• 대한전기학회:학술대회논문집
• /
• 대한전기학회 1998년도 하계학술대회 논문집 B
• /
• pp.781-786
• /
• 1998

Since a gas turbine is still a significant contributor to peak time, it is very important to tune the gains of P. I. D to get a maximum power and stability within permissible limits. In the gas turbine, the main control loop must adjust the fuel flow to ensure the correct output power and frequency. but it is not easy, because the control loop is composed of many subsystems. In this paper we acquire a transfer function based on the operations data of Gun-san gas turbine and study to apply a loop compensation type 2-DOF PID controller tuning by neural-network to control loop of gas turbine to reduce phenomena caused by integral and derivative actions through simulation. We obtained satisfactory results to disturbances of subcontrol loop such as, fuel flow, air flow, turbine extraction temperature.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2008년도 추계학술대회B
• /
• pp.2850-2855
• /
• 2008

Very High Temperature Reactor (VHTR) has been selected as a high energy heat source for a nuclear hydrogen generation. The VHTR heat is transferred to a thermo-chemical hydrogen production process through an intermediate loop. Both Process Heat Exchanger and sulfuric acid evaporator provide the coupled components between the VHTR intermediate loop and hydrogen production module. A small scaled Compact Nuclear Hydrogen Coupled Components test loop is developed to simulate the VHTR intermediate loop and hydrogen production module. Main objective of the loop is to screening the candidates of NHDD (Nuclear Hydrogen Development and Demonstration) coupled components. The operating condition of the gas loop is a temperature up to $950^{\circ}C$ and a pressure up to 6.0MPa. The thermal and fluid dynamic design of the loop is dependent on the structures that enclose the gas flow, especially primary side that has fast gas velocity. We designed and constructed a small scale sulfuric acid experimental system which can simulate a part of the hydrogen production module also.

• 대한기계학회논문집B
• /
• 제34권5호
• /
• pp.563-568
• /
• 2010

30톤급 액체산소/케로신 액체로켓엔진개발의 중간단계로 터보펌프-가스발생기 개회로 연계시험이 수행되었다. 터보펌프-가스발생기 개회로 연계시험은 엔진시스템 작동 모사 환경 시험으로서 가스발생기로의 추진제는 터보펌프 출구를 통해 공급되지만, 가스발생기 출구 가스는 터빈 구동에 이용되지 않고 외부로 배출된다. 터보펌프-가스발생기 개회로 연계시험 목적, 시험설비 구성, 제어시스템의 작동 조건, 시험 수행 절차, 연계시험기의 구성 형태, 개회로 연계시험 결과가 제시되었다. 터보펌프-가스발생기 개회로 연계시험 결과, 연계시험기의 예냉 절차와 시동 특성, 정격 작동성 및 안정적인 종료 특성이 액체로켓 엔진시스템 작동 환경 모사 조건에서 확인되었다.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2008년도 제31회 추계학술대회논문집
• /
• pp.125-128
• /
• 2008

30톤급 액체산소-케로신 액체로켓엔진 개발의 중간 단계로서 연소기를 제외한 터보펌프 등의 엔진 주요 구성품을 이용한 터보펌프+가스발생기 개회로 연계시험이 수행되었다. 터보펌프+가스발생기 개회로 연계시험의 시험기 구성 및 시험결과를 제시하였다. 연소기를 오리피스로 모사하는 상태에서의 터보펌프+가스발생기 개회로 연계시험기의 예냉, 시동기를 이용한 시동 및 가스발생기 점화, 터보펌프 정격 구동이 성공적으로 수행되었다. 개회로 연계시험 결과는 터보펌프+가스발생기 폐회로 연계시험 수행을 위해 활용되었다.

• Nuclear Engineering and Technology
• /
• 제55권3호
• /
• pp.1125-1139
• /
• 2023

The system-integrated modular advanced reactor 100 (SMART100), an integral-type pressurized water small modular reactor, is based on a novel design concept for containment cooling and radioactive material reduction; it is known as the containment pressure and radioactivity suppression system (CPRSS). There is a passive cooling system using a condensation with non-condensable gas in the SMART CPRSS. When a design basis accident such as a small break loss of coolant accident (SBLOCA) occurs, the pressurized low containment area (LCA) of the SMART CPRSS leads to steam condensation in an incontainment refuelling water storage tank (IRWST). Additionally, the steam and non-condensable gas mixture passes through the CPRSS heat exchanger (CHX) submerged in the emergency cooldown tank (ECT) that can partially remove the residual heat. When the steam and non-condensable gas mixture passes through the CHX, the non-condensable gas can interrupt the condensation heat transfer in the CHX and it degrades CHX performance. In this study, condensation heat transfer experiments of steam and non-condensable gas mixture in the natural circulation loop were conducted. The pressure, temperature, and effects of the non-condensable gas were investigated according to the constant inlet steam flow rate with non-condensable gas injections in the loop.

• 한국수소및신에너지학회논문집
• /
• 제30권4호
• /
• pp.312-319
• /
• 2019

Effect of loop seal geometry on solid circulation characteristics was investigated with two different types of upper loop seals and lower loop seals in a gas-solid fluidized bed system. Upper loop seal which has a wide gap between solid intake and outlet parts requires more fluidization gas to maintain smooth solid circulation. Moreover, the lower loop seal which has a wide gap requires more fluidization gas to achieve the same solid circulation rate. These results can be explained by results of minimum fluidization velocity in the lower loop seals. Consequently, if a loop seal has a wide gap between solid intake and outlet parts, more fluidization gases should be fed to ensure enough solid circulation rate and smooth solid circulation.

• Korean Chemical Engineering Research
• /
• 제52권4호
• /
• pp.522-529
• /
• 2014

연소전 $CO_2$ 포집용 SEWGS 시스템의 SEWGS 반응기와 재생반응기 사이의 고체순환을 위해 SEWGS 반응기 - 하부루프실 - 재생반응기 - 상승관 - 사이클론 - 상부 루프실로 구성된 순환유동층 시스템을 사용하고 있다. 현재 시스템의 경우 수직형 하부 루프실을 사용하고 있으나 하부 루프실의 유동화 및 안정적인 고체순환을 위해 유량이 많이 필요하고 가끔씩 슬러그가 발생하였다. 본 연구에서는 새로운 하부 루프실 형태로 경사형 하부 루프실을 제안하였으며, 상온, 상압 조건에서 $CO_2$ 흡수제(P-78)를 층물질로 사용하여 기포유동층-기포유동층-고속유동층 형태의 순환유동층 실험장치를 이용하여 하부 루프실의 형태 변화에 따른 고체순환특성을 측정 및 비교하였다. 경사형 하부루프실의 경우가 수직형인 경우보다 적은 유량으로 안정적인 고체순환을 유지할 수 있었으며 두 반응기 사이의 고체층 높이 차이도 발생하지 않는 것으로 나타나 경사형 하부 루프실을 사용하는 것이 유리한 것으로 결론지을 수 있었다.

• 한국연소학회지
• /
• 제18권2호
• /
• pp.17-22
• /
• 2013

In this study, we tested the absorption of $CO_2$ in combustion gas into an alkaline wastewater to simultaneously control $CO_2$ and wastewater. During the experiment, we investigated the effects of operating parameters on neutralization characteristics of the wastewater by using $CO_2$ in a bench-scale semi-batch jet loop reactor (0.1 m diameter and 1.0 m in height). The operating parameters investigated in the study are gas flow rate of 1.0-2.0 L/min, liquid recirculation flow rate of 4-32 L/min, and liquid temperature of $20-25^{\circ}C$. It was shown that the initial pH of wastewater rapidly decreased with increased gas flow rate for a given liquid recirculation flow rate. This was due to the increase in the gas holdup and the interfacial area at higher gas flow rate in the reactor. At constant gas flow rate, the time required to neutralize the wastewater initial pH of 10.1 decreased with liquid recirculation flow rate ($Q_L$), reached a minimum value in the range of $Q_L$ = 16-24 L/min, and then increased with further increase in $Q_L$. Further, the time required to neutralize the wastewater was shortened at higher temperatures.

• 한국연소학회지
• /
• 제18권3호
• /
• pp.38-43
• /
• 2013

In this study, we tested the absorption of $CO_2$ in combustion gas into an alkaline wastewater to simultaneously control $CO_2$ and wastewater. During the experiment, we investigated the effects of operating parameters on neutralization characteristics of the wastewater by using $CO_2$ in a bench-scale semi-batch jet loop reactor (0.1 m diameter and 1.0 m in height). The operating parameters investigated in the study are gas flow rate of 1.0-2.0 L/min, liquid recirculation flow rate of 4-32 L/min, and liquid temperature of $20-25^{\circ}C$. It was shown that the initial pH of wastewater rapidly decreased with increased gas flow rate for a given liquid recirculation flow rate. This was due to the increase in the gas holdup and the interfacial area at higher gas flow rate in the reactor. At constant gas flow rate, the time required to neutralize the wastewater initial pH of 10.1 decreased with liquid recirculation flow rate ($Q_L$), reached a minimum value in the range of $Q_L$ = 16-24 L/min, and then increased with further increase in $Q_L$. Further, the time required to neutralize the wastewater was shortened at higher temperatures.

• 대한기계학회논문집A
• /
• 제35권2호
• /
• pp.191-200
• /
• 2011

초고온가스로로부터 생성된 $950^{\circ}C$ 정도의 초고온 열을 이용하여 수소를 경제적이며 또한 대량으로 생산하는 원자력수소생산시스템에서 공정열교환기는 초고온 열과 화학반응 공정을 통해 수소를 생산하기 위한 핵심 기기이다. 한국원자력연구원에서는 초고온가스로에 사용될 기기에 대한 성능시험을 위해 소형가스루프를 구축하고 공정열교환기 시제품을 수정 제작하였다. 본 연구는 공정열교환기 수정 시제품을 소형가스루프에서 시험하기 전에 루프 시험조건하에서 공정열교환기 수정 시제품의 고온 구조건전성을 미리 평가하기 위한 작업의 일환으로 공정열교환기 수정 시제품에 대한 고온 구조해석 모델링, 거시적 열 해석 및 구조 해석을 수행하고 그 결과들을 정리한 것이다. 해석 결과는 공정열교환기 수정 시제품 성능시험 장치 설계에 반영할 것이다.