Get this from a library! Fuels and combustion: S.P. Sharma, Chander Mohan.. [ S P Sharma; Chander Mohan]. Get this from a library! Fuels and combustion. [S P Sharma; Chander Mohan]. Fuels And Combustion Start Download Portable Document Format (PDF) and E- books.. S.. P.. Sharma, Chander Mohan Statement.
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Would you also like to submit a review for this item? You already recently rated this item. Your rating has been recorded. Write a review Rate this item: Preview this item Preview this item. Fuels and combustion: Sharma, Chander Mohan. Gasoil is used during start up subsequently turbine of Ghom power plant, Iran during to Each nozzle has a liquid fuel These premature failures lead either to repair or to replace the injector in its core, cooling air channel, natural gas entrance nozzles.
High heat flux appeared to be the main cause of tube and main cooling air channel around the injector in crack out of many.
In this article, absorbed heat flux rate of order. Figure 8 nozzles is calculated to examine as a possible cause for Material constituents of the nozzles have been collected from cracks.
Some of the major activities considered for the power plant documents Table 1 , and analysis of fuels is calculating the absorbed heat flux rates and temperature presented in Table 2. Gas turbines are of Flame shape, which is the most important factor in Mitsubishi-Westinghouse D with an ISO capacity of combustion chamber design, is estimated separately for both On periodic overhaul of gas turbines equal to operating hours a few number of radial cracks with maximum dept of 3.
In next Pressurising type of liquid fuel burner is in use in Ghom overhaul which was performed on completion of power plant, initially the average diameter of gasoil drops, operating hours, the number of cracks had been increased, produced by injector, was measured to determine the while their depths remained same.
Similar phenomenon was dimensions of the gasoil flame.
Later on, maximum and observed during the third overhaul also. These cracks caused minimum diameter of flame and their distances from nozzle heterogeneity in fuel injection, and made disturbance in flame was calculated from the average time required for complete shape. All of these nozzles were replaced and some of them burning of a liquid drop.
The flame shape thus arrived was an sent to this centre, Mech. PWIT, for examination incomplete cone, side view of which is shown in figure 2.
Elongation of flame after the maximum diameter of cone is On preliminary examination, various reasons were considered as a possible cause of damage; such as over stress followed International Conference on Energy and Environment ICEE ineffective on radiation absorbed by nozzle; therefore this part by cooling air is much more than the others it could be seen hasn't been showed.
The flame envelope has 12 nozzles for gas firing. At Referring to figure 8, it can be observed that there are three first the flame shape of each nozzle was obtained, then flame kinds of flows in nozzle: envelop of all the 12 nozzle flames was simulated.
The shape a.