• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.38 no.9
• /
• pp.890-899
• /
• 2010

An experimental study has been conducted to analyze the operating forces on a partially admitted turbine blade using a linear cascade apparatus. Axial-type blades were used and the blade chord was 200mm. The rectangular nozzle was applied and its size was $200mm{\times}200mm$. The experiment was done at $3{\times}10^5$ of Reynolds number based on the chord. The rotational force and axial force on the blade were measured at steady state by moving the blade to the rotational direction. The operating forces were measured at three different nozzle install angles of $58^{\circ}$, $65^{\circ}$ and $72^{\circ}$ for off-design performance test. In addition, three different solidities of 1.25, 1.38 and 1.67 were applied. From the results, the maximum rotational force was increased when the solidity was decreased and the nozzle install angle was decreased. The axial force was increased by decreasing the nozzle install angle. The reverse axial force was obtained in the partially admitted region when the nozzle install angle was increased to $72^{\circ}$.

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

• Proceedings of the Korea Society for Simulation Conference
• /
• 1999.10a
• /
• pp.267-271
• /
• 1999

연료를 작동 유체의 내부 또는 외부에서 연소시켜서 발생된 고온 고압의 가스를 터빈에 공급하여 회전력을 발생시키는 원동기를 가스터빈이라 하며, 가스터빈을 이용한 발전기와 달리 기동 및 정지 시간이 대단히 짧고, 부하 변화에 대한 속응성이 뛰어나기 때문에 전력계통 운영상 양수 발전기나 수력 발전기와 더불어 첨두 부하용으로 주로 사용된다. 본 고에서는 전력 계통에 병렬 운전 중인 가스터빈 발전기의 부하가 탈락되어 입력 에너지가 과잉으로 되었을 때, 제어 시스템의 중요한 파라미터인 연료량과 가스터빈 속도 및 배기가스의 온도가 비상 정지 수준에 도달하지 않고 안전하게 운전될 수 있는지의 여부, 즉 안정성을 판별하기 위하여 수행한 모의 시험에 대하여 기술하였다. 또, 부하가 탈락되지 않고 입력되는 연료량이 크게 변동하는 경우, 즉 큰 부하 변동을 모의 시험한 내용에 대하여 기술하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2009.11a
• /
• pp.382-386
• /
• 2009

The life of a component decreases when it was exposed at the extreme condition. A turbine blade of a turbopump used for a liquid rocket engine is operated under the environment of high temperature and pressure, and experienced high centrifugal force. Thus the durability of the turbopump operated under the these conditions become lower than expected because of the severe fatigue and creep influence. The damage of the turbine being considered the fatigue and the creep influence is estimated to ensure the durability of turbopump turbine. ABAQUS/CAE and MSC.Fatigue are used for the fatigue analysis, and Larson-Miller parameter and robinson's rule are used for the creep analysis. In this paper, comparison and analysis of the fatigue and the creep influence were performed to ensure the life expectancy of turbopump turbine.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2009.05a
• /
• pp.18-21
• /
• 2009

The life of components under high thermal load is typically shorter than other components. The turbopump turbine of liquid rocket is operated under these environments like high temperature and high centrifugal dorce due to high rotating velocity during operating time. These conditions may often cause low-cycle fatigue problem in the turbopump turbine. First of all, to analyze heat stress, ABAQUS/CAE is used and Coffin-manson's equation is used to consider elasticity and plasticity strain. S.W.T's method is used to consider the mean stress effect, using strain history, low-cycle fatigue analysis is done for turbopump turbine which may have FCL(fracture critical location). In this paper, strain life method is applied to analyze low-cycle fatigue.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.17 no.6
• /
• pp.105-112
• /
• 2013

Turbopump is typically an assembly of rotors and casings, and there are a number of joints between them. Every joint should be leak-proof, so there is always a seal to accomplish the goal. Among various seals, metal seals are advantageous in that they are robust at high pressure, and at wide range of temperature. In this study, flange joints using conical seal made of stainless steel, solid flat metal seal made of copper and metal C seal made of Inconel 718 were structurally designed and analyzed, considering both initial tightening and operating conditions.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.19 no.4
• /
• pp.102-109
• /
• 2015

The methodology to calculate loads on the bearings of the gas-turbine engine is presented for design of high-speed bearing. Firstly, the loads on the bearings are formulated according to the force and moment equilibrium with gyroscopic moment in three-dimensional space. Afterward, operating loading conditions of the engine are presented by applying the Joint Service Specification Guide, and magnitudes of transient and steady bearing loads are estimated based on the operating conditions. The calculated loading conditions of the bearings will be used for the essential design boundaries for the detail structural design and rig test.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2010.11a
• /
• pp.339-342
• /
• 2010

Doosan Heavy Industries & Construction Co., Ltd. constructed a gas turbine engine test cell to verify operating characteristics and design parameters of 5MW class gas turbine engine for power generation under developing. Engine test cell was designed to satisfy critical requirements to scrutinize all performance parameters of the engine with safe and reliability in accordance with design specification. As the test cell developed can effectively reproduce engine operation conditions covering from start-up to maximum power condition, it can be utilized to make a continuing design improvement of the engine based on practical test data at full stretch. Moreover, it is expected to be serviceable to develop derivative engines and be utilized to put them into serial production and contribute to a competitiveness reenforcement as a gas turbine engine manufacturer.

• Proceedings of the Korean Nuclear Society Conference
• /
• 1996.05a
• /
• pp.594-601
• /
• 1996

가압기고압력 원자로정지여유도(high pressurizer pressure trip margin)에 영향을 주는 요인들에 대한 민감도 분석을 울진 3,4호기 성능해석코드인 LTCUCN computer code틀 이용하여 수행하였다. 그 결과, 초기 가압기압력, 증기우회제어계통의 quick open지연시간, 터빈우회밸브의 quick opening시간, 원자로출력 감발계통의 용량, 원자로출력감발 제어붕 낙하시간, 가압기 살수작동 설정치 둥이 완전부하상실시 가압기압력을 상승시키는 주요인자임을 알 수 있었으며, 증기우회제어계통 및 가압기살수계통의 용량은 최대 가압기 압력에 미치는 영향이 미미한 것으로 판명되었다. 울진 3,4호기의 참조발전소인 영광 3,4호기의 as-built 자료를 토대로 울진 3,4호기의 원자로정지여유도를 계산한 결과 울진 3,4호기는 완전부하상실사건시 37 psi의 정지여유도를 가질 수 있는 것으로 판단된다. 그러나, 원자로출력감발계통이 있는 ABB-CE type의 울진 3,4호기에서는 완전부하상실사건보다 원자로출력감발계통이 동작하지 않는 부하감발사건이 최대 가압기 압력치를 유발하는 사건이고, 다양한 부하상실사건중에도 운전여유도는 확보하고 있음을 알 수 있었다.

• 기계와재료
• /
• v.21 no.4
• /
• pp.38-46
• /
• 2010

고온 고압의 부식 환경 하에서 사용할 수 있는 고내구성 재료 개발은 항공기와 선박의 추진체 및 발전기 등과 같이 고온부에서 작동하는 장치 설비의 수명 확보 및 안전성 보장을 위해 관련 산업계의 지속적인 연구 개발이 요구되고 있는 분야이다. 최근 세계 각국에서 발전소를 중심으로 한 새로운 고효율 에너지 생산 시스템화 계획이 구체화됨에 따라, 과거 한 종류의 연료 연소 방식으로부터 다양한 연료를 사용할 수 있는 시스템으로 전환함과 더불어 극심한 고온 산화 환경 변화에 유연하게 대응할 수 있는 소재 개발이 주요한 기술적 이슈로 부각되고 있다. 이와 같은 측면에서, 소재 '표면'의 기계적 열화를 극복하면서 생산 경쟁력을 갖춘 '새로운' 보호 코팅 기술은 가스 터빈 엔진 제조업체와 같은 장치 설비 제조 업체의 요소 기술 영역으로 자리매김 하고 있다.