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484

5.5

Porous Burners

Dimosthenis Trimis, Olaf Picken cker, and Klemens Wawrzinek

5.5.1

Introduction

Combustion processes dominate the entire energy and transport sectors. The different burner types mainly depend on the fuel type (gaseous, liquid, or solid) and the application requirements (operating conditions, size, and emission limits). Although all possible fuel types are presently being used, there are clear signs that natural gas is becoming of increasing importance, especially in fields where lowemission thermal energy is needed. This is the case in domestic appliances such as household heating and hot-water supply systems, where low cost is another important factor that burner must have to be of interest to the market. In industrial processes such as drying, coating, and preheating, more stringent emission requirements and increased process efficiency are the driving forces for further developments in burner technology.

Two types of burner emissions are of major importance: 1) emissions due to incomplete combustion such as carbon monoxide and unburned hydrocarbons, and 2) hazardous combustion byproducts such as nitrogen oxides and sulfur oxides (greenhouse gases and/or toxic). Concerning emissions due to incomplete combustion, several measures can be applied, such as premixed combustion instead of diffusion-type flame, longer residence time in the reaction region, better insulation of the combustion chamber, higher combustion chamber temperature, more homogeneous mixing of the reactants, etc. Concerning combustion byproducts, the amount of sulfur oxides is related only to the sulfur content of the applied fuel (which is highest for solid fuels and lowest for natural gas), while the amount of nitrogen oxides, which are the most important nowadays in environmental protection, basically depends on the combustion temperature and the residence time at high temperatures. Thus, all efforts dealing with the abatement of nitrogen oxide emissions focus on reduction of the combustion temperature while taking into account that a spatially homogeneous minimum combustion temperature is compulsory to avoid incomplete combustion.

Several concepts for low-NOx burners emerged in the last two decades, especially for burners fired with natural gas. A reduction in combustion temperature is common to all concepts, but it is realized in different ways: exhaust gas recirculation, internal recirculation regions, staged combustion with heat decoupling, and direct

Cellular Ceramics: Structure, Manufacturing, Properties and Applications.

Michael Scheffler, Paolo Colombo (Eds.)

Copyright 2005 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim

ISBN: 3-527-31320-6

5.5 Porous Burners 485

heat extraction from the combustion region by interaction and heat exchange with a porous solid matrix are the major strategies applied to reduce the combustion temperature homogeneously (without allowing disturbances from hot spots and cold region) so that NOx emissions are reduced, without paying the penalty of increased emissions due to incomplete combustion.

A significant decrease in NOx emissions was achieved with the development of radiant porous surface burners. Such burners produce a flame sheet very near to the burner support, which operates at a high temperature and radiates a part of the heat released by combustion to the appliance. Thus, the combustion temperature and hence the NOx emissions decreases.

A further improvement was achieved by the development of volumetric porous radiant burners, which completely trap the flame inside a porous structure and have the same benefits as radiant surface burners even at significantly higher heat loads. They also show a higher turn-down ratio than conventional burners.

In recent years ceramic porous structures have been increasingly used as burner supports, mainly for natural gas combustion in domestic and industrial appliances. Cellular ceramic structures offer an interesting alternative to metallic burner supports due to higher operating temperatures, more efficient heat extraction through the radiating porous surface and/or volume, and potentially better performance concerning flashback safety. The burner supports can be categorized as those for catalytic combustion, for surface combustion, or for volumetric porous combustion (Fig. 1). In most cases flat plate geometries or cylinders are used. The ceramic supports can be sintered or fiber-based, while the materials range from mullites and alumina to silicon carbide fibers.

In this chapter an overview of the different burner types using porous ceramic burner supports is given, and the major properties affecting the combustion process

Surface Radiant Burners

Middle wave length

Thermal loads ca. 120-600 kW/m²

(up to 3000 kW/m2 in blue flame mode) Radiating temperature ca. 900-1100 °C

Catalytic radiators

Long wave length

Thermal load ca. 50 kW/m²

Radiating temperature ca. 600 °C

Volumetric Porous Burners

Short wave length

Thermal loads ca. 200-4000 kW/m² (up to 8000 kW/m2 with air preheating)

Radiating temperature ca. 1100-1500 °C

Fig. 1 Different types of porous burners operated with gas [1].

486 Part 5 Applications

and flame stabilization are discussed. The case of volumetric porous burners stabilized by flame quenching is discussed in more detail. Also an overview on the different structures, their characteristic properties, and the suitable applications is given.

5.5.2

Flame Stabilization of Premixed Combustion Processes in Porous Burners

Flame propagation of premixed fuel/oxidant mixtures in porous inert media depends on the structure and physical properties of the solid matrix and on the properties of the combustible gas. The resulting flame propagation modes can be classified into different regimes, of which some important parameters are given in Table 1. This chapter discusses only regimes in which no pressure gradient occurs in the reaction zone, that is, the low-velocity regime (LVR) and the high-velocity regime (HVR). The solid matrix strongly influences the reaction conditions of combustion. Heat transport in the burner is dominated by the properties of the solid material, especially under real operating conditions, where the porous matrix reaches high temperatures. Ceramic spheres and other packing material can be used, but cellular ceramics are the most interesting structures for practical applications. In Ref. [2] an overview on applicable porous media for porous burners is given.

Table 1 Flame propagation regimes in porous media [3–6].

Regime

Speed of combustion

Mechanism of flame propagation

 

wave/m s–1

 

 

 

 

Low-velocity regime (LVR)

0–10–4

heat conduction and interphase heat

 

 

exchange

High-velocity regime (HVR)

0.1–10

high convection

Rapid-combustion regime (RCR)

10–100

convection with low pressure gradient

Sound-velocity regime (SVR)

100–300

convection with significant pressure

 

 

gradient

Low-velocity detonation (LVD)

500–1000

self-ignition with shock wave

Normal detonation (ND)

1500–2000

detonation with momentum and heat

 

 

loss

Flame stabilization of premixed combustion in porous media differs significantly from that of free premixed flames. Stabilization depends mainly on the heat-trans- port properties of the solid matrix. Heat transport in a porous medium is often described by an effective thermal conductivity which comprises radiation and heat conduction of both solid and gas phases and additionally gas convection and dispersive mechanisms (see Chapter 4.3). The effective heat transport inside of a porous medium is 2–3 orders of magnitude higher than in free flames and can be considered the dominant parameter for flame propagation in most cases. Compared with free premixed flames, the higher heat transport leads to 10–30 times faster flame

5.5 Porous Burners 487

Combustion in porous media

Stationary

 

Instationary

 

 

 

 

 

 

 

 

Premixed Non-premixed

Convective

 

Active

 

Stabilization

 

Stabilization by

stabilization

 

cooling

 

by radiative cooling

 

thermal quenching

 

 

 

 

 

 

 

Fig. 2 Overview of flame stabilization methods in porous media.

propagation [7, 8], which hampers flame stabilization in porous media. For solving the problem of flame stabilization in porous media, different approaches have been developed, which are summarized in Fig. 2.

In the LVR and HVR regimes most relevant to burner applications, flame propagation or extinction can be described by a modified P clet number Pe formulated with the laminar flame speed SL instead of a flow velocity

Pe ¼

SL dp;eff f cp;f

SL dp;eff

(1)

 

¼

 

kf

af

where dp,eff is an equivalent porous cavity diameter, cp,f the specific heat capacity, f the density, kf the thermal conductivity, and af the thermal diffusivity of the gas mixture. The modified P clet number describes the ratio between the heat release due to combustion in a pore and the heat removal on the walls of a pore. It also describes the ratio of the characteristic porous cavity diameter to the laminar flame front thickness. This ratio must exceed a critical value for flame propagation in a cold porous medium. According to Ref. [3] flame propagation in porous media is possible if:

Pe ‡ 65 – 45.

(2)

If Pe < 65 then the flame structures extinguish (quenching), since heat is transferred to the porous matrix at a higher rate than it is produced. Flame propagation in porous media in the LVR and HVR regimes (Table 1) is mostly dominated by convection but the high conductivity and the radiation properties of the solid matrix also influence the flame speed, especially at higher temperatures. The quantity dp,eff represents an equivalent length scale of the pore size for heat transport. Whether or not flame propagation will occur in a porous inert medium can be decided by the choice of the pore size of the solid matrix. Thus, a critical pore size exists above which flame propagation and below which flame quenching occurs. Nevertheless, flame propagation may also occur in subcritical cavities if the temperature of the matrix is high enough that reactions are not quenched by the low wall temperature.

488 Part 5 Applications

Thus, combustion processes inside subcritical porous media need a special starting procedure to preheat the porous matrix to the operating temperature. This kind of operation is often called filtration combustion.

5.5.2.1

Flame Stabilization by Unsteady Operation

Combustion in subcritical porous media (low characteristic porous cavity size) will only take place if the temperature of the matrix is high enough to ignite the mixture. Flame propagation is driven mainly by the thermal conductivity of the solid material and interphase heat exchange, while the heat transport in the gas phase is negligible. The so-called combustion wave travels very slowly through the porous matrix with a speed of 10–5 to 10–4 m s–1 [9–11], either in or against the flow direction. In the former case superadiabatic and in the latter subadiabatic combustion temperatures occur (in comparison to the adiabatic flame temperature). The direction of the wave is mainly dependent on the heat capacities of the solid and gas phases and on interphase heat exchange. For a standing wave only one operational point is possible for a certain gas mixture. However, the very low speed of the combustion wave allows operation with varying gas velocities by changing the flow direction when the combustion wave reaches the end of the reactor. Figure 3 shows the temperature profiles in a reactor with a subcritical porous matrix. In this case the combustion wave travels in the flow direction. The heat of combustion heats the porous matrix downstream of the combustion wave.

When the flow direction is reversed, the hot porous matrix preheats the fresh gas mixture, and superadiabatic combustion occurs [10, 11]. With this principle gas mixtures with very low heat content can be burned. The flame speeds in such reactors are about 2–4 times higher than the laminar flame speed [12, 13].

 

 

T1

 

T2

reactor with subcritical

temperature

porous matrix

profile in

 

 

 

 

the gas

 

 

 

 

 

exhaust 2

 

 

 

 

exhaust 1

 

 

 

 

 

after change

 

 

 

 

 

 

of direction

 

 

 

 

 

 

 

 

shift of combustion wave with time

direction 1

direction 2

gas mixture

Fig. 3 Scheme of a subcritical porous reactor in alternating operation.

5.5 Porous Burners 489

5.5.2.2

Flame Stabilization under Steady Operation by Convection and Cooling

In porous media the same flame propagation mechanisms act as in free flames, but the higher effective thermal conductivity must be considered. The effective thermal conductivity and thermal diffusivity are 2–3 orders of magnitude higher than in a gas. Following the simplified theory of flame propagation [14] the flame speed S is

proportional to the square root of the temperature diffusivity:

 

S

 

rf

(3)

 

 

 

a

 

 

 

 

s

 

where af is the thermal diffusivity, and s a characteristic timescale of the reaction. From this it results that the flame speed in porous media is 10–30 times higher than the laminar flame speed. One possibility to stabilize combustion in porous media with supercritical pore sizes (flame propagation is possible) is to induce a change in flow speed by a stepwise or continuous change in the cross sectional area (convective stabilization). For methane/air mixtures in porous media the required flow speed to avoid flashback lies in the range of 4–12 m s–1, which is about 10–30 times higher than in free flames. The exact velocity depends on the heat-transport properties of the applied porous structures and the operating conditions. This type of flame stabilization was already used in the early 1900s [15–17]. The major drawback of this flame-stabilization principle is that the power modulation range is rather small, and for low powers with corresponding low flow velocities, flame flashback may occur.

Another possibility for convective stabilization is active control of the air and/or the fuel flow rate based on temperature measurements in the porous matrix. By changing the air and/or the fuel flow rate, the flow velocity and the flame speed changes and the flame front can be stabilized by active control in a desired position within the porous matrix [18]. This stabilization principle can be used for subcritical and for supercritical pore sizes with respect to the flame-propagation criterion according to Eq. (2), but the operational range is small, and for each configuration a single operating condition is found by active control.

Another possibility for flame stabilization is to cool the reaction zone, for example, by embedded water-cooled tubes in the main reaction zone, which was also already realized in the early 1900s [19]. In Fig. 4 (left) the principle of flame stabilization by cooling of the reaction zone is schematically shown. Combustion takes place inside the pores, and the heat of reaction is conducted to the embedded water tubes.

Cooling of the reaction zone can also alternatively be realized by intense radiation from it. This principle is used nowadays in surface radiant burners, which are widely used in domestic and industrial appliances. As shown in Fig. 4 (right) the combustion region must be located close to the surface of the porous matrix in order to extract heat by radiation. However, the combustion process may be completed outside of the porous matrix, depending on the operating conditions. The porous surface extracts heat from the flame and radiates it to the environment. Effective heat transport by radiation only occurs at high temperatures above the ignition limits. This means that for radiation-cooled burners the porous matrix must be subcriti-

490 Part 5 Applications

Fig. 4 Flame stabilization in porous media by cooling.

cal with respect the modified P clet number (Eq. (1)), because otherwise the flame could move into the porous matrix, which eventually would lead to flashback. A significant drawback of this stabilization principle is that by increasing the heat load and correspondingly the flow rate of the incoming gas/air mixture, the flame location moves completely outside of the porous matrix and the burner operates in the so called blue-flame mode with significantly increased emissions. Thus, the beneficial combustion process at least partly inside of the porous matrix is only possible for a small range of power modulation (see Section 5.5.4).

5.5.2.3

Flame Stabilization under Steady Operation by Thermal Quenching

Research and development on stationary combustion completely trapped in the cavities of porous inert media started in the early decades of the 1900s. Bone [20] designed the first boilers and muffle heaters, while Lucke [21] built radiant room heaters, crucible furnaces, and cooking stoves, operating with town gas. However, even earlier pioneers such as Welch [22], Mitchell [23], Ruby [24], and Schnabel [25] developed the first appliances for different fields, most probably independently of each other. The porous media used in the early stages were packings of aluminosilicate pebbles or spheres. Also in the 1930s [26] and up to the present time [18, 27–30], there was limited but continuous research and development activity in porous-medi- um combustion. Major drawbacks in porous-medium combustion were the deficiencies of the flame stabilization concepts for a stationary combustion process completely trapped inside a porous medium.

A novel combustion technique based on combustion in porous media was developed recently [2, 31–35]. The major novelty of this work is the combustion stabilization principle based on thermal quenching, which allows extremely stable operation of the premixed combustion process in the porous matrix for a wide range of power

5.5 Porous Burners 491

modulation. The flame stabilization layer is located inside the porous matrix and is well defined by the matrix design. The combustion process is stabilized by a sudden change of the pore size, corresponding to a change in the P clet number in the combustion reactor. In region A of the porous burner, the porous-body properties are chosen in such a way that flame propagation is not possible by reducing the equivalent porous cavity diameter (subcritical P clet number). Region A functions as a preheating region and flame trap at the same time. In combustion region C, the pores are large enough that flame propagation is possible (supercritical P clet number). At the interface between regions A and C the ignition temperature is reached. In Fig. 5 the schematic setup of such a porous burner with the preheating region A and the combustion region C is shown. Depending on the actual application, additional regions may be directly combined with the described basic design of the porous burner, for example, heat exchangers, insulation, premixing chambers, and so on.

exhaust gas

heat transport for stabilization of the combustion zone

heat extraction from the combustion zone by radiation and conduction of the matrix and by convective heat transfer and dispersion

large pores (Region C); Pe > 65

small pores (Region A); Pe < 65

heat transport in axial direction by radiation, conduction, dispersion and convection

combustion zone

ignition temperature

preheating zone

fresh gas mixture

Fig. 5 Heat transport and flame stabilization in a two-layer porous burner [31].

Under stationary conditions heat transfer from the combustion region C to the flame trap in region A may heat the latter to temperatures above the ignition temperature. To prevent flashback the amount of heat which is transported against the flow direction must not be higher than the amount which is carried convectively by the fresh gas mixture into the combustion region, because otherwise a combustion wave can develop starting from the hot interface between region A and C and possibly travel against the flow direction. This can be achieved by means of a region A of low effective thermal conductivity, which allows only a small amount of heat transport against the flow direction. In contrast, region C should have a high effective thermal conductivity, because this allows operation at high flow rates without the danger of blowoff. In this respect, besides the design criteria based on the modified P clet number and the corresponding equivalent porous cavity diameters, the choice of the heat-transfer properties of regions A and C is crucial for the power modulation range of such porous burners.

The principle of flame stabilization by changing the P clet number can be used advantageously in many application fields. However, in the P clet number criterion

492 Part 5 Applications

mainly heat-transport processes are considered and, if diffusive mass transport becomes dominant, incorrect critical pore diameters may be predicted.

5.5.2.4

Diffusive Mass-Transport Effects on Flame Stabilization

The influence of diffusive mass transport on the stabilization of a flame in a porous medium is not well known. In Refs. [3, 36] flame instabilities were observed for gas mixtures containing hydrogen. These instabilities were linked to the increased influence of diffusive mass transport, which decreased the dominance of the heat transport in the flame stabilization. The ratio between diffusive mass transport and heat transport can be described by the Lewis number Lec of a component c of the gas mixture:

Lec ¼

kf

¼

af

(4)

Dc f cP;f

Dc

which is the ratio between the temperature diffusivity af and the diffusion coefficient of the component Dc. According to Refs. [3, 37] the flame structure changes for Lewis numbers smaller than unity. For many widely used gases (e.g. methane/air mixtures), Le is close to unity and therefore its influence is often neglected. However, mixtures with Lewis numbers far below unity require the consideration of mass diffusion. For example hydrogen/air and hydrogen/chlorine mixtures have Lewis numbers of about 0.4. For such low values one can expect a strong influence of diffusion on flame stabilization in porous media. This influence is neglected in the previously described P clet number criterion, because only the laminar flame speed is considered, which does not account for deformations of the flame front. This means that the constant value of the critical P clet number is not sufficient for the design of a porous burner flame trap at low Lewis numbers.

Recent flame propagation experiments in porous media for mixtures with different Lewis numbers show the dependence of the critical P clet number on the Lewis number [38]. The flame propagation limits were experimentally determined in packed beds of spheres. For each packing the critical P clet number was calculated for the lean and rich flame propagation limits with the laminar flame speed at the corresponding equivalence ratio. The average of the critical P clet numbers of different packings was plotted against the Lewis number (Fig. 6). For Lewis numbers close to and larger than unity the criterion of Ref. [3] of Pecrit » 65 could be confirmed, but for mixtures with lower Lewis number the critical P clet number was found to lie far below this limit.

The results of this experimental study show that combustion gas mixtures with a high diffusivity compared with the thermal diffusivity of the mixture, that is, Lewis numbers less than unity, have smaller critical pore diameters or critical P clet numbers than mixtures with Lewis number equal to or larger than unity. The Lewis number must be calculated for the reaction component that is lacking for a stoichiometric mixture. The results of Fig. 6 can be used for better design of flame traps for highly diffusive mixtures.

5.5 Porous Burners 493

 

100

 

 

 

 

 

 

 

 

 

 

 

 

90

 

 

 

CH4/air

 

 

 

 

C3H8/air,

 

 

 

 

 

 

 

 

 

 

fuel lean

 

 

 

 

 

 

 

 

 

 

 

 

 

80

 

 

 

 

 

 

 

 

 

 

 

 

70

Pecrit = 65 ± 30 für Le = 1

 

 

 

 

 

 

 

 

60

 

 

 

 

 

 

 

 

 

 

 

crit

50

 

 

 

 

 

 

 

 

 

 

 

Pe

 

 

 

 

 

 

 

 

 

 

 

 

 

H2/air,

 

 

 

 

 

 

 

H2/air,

 

 

40

 

 

 

 

 

C2H6/air,

 

 

 

 

 

fuel lean

 

 

 

 

 

 

fuel rich

 

 

 

 

 

 

 

 

 

 

 

 

30

 

 

 

 

 

 

fuel lean

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

H2/Cl2/HCl*

 

 

 

 

 

 

 

 

 

 

20

 

 

 

 

 

 

 

 

 

 

 

 

10

 

 

 

C3H8/air,

 

 

 

 

 

 

 

 

 

 

 

fuel rich

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

0

 

 

 

 

 

 

 

 

 

 

 

 

0

0,2

0,4

0,6

0,8

1

1,2

1,4

1,6

1,8

2

2,2

 

* experiment in steady operation

 

Le

 

 

 

 

 

Fig. 6 Critical P clet number versus Lewis number [38].

5.5.3

Catalytic Radiant Surface Burners

Most catalytic surface burners operate with nonpremixed (i.e., diffusion) combustion. The gas flows through the flat burner support, which is coated with a catalyst (in most cases noble metals such as Pt and Pd distributed on a wash coat layer, e.g., c-alumina) on the combustion side. Ceramic burner supports may have the form of a porous plate or a flexible fiber mat. The oxygen for the combustion process is provided by the surrounding air and is transported to the catalytic combustion region by diffusion processes. The surface power load is very limited due to these diffusion processes, and typical values are in the range up to 50 kW m–2. The free radiating surface at such low heat loads leads to a very low surface and combustion temperatures in the range up to 600 C. Combustion at such low temperatures is only possible in the presence of a catalyst. According to Wien’s displacement law [39] the radiation maximum moves to shorter wavelength the higher the temperature of the emitting surface is. Thus, catalytic gas IR burners have a relatively long wavelength of the emitted radiation. Due to the relatively low temperatures and the flashbacksafe diffusion mode of operation, the material requirements for the burner support are relatively low, and the main focus of such developments lies on the catalyst technology.

Premixed catalytic radiant surface burners have not reached wide commercial usage yet and are mainly the subject of research activities. In most cases premixed catalytic supported combustion [40] is performed (in contrast to full catalytic combustion) at surface temperatures of about 1100 C.

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