• Journal of the KSME
• /
• v.32 no.7
• /
• pp.581-587
• /
• 1992

가스터빈 엔진의 설계는 압축기와 터빈의 효율 이외에도 여러 가지 현실적인 요소가 커다란 영 향을 미치므로 이러한 것들이 설계시에 고려되어야 하며 기존의 기술수준과 부품을 가능한 한 활용하는 것이 현명하다. 특히 산업용 터빈의 개발을 위한 시제 엔진 설계시에는 이러한 접근 방법이 현실적으로 성공 가능성이 크다. 예를 들어서, 기술축적과 연구를 위해서 산업용 엔진을 개발하고자 할 때에 엔진 전부를 설계하는 것보다는 구하기가 용이한 기존의 소형 항공기 엔진의 가스발생기 부분 (압축기, 연소기, 압축기 터빈으로 구성된 부분)을 개조하여 활용하고 동력터 빈과 동력전달 부분만을 자체 설계하여 결합시켜서 개발한다든가 하는 것이 효과적일 것이다.

• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.37 no.11
• /
• pp.1023-1029
• /
• 2013

The integration between a gas turbine and an air separation unit (ASU) is important in IGCC plants. The portion of ASU air extracted from the gas turbine and the degree of nitrogen supply from the ASU to the gas turbine side are important operating parameters. Their effect on the gas turbine performance and operability should be considered in a wide ambient temperature range. In this study, appropriate nitrogen dilution rate and turbine inlet temperature that satisfy the two limitations of turbine blade temperature and maximum allowable power output were predicted. The air integration was set at zero. The simulation showed that the power output increases and turbine blade temperature decreases as the nitrogen dilution increases. The maximum allowable power output can be obtained under medium and low ambient temperature ranges. Under a high ambient temperature range, the achievable power is less than the maximum power.

• 열병합발전
• /
• s.71
• /
• pp.3-9
• /
• 2009

최근 국내 발전분야 최고 관심사는 직렬형 축을 가지는 1000MW 이상의 대용량 고효율 증기터빈 개발 및 운영이다. 발전 산업계 요구를 충족시키기 위하여 터빈 설계사들은 새로운 대용량의 저압터빈 실린더 모듈을 개발하고 있는데 개발된 모듈의 특징은 진보된 유체역학과 구조적 분석 기술을 결합하고 기존 합금강 재질 최종단 익에 작용하는 응력한계 길이인 1000mm 이상 길이의 최종단 날개를 개발하는 것이다. 본 논고에서는 Alsthom사에서 새롭게 개발된 최종단 익(翼)의 공역학 및 기계적 특성 설계 개발내용과 실증시험 결과를 소개하고자 한다.

• Proceedings of the KIEE Conference
• /
• 1997.07b
• /
• pp.654-656
• /
• 1997

본 논문에서는 직접신경회로망제어기(DNNC)를 사용하여 결합된 PI제어기의 이득을 구하여 보일러 터빈시스템을 제어하고자 한다. 직접신경회로망제어기는 플랜트의 동특성을 학습시키는 에뮬레이터 없이 제어입력에 대한 플랜트의 동작방향에 대한 정보만을 사용하여 신경회로망을 학습시키고, 이 신경회로망을 사용하여 제어대상 플랜트인 다중입출력플랜트를 제어하기 위하여 결합된 PI 제어기의 이득을 구한다. 컴퓨터 시뮬레이션을 통하여 제안한 알고리즘의 타당성을 입증하고자 한다.

• Journal of Advanced Marine Engineering and Technology
• /
• v.28 no.7
• /
• pp.1082-1091
• /
• 2004

Analyzed Parametrically was an internal combustion engine combined with gas turbine the cycle of which is splitted into compression side cylinder and expansion side one, and heat adding of which is during constant volume pressure, temperature process. The advantages of each measures were analyzed by means of thermal cycle diagram. The thermal efficiency of partial load cutting off firstly isothermal heat adding and secondly isobaric heat adding also was analyzed The authors suggested some potentials about the performance as for thermal efficiency, mean effective pressure and reducing emissions and noise supposed were the operating parameter of the engine set to some values and were some problems solved.

• Proceedings of the KIEE Conference
• /
• 2000.11a
• /
• pp.256-258
• /
• 2000

• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.35 no.4
• /
• pp.399-407
• /
• 2011

This study analyzes the performance of hybrid power systems combining a solid oxide fuel cell (SOFC) and a gas turbine (GT). Research focus is given to the influence of the size-dependent gas turbine performance on hybrid system performance. Three hybrid systems adopting different gas turbines (kW, sub-MW, multi-MW classes) are designed. As the gas turbine power increases (i.e. as the gas turbine performance enhances), the gas turbine power portion increases and the hybrid system efficiency increases. The hybrid system shows efficiency improvement over the SOFC only system even in the case where the gas turbine net power is nearly zero. The increase of gas turbine pressure ratio contributes to the net hybrid system power output in all of the three cases, while system efficiency is almost independent on the pressure ratio.

• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.37 no.12
• /
• pp.1153-1157
• /
• 2013

A steam turbine blade is one of the core parts in a power plant. It transforms steam energy into mechanical energy. It is installed on the rim of a rotor disk. Many failure cases have been reported at the final stage blades of a low-pressure (LP) turbine that is cyclically loaded by centrifugal force because of the repeated startups of the turbine. Therefore, to ensure the safety of an LP steam turbine blade, it is necessary to investigate the fatigue strength and life. In this study, the low cycle fatigue life of an LP steam turbine blade is evaluated based on actual damage analysis. To determine the crack initiation life of the final stage of a steam turbine, Neuber's rule is applied to elastic stresses by the finite element method to calculate the true strain amplitude. It is observed that the expected life and actual number of starts/stops of the blade were well matched.

• Proceedings of the KIEE Conference
• /
• 2008.07a
• /
• pp.550-551
• /
• 2008

복합화력발전은 여러 가지 장점으로 오늘날 많이 사용되는 발전방식이며, 가스터빈과 스팀터빈의 결합으로 여러 운전 Mode를 갖는다. 본 연구에서는 이러한 특성을 고려하여 복합화력 발전사와 시장운영자와의 관계를 분석하고, 복합화력발전사가 운전 Mode 선택을 전략변수로 사용하는 입찰전략 수립 모형을 제시한다.

• Journal of the Korea Academia-Industrial cooperation Society
• /
• v.22 no.2
• /
• pp.386-391
• /
• 2021

Turbocharging is becoming a key technology for both diesel and gasoline engines. Regarding gasoline engines, turbocharging can help reduce carbon dioxide (CO2) emissions when used in conjunction with other technologies. This paper presents measurements of the turbine efficiency of pulsating flow in a twin-scroll turbocharger for gasoline engines. A cold gas test bench with a pulse generator was manufactured. The turbine efficiencies were calculated using the measured data of the instantaneous pressure and temperature of the inlet and exit of the turbine. The measurements were carried out at turbine speeds from 60,000 to 100,000 rpm under a pulsating flow of 25.0 Hz and 33.0 Hz. The turbine efficiencies ranged from 0.517 to 0.544. At the pulse frequency, 33.3 Hz, the variations in efficiency were 7.7% and 2.6% at turbine speeds of 60,000 rpm and 100,000 rpm, respectively. The turbine efficiency of the pulsating flow compared to those of steady flow was 7.0% and 3.0% lower at a turbine speed of 60,000 rpm and 100,000 rpm, respectively. The pulsating flow deteriorated the turbine efficiency, but the effects of pulsating flow decreased with increasing turbine speed.