• 에너지공학
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• 제13권3호
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• pp.205-213
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• 2004

본 연구에서는 고가인 고속도 CCD카메라가 아닌 비교적 간단한 광파이버 시스템을 이용한 자려진동연소 발생에 관한 검출과, 진동연소가 발생하기 전에 이를 미리 예견할 수 있는 통계학적 수법에 관해 조사를 하였다. 먼저 자려진동연소의 발생시에 사용될 수 있는 광파이버의 유용성이 검증되었다. 광파이버에 의해 검출되어진 OH 라디칼 자발광 강도는 고속도 CCD카메라에 의해 얻어진 값과 강한 자려진동연소가 발생할 때에 거의 일치를 하였다. 자려진동연소가 발생하면 시스템과 연소기기에 손상을 가하게 된다. 이러한 피해가 발생하기 전에 자려진동연소의 발생 징후를 미리 포착하려는 시도를 하였다. 이를 위해 압력과 OH라디칼 자발광과 같은 화염에서의 변동성분께 대한 통계학적 처리를 이용하여 자려진동연소의 발생을 예견할 수 있는 독특한 수법에 관해 조사를 하였다.

• 대한기계학회논문집B
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• 제32권9호
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• pp.659-668
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• 2008

Combustion instability has been considered as very important issue for developing gas turbine and rocket engine. There is a need for fundamental understanding of combustion instability. In this study, combustion instability was numerically and experimentally investigated in a dump combustor with bluff body. The fuel and air mixture had overall equivalence ratio of 0.9 and was injected toward dump combustor. The pressure oscillation with approximately 256Hz was experimentally obtained. For numerical simulation, the standard k-$\varepsilon$ model was used for turbulence and the hybrid combustion model (eddy dissipation model and kinetically controlled model) was applied. After calculating steady solution, unsteady calculation was performed with forcing small perturbation on initial that solution. Pressure amplitude and frequency measured by pressure sensor is nearly the same as those predicted by numerical simulation. Furthermore, it is clear that a combustion instability involving vortex shedding is affected by acoustic-vortex-combustion interaction. The phase difference between the pressure and velocity is $\pi$/2, and that between the pressure and heat release rate is in excitation range described by Rayleigh, which is obvious that combustion instability for the bluff body combustor meets thermoacoustic instability criterion.

• Journal of Advanced Marine Engineering and Technology
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• 제28권7호
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• pp.1111-1122
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• 2004

An idea to suppress the self-excited combustion oscillation was applied to the flames. The characteristics of unsteady combustion were examined and the unsteady combustion was driven by forced pulsating mixture supply that can modulate its amplitude and frequency. The self-excited combustion oscillation having weaker flow velocity fluctuation intensity than that of the forced pulsating supply can be suppressed by this method. The effects of the forced pulsation amplitude and frequency on controlling self-excited combustion oscillations were also investigated comparing with the steady mixture supply. The unsteady combustion used in this experiment plays an important role in controlling self-excited combustion oscillation. Symptoms of self-excited combustion oscillation were also studied in order to predict the onset of combustion oscillation before it proceeded to a catastrophic failure For the purpose, the unique measures to observe the onset of self-excited combustion oscillations based on the careful statistics of fluctuating properties in flames, such as pressure or emission of OH radicals, have been proposed.