• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.896-904
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• 2017

Lean premixed combustion was successful in meeting current NOx emission regulations. However, these often leads to combustion instability. This phenomena results from the feedback relationship between heat release perturbations and acoustic pressure oscillations in the combustor. Researches on the combustion instability in an annular combustor have recently received great attention due to the enhanced NOx requirement in aero-engines. In this study, the thermoacoustic network model has been developed in order to calculate the acoustics for longitudinal as well as circumferential modes in the annular combustor. The combustion model in the network model is calculated by flame transfer function(FTF). Numerical and analytical results are compared to an measurement data.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.3
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• pp.58-65
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• 2004

Thermal and structural finite element analyses were performed for the turbopump turbine bladed disk model with shroud of a liquid rocket engine. The only 1/80 part model was analyzed which consists of 3D eight node isoparametric solid elements. The applied loading history consists of a startup condition with a thermal spike and a steady state. Heat transfer coefficient on the blade was predicted using the commercial Navier-Stokes solver, Fluent. Transient thermal responses during startup and steady states were calculated using a 3D finite element code developed. Maximum stress and shroud tip displacement under the influence of centrifugal and thermal loading were also determined.

• Proceedings of the KIPE Conference
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• 2008.06a
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• pp.326-328
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• 2008

본 논문의 목표는 실제 시스템과 가장 유사한 이중여자 유도발전기(Doubly-Fed Induction Generator)의 시뮬레이터를 구현하고 실험을 통해서 그것을 검증하는 것이다. 바람의 속도를 2D 룩업 테이블을 이용하여 데이터화 한 후 터빈 모델의 입력으로 인가한다. 터빈 모델의 파라미터는 실험용 이중여자 유도발전기의 것과 동일하게 설정하여 실제 시스템과 유사하게 하였다. 지금까지는 이중여자 유도발전기를 모사하기 위하여 매트랩(Matlab) 등을 이용하였지만 실제와 다소 다르다는 문제와 구현하기 힘들다는 문제를 가지고 있었다. 하지만 본 논문에서는 심플로러(Simplorer)를 이용하여 쉽고 정확한 시뮬레이터를 구현하였다. 터빈과 이중여자 유도발전기는 기어를 이용하여 직결함으로써 실제 시스템과 매우 가깝게 모사하였으며 이중여자 유도발전기의 회전자를 여자시키기 위해 이산 캐리어 변조 방법을 이용하여 매트릭스 컨버터를 구동하였다. 그리고 실험을 통해서 시뮬레이터의 결과와 실험 결과의 비교 및 검증을 한다. 궁극적으로 어떤 지역의 바람의 품질과 발전량 등 중요한 정보를 얻기 위해 실제 크기의 발전기를 설치하지 않고 본 논문에서 개발한 시뮬레이터를 이용하여 쉽게 그 정보들을 얻을 수 있다.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.2 no.1
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• pp.33-44
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• 1982

In Order to study for the aeration characteristics which is one of the most important unit processes for the activated sludge process, a pitched blade type aeration model of octagonal shape with a draft tube in it was made as a pilot plant. Oxygen transfer rates, power consumptions and fluid velocities and behaviers were measured and evaluated with the various turbine shapes. And with these results, the dimensionless model analysis using the Buckingham ${\pi}$ theorem was discussed for a proper turbine shape determination.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.339-342
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• 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 Society of Propulsion Engineers Conference
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• 1996.11a
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• pp.97-104
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• 1996

DYGABCD 프로그램을 이용해 선형모델의 구성에 필요한 시스템 행렬을 구하고 최소자승법을 이용하여 실시간 선형모사를 행한 후 DYNGEN 프로그램을 이용한 비선형 모사와 비교하여 그 타당성을 입증하였다. 그리고 가제어성과 가안정성을 시험하여 시스템에 대해 제어기설계가 가능한지 확인하고 엔진의 성능과 직결되는 터빈입구 온도의 Overshoot 제어를 위해 고전적 제어기법인 PI제어기와 현대적 최적제어기법인 LQR 제어기를 설계하여 각각의 성능을 비교해 보았다.

• Proceedings of the KIEE Conference
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• 1997.07b
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• pp.639-641
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• 1997

전력계통의 주파수는 전력의 수요와 공급량의 평형상태에 따라 수시로 변동하며, 각 발전소에서는 이 주파수를 입력 신호로 사용하여 발전기의 출력을 제어하고 있다. 본 논문에서는 국내에서 운영하고 있는 한 개스터빈 발전소의 터빈제어 시스템을 모델로 하여 주파수 추종성에 영향을 미치는 파라미터들을 분석하고, 시뮬레이션을 통해 주파수 추종성을 향상시키기 위한 방안을 제시하였으며, 현장에 적용한 결과를 통해 제안된 주파수 추종성 향상방안의 타당성을 검증하였다.

• The Journal of the Acoustical Society of Korea
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• v.21 no.2
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• pp.134-141
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• 2002

In this paper, a free wake analysis based on the curved vortex element and CVC wake model is used to predict the aerodynamic performance and noise for HAWT. Also for prediction of RPM, a maximum value through a quadratic regression was suggested. And for a noise prediction, the broadband noise prediction method based on experimental equation was used. The curved vortex element uses a BCVE and an SIVE instead of a straight vertex element. In the CVC wake model, the vortex strengths are assumed to be constant along a span and a vortex filament. The free wake structure made by the curved vortex element and CVC was substituted for a vortex lattice, so it has an advantage for the less calculation time and a depiction of accurate wake structure. For the verification of this program, calculated results are compared with Mr. Kim's experiment model and Zond Z-40FS for performance and with WTS-4 and USWP models for noise. Good agreements are obtained between the predicted and the measured data for the performance and far-field noise spectra.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.37 no.2
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• pp.161-170
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• 2013

The flow and combustion characteristics in a premixed swirl combustor with a double cone burner are numerically analyzed to adopt a swirler model. The internal recirculation zone formed at the burner exit can be realized by a swirler with inner and outer diameters of 56 and 152 mm, respectively, and accordingly, the flow rate and radial velocity were determined. To select the tangential velocity, swirl and recirculation angles are introduced. A tangential velocity of 40 m/s produces an internal recirculation zone similar to that in a combustor. At the liner exit, the errors in temperature and velocity are 2.8% and 0%, respectively, and they are negligibly small. However, NOx emissions are underestimated by 67% in the numerical results obtained using the swirler model. Although considerable quantitative errors are induced by the swirler model, it can be useful numerical model for the EV burner because it can approximately simulate the essential flow and combustion characteristics in a premixed swirl combustor with a double cone burner and it is expected to make combustion analysis efficient in a gas turbine combustor with complex geometries.

• Journal of the Korean Society of Propulsion Engineers
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• v.25 no.1
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• pp.12-18
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• 2021

In this study, the performance modeling of MT30 gas turbine engine is performed. The design point is determined, and the component performance maps to which the scaling technique is applied are generated using standard maps provided by the commercial program. Off-design point performance analysis is performed with the generated performance model, and this is compared with the performance deck data of the engine. It is confirmed that the data of the performance maps generated by the one-point scaling method had some errors from the performance deck data, and it is determined that correction is necessary to increase the accuracy of the performance model. Therefore, the off-design point analysis is performed by creating the correction performance model in a manner that obtains the scaling factors for each operating point(off-design point) according to the high pressure spool speed.