• Journal of Mechanical Science and Technology
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• 제16권6호
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• pp.839-850
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• 2002

A performance simulation program for the turboprop engine (PT6A-62), which is the power plant of the first Korean indigenous basic trainer KT-1, was developed for performance prediction, development of an EHMS (Engine Health Monitoring System) and the flight simulator. Characteristics of components including compressors, turbines, power turbines and the constant speed propeller were required for the steady state and transient performance analysis with on and off design point analysis. In most cases, these were substituted for what scaled from similar engine components'characteristics with the scaling law. The developed program was evaluated with the performance data provided by the engine manufacturer and with analysis results of GASTURB program, which is well known for the performance simulation of gas turbines. Performance parameters such as mass flow rate, compressor pressure ratio, fuel flow rate, specific fuel consumption and turbine inlet temperature were discussed to evaluate validity of the developed program at various cases. The first case was the sea level static standard condition and other cases were considered with various altitudes, flight velocities and part loads with the range between idle and 105% rotational speed of the gas generator. In the transient analysis, the Continuity of Mass Flow Method was utilized under the condition that mass stored between components is ignored and the flow compatibility is satisfied, and the Modified Euler Method was used for integration of the surplus torque. The transient performance analysis for various fuel schedules was performed. When the fuel step increase was considered, the overshoot of the turbine inlet temperature occurred. However, in case of ramp increase of the fuel longer than step increase of the fuel, the overshoot of the turbine inlet temperature was effectively reduced.

• 항공우주기술
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• 제13권1호
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• pp.70-75
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• 2014

액체 로켓 엔진에 대한 에너지 밸런스 해석, 모드 해석, 비정상 해석 프로그램을 소개하였다. 유사 프로그램에 대한 결과, 공개된 실험 결과와 비교하여 해석 방법을 검증하였다. 에너지 밸런스 해석은 초기 개발 단계에서 활용된다. 모드 해석은 엔진 작동 조건, 시험조건 설정 및 엔진 성능 분산 분야에 활용된다. 비정상 해석을 통하여 추진제 유량, 추력, 비정상 조건에 대한 임펄스를 예측할 수 있다. 비정상 해석은 시동/종료 시퀀스 설정에 필수적이다. 본 해석 프로그램들은 한국형 발사체 엔진 개발에 활용될 것이다.

• 한국통신학회논문지
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• 제34권2C호
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• pp.181-185
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• 2009

프레임 단위로 식별 데이터베이스에 저장된 참조 신호의 특징 벡터와 유사성을 비교하여 입력 신호를 식별하는 경우에, 참조 신호의 특징 벡터로 데이터베이스를 어떻게 구성하는가에 따라 식별 성능은 영향을 받을 수 있다. 즉, 식별 데이터베이스의 구성 방법에 따라 데이터베이스의 크기와 식별을 위한 계산량, 식별 성능 등이 결정되며, 이것은 실제로 수중 천이신호 식별 시스템을 구성할 때 중요한 문제이다. 본 논문에서는 LBG 벡터 양자화 기법을 이용하여 식별 데이터베이스의 크기를 줄여 줌으로써 프레임 기반 수중 천이신호 식별 기법의 효율성을 증가시킬 수 있는 방법을 제안하고, 실험을 통하여 제안한 방법의 타당성을 검증하였다.

• 항공우주시스템공학회지
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• 제18권4호
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• pp.109-116
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• 2024

본 연구에서는 단열 시험 결과를 기반으로 해석 결과의 유효성 검증을 수행하였으며, 공통격벽에서 발생하는 기화 질량을 산출하여 공통격벽 추진제 탱크의 단열 성능을 평가하였다. 과도 열전달 해석 결과와 단열 시험 결과를 비교하여 해석 결과의 유효성을 검증하였다. 이후 추진제 탱크에서 발생하는 내부 열전도와 외기로 인한 자연 대류 열전달을 고려하여, 공통격벽 추진제 탱크에 대한 과도 열전달 해석을 수행하였다. 이를 통해, 공통격벽에서 발생하는 열 유속을 추출하고, 단열 성능의 정량적 지표인 기화 질량을 산출하였다. 그 결과 공통격벽 추진제 탱크의 단열 설계 기준인 0.12 kg 보다 낮은 0.09 kg의 기화질량이 산출되어 단열 성능 기준에 부합함을 확인하였다.

• 한국산학기술학회논문지
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• 제15권7호
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• pp.4494-4499
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• 2014

약한 계통은 단락비가 작고 임피던스가 크므로 과도 안정도 여유도가 매우 낮다. 약한 계통에 사고가 발생하면 보호 시스템은 사고 선로를 개방함으로써 사고를 제거하는데 이것은 시스템의 안정도를 더욱 약하게 만든다. 그러므로 약한 계통의 안정도 여유를 증가시키기 위한 하나의 방법은 시스템에 추가적인 발전기를 연결하는 것이다. 본 논문에서는 약한 계통의 안정도 여유도를 증가시키기 위하여 기존의 동기발전기를 추가하는 경우와 풍력발전기의 를 추가하는 경우의 안정도 여유도를 비교한다. PSSE를 이용한 과도안정도 시뮬레이션 결과 풍력발전기가 충분한 제동력을 제공하고 안정도 여유를 증가시킴을 확인할 수 있었다. 풍력발전기를 추가할 때 안정도 여유도는 CCT 기준으로 5배까지 향상되었다.

• 수산해양교육연구
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• 제7권1호
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• pp.111-126
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• 1995

In general, the electromagnetic transient phenomenon always exists in induction motor(IM) with the torque change. The control performance of IM is very worse than that of D.C motor owing to this transient phenomenon. So many studies about the elimination methods of the transient phenomenon have been making progress. Interesting methods of them are the Field acceleration method(FAM) and the method of impulse addition on the input voltage at the time point of torque change. In this paper, first, the circuit equation of IM is derived from the phase segregation method. The torque equation consisted of the stator and rotor currents is derived from the solving of the circuit equation. As we well known, the transient terms exist in this the torque equation. The method of impulse addition on the input voltage at the instance of torque change is confirmed theoretically for the elimination of the transient phenomenon. With the base on it, the author proposed a real time algorithm to eliminate the transient terms. The control system is consisted of the PI controller with the feedforward of torque change. The author could confirm that the quick stepwise responses of torque and speed can be obtained from response simulations.

• Journal of Computing Science and Engineering
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• 제5권2호
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• pp.121-130
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• 2011

Recent research indicates that transient errors will increasingly become a critical concern in microprocessor design. As embedded processors are widely used in reliability-critical or noisy environments, it is necessary to develop cost-effective fault-tolerant techniques to protect processors against transient errors. The register file is one of the critical components that can significantly affect microprocessor system reliability, since registers are typically accessed very frequently, and transient errors in registers can be easily propagated to functional units or the memory system, leading to silent data error (SDC) or system crash. This paper focuses on investigating the impact of register file soft errors on system reliability and developing cost-effective techniques to improve the register file immunity to soft errors. This paper proposes the register vulnerability factor (RVF) concept to characterize the probability that register transient errors can escape the register file and thus potentially affect system reliability. We propose an approach to compute the RVF based on register access patterns. In this paper, we also propose two compiler-directed techniques and a hybrid approach to improve register file reliability cost-effectively by lowering the RVF value. Our experiments indicate that on average, RVF can be reduced to 9.1% and 9.5% by the hyperblock-based instruction re-scheduling and the reliability-oriented register assignment respectively, which can potentially lower the reliability cost significantly, without sacrificing the register value integrity.

• 에너지공학
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• 제13권3호
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• pp.181-190
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• 2004

Computational models for analyzing the in-reactor behavior of metallic fuel pins under transient conditions in liquid-metal reactors are developed and implemented in the TRAMAC (TRAnsient thermo-Mechanical Analysis Code) for a metal fuel rod under transient operation conditions. Not only the basic models for a fuel rod performance but also some sub-models used for transient condition are installed in TRAMAC. Among the models, a fission gas release model, which takes the multi-bubble size distribution into account to characterize the lenticular bubble shape and the saturation condition on the grain boundary and the cladding deformation model have been developed based mainly on the existing models in the MAC-SIS code. Finally, cladding strains are calculated from the amount of thermal creep, irradiation creep, and irradiation swelling. The cladding strain model in TRAMAC predicts well the absolute magnitudes and gen-eral trends of their predictions compared with those of experimental data. TRAMAC results for the FH-1,2,6 pins are more conservative than experimental data and relatively reasonable than those of FPIN2 code. From the calculation results of TRAMAC, it is apparent that the code is capable of predicting fission gas release, and cladding deformation for LMR metal fuel finder transient operation conditions. The results show that in general, the predictions of TRAMAC agree well with the available irradiation data.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2010년도 추계학술대회 논문집
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• pp.65-70
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• 2010

This paper presents experimental performance evaluation of a magnetorheological (MR) damper for integrated isolation mount for ultra-precision manufacturing system. The vibration sources of the ultra-precision manufacturing system can be classified as follows: the one is the environmental vibration from the floor and the other is the transient vibration occurred from stage moving. The transient vibration occurred from the stage moving has serious adverse effect to the process because the vibration scale is quite larger than other vibrations. Therefore in this research, a semi-active MR damper, which can control the transient vibration, is adopted. Also the stage needs to be isolated from tiny vibrations from the floor. For this purpose, a dry-frictionless MR damper is required. In order to achieve this goal, a novel type of MR damper is originally designed and manufactured in this work. Subsequently, the damping force characteristics of MR damper are evaluated by simulation and experiment. In addition, the vibration control performance of the MR damper associated with the stage mass is evaluated.

• 전기학회논문지
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• 제62권5호
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• pp.723-729
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• 2013

This paper presents an parallel type Linear Induction Motor with ununiform airgap for a shallow-depth underground train with 100‰ grade and 15 m curvature. This parallel type LIM has enough gradability but has inherently ununiform airgap between center and end parts. Consequently, performance when the train passes curved section should be considered with transient analysis. Moreover, general parallel operation, 1C2M which is usually used for train operation, deteriorates LIM performance because of different line velocity between inner and outer LIMs. Transient analysis has many problems such as huge model, lots of meshes, very long calculation time, truncation error and so on. This paper has presented a novel technique using equivalent linear rotating model in order to solve these problems and has analyzed parallel type LIM by using the proposed technique. Finally, LIM performance according to independent operating control has been investigated.