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Combustion wave quenching

Design of explosion suppression systems is clearly complex, since the effectiveness of an explosion suppression system is dependent on a large number of parameters. One Hypothesis of suppression system design identifies a limiting combustion wave adiabatic flame temperature, below which combustion reactions are not sustained. Suppression is thus attained, provided that sufficient thermal quenching results in depression of the combustion wave temperature below this critical value. This hypothesis identifies the need to deliver greater than a critical mass of suppressant into the enveloping fireball to effect suppression (see Fig. 26-43). [Pg.2329]

The microstructure of the initial titanium-graphite mixture is shown in Figure 62a. When the temperature in the combustion wave reaches 1660°C, titanium melts. It was determined from quenching results that a thin film ( 0.1 / m) of the Ti melt spreads over the solid carbon surface with simultaneous formation of titanium carbide grains (Fig. 62b). Small rounded TiC particles were observed to appear within the liquid rather than in the form of a continuous product layer (Rogachev et al, 1987). To illustrate this fact further, the typical microstructure formed during combustion reaction of titanium melts with graphite whiskers (10 /.im in diameter) is shown in Fig. 62c. [Pg.187]

For the boron-nitrogen system, because the high gas pressure is required for the synthesis, it is difficult to apply any dynamic method for investigation of the microstructural transformations, which occur in the combustion front. Thus, the static quenching technique was used [26, 23, 27]. The idea of this method is to extinguish the combustion wave and quickly cool the sample it is necessary to freeze all zones with the characteristic microstructure, chemical and phase structure of the reactants, intermediates, and final products. For quenching to take place, the heat loss from the reaction front at some point must exceed the critical... [Pg.62]

The second type of quenching method is based on the gradual increase of the heat loss with movement of the combustion front through the sample. The prototype of these methods was considered for experiments by Belyaev and coworkers [29] to determine the critical diameter of combustion of condensed matter. During movement of the combustion front from the base of the cone to its top, the specific heat loss increased, reaching the critical value in some cross-section of the cone where the extinction occurred. The most widely used method is the quenching of combustion waves in a wedge-shaped cutout of a massive copper block [27]. [Pg.63]

Rogachev, A.S., Mukasyan, A.S., and Varma, A. (2003) Quenching of gasless combustion wave time-resolved thermal... [Pg.74]

To understand the process of ferrosilicon nitriding in the combustion mode, the method of stopping the combustion wave by rapid nitrogen pressure release and filling the apparatus by argon was used. The microstructure analysis of quenched samples with the use of X-ray microanalysis and SEM analysis allowed us to... [Pg.193]

A distinctive peculiarity of high-grade ferrotitanium is the lowest melting temperature among examined ferroalloys (1085 °C). To understand the mechanism for nitriding of ferrotitanium, we stopped the combustion wave by quenching. [Pg.209]

Nitrogen and Ta in the combustion wave form the intermediate product TaN with a single phase if the process is quenched after the combustion wave has passed (44). If the sample is heated by the combustion wave in nitrogen, repeated combustion takes place with the formation of the TaN phase. It should be noted that experiments at ambient nitrogen pressure (—40 atm) produce a hexagonal modification of TaN, but those at high pressures (—3000 atm) yield a cubic one. The cubic modification is synthesized by the combustion of Ta in liquid nitrogen (44). [Pg.27]


See other pages where Combustion wave quenching is mentioned: [Pg.174]    [Pg.179]    [Pg.122]    [Pg.463]    [Pg.79]    [Pg.179]    [Pg.183]    [Pg.183]    [Pg.183]    [Pg.184]    [Pg.185]    [Pg.185]    [Pg.191]    [Pg.193]    [Pg.204]    [Pg.79]    [Pg.179]    [Pg.183]    [Pg.183]    [Pg.183]    [Pg.184]    [Pg.185]    [Pg.185]    [Pg.191]    [Pg.193]    [Pg.204]    [Pg.3]    [Pg.63]    [Pg.64]    [Pg.64]    [Pg.174]    [Pg.216]    [Pg.515]    [Pg.2301]   
See also in sourсe #XX -- [ Pg.183 , Pg.184 , Pg.185 , Pg.186 , Pg.187 , Pg.188 ]

See also in sourсe #XX -- [ Pg.183 , Pg.184 , Pg.185 , Pg.186 , Pg.187 , Pg.188 ]




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Quenching of the Combustion Wave

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