• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.4
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• pp.332-337
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• 2018

This paper presents the design optimization of fuel sensor location used to measure remained fuel amount in aircraft conformal fuel tank. The conformal fuel tank is utilized to expand the mission range in airplane, and the sensor location is a critical design variable determining the measurement accuracy. In this work, the sensor location is optimized to minimize unmeasurable fuel amount due to non-contact between fuel and sensor. The simplified model is prepared from the conformal fuel tank CATIA model, and the unmeasurable fuel amount is calculated. Then, the optimization is performed using MATLAB optimization solver. The optimized sensor location is validated by comparing with the location obtained using parametric study.

• 한국신재생에너지학회:학술대회논문집
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• 2011.05a
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• pp.90.2-90.2
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• 2011

세계 각 국에서는 선진국을 중심으로 기후변화와 치솟는 유가에 대응하기 위하여 다양한 에너지원의 확보를 위해 부단히 노력하고 있다. 특히, 신재생에너지원 중 에너지 지속성이 가장 우수한 연료전지의 경우 1kW급 건물용 연료전지시스템이 도시가스 인프라가 가장 우수한 한국 및 일본을 중심으로 상용화에 가장 근접해 있는 실정이다. 일본의 경우 가정용 연료전지시스템 '에너팜'의 일부 제품이 올해부터 200만엔대로 가격을 내려 보급되어질 예정이고, 아직은 경제성이 떨어지지만 연료전지 조기 상용화를 위해 시스템 가격저감을 통한 기술개발이 한창이다. 또한 700W급 고체산화물형 연료전지시스템을 세계에서 처음 시판 계획을 가지고 있다. 국내의 경우 2009년도부터 시작된 '그린홈 보급확대를 위한 건물용 연료전지 보조기기 가격저감 기술개발'연구를 통해 블로워, 밸브, 유량계 및 펌프 등의 보조기기의 단가를 낮추고자 기술개발에 박차를 가하고 있다. 이에 따른 연료전지 부품 가격저감 기술이 국내 건물용 연료전지 시장보급의 활력소가 되기를 기대한다. 본 연구에서는 건물용 연료전지의 보조기기인 블로워의 가격저감을 위한 연구의 일환으로 블로워의 안전성능 평가를 통한 보조기기의 가격저감 및 안전성을 확보하고자 한다. 1kW급 건물용 연료전지시스템의 여러 블로워 중 도시가스용 연료승압 블로워, 선택산화 공기 블로워, 버너 공기 블로워 및 캐소드 공기 블로워의 안전성능 평가를 수행하였고, 평가결과의 공유를 통하여 국내 블로워 제조사의 설계방향을 제시하고 연료전지시스템의 안전성을 확인하고자 한다. 특히, 내구성, 기밀, 가혹조건시험 및 소음, 진동, 습도, 온도와 같은 내주위환경시험 등의 평가결과 비교를 통하여, 연료전지 부품 인증기준을 재정립하여 연료전지 부품산업의 조기 활성화를 도모하고자 한다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.18 no.7
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• pp.709-713
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• 2017

In urgent situations such as crashes, the integrity of an aircraft's fuel tank is directly related to the survivability of the crew. Thus, an external auxiliary fuel tank should be robust against bird strikes. In this study, a numerical analysis was carried out using impact analysis software to analyze the influence of bird strike on a composite container for an external auxiliary fuel tank. The structure was modeled as a shell element, and the fluid and bird were modeled by the particle method. The behavior of the internal fluid was also examined. The maximum stress, deformation, and strain of the composite container were also calculated.

• Journal of Aerospace System Engineering
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• v.13 no.4
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• pp.60-65
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• 2019

This study did a structural design of a fuel system of auxiliary fuel tank applied to aircraft then analyzed it. The safety of the structural design result was investigated. Aluminum alloy metal structure was applied to the fuel system structure. The structural analysis was conducted using commercial finite element software. The design requirement was maximum accelerate condition of the structure. Therefore, structural design was done considering the maximum accelerate condition.

• Resources Recycling
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• v.28 no.1
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• pp.47-54
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• 2019

In this study, the wastes were used as fuels for direct reduction iron (DRI) production to reduce production cost and recycle the wastes. We examined the effects of wastes on the reduction behavior of DRI manufacture and the possibility of using wastes as auxiliary fuels. The proximate and Ultimate analysis were carried out to confirm the properties of wastes as fuels, and high-quality reduced irons were fabricated by using the waste as an auxiliary fuel. The metallization of reduced irons increased as the calorific value increase of auxiliary fuel. Especially, the reduced irons fabricated from the waste tires and vinyl plastics which had high heat energy and volatile matters showed higher metallization than the others. The high calorific value and volatility of waste were significant properties as fuel. The high quality DRI could be fabricated with wastes as auxiliary fuels through optimization of reaction conditions.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.908-911
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• 2011

Aircraft Auxiliary Power Unit can start and operate using not only main fuel(JP-8) but also specified emergency fuels for emergency operation. In oder to verify emergency fuel requirement, emergency fuel test using commercial diesel fuel was performed. Changes in specific fuel consumption due to use of diesel fuel are 3.5%~7.8%, which satisfied requirement. Diesel fuel showed similar starting characteristic to the JP-8. The specific fuel consumption of diesel increased by 2.0%~3.4% compared with that of JP-8.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.11
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• pp.927-933
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• 2020

This paper presents a fuel quantity measurement system (FQMS) for an aircraft supplementary fuel tank considering the change of aircraft attitude. The developed FQMS consists of fuel sensors, a signal process unit, an indicator and a software to estimate the fuel quantity from the sensor data. To replicate the change of the roll and pitch attitude on the ground, the test simulator is developed in this work. Using the test simulator, the sensor data at various fuel quantities, roll and pitch angles are automatically measured to build a training data set. The data-driven software to estimate the fuel quantity is then developed using a trilinear interpolation method with the training data set. The developed FQMS is verified by investigating the fuel estimation error of the test data set that we know the true values. Through the test, it is confirmed that the error of the developed FQMS system satisfies the criteria of TSO-C55 document.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.957-967
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• 2017

Firing test of the fuel grain for solid fuel ramjet with additives and ignition support material was conducted. Fuel grain consist of HTPB mixed with AP particle 15 wt.%, Boron particle 5 wt.%. To cause the short ignition delay, ignition support consist of $NC/BKNO_3$ and composite propellant was coated to the fuel grain. An oxidant gas having a controlled temperature, pressure and oxygen composition close to the air condition in the ramjet combustor was supplied using the Ethanol blended $H_2O_2$ gas generator. Gas was set to flow at a mass flow rate of 150 g/s and mass flux of $200kg/m^2s$ in the grain port. Through the test, ignition support operated well and ignition delay of 0.5. During the test, stable chamber pressure with 8 bar and high combustion efficiency of 0.86 was confirmed.

• Proceedings of the KIEE Conference
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• 2007.10c
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• pp.189-191
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• 2007

본 연구에서는 고분자전해질연료전지(PEFC)를 이용하여 보조전 원용으로 사용할 수 있는 계통연계 연료전지 시스템을 개발하였다. 또한 본 연구에서 DSP(Digital Signal Processor)를 이용한 계통연계형 전력변환장치(PCS, Power Conditioning System)와 시스템 제어기의 개발도 병행하여 수행되었다. 개발된 1kW급 보조전원용 연료전지 시스템은 다양한 조건에서의 스택 성능 실험 및 BOP 연계 시험을 통해 최적의 운전점을 도출할 수 있었으며, PID(Proportional, Integral, Differential) 운전제어 방식을 통하여 시스템의 안정적인 운전 특성을 확보하였다. 향후 본 시스템은 계통연계용은 물론 독립전원용으로도 사용이 가능할 수 있도록 전력변환장치를 설계하여 적용할 예정이다.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2015.10a
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• pp.324-325
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• 2015

한로표지는 선박의 안전한 항행을 위하여 설치 운영하고 있으며, 전자기술의 발전과 안전한 항해에 도움을 주는 각종 시스템들이 설치되고 있다. 이에 따라 항로표지에서의 전력 수요는 과거보다 훨씬 더 많이 요구되고 있는 실정이다. 그러나 지구온난화 및 기상이변 등의 영향으로 태양광발전에 의존하는 많은 항로표지에서는 전력공급이 원활하지 않은 문제가 발생하고 있다. 태양광발전에 대한 보조발전시스템으로의 연료전지시스템을 검토하고 항로표지에 적용하기 위한 방안을 제시하고자 한다.