• Journal of Aerospace System Engineering
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• v.18 no.3
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• pp.17-26
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• 2024

Aircraft engines are exposed to high temperatures, high pressures, and stress caused by the rotation of the turbine shaft during flight. These loads can result in microcracks both on the inside and outside surfaces of the structure. Consequently, this can lead to structural defects and negatively impact the lifespan of the parts. To proactively prevent these defects, a finite element analysis is carried out to identify cracks. However, this process is time-consuming and requires significant effort due to the repetitive nature of crack modeling. This study aims to develop a crack modeling method based on the finite element model. To achieve this, the Constrained Delaunay Triangulation (CDT) technique is employed to triangulate the space while considering limitations on point connections. The effectiveness of this method is validated by comparing stress intensity factors for semi-elliptical cracks in plates and cylindrical vessels. This approach proves to be a valuable tool for crack analysis studies.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.36 no.3
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• pp.251-257
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• 2012

This work presents an experimental investigation of NOx emissions according to inlet air temperature (550-660 K), stoichiometric air ratio (${\lambda}$, 1.4-2.1), and elevated pressure (2-5 bar) in a High Press Combustor (HPC) equipped with a double cone burner, which was designed by Pusan Clean Coal Center (PC3). The exhaust-gas temperature and NOx emissions were measured at the end of the combustion chamber. The NOx emissions generally decreased as a function of increasing ${\lambda}$. On the other hand, NOx emissions were influenced by ${\lambda}$, inlet air temperature and pressure of the combustion chamber. In particular, when the inlet air temperature increased, the flammability limit was extended to leaner conditions. As a result, a higher adiabatic temperature and lower NOx emissions could be achieved under these operation conditions. The NOx emissions that were governed by thermal NOx were greatly increased under elevated pressures, and slightly increased at sufficiently low fuel concentrations (${\lambda}$ >1.8).

• 한국신재생에너지학회:학술대회논문집
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• 2011.11a
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• pp.71.2-71.2
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• 2011

300MW 급 태안 IGCC 가스화 플랜트 및 기존 발전소에 CCS 를 설치할 경우에 대해 기술 타당성 검증을 목적으로 CCS 모델링을 수행하였다. CCS Case Studies 는 플랜트 운전부하에 따른 $CO_2$ 제거율, $H_2S$ 제거율, 소모동력 범위 등 플랜트 성능을 예측할 수 있다. Case Studies 결과를 활용하여 설계된 CCS 설비 용량이 운전범위에 적합한지를 판단할 수 있고 과잉 설계되었을 경우 플랜트 건설비를 절감할 수 있다. IGCC 가스화 플랜트에서 생산되는 합성가스의 $CO_2$ 분압, 목표 $CO_2$ 제거율, 경제성을 기준으로 적합한 CCS 공정을 판단한 결과 Selexol 공정이 선정되었다. Selexol 공정은 고압, 고농도의 산성가스 제거에 적합하며 다른 물리적 용매인 Rectisol 공정에 비해 건설비용이 경제적이고 화학 흡수제인 아민과 비교하여 운전 온도 범위가 넓다. CO, $H_2O$ 를 $CO_2$, $H_2$ 로 전환하는 Water Gas Shift Reaction (WGSR) 공정은 Co/Mo 촉매 반응기로 구성되었고 Selexol 공정은 $H_2S$ Absorber, $H_2S$ Stripper, $CO_2$ Absorber, $CO_2$ Flash Drum 로 구성되었다. WGSR+Selexol 모델링은 Wet Scrubber 후단의 합성가스 (40.5 bar, $136{\sim}139^{\circ}C$) 를 대상으로 하였다. WGSR+Selexol 공정 운전 조건 변화 [Process Design Case(PDC), Equipment Design Case(EDC), Turndown Design Case(TDC)] 에 따른 플랜트 모델링 결과를 비교분석 하였다. 주요 분석 내용은 WGSR 설비에서의 CO 의 $CO_2$ 전환 효율, Selexol 설비에서 $CO_2$ 제거 효율, $H_2S$ 제거 효율이다. 모델링 결과 WGSR 설비에서의 CO 의 $CO_2$ 로의 전환율 99.1% 이상, Selexol 설비에서 $CO_2$ 제거율은 91.6% 이상, $H_2S$ 제거율 100%이었다. CCS 설비 설치에 따른 플랜트 성능 영향을 분석하기 위해서 CCS 설비의 Chiller, Compressor, Pump 소비동력을 계산하였다. 모델링 결과 Chiller 는 2.6~8.5 MWth, Compressor 는 3.0~9.6 MWe, Pump 는 1.4~3.0 MWe 범위 이었다. 플랜트 로드가 50%인 TDC 소모동력은 플랜트 로드가 100%인 PDC 소모동력의 절반 수준이었다. 합성가스를 WGS+Selexol 공정을 통해 수소가스로 전환시키면 가스터빈 연료가스의 Lower Heating Value (LHV) 값이 평균 11.5% 감소하였다.

• Korean Journal of Materials Research
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• v.10 no.4
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• pp.312-316
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• 2000

A study has been made to investigate the effects of hot isostatic pressing(HIP ping) on bond strength and elevated temperature characteristics of thermal barrier coating(TBC). The specimens were prepared by HIPping of TBC which is composed of the ceramic top coat(8wt%$Y_2$$O_3$-$ZrO_2$) and the metallic bond coat on the matrix of IN738LC superalloy. The results showed that the porosity and microcracks in the ceramic top coat of TBC were significantly decreased by HIP. As a result, the bond strength of the HIPped coating was increased above 48% compared to that of as-coated specimen and microstructure was homogenized. It was found that the thermal cycle resistance of HIPped coating was inferior to that of as-coated specimen. It was considered that this result was mainly caused by the reduction of internal defects in the top coat layer which could play a role in relaxing the thermal stress due to a large difference in thermal expansion between TBC and matrix.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.22 no.2
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• pp.774-780
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• 2021

The auxiliary power unit (APU) of a rotorcraft starts the engine during operation/flying. The APU is composed of a gas turbine engine type. The starting principle of the component is that the electric start motor generates the power required for starting by rotating the shaft. In this study, quality improvement was performed by applying an over-running clutch (ORC) between the APU and the starter motor to secure the operability of the starter motor of the APU mounted on the rotorcraft. The starter motor has the main role of starting the APU, but during operation, it is rotated without load by the rotational force of the APU gear shaft, resulting in friction at the brush. This phenomenon causes abrasion of the brush of the starter motor. Consequently, when the APU operation time increases, the brush life decreases, and the operability of the APU is affected. In this study, an ORC that separates the interlocking between the start motor brush abrasion and the APU operation time was applied to improve the operability/durability of the APU starter motor. The effect was verified through a test, and the technical feasibility of the design change was analyzed.

• Journal of the Korean Institute of Gas
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• v.25 no.6
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• pp.22-28
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• 2021

Combustion characteristics were examined experimentally for a swirl-stabilized double cone premixed burner nozzle used for industrial gas turbines for power generation. An original model and a variant with a different fuel injection pattern are tested to compare their combustion characteristics such as NOx, CO and stability in pressurized conditions with single burner-flame and in an ambient multi-flame conditions with multi-burners. Test results show that NOx emissions are smaller for the variant, whose number of fuel holes is reduced with the same total area of fuel holes, in ambient and pressurized single-flame conditions with single burner, which results from enhanced fuel/air mixing due to a higher penetration of fuel into the air stream. The multi-burnerflame test results show that NOx emissions are smaller for the variant due to reduced flame interactions, which, on the contrary, slightly reduces the stability margin. On-site test results fromin an actual power plants also show that NOx emissions are reduced for the variant, compared with the original one, which is in agreement with the lab test results stated above.