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Thermal cycling, models

The thermal cycle model has been proposed by Zhang et al. (2010) and matches well with the experimental data. Figure 7.4a. The performance will also be decreased by the mismatch of the two phases, which result in an increased polarization resistance due to the break of the interface between the electronic and ionic phases. When TEC of the electrol)4e (a,) and the electro-catalyst (ccj) are different, a misfit strain will be resulted from a temperature change, AT ... [Pg.190]

The evolution of T, is just an exercise in mesoscale thermodynamics [13]. These expressions, in combination with (7.54), incorporate concepts of heterogeneous deformation into a eonsistent mierostruetural model. Aspects of local material response under extremely rapid heating and cooling rates are still open to question. An important contribution to the micromechanical basis for heterogeneous deformation would certainly be to establish appropriate laws of flow-stress evolution due to rapid thermal cycling that would provide a physical basis for (7.54). [Pg.243]

The Carnot cycle is not a practical model for vapor power cycles because of cavitation and corrosion problems. The modified Carnot model for vapor power cycles is the basic Rankine cycle, which consists of two isobaric and two isentropic processes. The basic elements of the basic Rankine cycle are pump, boiler, turbine, and condenser. The Rankine cycle is the most popular heat engine to produce commercial power. The thermal cycle efficiency of the basic Rankine cycle can be improved by adding a superheater, regenerating, and reheater, among other means. [Pg.110]

Hydrostatic stress in the SiC particles in a magnesia-10%SiC nanocomposite during a thermal cycle to 1550°C. Note the small amount of relaxation during the cycle and the good agreement with the prediction of a simple elastic model for the stresses [17]. [Pg.104]

A transient control volume model of the S-I and HyS cycle is presented. An important conclusion based on the results of this model is that the rate-limiting step of the entire S-I cycle is the HI decomposition section. In the HyS cycle, the rate-limiting step is the H2S04 decomposition. A generalised methodology for coupling these thermochemical cycle models to a nuclear reactor model is overviewed. The models were coupled to a THERMIX-DIREKT thermal model of a PBMR-268 and a point kinetics model. Key assumptions in the PBMR-268 model include flattening of the core and parallelisation of the flow channels. [Pg.370]

Fig. 23. Computer simulations of the profile of a Pt(llO) surface in a reacting CO/O, mixture as a function of time (number of cycles), modeling the formation of facets. After 4000 cycles the parameters simulating the partial pressures were switched off and the surface became flat again due to thermal annealing. (From Ref. 110.)... Fig. 23. Computer simulations of the profile of a Pt(llO) surface in a reacting CO/O, mixture as a function of time (number of cycles), modeling the formation of facets. After 4000 cycles the parameters simulating the partial pressures were switched off and the surface became flat again due to thermal annealing. (From Ref. 110.)...
The holding times of this cycle profile are not optimized, but can be shortened. Optimal holding times are dependent on the type of temperature (external or internal thermal probes) and time control (the clock usually starts below or above the holding temperature and the exact temperature difference varies among different models of the thermal cycling machines). [Pg.310]

The alumina-superalloy joints are intended to withstand high service temperatures (700 -1000 C) and thermal cycles typical in power generation processes. The fabrication of a joint should provide a relatively good strength but more important that it will remain relatively stable in the service conditions. Therefore, experimental studies for the joint design optimisation should be carried out and the data for novel procedures and for modelling the FG-structure and FE-analysis should be created. [Pg.314]

Finite element model analysis simulating the thermal cycle tests demonstrated that the top coat spallation of both types of coating is caused by the buckling driven by delamination due to the transient large in-plane compressive stress development immediately after initiate heating. [Pg.418]

Thermal cycling between temeratures 7 , and T2 = T1 + AT, Coffin-Manson model ... [Pg.218]

Hie effects of long-term exposure to elevated temperatures and repeated thermal cycling on heat pipes and thermosyphons can be approximated using a model developed by Baker [32], which utilizes an Arrhenius model to predict the response parameter F,... [Pg.874]

Chapter 4, Microstructure Development in Aluminum Alloy Friction Stir Welds, discusses the main microstructural observations in the FSW of wrought aluminum alloys. The evolution of microstructure in welded heat treatable aluminum alloys has been modeled in great detail. The methods were mostly developed for arc welding and have been more recently applied to the thermal cycles inFSW (Ref4,72-79). For the heat-affected zone, the problem is purely thermal for the TM AZ and nugget, there is the potential added complexity of coupling between the deformation microstructure and precipitation. [Pg.208]

The second step is to apply the isothermal model to the thermal cycles T(t) predicted from heat flow analysis. Writing the microstructure evolution law (Eq 10.9) in differential form, this may be integrated directly over the cycle, such that Eq 10.9 is replaced by ... [Pg.209]

Beyond a certain number of cycles there was stabilization in the mechanical properties. After the thermal cycling process was concluded the bars were measured for their Modulus of Rupture using a 3-point bend test method, with a span of 40mm between the suf rts and a crosshead speed of O.Smm/min (Tinius Olsen (Surrey, England) machine, model H25KS). This value of MOR was compared to the value for as-sintered samples. [Pg.131]


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