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Adiabatic temperature change

When a reactor is operated adiabatically, and when only one reaction takes place, there is a simple relationship between the temperature and the fractional conversion. [Pg.264]

For an adiabatic flow reactor operating at steady state with no shaft work, Eqn. (8-6) simplifies to [Pg.264]

Equation (8-18a) shows that the temperature, T, is proportional to the fractional conversion, jca, for an adiabatic flow reactor at steady state. If the fractional conversion is known, the corresponding temperature can be calculated. Of comse, the thermochemical data required to calculate A/Ir and aU of the Cp,-, as functions of T, must be available. [Pg.264]

The symbol Cp,(Fo — Fad) indicates that the average heat capacities, i.e., the Cp,-, are averages over the temperature range from Fq to Fad. If A r and the Cp,- are strong functions of temperature, a trial-and-error solution of Eqn. (8- 19a) is required to obtain a value of Fad. [Pg.264]

Fortunately, for many systems, Fao(—AffR(F))/ S FjoCp,- is not a strong function of temperature, and can be assumed to be constant. If so, Eqn. (8-18a) can be written as [Pg.264]


Adiabatic lapse rate The adiabatic temperature change that takes place with height of a rising (or falling) parcel of air, approximately -1 C/100 m. [Pg.1406]

Use enough diluents so that the adiabatic temperature change is acceptable. [Pg.174]

Interestingly, this compound was known for some years [38, 39] before MCE research came back into vogue. Here, the maximum — ASM for a decoupled system is 42 J kg-1 K-1 and is almost met for AH = 0 - 7 T and 1.8 K. So, we have a reasonably high metal content, with a small, though ferromagnetic, interaction, with the appropriate high spin metals. Heat capacity data allow the adiabatic temperature change to be calculated here, this was found to be 12.7 K below 2 K, one of the best by this measure until recently. [Pg.311]

The experiments are usually carried out at atmospheric pressure and the initial goal is the determination of the enthalpy change associated with the calorimetric process under isothermal conditions, AT/icp, usually at the reference temperature of 298.15 K. This involves (1) the determination of the corresponding adiabatic temperature change, ATad, from the temperature-time curve just mentioned, by using one of the methods discussed in section 7.1 (2) the determination of the energy equivalent of the calorimeter in a separate experiment. The obtained AT/icp value in conjunction with tabulated data or auxiliary calorimetric results is then used to calculate the enthalpy of an hypothetical reaction with all reactants and products in their standard states, Ar77°, at the chosen reference temperature. This is the equivalent of the Washburn corrections in combustion calorimetry... [Pg.125]

The adiabatic temperature change ATa helps to evaluate the importance of heat effects in a design of a chemical reactor, even if the reactor itself is not an adiabatic one. Table 2.10 presents some useful heuristics. The use of an inert to remove or add heat is the most employed in low-cost adiabatic reactors. Considering heat-transfer devices is more expensive, but better for energy integration. [Pg.47]

Determination of the adiabatic temperature change Ar from experimental T(t) measurements made in nonideal calorimeters ... [Pg.150]

For each run, plot temperature versus time using an expanded, interrupted temperature scale as shown in Fig. VI-16 and determine the initial and final drift rates dTldi)j and dJldi)f. Then make an overall Tversus t plot like Fig. VI-36, choose tf, and determine 6 and tj Finally, the adiabatic temperature change L.T= — Tq can be calculated from Eq. (VI-22). This determination of AT could be made directly from the overall T versus t plot as shown in Fig. VI-36, but the procedure described above provides greater precision. [Pg.157]

Use the plotting and calculation procedures described in Exp. 6 in order to determine the adiabatic temperature change associated with each combustion run. The same extrapolation procedure should be used for both esters and used in as consistent a maimer as possible so that any systematic errors inherent in the procedure will cancel out in the calculation of the strain energy. [Pg.165]

When the heat of reaction is not known, experiments are conducted on a well-stirred calorimeter (either batch or continuous). The adiabatic temperature change is measured and the heat of reaction is determined from the energy balance equation. [Pg.16]

Figure 5.36 Magnetic entropy change and adiabatic temperature change, derived from specific heat data, for [Fei4(bta)606Cl6(0Me)i8] on an applied field change of 7 to 0 T. Solid line is the entropy for an 5 = 25 paramagnet. Reprinted with permission from Evangelisti et al., 2006 [19]. Copyright (2006) Royal Society of Chemistry... Figure 5.36 Magnetic entropy change and adiabatic temperature change, derived from specific heat data, for [Fei4(bta)606Cl6(0Me)i8] on an applied field change of 7 to 0 T. Solid line is the entropy for an 5 = 25 paramagnet. Reprinted with permission from Evangelisti et al., 2006 [19]. Copyright (2006) Royal Society of Chemistry...
The choice between NINA and adiabatic reactors is not easy for moderately to highly exothermic reactions. The values of the adiabatic temperature change ATC and temperature sensitivity given by... [Pg.883]

Thermal effects are often the key concern in reactor scaleup. The generation of heat is proportional to the volume of the reactor. Note the factor of V in Equation 5.31. For a scaleup that maintains geomedic similarity, the surface area increases only as Sooner or later, temperature can no longer be controlled by external heat transfer, and the reactor will approach adiabatic operation. There are relatively few reactions where the full adiabatic temperature change can be tolerated. Endothermic reactions will have poor yields. Exothermic reactions will have thermal runaways giving undesired byproducts. It is the reactor designer s job to avoid limitations of scale or at least to understand them so that a desired product will result. There are many options. The best process and the best equipment at the laboratory scale are rarely the best for scaleup. Put another way, a process that is less than perfect at a small scale may be better for scaleup precisely because it is scaleable. [Pg.185]

Equilibrium gas compositions, heats of reaction, and adiabatic temperature changes were calculated for each initial reaction temperature. The variables studied were temperature, pressure, feed steam-carbon ratio, and feedstock. [Pg.205]

A good measure of the heat effects associated with a chemical reaction is the adiabatic temperature change, ATad- This can be computed from the relation ... [Pg.251]

Hence, a good approximation in an adiabatic operation is that the temperature variation is proportional with the adiabatic temperature change multiplied by conversion. [Pg.323]


See other pages where Adiabatic temperature change is mentioned: [Pg.161]    [Pg.174]    [Pg.196]    [Pg.350]    [Pg.617]    [Pg.435]    [Pg.436]    [Pg.295]    [Pg.296]    [Pg.134]    [Pg.56]    [Pg.203]    [Pg.22]    [Pg.435]    [Pg.161]    [Pg.174]    [Pg.196]    [Pg.350]    [Pg.433]    [Pg.449]    [Pg.148]    [Pg.16]    [Pg.34]    [Pg.116]    [Pg.120]    [Pg.173]    [Pg.356]    [Pg.641]    [Pg.323]    [Pg.324]   
See also in sourсe #XX -- [ Pg.161 ]

See also in sourсe #XX -- [ Pg.161 ]

See also in sourсe #XX -- [ Pg.173 , Pg.466 ]

See also in sourсe #XX -- [ Pg.324 ]

See also in sourсe #XX -- [ Pg.264 ]




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