• 한국전산유체공학회:학술대회논문집
• /
• 2002.05a
• /
• pp.94-101
• /
• 2002

The steam turbine rotor blade is designed using the Turbine Rotor Design Package developed by the authors. It can quickly accomplish blade shape design in the power plant industry. The quasi-3d code is employed for analysis of passage flow in the blade sections. Iterative change of each blade shape is made by moving position of control points in the Bezier curve under GUI(graphic user interface) environment. The full 3-D blade shape is obtained by stacking of the section blades.

• Proceedings of the KIEE Conference
• /
• 2007.07a
• /
• pp.1628-1629
• /
• 2007

1990년대에 이 전 건설된 발전소 및 기타 플랜트 자동제어시스템으로 거의 아날로그 연산방식 시스템이 적용되었다. 이제 장기간 사용으로 인한 수명감소와 고장률이 증가하는 추세에 있으므로, 기존 아날로그 제어시스템을 디지털 제어시스템으로 개조하는 사업이 추진되고 있다. 아날로그 제어시스템에 설정되어 있는 주요 파라미터들은 플랜트의 운전특성을 장기간 반영하여 이루어진 것이므로, 개조에 사용될 새로운 디지털제어시스템의 초기 파라미터 설정에 그대로 적용하면 개조후 시운전이 원활하고 튜닝 기간을 단축할 수 있다. 본 논문에서는 현재 진행하고 있는 급수펌프 구동터빈 제어시스템 개조 프로젝트에서 제어 파라미터를 구하는 과정 및 디지털 시스템에 구현할 내용들을 제시하였다.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.14 no.6
• /
• pp.60-68
• /
• 2010

In this study, the conventional plane tip, double squealer tip, and various groove tip blades were tested in a linear cascade in order to measure the effect of the tip shapes on tip surface heat transfer coefficient distributions. Detailed heat transfer coefficient distributions were measured using a hue-detection based transient liquid crystals technique. Two tip gap clearances of 1.5% and 2.3% of blade span were investigated and the Reynolds number based on cascade exit velocity and chord length was $2.48{\times}10^5$. Results showed that the overall heat transfer coefficients on the tip surface with various grooved tips were lower than those with plane tip blade. The overall heat transfer coefficient on grooved along suction side tip was lower than that on the squealer tip.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2010.05a
• /
• pp.311-318
• /
• 2010

In this study, the conventional plane tip, double squealer tip, and various groove tip blades were tested in a linear cascade in order to measure the effect of the tip shapes on tip surface heat transfer coefficient distributions. Detailed heat transfer coefficient distributions were measured using a hue-detection based transient liquid crystals technique. Two tip gap clearances of 1.5% and 2.3% of blade span were investigated and the Reynolds number based on cascade exit velocity and chord length was $2.48{\times}10^5$. Results showed that the overall heat transfer coefficients on the tip surface with various grooved tips were lower than those with plane tip blade. The overall heat transfer coefficient on grooved along suction side tip was lower than that on the squealer tip.

• Journal of IKEEE
• /
• v.23 no.2
• /
• pp.675-680
• /
• 2019

The coal-fired power plant is operated by a combined operation method, which is operated by sliding pressure operation under low load and by fixed pressure operation under high load for improved efficiency. The combined operation is divided into two and three valve open modes. Each plant is operated by selecting the turbine control valve mode in accordance with the manufacturer's recommendation, but is not really operating at the optimal sliding pressure operation according to load range, also Load range of each plant is configured differently. The internal efficiency of the high-pressure turbines is reduced due to loss of the turbine valves and the plant efficiency is reduced. To solve these problems, In this paper, the optimum load range is selected through the analysis method of thermal performance by each load in order to improve the optimum variable pressure operation load range by turbine control valve mode.

• Journal of the Computational Structural Engineering Institute of Korea
• /
• v.34 no.5
• /
• pp.279-286
• /
• 2021

In this study, we investigated the behavior characteristics of the L-type flange bolt connection, which is used to connect upper and lower flanges having L-type ring sections, by bolts. This connection is mainly used in domestic wind turbine structures, wherein it is a vital component as any imperfection could cause the collapse of the entire structural system. Therefore, understanding the behavior characteristics of the L-type flange bolt connection is imperative. In this study, the connection's response to external force was simulated using finite element (FE) analysis and the FE model was idealized to behave as a single L-type bolt flange. The variation in the bolt tension and the L-type flange stress were analyzed to understand the behavior characteristics of the connection. Moreover, the bolt-load function models proposed by Petersen, Schmidt/Neuper and VDI 2230, theoretically expressing a relation between bolt tension and external force, were compared to evaluate the suitability of the FE analysis and analyze the significant behavior characteristics of the connection. Furthermore, the changes in the bolt-load curve due to the variations in the partial dimensions of the L-type flange bolt connection were analyzed.

• Proceedings of the KIEE Conference
• /
• 2015.07a
• /
• pp.141-142
• /
• 2015

풍력발전은 신재생에너지 분야에서 태양광 발전과 함께 중요한 에너지원으로서 최대 전력 생산과 전력계통에 대한 적용 문제를 다루기 위해 상당한 노력들이 기울여지고 있는 분야인데, 발전기가 풍속에 따라 최대전력을 생산할 수 있는 속도를 추적해야 하는 어려움이 따른다. 본 논문에서는 풍력발전기의 출력방식을 조사하고 최대출력을 얻기 위한 MPPT출력제어방식에 대하여 조사하고, 풍력발전시스템의 전력계통에서의 적용성을 높이기 위한 기술요소를 제시한다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2002.04a
• /
• pp.62-63
• /
• 2002

램젯 엔진을 장착한 미사일은 기존의 터보젯 이나 터보팬 엔진에 비해 압축기와 터빈과 같은 엔진 구성품이 없어 무게가 가볍고 초음속에서 저항도 적으며 고속의 비행영역에서 연료효율과 생존성능이 뛰어나기 때문에 차세대 미사일 추진 시스템으로서 세계 여러 국가에서 개발 및 운용이 이루어지고 있다. 하지만 램젯 엔진은 충분한 램 효과를 얻어야 초기 점화가 가능하기 때문에 현재 개발되고 있는 대부분의 시스템은 최초 발사시 로켓 부스터에 의해 가속하고 로켓연료를 모두 소모하고난 후에 흡입구가 개방되어 램젯 엔진이 점화하는 방식을 취하고 있다.

• Proceedings of the Korean Society of Fisheries Technology Conference
• /
• 2001.10a
• /
• pp.75-76
• /
• 2001

산업적으로 강제 Swirl 유동은 난류를 촉진하기 위하여 많이 이용된다. 특히 Swirl유동은 난류 강도를 증가시켜 물질과 열의 전달 효과를 증진시켜 터빈 연소기, 열교환기 및 각종 산업용 버너 등의 공업분야에 폭넓게 이용되고 있다. Swirl강제 유동 발생 방법은 원추형 덕트방식, 베인형, 프로펠러형 등이 많이 이용되고 있으나 대부분의 방법은 강제로 와류(Swirl)를 발생, 촉진 및 증가 시키므로 유동손실 및 압력 손실 등을 수반하게 되어 많은 에너지 손실을 가져온다. (중략)

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2001.11a
• /
• pp.11-14
• /
• 2001

3-D compressible flow analysis was conducted by using mixing plane method for turbine system which is consisted of partial admission nozzle and rotor. Computational results are shown oblique shock wave in blade leading and trailing edge and also shown flow separation along suction surface of blade due to abrupt blade curvature. But computational results are well agree with 1-D calculation results and experimental data.