• Title/Summary/Keyword: 연료 온도

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Effect of Hot Pressing Conditions in Fabrication of Membrane & Electrode Assembly for Proton Exchange Membrane Fuel Cell (고분자 전해질형 연료전지에서 막-전극 어셈블리 제조지 Hot-pressing조건에 대한 영향)

  • 최경환;이승재;설용건;이태희;노용우;고영태
    • Proceedings of the Korea Society for Energy Engineering kosee Conference
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    • 1994.11a
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    • pp.23-27
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    • 1994
  • 고분자 전해질형 연료전지의 성능을 향상시키기 위하여 막-전극 어셈블리 제조시 hot-pressing 온도와 압력조건을 변화시켜며 단위전지 성능을 관찰하였으며 이에 대한 분석은 열무게분석법(TGA), 기공도, 이온투과계수 등을 사용하였다. 또한 전지의 작동온도 및 압력을 변화시켜가며 전지의 성능을 관찰하였다. 성능 실험은 가습기의 온도와 cell의 온도, 압력을 변화시켜가며 측정하였다.

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Study on Fuel Lubrication Performance of a High Speed Rolling Element Bearing (소형 고속 구름베어링의 연료윤활 특성 연구)

  • Kim, Ki-Tae;Kim, Sung-Kyun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.11a
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    • pp.424-426
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    • 2008
  • A parametric study was carried out to find the fuel lubrication performance of high speed small rolling element bearings. Both MIL-PRF-7808 turbine oil and JP-8 aircraft fuel were used as the lubricant to compare the operational characteristics. 17 mm inner diameter deep groove ball bearing and 20 mm cylindrical roller bearing were used. A high speed bearing test rig was developed and the testing was done with varying applied load, cooling air temperature, lubricant flow rate, and speed. Fuel caused more cage wear than oil for ball bearing with increasing axial load and rotational speed. The bearing temperature using fuel was lower than that using oil, and this seems to be the result of the high cooling capacity of fuel. According to various tests, the fuel lubrication is applicable for the lubrication on the main shaft bearings of expendable small gas turbines.

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Performance Analysis of 1.5kW-class Molten Carbonate Fuel Cell Stack (1.5kW급 용융탄산염 연료전지 스택의 성능 분석)

  • 남석우;황정태;이갑수;임태훈;오인환;하흥용;윤성필;홍성안;임희천
    • Journal of Energy Engineering
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    • v.8 no.1
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    • pp.23-33
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    • 1999
  • 용융탄산염 연료전지의 대형화에 관한 기본 기술을 확립하기 위하여 전극의 유효면적이 625 $\textrm{cm}^2$인 단위전지를 20단 적층한 내부 분배형 용융탄산염 연료전지 스택을 제작하고 그 성능을 살펴보았다. 연료로 72% H2/18% CO2/10% H2O를 , 산화제로는 70% air/30% CO2의 혼합 기체를 사용하여 운전한 결과 전류밀도가 150 mA/$\textrm{cm}^2$이고 연료 및 산화제의 이용율이 0.4일 때, 스택 전압이 16.62 V로 1.56 kW의 높은 초기출력을 나타내었다. 스택 내 분리판에서의 온도 분포는 가스 흐름 방향으로 온도가 증가하였으며 스택출력이 높아질수록 가스 배출 부분의 온도가 상승하였다. 스택 내 각 단위전지간의 성능 분포는 균일하지 않았으며, 가스이용율에 따라 그 편차가 증가하였다. 연속 운전 300시간 후부터 스택의 성능이 감소하였으며, 그 원인을 분석한 겨로가 탄소 석출과 부식 생성물에 의한 전기 단락 때문으로 밝혀졌다. 본 연구를 통하여 anode 출구에서의 가스 조성을 분석함으로써 전기 단락에 의한 전압 손실량을 계산하는 기법을 확립하였다. 또한 본 연구에서 얻은 결과를 통하여 향후 스택의 대형화와 장수명화에 대한 대책을 제시하였다.

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Prediction of Autoignition Temperatures of Gasoline-Ethanol Blended Fuels (휘발유/에탄올 혼합연료의 자연점화온도 예측)

  • Kim, Shin-Woo;Lee, Eui-Ju
    • Fire Science and Engineering
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    • v.33 no.5
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    • pp.1-6
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    • 2019
  • The recent development of biofuel production technology facilitates the widespread use of bioethanol and biodiesel by mixing them with fossil fuels. However, the use of these new blended fuels in combustion could result in severe safety problems, such as fire and explosion. In this study, numerical simulation was performed on the well-stirred reactor (WSR) to simulate the autoignition temperature (AIT) in homogeneous combustion and clarify the effect of ethanol addition on the AIT, the most important property for assessing the potential for fire and explosion. Response surface methodology (RSM) was introduced as a design of experiment (DOE), enabling the AIT to be predicted and optimized systematically with respect to three independent variables: ethanol mole fraction, equivalence ratio, and pressure. The results show that the autoignition temperature primarily depends on the ethanol mole fraction and pressure, while the effects of the equivalence ratio are independent of the AIT. RSM accurately predicted the experimental AIT, indicating that this method can be used to effectively predict the key properties involved in fires and explosions.

Cooling Fluid Study in Proton Exchange Membrane Fuel Cell (고분자전해질형 연료전지의 냉각유체에 대한 연구)

  • 김준범;이흥주
    • 한국전기화학회:학술대회논문집
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    • 2005.07a
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    • pp.93-96
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    • 2005
  • 고분자전해질형 연료전지에서는 수소이온의 이온전도성 저하를 방지하기 위하여 외부에서 가습하여 주는 방식이 일반적이지만, 가습에 소요되는 부품을 일부라도 제거할 경우 연료전지의 효율은 높이고 제작단가도 경감할 수 있다. 이를 위하여 저가습 및 무가습 실험을 수행하였으며, 정확한 data의 수집과 시험장비의 자동제어를 위하여 National Instrument사의 compact field point (cFP)를 사용하였다. Humidifier와 heater의 온도를 조절하여 공급유체의 상대습도 및 온도를 각각 조절하였으며, 이에 필요한 이론적 온도는 Antoine equation 을 사용하여 산정하였다. Anode와 cathode 양측 $100\%$ 가습 경우를 기준으로 가습량을 조절하면서 실험을 수행하였으며 성능 차이를 그래프로 도시하여 양측의 변화에 대한 영향을 볼수 있도록 하였다. Stack의 온도가 $70^{\circ}C$이고 양측 무가습일 경우에 성능 측정이 어려워서 stack의 온도를 저온에서부터 변화시키면서 무가습 성능을 실시간으로 측정하여 보았다. 일반적으로 hydronium ion은 anode측에서 cathode측으로 계속 이동하여야 전기를 생성할 수 있으므로 cathode측 무가습이 anode측 무가습보다 성능이 더 잘 나오는 것으로 예측하였으나 이와 반대되는 경향의 실험 결과를 얻었다. 양측 무가습의 경우에는 공기 중의 상대습도와 back diffusion 등에 영향을 받을 수 있으므로 각종 변수들의 영향을 분리하여 관찰할 수 있는 실험을 수행 중에 있다.

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A study on the performance enhancement for combined cycle using cold heat of LNG (LNG 냉열을 이용한 복합사이클 발전시스템의 성능개선연구)

  • 김용희;김병일
    • Proceedings of the Korea Society for Energy Engineering kosee Conference
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    • 1996.10b
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    • pp.77-80
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    • 1996
  • 우리나라에서 피크부하용으로 사용하는 복합발전이 하계시에서 외기온도가 상승함에 따라 실제로는 정격출력을 내지 못하고 있다. 따라서 본 연구에서는 연료(LNG)의 냉열을 이용하여 가스터빈의 연소용공기를 냉각시킬 경우, 복합발전 시스템의 성능변화를 분석하기 위하여 시뮬레이션을 수행하였다. 그 결과 LNG의 냉열을 이용하여 연소용공기를 원하는 온도까지 냉각시킬 수 있음을 확인할 수 있었다. 또한 연소기로 연료를 투입하기전에 설계온도까지 예열시키는 열교환기를 통해 배기가스에 함유된 현열을 더욱 많이 회수하면서, 가스터빈 투입연료의 온도를 상승시킬 수 있어, 시스템효율이 더욱 상승함을 알 수 있었다. 결론적으로 외기온도가 변하는 경우에, 본 시스템의 도입을 위해서는 경제성분석과 더불어 열교환기 시스템의 최적합성이 추후 진행되어야 할 것이며, 이를 통해 최적의 발전시스템을 구성할 수 있으리라 생각된다.

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A Numerical Analysis on Transient Fuel temperatures in a Military Aircraft under Non-operating Ground Static Condition (지상 정적 상태에서의 항공기내 연료온도변화에 대한 수치해석)

  • 김영준;김창녕
    • Journal of Energy Engineering
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    • v.12 no.1
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    • pp.11-16
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    • 2003
  • A numerical study was performed on the transient fuel temperatures of a military aircraft stationed under non-operating static condition. Numerical calculation was peformed by an explicit method using modified Dufort-Frankel scheme. It was assumed that the non-operating aircraft is subjected to repeated daily cycles of air temperature with the solar radiation and wind speed corresponding to the 1 % hot day ambient condition. And, the aircraft was assumed to be in turbulent flow. The convective heat transfer coefficient for turbulent flow on the flat plate suggested by Eckert was employed to calculate heat transfer between the aircraft surface and the ambience. The energy conservation equation on fuel was used as governing equation for this analysis. As a result of this analysis, the wing tank temperature showed the highest temperature and the largest rate of temperature changes among fuel tanks. The results of this analysis could be used as initial foe] temperatures for analysis of the transient fuel temperatures in various flight missions. Also, this analysis method could be used to analysis and design of an aircraft thermal energy management system.

Effect of Fuel/Air Mixing Quality on Temperature Characteristics in a Lean Premixed Model Gas Turbine (희박 예혼합 모형 가스터빈 내에서 연료/공기 혼합정도가 온도 특성에 미치는 영향)

  • Lee Jong Ho;Chang Young June;Jeon Chung Hwan
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • v.y2005m4
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    • pp.274-280
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    • 2005
  • Experimental investigations were carried out in an atmospheric pressure, optically accessible and laboratory-scale dump combustor. The objective of this study is to obtain the phase-resolved gas temperatures at different phases of the oscillating pressure cycle during unstable combustion. To see the effect of incomplete fuel-air mixing on phase-resolved temperature characteristics, CARS temperature measurements were performed. Results including phase-resolved averaged temperature, normalized standard deviation and temperature probability distribution functions (PDFs) were provided in this paper. It could be found that the profile of mean temperature showed the in-phase relationship with pressure cycle. Temperature PDFs give an insight on the flame behavior as well as NOx emission characteristics. These results would be expected to play an important role in better understanding of driving mechanisms and thermo-acoustic interactions.

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Axisymmetric Simulation of Nonpremixed Counterflow Flames - Effects of Fuel Concentration on Flame Structure - (비예혼합 대향류 화염의 축대칭 모사 - 연료농도가 화염구조에 미치는 영향 -)

  • Park Woe-Chul
    • Journal of the Korean Institute of Gas
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    • v.7 no.3 s.20
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    • pp.44-50
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    • 2003
  • The axisymmetric methane-air counterflow flame was simulated to investigate changes in the flame structure due to the fuel concentration and to evaluate the numerical method. The global strain rates $a_g=20,\;60,\;90\;s^{-1}$ and the mole fractions of methane $x_m=20,\;50,\;80\%$ in the fuel stream were taken to be numerical parameters. The axisymmetric simulation was conducted by using the Fire Dynamics Simulator (FDS) which employed a mixture fraction combustion model, and the results were compared with those of OPPDIF, which is an one-dimensional flamelet code and includes detail chemical reactions. In all the cases tested, there was good agreement in the temperature and axial velocity profiles between the axisymmetric and one-dimensional simulations. It was shown that the flame thickness and peak flame temperature increase and the flame radius decreases as the fuel concentration increases.

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Combustion Characteristics of Bio Emulsion Fuel (바이오에멀젼 연료의 연소 특성)

  • Kim, Moon-Chan
    • Journal of the Korean Applied Science and Technology
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    • v.35 no.4
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    • pp.1421-1432
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    • 2018
  • Water soluble oil was obtained from the pyrolysis of coconut waste as a biomass at $600^{\circ}C$. It was studied that the combustion characteristics of bio-emulsion fuel by mixing and emulsifying 15~20% of water soluble oil which obtained from pyrolysis of coconut waste as a biomass and MDO(marine diesel oil) as a marine fuel. Engine dynamometer was used for detecting emissions, temperature, and power. The temperature of combustion chamber was decreased because the moisture in bio-emulsion fuel deprived of heat of evaporation in combustion chamber. While combustion, micro-explosion took place in the combustion chamber by water in the bio-emulsion fuel, MDO fuel scattered to micro particles and it caused to smoke reduction. The temperature reduction of combustion chamber by using bio-emulsion fuel reduced the NOx emission. The increasing of bio-oil content caused increasing water content in bio-emulsion fuel so total calorific value was reduced. So the characteristics of power was decreased in proportion to using the increasing amount of bio-emulsion fuel. Heavy oil as a marine fuel exhausts a lot of smoke and NOx. We expect that we can reduce the exhaust gas of marine engine such as smoke and NOx by using of bio-emulsion fuel as a marine fuel.