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Oxygen combustion constants

Figure 5.3 Aluminum-oxygen combustion. Prorducts and adiabatic flame temperature for varying pressure and constant O/F = 0.9. Figure 5.3 Aluminum-oxygen combustion. Prorducts and adiabatic flame temperature for varying pressure and constant O/F = 0.9.
After combustion, oxygen pressure is sensed by another stabilised zirconia probe and still another electrolysis reestablishes the original O2 pressure. Integration over time of current passed to keep the oxygen pressure constant after combustion gives a direct measure of the amount of oxygen answered thus COD. It was claimed that COD values can be obtained in two minutes which represent a vast saving of time over wet chemical methods. [Pg.453]

Combustion occurs with a large number of intermediate steps and even simple processes, such as the ones listed in Table 10.1, occur through dozens of coupled elementary reactions. With computer simulations it is possible to describe the interaction between the reactions, and concentration profiles can be calculated. In order to perform the computer calculations it is necessary to know the rate constants for the individual elementary reactions. Comparisons between theory and experiments are best made for a flat, premixed flame, which in its central part can be considered to have only onedimensional (vertical) variation, allowing computer calculations to be performed comparatively easily. The most important reactions are included in the computer description. In Fig. 10.1 experimental and theoretically calculated concentration curves are given for the case of low-pressure ethane/ oxygen combustion. As examples of important elementary processes we give the reactions... [Pg.303]

One mole of ethane, C2H6, is burned in excess oxygen at constant pressure and 600°C. What is the ACT of the process The amount of heat given offby the combustion of 1 mole of ethane is 1560 kj (that is, it is an exothermic reaction). [Pg.66]

Figure E2.15A Schematic of complete combustion of propane in a stoichiometric mixture of oxygen at constant pressure. The closed system is adiabatic. Figure E2.15A Schematic of complete combustion of propane in a stoichiometric mixture of oxygen at constant pressure. The closed system is adiabatic.
Figure 6-17 illustrates a constant-volume calorimeter of a type that is often used to measure q for combustion reactions. A sample of the substance to be burned is placed inside the sealed calorimeter in the presence of excess oxygen gas. When the sample bums, energy flows from the chemicals to the calorimeter. As in a constant-pressure calorimeter, the calorimeter is well insulated from its surroundings, so all the heat released by the chemicals is absorbed by the calorimeter. The temperature change of the calorimeter, with the calorimeter s heat capacity, gives the amount of heat released in the reaction. [Pg.393]

The heat of combustion of solids or liquids is usually measured in a device known as an oxygen bomb calorimeter. Such a device operates at a constant volume between states 1 and 2, and its heat loss is measured by means of the temperature rise to a surrounding water-bath. This is schematically shown in Figure 2.2. The combustion volume is charged with oxygen and a special fuel is added to ensure complete combustion of the fuel to be measured. Since the process is at constant volume (V), we have... [Pg.30]

Values of yields for various fuels are listed in Table 2.3. We see that even burning a pure gaseous fuel as butane in air, the combustion is not complete with some carbon monoxide, soot and other hydrocarbons found in the products of combustion. Due to the incompleteness of combustion the actual heat of combustion (42.6 kJ/g) is less than the ideal value (45.4 kJ/g) for complete combustion to carbon dioxide and water. Note that although the heats of combustion can range from about 10 to 50 kJ/g, the values expressed in terms of oxygen consumed in the reaction (Aho2) are fairly constant at 13.0 0.3 kJ/g O2. For charring materials such as wood, the difference between the actual and ideal heats of combustion are due to distinctions in the combustion of the volatiles and subsequent oxidation of the char, as well as due to incomplete combustion. For example,... [Pg.37]

Room volume Ambient temperature Ambient density Heat of combustion Fuel gas entering temperature Exiting gas temperature Exiting oxygen mass fraction Specific heat at constant pressure... [Pg.73]

The energy of combustion of benzoic acid determined by standardizing laboratories normally refers to the following certification conditions [21,25,39-43] (1) The benzoic acid sample is burned in a bomb at constant volume, in pure oxygen at an initial pressure of 3.04 MPa (2) the mass of sample burned, expressed in grams, is equal to three times the internal volume of the bomb in dm3 (3) the amount of water inside the bomb, expressed in grams, is also equal to three times the internal volume of the bomb in dm3 (4) the combustion reaction is referred to 298.15 K. If calibrations are not made strictly under the certification conditions, the value of Acm(BA) under the actual bomb conditions should... [Pg.94]

In equations 7.27 and 7.28 m(BA), m(cot), m(crbl), and m(wr) are the masses of benzoic acid sample, cotton thread fuse, platinum crucible, and platinum fuse wire initially placed inside the bomb, respectively n(02) is the amount of substance of oxygen inside the bomb n(C02) is the amount of substance of carbon dioxide formed in the reaction Am(H20) is the difference between the mass of water initially present inside the calorimeter proper and that of the standard initial calorimetric system and cy (BA), cy(Pt),cy (cot), Cy(02), and Cy(C02)are the heat capacities at constant volume of benzoic acid, platinum, cotton, oxygen, and carbon dioxide, respectively. The terms e (H20) and f(sin) represent the effective heat capacities of the two-phase systems present inside the bomb in the initial state (liquid water+water vapor) and in the final state (final bomb solution + water vapor), respectively. In the case of the combustion of compounds containing the elements C, H, O, and N, at 298.15 K, these terms are given by [44]... [Pg.96]

Flame combustion calorimetry in oxygen is used to measure the enthalpies of combustion of gases and volatile liquids at constant pressure [54,90]. Some highly volatile liquids (e.g., n-pentane [91]) have also been successfully studied by static-bomb combustion calorimetry. In general, however, the latter technique is much more difficult to apply to these substances than flame combustion calorimetry. In bomb combustion calorimetry, the sample is burned in the liquid state and must be enclosed in a container prior to combustion. Encapsulation may be difficult, because it is necessary to minimize the amount of vaporized compound inside the container as much as possible. In addition, volatile liquids tend to burn violently under a pressure of 3.04 MPa of oxygen, which leads to incomplete combustion. These problems are avoided in flame combustion calorimetry, where the sample is carried to the combustion zone as a vapor and burned under controlled conditions at atmospheric pressure. [Pg.114]

In the fluidized bed gasifier, crushed coal is introduced into a fluidized bed of char together with oxygen or air and steam. Coal undergoes drying, devolatilization, gasification and combustion at essentially constant temperature of about 1000 C because of the rapid mixing characteristics of fluidized beds. [Pg.299]

Zone I combustion proceeds at an overall rate equal to the product of the intrinsic burning rate, evaluated at the ambient oxygen concentration, and the total internal surface area. The char diameter necessarily stays constant and the particle density continually decreases as particle mass is evenly removed throughout the particle on the pore surfaces (constant-diameter combustion). [Pg.540]

In Zone III combustion, the burning rate is determined by the diffusive flux of oxygen through the particle boundary layer. The particle density remains constant throughout burnout and the particle size continually decreases as mass is removed solely from the particle surface (constant-density combustion). [Pg.540]

With appropriate choices of kinetic constants, this approach can reproduce the NSC experimental data quite well. Park and Appleton [63] oxidized carbon black particles in a series of shock tube experiments and found a similar dependence of oxidation rate on oxygen concentration and temperature as NSC. Of course, the proper kinetic approach for soot oxidation by 02 undoubtedly should involve a complex surface reaction mechanism with distinct adsorption and desorption steps, in addition to site rearrangements, as suggested previously for char surface combustion. [Pg.548]

Scheme (a) was compared to a system in which the combustion air temperature was adjusted, but the air flow rate maintained constant, thereby allowing the amount of oxygen to the kiln to vEu-y. This system is closed-loop scheme (b) and is shown in Fig. 26. [Pg.40]

Possible solutions to overcome this problem are (1) decrease the residence time the decrease of conversion is more than compensated by an increase of selectivity (due to the lower extent of methacrylic acid combustion), and in overall the productivity increases (2) increase the total pressure, while simultaneously increasing both the oxygen and the isobutane partial pressure, as well as the total gas flow (so as to keep a constant contact time in the reactor). A higher pressure also implies smaller reactor volume, and hence lower investment costs. Under these circumstances, productivity as high as 6.4 mmol/h/gcat was reached, which is acceptable for industrial production. The additional heat required for the recirculation of unconverted isobutane and for increased pressure would be equalized by the higher heat generated by the reaction. [Pg.270]


See other pages where Oxygen combustion constants is mentioned: [Pg.200]    [Pg.85]    [Pg.29]    [Pg.112]    [Pg.15]    [Pg.228]    [Pg.166]    [Pg.390]    [Pg.419]    [Pg.1099]    [Pg.1910]    [Pg.1960]    [Pg.211]    [Pg.521]    [Pg.2359]    [Pg.139]    [Pg.248]    [Pg.450]    [Pg.173]    [Pg.109]    [Pg.435]    [Pg.39]    [Pg.496]    [Pg.438]    [Pg.370]    [Pg.139]    [Pg.278]    [Pg.95]    [Pg.100]    [Pg.125]    [Pg.369]    [Pg.422]    [Pg.40]   
See also in sourсe #XX -- [ Pg.422 ]




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