• 한국유체기계학회 논문집
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• 제15권1호
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• pp.52-57
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• 2012

Stall inception characteristics are researched to understand stall well. To realize different stall inception patterns, IGV stagger angle was changed. At design IGV stagger angle, spike, which is short length scale, is observed. Decreasing IGV stagger angle, spike changes to mode, which is long length scale, and further decreasing get multi cell. Compressor maps for each IGV stagger are shown to compare different stall inceptions. The characteristics of both spike and mode are confirmed in this experiment. Furthermore, transient from spike to mode is find. multi cell has 4cells and is little bit faster than mode. and multi cell shows 2nd, 3rd characteristics on compressor map.

• 한국추진공학회지
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• 제19권5호
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• pp.52-61
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• 2015

본 연구에서는 가변 입구 안내익과 블리드 공기 스케줄에 따른 터보팬 엔진에서의 천이 성능특성을 수치적으로 분석하였다. 대상 엔진으로 저 바이패스비 혼합 흐름 터보팬 엔진을 선정하였다. 압축기 가변 입구 안내익에 따른 성능 변화를 고려하기 위해 평균 반경 해석법을 이용하여 압축기 성능성도를 도출하고 엔진 해석 프로그램에 입력하였다. 정상상태 조건에서 축류 압축기 서지마진 10%를 만족하도록 회전속도에 따른 가변 입구 안내익과 블리드 공기 스케줄을 각각 도출하였다. 도출된 스케줄을 이용하여 엔진 천이 성능해석을 수행하였다. 엔진 천이 성능해석 수행 결과 가변 입구 안내익을 사용하는 경우가 블리드 공기를 사용하는 경우보다 천이과정에서 높은 서지마진과 낮은 터빈 입구 온도를 보였다.

• 한국유체기계학회 논문집
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• 제5권3호
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• pp.46-53
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• 2002

This paper reports an experimental investigation on a centrifugal compressor with the adjustable inlet guide vane. The compression system is composed of a radial impeller, a vaneless diffuser, and an IGV. The results have shown that surge line on the performance map is affected by the amount of prewhirl and the prewhirl has an effect on transient region between rotating stall and surge. The surge lines have been shifted toward the lower flow region with the increased positive prewhirl and the higher flow region with the increased negative prewhirl. During the unsteady performance test, it was also found that the transient region was reduced with the increased negative prewhirl, and weak signals of rotating stall were detected just before surge as the positive prewhirl was increased.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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• pp.290-297
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• 2002

This paper presents analysis results for the effect of power control strategies on the part load performance of gas turbine based power generation systems utilizing exhaust heat of the gas turbine such as cumbined cycle power plants and regenerative gas turbines. For the combined cycle, part load efficiency variations were compared among different single shaft gas turbines representing various technology levels. Power control strategies considered were fuel only control and IGV control. It has been observed that gas turbines with higher design performances exhibit superior part load performances. Improvement of part load efficiency by adopting air flow modulation was analyzed and it is concluded that since the average combined cycle performance is affected by the range of IGV control as well as its temperature control principle, a control strategy appropriate for the load characteristics of the individual plant should be adopted. For the regenerative gas turbine, it is likewise concluded that maintaining exhaust temperature as high as possible by air flow rate modulation is required to increase part load efficiency.

• 한국유체기계학회 논문집
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• 제6권3호
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• pp.28-35
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• 2003

This paper presents analysis results for the effect of power control strategies on the part load performance of gas turbine based power generation systems utilizing exhaust heat of the gas turbine such as combined cycle power plants and regenerative gas turbines. For the combined cycle, part load efficiency variations were compared among different single shaft gas turbines representing various technology levels. Power control strategies considered were fuel only control and IGV control. It has been observed that gas turbines with higher design performances exhibit superior part load performances. Improvement of part load efficiency of the combined cycle by adopting air flow modulation was analyzed and it was concluded that since the average combined cycle performance is affected by the range of IGV control as well as its temperature control principle, a control strategy appropriate for the load characteristics of the individual plant should be adopted. For the regenerative gas turbine, it is likewise concluded that maintaining exhaust temperature as high as possible by air flow rate modulation is required to increase part load efficiency.

• 한국항공우주학회지
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• 제41권7호
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• pp.539-546
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• 2013

항공기용 터보팬 엔진에서 압축기 성능이 단 시간에 변화가 클 경우, 이를테면 항공기가 이륙하는 상황에서와 같이 엔진 회전속도(RPM)를 공회전(idle) 상태에서 최대로 증가 시킬 때, 항공기의 엔진 성능이 급격하게 변화하므로 압축기 내에서 서지현상이 발생할 수 있다. 본 연구에서는 서지현상 발생 방지를 그 목적으로 하였다. Simulink를 이용하여 특정 상황에서 압축기 내에 일어나는 동적 움직임을 모사하였다. 연료유량을 입력값으로 하고 그에 따른 RPM, 공기유량은 전달함수로 나타냈으며, NPSS를 통해서 획득한 압축기 성능 맵을 통해 서지마진을 출력하였다. 서지마진을 기준 값 10%와의 차이를 PD제어하여 IGV(Inlet Guide Vane)각을 변화시킴으로써 즉, VIGV를 이용하여 압축기 내의 서지라인과 운용점 사이의 마진을 증가시켜 서지현상이 발생하는 것을 방지하였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집D
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• pp.751-758
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• 2001

Exergy concept is applied to the analysis of part-load performance of gas turbine engine. Exergy is a useful tool to find the source of irreversibility in thermal system. In this study, details of the performance characteristics of a heavy-duty gas turbine, l50MW-class GE 7FA model, are described by theoretical investigations with exergy analysis. Result shows that exergy destruction rate of gas turbine increases with decreased load, which means increase of irreversibility. Also, it is found that variations of IGV angle and amount of cooling air for turbine blades are closely related to the inefficiencies of compressor and turbine, respectively.

• 한국유체기계학회 논문집
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• 제7권3호
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• pp.23-31
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• 2004

An experimental study on the performance and instability development characteristics of a centrifugal compressor equipped with an adjustable inlet guide vane has been performed with varying guide vane angles. The test was conducted at the design speed of 20,800 rpm for 6 guide vane angles : $-30^{\circ},\;-20^{\circ},\;10^{\circ},\;0^{\circ},\;10^{\circ},\;20^{\circ},\;30^{\circ}$. Unsteady pressures were measured using high-frequency pressure transducers at the inducer to investigate the instability phenomena such as rotating stall and surge inside the compressor. From the unsteady measurements, it is found that the transient process from rotating stall to surge was mainly affected by inlet guide vane angles. The results of the present study can be applied to the instability control of the centrifugal compressors using a adjustable inlet guide vane.

• 한국유체기계학회 논문집
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• 제14권2호
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• pp.41-46
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• 2011

This study investigated the changes in performance and operating characteristics of an F-class gas turbine according to the change of working fluid from air to carbon dioxide. The revised gas turbine is the topping cycle of the semi-closed oxy-fuel combustion combined cycle. With the same turbine inlet temperature, the $CO_2$ gas turbine is expected to produce about 85% more power. The main contributor is the greater compressor mass flow and the added oxygen flow for the combustion. Compressor pressure ratio increases about 50%. However, the gas turbine efficiency reduces about 10 %. Modulation of inlet guide vane to reduce the compressor inlet mass flow, the major purpose of which is to reduce the compressor inlet Mach number, was also performed.