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Time-of-Flight Models

Ion Diffusion in Paper. Using the "time of flight" model, it has been found that the mobility of the ionic species is approximately i orders of magnitude lower in these systems than for the case in normal aqueous systems. Based on this result, an... [Pg.526]

Figure 5.1.1b illustrates the other modeling approach time-of-flight modeling. Here, the particle s migration to the wall is considered, neglecting the... [Pg.89]

The strong influence of the vortex finder diameter, Dx, on the efficiency of cyclones is not directly evident in the reasoning behind the time-of-flight models. For the Rosin-Rammler-Intelmann model, Zenz (2001) argued that... [Pg.94]

In conclusion, we can say that the time-of-flight modeling concept is entirely different in nature from the equilibrium-orbit concept. It is peculiar that these two very different concepts should result in efficiency models that agree well, both absolutely and in trends, over a wide range of cyclone designs... [Pg.95]

In Appendix 5.B, we give the model equations for one more cyclone performance model that of Mothes and Ldffler. This model is built on the approach of Dietz, and is hybrid between the equilibrium-orbit and the time-of-flight models. [Pg.96]

Barth Efficiency model valid for all cyclones and swirl tubes (but see Table 4.5.1). Equilibrium-orbit model. Calculates the cut size, then fits an empirical grade-efficiency curve through it. Time-of-flight model. Derivation considers particle motion, but the final model relates cut size to pressure drop. [Pg.102]

The models of Dietz (1981) and of Mothes and Loffler (1988) consider both the exchange of dust between the inner and outer part of the swirl and the migration of particles to the wall. They can therefore be considered as hybrids between the equilibrium-orbit and the time-of-flight models. [Pg.106]

Figure A3.9.3. Time-of-flight spectra for Ar scattered from Pt(l 11) at a surface temperature of 100 K [10], Points in the upper plot are actual experimental data. Curve tinough points is a fit to a model in which the bimodal distribution is composed of a sharp, fast moving (lienee short flight time), direct-inelastic (DI) component and a broad, slower moving, trapping-desorption (TD) component. These components are shown... Figure A3.9.3. Time-of-flight spectra for Ar scattered from Pt(l 11) at a surface temperature of 100 K [10], Points in the upper plot are actual experimental data. Curve tinough points is a fit to a model in which the bimodal distribution is composed of a sharp, fast moving (lienee short flight time), direct-inelastic (DI) component and a broad, slower moving, trapping-desorption (TD) component. These components are shown...
Bushnell and co-workers [117] employed extensive molecular modelling to understand the nature of cis and trans isomerism in tetrahedral p-phenylene vinylene oligomers, and to aid the interpretation of time of flight mass spectrometry and ion mobility studies. Molecules such as T4R, shown in Figure 18, with four equivalent arms can be used to control the crystallinity in thin films. The authors reported the observation of a species in the mass spectrum resulting from the loss of an arm from the central carbon. This species will be referred to as P4R. [Pg.714]

There are several future directions that NIR brain sensing and imaging research can take. In instrumentation, advances in time-resolve spectroscopic equipment may yield less expensive equipment and thus a more prolific use. This will allow for approximation of time of flight parameter providing a possible avenue for inferring path length. Theoretically, there is a need for better theoretical modeling to eliminate crosstalk noise. Possible improvements have already been introduced by Boas, et. al [8]. However, more human subject studies need to be conducted to... [Pg.363]

Mass spectral data were obtained either on electrospray infusion (EDI) Model TSQ 700 mass spectrometer (Finnigan MAT) or a Matrix Assisted Laser Desorption Time-of-Flight (MALDI-TOF) (Finnigan, Model 2000). [Pg.627]

Foret et al.98 collected fractions of model proteins and variants of human hemoglobins after fractionation by CIEF, and then analyzed them by matrix-assisted laser desorption-time-of-flight-mass spectrometry (MALDI-TOF-MS). As the authors point out, MS is an orthogonal method to CIEF because it separates according to molecular mass. [Pg.199]

Mass spectrometry methods based on soft ionization techniques, 59,61,88,89 matrix-assisted laser desorption ionization/time-of-flight (MALDI-TOF), have been successfully applied for the direct analysis of grape and wine extracts and for monitoring flavonoid reactions in model solution studies. They give access to the molecular weights of the different species present in a fraction or extract and, through fragmentation patterns, provide important information on their constitutive units. Description of the various MS techniques can be found in Chapters 1 and 2. [Pg.271]

The time-of-flight secondary ion mass spectroscopy (ToF-SIMS) analysis was performed on a CAMECA ION-TOF Model IV spectrometer. This instrument was equipped with a reflection-type ToF mass analyzer and a pulsed 25 kV primary... [Pg.186]

It was actually shown by the time of flight method [32-34] that coulomb type traps control the drift mobility. The concentration of such traps is 1015 m 3. The real mobility (without traps) was estimated [35] to be of the order 5x10 8 m2 V 1 s 1 with a thermal activation energy of 0.28 eV. There are no correct data as yet confirming the impurity hopping model in PVC. The drift mobility is due rather to the jumps between neighbouring molecules and not shallow traps of the semiconductor. [Pg.17]

Wagner et al. [108] developed a PLS model to predict the amount of protein adsorbed in a metallic basis using time-of-flight SIMS (TOF-SIMS) spectra. Study of the multivariate models yielded insight into the surface chemistry and the mechanism for protein resistance of the coatings. The same group reported two other similar studies with satisfactory results [109,110]. [Pg.236]

Fig. 1. Energy distribution of neutrons scattered by hydrogen in liquid argon at 100"K and 26.5 atm, as a function of time of flight for various scattering angles, 6. Solid curve, interpolation model. Dashed curve, Sears itinerant oscillator model. Jagged curve, Experiment. Abscissa is time of flight in usec/m and ordinate is cross section in mb sr-1 usee-1. Fig. 1. Energy distribution of neutrons scattered by hydrogen in liquid argon at 100"K and 26.5 atm, as a function of time of flight for various scattering angles, 6. Solid curve, interpolation model. Dashed curve, Sears itinerant oscillator model. Jagged curve, Experiment. Abscissa is time of flight in usec/m and ordinate is cross section in mb sr-1 usee-1.

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Flight time

Time-of-flight

Timed models

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