2019
DOI: 10.1016/j.energy.2019.04.223
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Influence of injection mode on the combustion characteristics of slight temperature rise combustion in gas turbine combustor with cavity

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Cited by 22 publications
(3 citation statements)
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“…erefore, the heat loss to the surrounding environment will increase, and the heat cannot be trapped in the combustor chamber. At the same time, as the increase of methane intake concentration will reduce the temperature in the combustor chamber, if the intake concentration is properly adjusted according to the real-time temperature feedback from the monitoring system, the heating time can be shortened [32][33][34].…”
Section: Temperature Rise Test Of Heat Storage Oxidationmentioning
confidence: 99%
“…erefore, the heat loss to the surrounding environment will increase, and the heat cannot be trapped in the combustor chamber. At the same time, as the increase of methane intake concentration will reduce the temperature in the combustor chamber, if the intake concentration is properly adjusted according to the real-time temperature feedback from the monitoring system, the heating time can be shortened [32][33][34].…”
Section: Temperature Rise Test Of Heat Storage Oxidationmentioning
confidence: 99%
“…As current aeroengine technology advances towards higher temperatures [1][2][3], heat capacity, and efficiency [4,5], the oxygen content in the incoming flow of the afterburner is reduced significantly. The decline in oxygen content significantly affects the combustion reaction rate and flame propagation speed, thus resulting in significant changes in the combustion dynamics, including vortex-flame interactions, vortex-shedding patterns, flame morphology, exothermicity, and pressure pulsations, which significantly affect the combustion efficiency, flame stability, and burn flammability limits [6][7][8][9].…”
Section: Introductionmentioning
confidence: 99%
“…Thrust-to-weight ratio is a comprehensive index to measure the performance level and working ability of aero engines. One of the main ways to improve the thrust-to-weight ratio of modern aero engines is to increase the outlet temperature of the combustion chamber (Zhang et al, 2019). As the temperature rises, turbine blades and vanes need to bear a greater thermal load.…”
Section: Introductionmentioning
confidence: 99%