• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.11a
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• pp.561-565
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• 2009

The performance of supersonic impulse turbine was investigated experimentally. Experiment was performed with the compressed air instead of the high temperature burned gas because of the limitation of test facility and danger. As a result of the experiment with the compressed air, the performance in the real gas(burned gas) was predicted by the similarity method. The nozzle area of prototype turbine was calculated based on the real gas. So, it is difficult to satisfy the similarity conditions completely. Two similarity conditions were set and the design point for real gas was existed between two similarity conditions. And, the new turbine test model with calculated nozzle area based on the compressed air was tested. Therefore, similarity point of the new turbine test model was also existed between above two similarity points. It means that the design point for real gas was similar to the test point with the new turbine model.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1999.05a
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• pp.45-48
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• 1999

석탄가스화복합발전(Integrated Gasification Combined Cycle)기술은 우수한 환경성능과 열성능을 지니고 있어 장래 미분탄화력을 대신할 수 있는 대체기술로서 각광을 받고 있다. IGCC는 석탄가스화, 정제, 복합발전계통 및 공기분리계통 등 그 구성요소가 복잡하여 이들간의 시스템 최적화 정도에 따라 경제성 및 플랜트 성능이 크게 좌우된다. 최근에 가스터빈과 공기분리설비(Air Separation Unit)를 연계시켜 IGCC플랜트 성능을 향상시키는 연구가 다수 진행되었다[1],[2],[3]. 본 연구에서는 가스터빈과 ASU 간의 연계시 공기추출량을 결정하는 인자들을 검토하고 Texaco quench 가스화공정을 채용한 IGCC 플랜트에 대해 GatecCyle code등 상용코드를 이용하여 모델링하고 가스터빈 압축기 공기추출량에 따른 IGCC 플랜트 성능을 분석하였다. 본 연구 결과를 통하여 대상 IGCC 플랜트의 적정 공기추출량을 결정하고 플랜트 성능을 계산하였다. 본 연구 결과는 전력연구원에서 수행중인 300MW급 IGCC 예비기본설계에 활용될 것이다.(중략)

• Transactions of the Korean Society of Mechanical Engineers B
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• v.34 no.1
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• pp.35-43
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• 2010

In this study, an ideal water-recirculated oxy-fuel power generation system is proposed. The results of parametric studies of the performance characteristics of the system are discussed. For a given choice of the turbine inlet temperature, the turbine, which produces power, can be either a gas or a steam turbine. For maximum efficiency, the turbine inlet temperature is selected as the level of state-of-the-art gas turbines and the reheat cycle may be adopted not only to enhance the turbine power but also to maintain dryness of the water with a turbine exhaust temperature that is as high as possible. To obtain a low condensation temperature for a high purity of $CO_2$, a relatively low pressure expansion process may be added. Finally, the performance of the water-recirculated oxy-fuel power generation system is discussed with reference to various operating parameters and system configurations. The optimal operating conditions for high performance and a high purity of $CO_2$ are proposed.

• 한국신재생에너지학회:학술대회논문집
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• 2007.06a
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• pp.400-403
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• 2007

소형 풍력터빈 설계 시 고려해야 할 익형의 선택, 익형의 붙임각 및 Solidity 등이 터빈의 성능에 미치는 영향을 고찰하였다. 한 개의 익형에 대한 공력계수를 이용하여 수학적 모델링을 통하여 최적 붙임각을 예측하여 경향을 파악하였다. 받음각에 따른 익형의 공력특성을 CFD 기법으로 파악한 후 5개의 Blade를 갖는 Turbine의 성능을 익형의 붙임각에 따라 파악하여 최대 성능을 갖는 붙임각을 최종 산출하였다. 익형 선정시 받음각에 대한 양력/항력 곡선을 이동시키는 캠버 익형의 기능보다는 항력 대양력의 비(L/D) 가 최대인 익형을 선정하는 것이 더욱 중요하며, Blade수가 적을수록 Torque의 양은 증가하고 Blade가 6이상이변 효율이 급격히 감소함을 알 수 있다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.35 no.12
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• pp.1391-1398
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• 2011

Design and performance analysis of a steam turbine for variations of degree of reaction were performed by computer simulation. Design parameters such as blade angles, exit areas, and heights of the nozzle and moving blade were represented as functions of the degree of reaction. The main performance factors such as turbine power, diagram efficiency, and axial thrust were also expressed in terms of the degree of reaction. For further information about the design and performance, the blade angles and main performance factors were investigated as functions of the flow coefficient. The turbine power and diagram efficiency reached a maximum value for a given degree of reaction and flow coefficient, and the symmetric shape of the moving blade showed distortion as the degree of reaction was increased.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.47 no.3
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• pp.177-186
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• 2019

Wind power tower has been used to augment the performance of VAWT (Vertical Axis Wind Turbine). However, inappropriately designed wind power tower could reduce the performance of VAWT. Hence, an optimization study was conducted on a wind power tower. Six design variables were selected, such as the outer radius and the inner radius of the guide wall, the adoption of the splitter, the inner radius of the splitter, the number of the guide wall and the circumferential angle. For the objective function, the periodic averaged torque obtained at the VAWT was selected. In the optimization, Design of Experiment (DOE), Genetic Algorithm (GA), and Artificial Neural Network (ANN) have been applied in order to avoid a localized optimized result. The ANN has been continuously improved after finishing the optimization process at each generation. The performance of the VAWT was improved more than twice when it operated within the optimized wind power tower compared to that obtained at a standalone.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.37 no.1
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• pp.1-7
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• 2013

An aerodynamic rig test of a radial turbine for an auxiliary power unit (APU) was performed at a high-temperature turbine test facility at the Korea Aerospace Research Institute. The pressure ratio, Mach number, and flow coefficient in the rig test are the same as those under normal engine operation conditions. The design pressure ratio is 3.096, design test speed is 34909 rpm, and turbine inlet temperature is $160^{\circ}C$. The turbine has airfoil-type nozzles, and the diameter of the turbine wheel is 175.74 mm. The turbine map is experimentally measured, and the detailed flow at the turbine inlet is measured. The pressure distribution in the nozzle at both the hub and the shroud sides and the pressure distribution along the shroud casing of the turbine wheel were measured, and this confirmed that the expansion process in the turbine wheel is acceptable.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.18 no.6
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• pp.29-36
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• 2017

In this study, acombined cogeneration power plant produced two types of thermal energy and electric or mechanical power in a single process. The performance of each component of the gas turbine-combined cogeneration system was expressed as a function of the fuel consumption of the entire system, and the heat and electricity performance of each component. The entire system consisted of two gas turbines in the upper system, and two heat recovery steam generators (HRSG), a steam turbine, and two district heat exchangers in the lower system. In the gas turbine combined cogeneration system, the performance test after 10,000 hours of operation time, which is subject to an ASME PTC 46 performance test, was carried out by the installation of various experimental facilities. The performance of the overall output and power plant efficiency was also analyzed. Based on the performance test data, the test results were compared to confirm the change in performance. This study performed thermodynamic system analysis of gas turbines, heat recovery steam generators, and steam turbines to obtain the theoretical results. A comparison was made between the theoretical and actual values of the total heat generation value of the entire system and the heat released to the atmosphere, as well as the theoretical and actual efficiencies of the electrical output and thermal output. The test results for the performance characteristics of the gas turbine combined cogeneration power plant were compared with the thermodynamic efficiency characteristics and an error of 0.3% was found.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1993.05a
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• pp.120-125
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• 1993

석탄가스화 복합사이클 발전시스템에서 스팀터빈 발전시스템은 1차 사이클인 가스터빈사이클에서 나오는 폐열을 이용하여 발생하는 증기로 구동되며, 증기의 일부는 가스화기로 들어가서 가스화 반응에 이용된다. 이와 같은 시스템의 설계나 평가를 위해서는, 주어진 시스템에 대한 열 및 물질수지 정산을 구할 수 있는 능력을 갖추는 것이 필요하다. 본 연구에서는 주어진 시스템의 성능을 평가할 수 있는 프로그램을 개발하여 IGCC(Integrated Gasification Combined Cycle)System의 증기터빈 사이클과 유사한 증기터빈기계의 열 및 물질정사고 성능 해석에 적용하였다. (중략)

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.05a
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• pp.362-366
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• 2010

Numerical Analysis of two-stage supersonic turbines were conducted, and the results were analyzed. $FLUENT^{TM}$ commercial flow analysis package was employed for the calculation of the turbine. Characteristics of the turbine performance were investigated according to the overlap height and existence of the shroud at the second rotor blade through the calculations.