the Open and Fully Ventilated Fires 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.
2 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)
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)
Fire generates hot gases (convective fraction) and emits radiative heat (radiative fraction)
Generally applies to fires in the open or fires in large compartments
Generally applies to fires in the open or fires in large compartments
    - A nuclear power plant has lots of large compartments 2
- A nuclear power plant has lots of large compartments


Heat Release Rate (HRR)
3 Heat Release Rate (HRR)
For a simple fire, the HRR can be estimated using the following equation:
For a simple fire, the HRR can be estimated using the following equation:
Q&= m      &  A  H c
is the burning mass flux (kg/sm2)
      - m  & is the burning mass flux (kg/sm2)
- Hc is the net* heat of combustion (kJ/kg)
      - Hc is the net* heat of combustion (kJ/kg)
- A is the burning area (m2)
      - A is the burning area (m2)
So HRR ends up as kJ/s or kW
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&
* net heat of combustion implies that a burn efficiency has been included - fuels dont burn at 100% efficiency in real fires c
Fuel q&
H A
3
m Q


Heat Release Rate HRR can be estimated experimentally using oxygen consumption calorimetry Q&= m&O2  H c (kJ / kg O2 )
= &
where:
m&
H c ~ 13.1 MJ/kgO2 for many common fuels 4
Energy Released Rate Fuel m&
q&


Flames Laminar - very small fires Turbulent - most real fires Fuel              Oxygen Reaction Zone 5
4 Heat Release Rate HRR can be estimated experimentally using oxygen consumption calorimetry where:
~ 13.1 MJ/kgO2 for many common fuels
)
/
(
2 2
O c
O kg kJ H
m Q


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.
c H
 
5 Flames Laminar - very small fires Turbulent - most real fires Fuel Oxygen Reaction Zone
 
6 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.
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.
- 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
7 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.
- 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 solids.  
                                                                            *
- The flash-point is the temperature at which the amount of liquid evaporated from the surface achieves the lower flammable limit.
      - 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.
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.
The auto-ignition temperature of a gas will be higher than the boiling point of the liquid.
Liquids 7
Liquids Evaporating fuel
* Spark


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.
8 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.
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).
Typically, piloted ignition temperatures for solids range from 250°C (~480°F) to 450°C(~840°F).
      - For a given material, these temperatures are not constants and can change with the nature of heating.
Auto-ignition temperatures can exceed 500°C (~930°F).  
* Spark Radiant Heat
- For a given material, these temperatures are not constants and can change with the nature of heating.  
      - For practical purposes, a (piloted) ignition temperature (Tig) may be treated as a property of a combustible solid.
- 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
We shall consider thin (less than ~1 mm) and thick solids to have different time responses to ignition when exposed to impinging heat flux Hot Surface Solids Radiant Heat Pyrolysis products Spark


Flame Spread Motion of vaporization front at the ignition temperature for solids and liquids                                 Cable tray
9 Flame Spread Motion of vaporization front at the ignition temperature for solids and liquids
      - The surface is heated by the existing flames
- The surface is heated by the existing flames
      - More material pyrolyzes (or                     zf evaporates) ahead of the flame front
- More material pyrolyzes (or evaporates) ahead of the flame front
      - The existing flame acts as the pilot
- The existing flame acts as the pilot
      - The flame (fire) spreads                       xp Fire 9
- The flame (fire) spreads Cable tray Fire xp zf


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.
10 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.
Nevertheless, we can estimate approximate magnitudes for spread rates for various cases.
Spread case                       Spread Rate (cm/s)
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)
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.
Horizontal spread on liquids 1.0 to 100.
Premixed flames (gaseous)         10. to 100.(laminar) 105 (detonations) 10
Premixed flames (gaseous)
: 10. to 100.(laminar) 105 (detonations)


Zone of Influence Regions near the fire where damage or fire propagation is expected.
11 Zone of Influence Regions near the fire where damage or fire propagation is expected.
For fires in the open we consider:
For fires in the open we consider:
- Flame Radiation
- Convection, especially inside the fire plume x
Target q&
Target
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
12 Buoyant Flow Temperature rise causes a decrease in gas density Potential energy converted into kinetic energy - gasses flow upwards Z
Unit volume at plume gas at density and temperature T Z                            Unit volume of air at density a and temperature Ta D
V D
12
Buoyant plume Unit volume at plume gas at density and temperature T Unit volume of air at density a and temperature Ta
 
13 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 Flame Eddies
 
14 Turbulent Fire Plume Very low initial fuel velocity Entrainment and flame height controlled by buoyancy
 
15 Fire Plume Temperature Along the Centerline
 
16 Example Case - Zone-of-Influence Calculation Flame Height and Plume Temperature Heskdestad's Flame Height Correlation Input D - Fire diameter [m]
0.6 Qf - HRR [kW]
250 Result L - Flame height [m]


Turbulent Entrainment Entrainment is air drawn into the fire plume by upward movement of the buoyant plume
===1.5 where===
      - 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.
Heskestad's Plume Temperature Correlation Input Tamb - Ambient temp. [C]
Buoyant force Eddies Flame 13
20 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 D
Q L
f 02
.1 235
.0 5
2
=
(
)
(
)
(
)
(
)
3 5
5 2
1 25


Turbulent Fire Plume Very low initial fuel velocity Entrainment and flame height controlled by buoyancy 14
+
=
o e
p r
f f
amb pl z
F H
Q k
T T


Fire Plume Temperature Along the Centerline 15
D Q
z f
o 02
.1 083
.0 5
2
=


Example Case - Zone-of-Influence Calculation Flame Height and Plume Temperature
17 Example Case - Zone-of-Influence Calculation Radiation Heat Flux Flame Radiation: Point Source Model 2
(              )
4 R Q
53 k Q& (1  ) 2 5 T pl = Tamb + 25 f  f       r Heskdestad's Flame Height Correlation                    ((H p  Fe )  zo )
q r
f irr


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
Input Parameters:
                                  =
q&irr 4R  2 Input Parameters:
Qf: Fire heat release rate (kW)
Qf: Fire heat release rate (kW)
R: Distance from flames (m)
R: Distance from flames (m)
Xr: Radiative fraction (FIVE recommends 0.4)
Xr: Radiative fraction (FIVE recommends 0.4)
D: Fire diameter (m) 17
D: Fire diameter (m)
 
18 Example Case - Zone-of-Influence Calculation Radiation Heat Flux 2
4 R Q
q r
f irr
 
& =


Example Case - Zone-of-Influence Calculation Radiation Heat Flux Q&f  r
Point Source Flame Radiation Model Inputs Fire heat release rate [kW]
                              =
317 Radiation fraction 0.40 Distance from flames [m]
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}}
1.5 Results Heat flux [kW/m2]
4.5}}

Latest revision as of 16:05, 5 January 2025

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:
Shared Package
ML18213A072 List:
References
Download: ML18213A076 (18)


Text

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

2 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

3 Heat Release Rate (HRR)

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

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 c

H A

m Q

= &

m&

Energy Released Rate Fuel m&

q&

4 Heat Release Rate HRR can be estimated experimentally using oxygen consumption calorimetry where:

~ 13.1 MJ/kgO2 for many common fuels

)

/

(

2 2

O c

O kg kJ H

m Q

= &

c H

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

6 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.

7 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.

- In general, this temperature can be called the piloted ignition temperature and 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.

Liquids Evaporating fuel

  • Spark

8 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.

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°C (~930°F).

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

- 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 Hot Surface Solids Radiant Heat Pyrolysis products Spark

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

- The surface is heated by the existing flames

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

- The existing flame acts as the pilot

- The flame (fire) spreads Cable tray Fire xp zf

10 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)

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

For fires in the open we consider:

- Flame Radiation

- Convection, especially inside the fire plume x

Target q&

Target

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

V D

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

13 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 Flame Eddies

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

15 Fire Plume Temperature Along the Centerline

16 Example Case - Zone-of-Influence Calculation Flame Height and Plume Temperature Heskdestad's Flame Height Correlation Input D - Fire diameter [m]

0.6 Qf - HRR [kW]

250 Result L - Flame height [m]

1.5 where

Heskestad's Plume Temperature Correlation Input Tamb - Ambient temp. [C]

20 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 D

Q L

f 02

.1 235

.0 5

2

=

(

)

(

)

(

)

(

)

3 5

5 2

1 25

+

=

o e

p r

f f

amb pl z

F H

Q k

T T

D Q

z f

o 02

.1 083

.0 5

2

=

17 Example Case - Zone-of-Influence Calculation Radiation Heat Flux Flame Radiation: Point Source Model 2

4 R Q

q r

f irr

& =

Input Parameters:

Qf: Fire heat release rate (kW)

R: Distance from flames (m)

Xr: Radiative fraction (FIVE recommends 0.4)

D: Fire diameter (m)

18 Example Case - Zone-of-Influence Calculation Radiation Heat Flux 2

4 R Q

q r

f irr

& =

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