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By 
T SHYAMKUMAR 
14TH14F
Why micro combustion ? 
 Batteries have low specific energy 
 Liquid hydrocarbon fuels have a very high specific 
energy 
 To reduce system weight 
 To increase operational lifetimes 
 To reduce unit cost 
 Easily rechargeable
APPLICATIONS 
 Micro-satellite thrusters for station keeping require a 
small thrust and a high specific impulse for an 
operation period of years. An efficient micro-thruster 
requires propellants with a large energy density 
 Micro-air vehicles for reconnaissance and surveillance 
in urban and battle field.
SCALING PARAMETERS 
1.Based on physical dimension of the combustor 
if physical length < 1mm :microcombustion 
if physical length is between 1mm -10mm : mesoscale combustion 
2.Based on quenching diameter 
The combustion is called micro-scale (mesoscale) if the combustor 
size is smaller (larger) than the quenching diameter 
3. By the relative length scale of the entire device to that of 
conventional large scale devices for similar purposes.
Thermo physical Issues 
 As the characteristic length of the device is reduced, the 
Reynolds and Peclet numbers decrease and fluid flow tends to 
be less turbulent, so the viscous effects and the diffusive 
transport of mass and heat become increasingly important. 
 From the point of view of combustion, an important issue is the 
magnitude of the residence time, because it decreases as the 
length of the combustor decreases, and it has to be larger than 
the chemical time, for complete combustion to occur. 
 At the length scales of microcombustion devices, heat 
transfer by natural convection becomes small because the 
induced buoyant flow is small
 However, heat transfer by conduction through the gas to 
the surrounding surfaces and by forced convection in the 
intake and exhaust channels and in the combustion 
chamber is significant. 
 Heat transfer by radiation also increases as the 
characteristic length decreases because of the large view 
factor. 
 Problematic for combustion chambers due to wall 
quenching 
 Silica aerogel can be used to insulate the combustor. 
 Reduced thermal gradients will reduce thermal expansion 
stresses and subsequent misalignments in moving parts. 
Biot number for a steel or a silicon device with a length 
scale of 10 mm,and subjected to moderate convection and 
radiation (combined convection and radiation heat transfer 
coefficient of 100 W/m2K), will be of the order of 0.002
Combustion 
 Physical time available for combustion (residence time) must be larger 
than the time required for the chemical reaction to occur (combustion 
time). 
 Since in general the residence time will be small in micro combustors, 
it is important to have small chemical times to ensure completion of 
the combustion process within the combustor . 
 As engine size or combustion volume decreases, the surface-to-volume 
ratio increases, resulting in increased combustor surface heat losses 
and increased potential destruction of radical species at the wall. 
 Ceramic materials, such as SiO2, SiC, and Si3N4, can withstand 
temperatures of around 1700 K, which are high enough to ensure short 
chemical times 
 Although the increase of the surface-to-volume ratio of the combustor 
presents a problem for gas-phase combustion, it favors catalytic 
combustion
Flame propagation and 
stabilization 
 When flames (e.g., a torch) are put in narrow 
channels, they do not propagate through, when the 
gap size is below what is known as the quenching 
distance 
 Quenching distance is in the range of ~2.5 mm for cold 
walls (500 K) 
 Burner insulation and thermal management are 
important in minimizing heat loss and mitigating 
thermal quenching
Characteristics of homogeneous 
micro burners 
Quenching mechanisms 
 Thermal - heat loss from the burner walls and gases 
 Radical quenching - diffusion of radicals from the 
flame to the walls followed by their recombination on 
walls to produce stable molecules. 
 In the mesoscopic range radical quenching plays only a 
secondary role.
The excess enthalpy principle 
 Qin - enthalpy of the inlet stream . 
 Qc - heat generated on combustion. 
 Qin + Qc - outlet enthalpy in an adiabatic system. 
 Sufficient pre-heating of the incoming gases is 
required to stabilize combustion in microburners. 
 Qr is recirculted to cold inlet stream. 
 Maximum temperature is greater than the adiabatic 
temperature rise .
The role of burner walls 
 Wall conductivity and the wall thickness are key 
parameters for flame stability. 
 Direction of transverse heat transfer downstream of 
the flame is from hot gases to the wall and upstream of 
the flame is from the wall to the cold inlet gases 
 Micro burner can be split into three distinct zones: the 
pre-heating, the combustion and the post-combustion 
zones.
Micro burner stability 
1 The dual role of walls in heat 
exchange 
 As the wall conductivity decreases, the flame 
temperatures become higher and the flame remains 
localized but drifts downstream due to insufficient 
pre-heating. 
 Highly conductive walls, on the other hand, dissipate 
heat to the environment and also longitudinally, 
causing the entire burner surfaces to be hot 
 Two modes of flame quenching occur: a spatially 
‘distributed’ type for high wall thermal conductivities, 
thick walls, and/or low flow velocities and blowout at 
high velocities, low wall conductivity, or thin walls.
2 Effect of flow velocity 
 The inlet velocity is easily varied experimentally and 
controls the power input to a burner 
 At low flow velocities, the power input is low, the 
burner temperatures are low and extinction is the 
dominant quenching mechanism. 
 At high flow velocities the power input is high but the 
residence time is low, and as a result blowout is the 
dominant quenching mechanism. 
 For fast flows, higher wall conductivity facilitates heat 
transfer upstream resulting in more stable flames
Excess enthalpy burners(heat 
recirculation) 
 Thermal enthalpy of the 
incoming reactants is 
increased via preheating 
without diminishing the 
chemical enthalpy via 
chemical reaction. 
 A PC with LabView 
software is used to control 
mass flow controllers for 
fuel and air and to record 
data from thermocouples 
for temperature 
measurement. The 
exhaust gas composition 
was analyzed with a gas 
chromatograph. 
Electrically heated Kantal 
wire is used for ignition
Heat recuperation in reverse-flow 
micro burners 
 Temporal thermal coupling between the hot product 
and the cold reactant streams, achieved through 
periodic flow reversal in reverse-flow (RF) reactors. 
 Requirements - high gas-solid heat transfer rates and 
reasonably high heat capacity of the burner solid 
structure. Porous beds are required to increase the 
gas-solid heat transfer rates 
 The RF operation improves the microburner stability 
at the blowout limit, but does not affect the stability at 
extinction.Micro burner stability increases as the wall 
thermal conductivity is reduced.
Swiss-roll micro burners 
 The central section of a SR 
acts as a combustion zone, 
where the flame is 
stabilized. 
 The spiralling inlet and 
outlet channels form the 
heat exchange section. 
 Each inlet channel adjoins 
two outlet channels and 
vice versa.
Continued.. 
 A catalyst may also be included in the combustion zone to 
improve burner stability and to reduce the ignition 
temperature 
 At low inlet velocities, close to or lower than the laminar 
flame speed, the flames are located upstream of the 
combustion zone. 
 The SR heat exchanger then acts as a net heat sink. 
 When the velocity is increased, the flame gets anchored in 
the central combustion zone. Further increase in the 
velocity pushes the flame downstream and into the 
recirculating section. Blowout is reached soon thereafter
Micro burner geometry 
 The wall thickness, gap width, and reactor length are 
the three parameters that can be varied 
 Increasing the gap width decreases the net transverse 
heat transfer;higher gap sizes are preferable at the 
extinction limits, where heat loss from the flame 
results in thermal quenching. 
 Narrower gap sizes improve the heat transfer that can 
stabilize the blowout limit. 
 Increasing the reactor length shrinks the region of 
self-sustained combustion, due to increased heat 
losses through the reactor solid structure.
Catalytic micro combustion 
 In contrast to gas phase combustion, catalytic combustion 
occurs at a surface reaction without a flame. 
 Surface reactions are not very sensitive to the reduced size 
of micro-combustors, which implies the possibility of 
further shrinking of micro-combustors. 
 Lower temperature of catalytic combustion makes thermal 
stresses, materials limitations and heat losses less 
problematic. 
 Self-starting fuels and catalysts are highly desirable 
because it would eliminate the need for glow plugs, 
supplemental battery, electronics, etc
Combustion characteristics 
 Reactants diffuse from the bulk gas to the washcoat and 
then inside the porous support (catalyst layer). 
 Reaction takes place on catalyst sites within the support, 
and products diffuse outwards through the support and 
eventually to gas.
Stability of catalytic micro 
burners 
 Catalytic micro burners have superior stability than 
homogeneous ones. 
 Blowout stability limit is much higher in catalytic 
combustion than in homogeneous combustion. 
catalytic burner stability is affected from the fuel 
choice. 
Catalytic combustion of methane is difficult to sustain 
whereas combustion of propane, hydrogen, and 
methanol on Pt can be sustained .
 . 
 Hydrogen dissociation is a non-activated reaction 
 Hydrogen self-ignites on Pt at room temperature (i.e., 
it does not require external heating). 
 Methane adsorption on noble metals is activated (an 
activation energy of~11 kcal/mol on Pt) rendering its 
combustion slow. As a result, heat is not generated fast 
enough to compensate for heat losses
Where is catalyst placed? 
 For a microburner length is 2 cm only 1cm is catalytic. 
The catalyst is placed in the front, middle, or rear part 
of the burner. 
 Catalyst placement is more important for low 
conductivity walls where axial heat transfer is slow. At 
high conductivities, catalyst placement is of secondary 
importance.
Porous media micro-combustion 
 In conventional combustion, the combustion process 
occurs in a mostly gaseous environment, convection is the 
main mode of pre-heating. 
 Whereas in porous media, the combustion takes place in a 
three dimensional solid porous matrix having 
interconnected pores. Apart from convection, the 
conduction and radiation modes of heat transfer are also 
activated. This enhances the heat transfer (pre-heating) 
from the burned hot gases to unburned mixture. 
 These characteristics seem favorable to micro-combustion 
because the pre-heating is useful in increasing the flame 
temperature, and therefore sustaining flames in a smaller 
space. 
 A higher and more uniform temperature distribution can 
be achieved along the wall of the microcombustor.
Conclusions 
 Given the nearly hundredfold mass-based greater 
energy density of fuels, an improvement over batteries 
could be achieved if greater than 1% of the energy 
stored in chemical bonds could be converted to 
electricity 
 Catalytic combustion is superior at these scales over its 
homogeneous counterpart and can be sustained for 
fairly large heat losses, much lower wall conductivity 
materials, and much higher inlet velocities but not 
necessarily with complete fuel conversion.
References 
[1].S.K. Chou, W.M. Yang, K.J. Chua , J. Li K.L. Zhang,” Development of micro 
power generators – A review”, Applied Energy 88 (2011) 1–16 
[2]. A.Carlos Fernandez-Pello, “micropowergeneration using combustion:Issues 
and Approaches”, Proceedings of the Combustion Institute, Volume 29, 
2002,pp. 883–899 
[3]. Uttam Rana, Suman Chakraborty, S.K. Som,” Thermodynamics of premixed 
combustion in a heat recirculating micro combustor”, Energy 68 (2014) 510-518 
[4].Niket S. Kaisare a, Dionisios G. Vlachos,” A review on microcombustion: 
Fundamentals, devices and applications”, Progress in Energy and Combustion 
Science 38 (2012) 321-359 
[5]. Nam Kim , Souichiro Kato , Takuya Kataoka , Takeshi Yokomori , 
Shigenao Maruyama, Toshiro Fujimori , Kaoru Maruta ,” Flame stabilization and 
emission of small Swiss-roll combustors as heaters”, Combustion and Flame 141 
(2005) 229–240..

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Flame stabilisation in microcombustors

  • 1. By T SHYAMKUMAR 14TH14F
  • 2. Why micro combustion ?  Batteries have low specific energy  Liquid hydrocarbon fuels have a very high specific energy  To reduce system weight  To increase operational lifetimes  To reduce unit cost  Easily rechargeable
  • 3. APPLICATIONS  Micro-satellite thrusters for station keeping require a small thrust and a high specific impulse for an operation period of years. An efficient micro-thruster requires propellants with a large energy density  Micro-air vehicles for reconnaissance and surveillance in urban and battle field.
  • 4. SCALING PARAMETERS 1.Based on physical dimension of the combustor if physical length < 1mm :microcombustion if physical length is between 1mm -10mm : mesoscale combustion 2.Based on quenching diameter The combustion is called micro-scale (mesoscale) if the combustor size is smaller (larger) than the quenching diameter 3. By the relative length scale of the entire device to that of conventional large scale devices for similar purposes.
  • 5. Thermo physical Issues  As the characteristic length of the device is reduced, the Reynolds and Peclet numbers decrease and fluid flow tends to be less turbulent, so the viscous effects and the diffusive transport of mass and heat become increasingly important.  From the point of view of combustion, an important issue is the magnitude of the residence time, because it decreases as the length of the combustor decreases, and it has to be larger than the chemical time, for complete combustion to occur.  At the length scales of microcombustion devices, heat transfer by natural convection becomes small because the induced buoyant flow is small
  • 6.  However, heat transfer by conduction through the gas to the surrounding surfaces and by forced convection in the intake and exhaust channels and in the combustion chamber is significant.  Heat transfer by radiation also increases as the characteristic length decreases because of the large view factor.  Problematic for combustion chambers due to wall quenching  Silica aerogel can be used to insulate the combustor.  Reduced thermal gradients will reduce thermal expansion stresses and subsequent misalignments in moving parts. Biot number for a steel or a silicon device with a length scale of 10 mm,and subjected to moderate convection and radiation (combined convection and radiation heat transfer coefficient of 100 W/m2K), will be of the order of 0.002
  • 7. Combustion  Physical time available for combustion (residence time) must be larger than the time required for the chemical reaction to occur (combustion time).  Since in general the residence time will be small in micro combustors, it is important to have small chemical times to ensure completion of the combustion process within the combustor .  As engine size or combustion volume decreases, the surface-to-volume ratio increases, resulting in increased combustor surface heat losses and increased potential destruction of radical species at the wall.  Ceramic materials, such as SiO2, SiC, and Si3N4, can withstand temperatures of around 1700 K, which are high enough to ensure short chemical times  Although the increase of the surface-to-volume ratio of the combustor presents a problem for gas-phase combustion, it favors catalytic combustion
  • 8. Flame propagation and stabilization  When flames (e.g., a torch) are put in narrow channels, they do not propagate through, when the gap size is below what is known as the quenching distance  Quenching distance is in the range of ~2.5 mm for cold walls (500 K)  Burner insulation and thermal management are important in minimizing heat loss and mitigating thermal quenching
  • 9. Characteristics of homogeneous micro burners Quenching mechanisms  Thermal - heat loss from the burner walls and gases  Radical quenching - diffusion of radicals from the flame to the walls followed by their recombination on walls to produce stable molecules.  In the mesoscopic range radical quenching plays only a secondary role.
  • 10. The excess enthalpy principle  Qin - enthalpy of the inlet stream .  Qc - heat generated on combustion.  Qin + Qc - outlet enthalpy in an adiabatic system.  Sufficient pre-heating of the incoming gases is required to stabilize combustion in microburners.  Qr is recirculted to cold inlet stream.  Maximum temperature is greater than the adiabatic temperature rise .
  • 11. The role of burner walls  Wall conductivity and the wall thickness are key parameters for flame stability.  Direction of transverse heat transfer downstream of the flame is from hot gases to the wall and upstream of the flame is from the wall to the cold inlet gases  Micro burner can be split into three distinct zones: the pre-heating, the combustion and the post-combustion zones.
  • 12. Micro burner stability 1 The dual role of walls in heat exchange  As the wall conductivity decreases, the flame temperatures become higher and the flame remains localized but drifts downstream due to insufficient pre-heating.  Highly conductive walls, on the other hand, dissipate heat to the environment and also longitudinally, causing the entire burner surfaces to be hot  Two modes of flame quenching occur: a spatially ‘distributed’ type for high wall thermal conductivities, thick walls, and/or low flow velocities and blowout at high velocities, low wall conductivity, or thin walls.
  • 13. 2 Effect of flow velocity  The inlet velocity is easily varied experimentally and controls the power input to a burner  At low flow velocities, the power input is low, the burner temperatures are low and extinction is the dominant quenching mechanism.  At high flow velocities the power input is high but the residence time is low, and as a result blowout is the dominant quenching mechanism.  For fast flows, higher wall conductivity facilitates heat transfer upstream resulting in more stable flames
  • 14. Excess enthalpy burners(heat recirculation)  Thermal enthalpy of the incoming reactants is increased via preheating without diminishing the chemical enthalpy via chemical reaction.  A PC with LabView software is used to control mass flow controllers for fuel and air and to record data from thermocouples for temperature measurement. The exhaust gas composition was analyzed with a gas chromatograph. Electrically heated Kantal wire is used for ignition
  • 15. Heat recuperation in reverse-flow micro burners  Temporal thermal coupling between the hot product and the cold reactant streams, achieved through periodic flow reversal in reverse-flow (RF) reactors.  Requirements - high gas-solid heat transfer rates and reasonably high heat capacity of the burner solid structure. Porous beds are required to increase the gas-solid heat transfer rates  The RF operation improves the microburner stability at the blowout limit, but does not affect the stability at extinction.Micro burner stability increases as the wall thermal conductivity is reduced.
  • 16. Swiss-roll micro burners  The central section of a SR acts as a combustion zone, where the flame is stabilized.  The spiralling inlet and outlet channels form the heat exchange section.  Each inlet channel adjoins two outlet channels and vice versa.
  • 17. Continued..  A catalyst may also be included in the combustion zone to improve burner stability and to reduce the ignition temperature  At low inlet velocities, close to or lower than the laminar flame speed, the flames are located upstream of the combustion zone.  The SR heat exchanger then acts as a net heat sink.  When the velocity is increased, the flame gets anchored in the central combustion zone. Further increase in the velocity pushes the flame downstream and into the recirculating section. Blowout is reached soon thereafter
  • 18. Micro burner geometry  The wall thickness, gap width, and reactor length are the three parameters that can be varied  Increasing the gap width decreases the net transverse heat transfer;higher gap sizes are preferable at the extinction limits, where heat loss from the flame results in thermal quenching.  Narrower gap sizes improve the heat transfer that can stabilize the blowout limit.  Increasing the reactor length shrinks the region of self-sustained combustion, due to increased heat losses through the reactor solid structure.
  • 19. Catalytic micro combustion  In contrast to gas phase combustion, catalytic combustion occurs at a surface reaction without a flame.  Surface reactions are not very sensitive to the reduced size of micro-combustors, which implies the possibility of further shrinking of micro-combustors.  Lower temperature of catalytic combustion makes thermal stresses, materials limitations and heat losses less problematic.  Self-starting fuels and catalysts are highly desirable because it would eliminate the need for glow plugs, supplemental battery, electronics, etc
  • 20. Combustion characteristics  Reactants diffuse from the bulk gas to the washcoat and then inside the porous support (catalyst layer).  Reaction takes place on catalyst sites within the support, and products diffuse outwards through the support and eventually to gas.
  • 21. Stability of catalytic micro burners  Catalytic micro burners have superior stability than homogeneous ones.  Blowout stability limit is much higher in catalytic combustion than in homogeneous combustion. catalytic burner stability is affected from the fuel choice. Catalytic combustion of methane is difficult to sustain whereas combustion of propane, hydrogen, and methanol on Pt can be sustained .
  • 22.  .  Hydrogen dissociation is a non-activated reaction  Hydrogen self-ignites on Pt at room temperature (i.e., it does not require external heating).  Methane adsorption on noble metals is activated (an activation energy of~11 kcal/mol on Pt) rendering its combustion slow. As a result, heat is not generated fast enough to compensate for heat losses
  • 23. Where is catalyst placed?  For a microburner length is 2 cm only 1cm is catalytic. The catalyst is placed in the front, middle, or rear part of the burner.  Catalyst placement is more important for low conductivity walls where axial heat transfer is slow. At high conductivities, catalyst placement is of secondary importance.
  • 24. Porous media micro-combustion  In conventional combustion, the combustion process occurs in a mostly gaseous environment, convection is the main mode of pre-heating.  Whereas in porous media, the combustion takes place in a three dimensional solid porous matrix having interconnected pores. Apart from convection, the conduction and radiation modes of heat transfer are also activated. This enhances the heat transfer (pre-heating) from the burned hot gases to unburned mixture.  These characteristics seem favorable to micro-combustion because the pre-heating is useful in increasing the flame temperature, and therefore sustaining flames in a smaller space.  A higher and more uniform temperature distribution can be achieved along the wall of the microcombustor.
  • 25. Conclusions  Given the nearly hundredfold mass-based greater energy density of fuels, an improvement over batteries could be achieved if greater than 1% of the energy stored in chemical bonds could be converted to electricity  Catalytic combustion is superior at these scales over its homogeneous counterpart and can be sustained for fairly large heat losses, much lower wall conductivity materials, and much higher inlet velocities but not necessarily with complete fuel conversion.
  • 26. References [1].S.K. Chou, W.M. Yang, K.J. Chua , J. Li K.L. Zhang,” Development of micro power generators – A review”, Applied Energy 88 (2011) 1–16 [2]. A.Carlos Fernandez-Pello, “micropowergeneration using combustion:Issues and Approaches”, Proceedings of the Combustion Institute, Volume 29, 2002,pp. 883–899 [3]. Uttam Rana, Suman Chakraborty, S.K. Som,” Thermodynamics of premixed combustion in a heat recirculating micro combustor”, Energy 68 (2014) 510-518 [4].Niket S. Kaisare a, Dionisios G. Vlachos,” A review on microcombustion: Fundamentals, devices and applications”, Progress in Energy and Combustion Science 38 (2012) 321-359 [5]. Nam Kim , Souichiro Kato , Takuya Kataoka , Takeshi Yokomori , Shigenao Maruyama, Toshiro Fujimori , Kaoru Maruta ,” Flame stabilization and emission of small Swiss-roll combustors as heaters”, Combustion and Flame 141 (2005) 229–240..