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Air ratio

Thus the quantitative elemental analysis of the fuel establishes an overall formula, (CH O ) , where the coefficient x, related to the average molecular weight, has no effect on the fuel-air ratio. [Pg.179]

In a general manner, diesel engines, jet engines, and domestic or industrial burners operate with lean mixtures and their performance is relatively insensitive to the equivalence ratio. On the other hand, gasoline engines require a fuel-air ratio close to the stoichiometric. Indeed, a too-rich mixture leads to an excessive exhaust pollution from CO emissions and unburned hydrocarbons whereas a too-lean mixture produces unstable combustion (reduced driveability and misfiring). [Pg.180]

Several parameters come into the relation between density and equivalence ratio. Generally, the variations act in the following sense a too-dense motor fuel results in too lean a mixture causing a potential unstable operation a motor fuel that is too light causes a rich mixture that generates greater pollution from unburned material. These problems are usually minimized by the widespread use of closed loop fuel-air ratio control systems installed on new vehicles with catalytic converters. [Pg.188]

The diesel engine operates, inherently by its concept, at variable fuel-air ratio. One easily sees that it is not possible to attain the stoichiometric ratio because the fuel never diffuses in an ideal manner into the air for an average equivalence ratio of 1.00, the combustion chamber will contain zones that are too rich leading to incomplete combustion accompanied by smoke and soot formation. Finally, at full load, the overall equivalence ratio... [Pg.212]

Measured in MJ/m or Btu/ft, the Wobbe Index has an advantage over the calorific value of a gas (the heating value per unit volume or weight), which varies with the density of the gas. The Wobbe Index Is commonly specified in gas contracts as a guarantee of product quality. A customer usually requires a product whose Wobbe Index lies within a narrow range, since a burner will need adjustment to a different fuel air ratio if the fuel quality varies significantly. A sudden increase in heating value of the feed can cause a flame-out. [Pg.108]

Laboratory experiments using rodents, or the use of gas analysis, tend to be confused by the dominant variable of fuel—air ratio as well as important effects of burning configuration, heat input, equipment design, and toxicity criteria used, ie, death vs incapacitation, time to death, lethal concentration, etc (154,155). Some comparisons of polyurethane foam combustion toxicity with and without phosphoms flame retardants show no consistent positive or negative effect. Moreover, data from small-scale tests have doubtful relevance to real fine ha2ards. [Pg.481]

Many commercial gases are generated by burning hydrocarbons (qv) eg, natural gas or propanes, in air (see Gas, natural Liquified petroleum gas). The combustion process, especially the amount of air used, determines the gas composition. For a given fuel-to-air ratio, the gas composition can be used to determine the water vapor content required to achieve a desired equiUbrium carbon content of the austenite (see Combustiontechnology). [Pg.213]

Ratio and Multiplicative Feedforward Control. In many physical and chemical processes and portions thereof, it is important to maintain a desired ratio between certain input (independent) variables in order to control certain output (dependent) variables (1,3,6). For example, it is important to maintain the ratio of reactants in certain chemical reactors to control conversion and selectivity the ratio of energy input to material input in a distillation column to control separation the ratio of energy input to material flow in a process heater to control the outlet temperature the fuel—air ratio to ensure proper combustion in a furnace and the ratio of blending components in a blending process. Indeed, the value of maintaining the ratio of independent variables in order more easily to control an output variable occurs in virtually every class of unit operation. [Pg.71]

FAR or AFR. The composition of a mixture of fuel and air or oxidant is often specified according to the Fuel to Air Ratio (FAR), and can be expressed on a mass, molar, or volume basis. The FAR is normalized to the stoichiometric composition by defining the equivalence ratio ( ) as in equation 1, where = mass of fuel, kg and = mass of oxidizer, kg. [Pg.514]

L. Eltinge, Fuel-Air Ratio and Distribution from Exhaust Gas Composition, SAE 680114, Society of Automotive Engineers, Warrendale, Pa., 1968. [Pg.495]

While process design and equipment specification are usually performed prior to the implementation of the process, optimization of operating conditions is carried out monthly, weekly, daily, hourly, or even eveiy minute. Optimization of plant operations determines the set points for each unit at the temperatures, pressures, and flow rates that are the best in some sense. For example, the selection of the percentage of excess air in a process heater is quite critical and involves a balance on the fuel-air ratio to assure complete combustion and at the same time make the maximum use of the Heating potential of the fuel. Typical day-to-day optimization in a plant minimizes steam consumption or cooling water consumption, optimizes the reflux ratio in a distillation column, or allocates raw materials on an economic basis [Latour, Hydro Proc., 58(6), 73, 1979, and Hydro. Proc., 58(7), 219, 1979]. [Pg.742]

Excess Air for Combustion More than the theoretical amount of air is necessary in practice to achieve complete combustion. This excess air is expressed as a percentage of the theoretical air amount. The equivalence ratio is defined as the ratio of the actual fuel-air ratio to the stoichiometric fuel-air ratio. Equivalence ratio values less than... [Pg.2379]

Products of Combustion For lean mixtures, the products of combustion (POC) of a sulfur-free fuel consist of carbon dioxide, water vapor, nitrogen, oxygen, and possible small amounts of carbon monoxide and unburned hydrocarbon species. Figure 27-12 shows the effect of fuel-air ratio on the flue gas composition resulting from the combustion of natural gas. In the case of solid and liquid fuels, the... [Pg.2379]

Carhon Monoxide Carbon monoxide is a key intermediate in the oxidation of all hydrocarbons. In a well-adjusted combustion system, essentially all the CO is oxidized to CO9 and final emission of CO is veiy low indeed (a few parts per million). However, in systems which have low temperature zones (for example, where a flame impinges on a wall or a furnace load) or which are in poor adjustment (for example, an individual burner fuel-air ratio out of balance in a multiburner... [Pg.2382]

Nozzle-Mix Burners The most widely used industrial gas burners are of the nozzle-mix type. The air and fuel gas are separated until they are rapidly mixed and reacted after leaving the ports. Figure 27-32c, d, e,f, h shows some examples of the variety of nozzle-mix designs in use. These burners allow a wide range of fuel-air ratios, a wide vari-... [Pg.2392]

Minimization of pollutants from the combustion chamber. This approach consists of designing the engine with improved fuel-air distribution systems, ignition timing, fuel-air ratios, coolant and mixture temperatures, and engine speeds for minimum emissions. The majority of automobiles sold in the United States now use an electronic sensor/control system to adjust these variables for maximum engine performance with minimum pollutant emissions. [Pg.525]

Where Tja is the aetual temperature at the eompressor exit. The regenerator inereases the temperature of the air entering the burner, thus redueing the fuel-to-air ratio and inereasing the thermal effieieney. [Pg.72]

Figure 10-5. Range of burnabie fuei-air ratios versus eombustor gas veioeity. Figure 10-5. Range of burnabie fuei-air ratios versus eombustor gas veioeity.
The importanee of air veioeity in the primary zone is known. In the primary zone fuel-to-air ratios are about 60 1 the remaining air must be added somewhere. The seeondary, or dilution, air should only be added after the primary reaetion has reaehed eompletion. Dilution air should be added gradually so as not to queneh the reaetion. The addition of a flame tube as a basie eombustor eomponent aeeomplishes this, as shown in Figure 10-6. Flame tubes should be designed to produee a desirable outlet profile and to last a long time in the eombustor environment. Adequate life is assured by film eooling of the liner. [Pg.378]

Volumetric heat-release rate. The heat-release rate is proportional to the fuel-to-air ratio and the combustor pressure, and it is a function of... [Pg.383]

Figure 10-22. Effect of fuel /air ratio on flame temperature and NOx emissions. Figure 10-22. Effect of fuel /air ratio on flame temperature and NOx emissions.
The firing controls that best ensure an air-rich mixture are often referred to as metering type controls, because gas flow and air flow are metered, thus the fuel-air ratio is controlled. The fuel-air ratio is the most important factor for safe, economical firing, so it is better to control it directly. Do not settle for low budget controllers that... [Pg.139]

Corrosion of metals by fuel ashes only occurs where the fuel ash contains a liquid phase. Temperatures at which the first liquid will form are inversely proportional to the oxygen partial pressure. Thus, when firing fuels at high excess air ratios, fuel ash corrosion occurs at lower temperatures than when firing fuels with low excess air ratios. [Pg.266]

The temperature rise in the combustion chamber may then be determined from Eq. (3.33), in the approximate form (Tj T2) = (af + b). Strictly a and b are functions of the temperature of the reactants and the fuel-air ratio/, but fixed values are assumed to cover a reasonable range of conditions. Accordingly, the fuel-air ratio may be expressed as... [Pg.41]

Calculation of the specific work and the arbitrary overall efficiency may now be made parallel to the method used for the a/s cycle. The maximum and minimum temperatures are specified, together with compressor and turbine efficiencies. A compressor pressure ratio (r) is selected, and with the pressure loss coefficients specified, the corresponding turbine pressure ratio is obtained. With the compressor exit temperature T2 known and Tt, specified, the temperature change in combustion is also known, and the fuel-air ratio / may then be obtained. Approximate mean values of specific heats are then obtained from Fig. 3.12. Either they may be employed directly, or n and n may be obtained and used. [Pg.41]

Thus there are three modifications to the a/s efficiency analysis, involving (i) the specific heats ( and n ), (ii) the fuel-air ratio / and the increased turbine mass flow (I +/), and (iii) the pressure loss term S. The second of these is small for most gas turbines which have large air-fuel ratios and / is of the order of l/IOO. The third, which can be significant, can also be allowed for a modification of the a/s turbine efficiency, as given in Hawthorne and Davis [I]. (However, this is not very convenient as the isentropic efficiency tjt then varies with r and jc, leading to substantial modifications of the Hawthome-Davis chart.)... [Pg.42]

Guha [5] pointed out some limitations in the linearised analyses developed by Horlock and Woods to determine the changes in optimum conditions with the three parameters n (and n ),/ and Not only is the accurate determination of (Cpg)i3 (and hence n ) important but also the fuel-air ratio although small, it cannot be assumed to be a constant as r is varied. Guha presented more accurate analyses of how the optimum conditions are changed with the introduction of specific heat variations with temperature and with the fuel-air ratio. [Pg.42]

Fig. 6.3. HRSG performance of STIC plant at different steam/air ratio.s (after Lloyd [2]). Princeton University... Fig. 6.3. HRSG performance of STIC plant at different steam/air ratio.s (after Lloyd [2]). Princeton University...
A similar argument can be used for a fuelled semi-closed cycle, assuming that it can be regarded as the addition of an open CBT plant and a closed CHT cycle with identical working gas mass flow rates (and small fuel air ratios). Suppose the latter receives its heat supply from the combustion chamber of the former in which the open cycle combustion takes place. If the specific heats of air and products are little different, then the work output is doubled when the two plants are added together, but the fuel supply is also approximately doubled. The efficiency of the combined semi-closed plant is, therefore, approximately the same as that of the original open cycle plant. [Pg.140]

Fig. 8.10. Overall eftieieneies of a sleam/TCR plant and a ba.sie STIG plant, as functions of the steam/air ratio... Fig. 8.10. Overall eftieieneies of a sleam/TCR plant and a ba.sie STIG plant, as functions of the steam/air ratio...
Newby et al. 6 also studied a steam/TCR cycle with similar parameters and steam/air ratio. They calculated an efficiency of 48.7%, compared with 35.7% for a comparable CBT plant, 45.6% for a STIG plant and 56.8% for a CCGT plant, all for similar pressure ratios and top temperatures. [Pg.150]


See other pages where Air ratio is mentioned: [Pg.195]    [Pg.196]    [Pg.196]    [Pg.339]    [Pg.2379]    [Pg.2380]    [Pg.2509]    [Pg.2514]    [Pg.371]    [Pg.372]    [Pg.377]    [Pg.400]    [Pg.403]    [Pg.335]    [Pg.335]    [Pg.47]    [Pg.219]   
See also in sourсe #XX -- [ Pg.114 ]




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Air to cloth ratio

Air to liquid ratio

Air-to-fuel ratio

Air-to-solid ratio

Air/fuel ratio

Air/fuel ratio control

Air/gas ratio

Excess air ratio

Steam air ratios

Stoichiometric air-fuel ratio

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