• 제목/요약/키워드: Air-Breathing

검색결과 277건 처리시간 0.028초

Cathode에 따른 소형 PEM 연료전지의 성능 변화 (Performance of the Small PEMFC according to Cathode)

  • 이세원;이강인;박민수;주종남
    • 한국수소및신에너지학회논문집
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    • 제19권4호
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    • pp.283-290
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    • 2008
  • In this paper, experiments with an air-breathing proton exchange membrane fuel cell (PEMFC) for mobile devices were carried out according to cathode conditions. These conditions are defined by the cathode flow field plate type (the channel type, the open type) and the cathode surface direction. Single-cell and 6-cell stack were used in the experiments. The experimental results showed that the open-type cathode flow field plate gave a better performance than the small channel type. In the experiments related to the direction of the slits on the cathode flow field plate, the horizontal slit cell was better than the vertical one. With respect to the cathode surface direction, when the cathode surface is placed in the direction normal to the ground, the PEMFC generated more stable power in the mass transport loss region. Since stable power in the mass transport region is closely related to the air supply, computational fluid dynamics (CFD) analysis for air-breathing PEMFC of different cathode surface directions was performed.

수동급기 직접 메탄올 연료전지의 동적 모델 (Dynamic Model of a Passive Air-Breathing Direct Methanol Fuel Cell)

  • 하승범;장익황;차석원
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2008년도 춘계학술대회 논문집
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    • pp.33-36
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    • 2008
  • The transient behavior of a passive air breathing direct methanol fuel cell (DMFC) operated on vapor-feeding mode is studied in this paper. It generally takes 30 minutes after starting for the cell response to come to its steady-state and the response is sometimes unstable. A mathematical dynamic one-dimensional model for simulating transient response of the DMFC is presented. In this model a DMFC is decomposed into its subsystems using lumped model and divided into five layers, namely the anodic diffusion layer, the anodic catalyst layer, the proton exchange membrane (PEM), the cathodic catalyst layer and the cathodic diffusion layer. All layers are considered to have finite thickness, and within every one of them a set of differential-algebraic governing equations are given to represent multi-components mass balance, such as methanol, water, oxygen and carbon dioxide, charge balance, the electrochemical reaction and mass transport phenomena. A one-dimensional, isothermal and mass transport model is developed that captures the coupling between water generation and transport, oxygen consumption and natural convection. The single cell is supplied by pure methanol vapor from a methanol reservoir at the anode, and the oxygen is supplied via natural air-breathing at the cathode. The water is not supplied from external source because the cell uses the water created at the cathode using water back diffusion through nafion membrane. As a result of simulation strong effects of water transport were found out. The model analysis provides several conclusions. The performance drop after peak point is caused by insufficiency of water at the anode. The excess water at the cathode makes performance recovery impossible. The undesired crossover of the reactant methanol through the PEM causes overpotential at the cathode and limits the feeding methanol concentration.

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지상레이다의 PT-파형 수신신호와 항공기 추적정보를 이용한 항공기 도플러 프로파일 추출 (Doppler Profile Extraction to Air-Breathing Targets with PT-Waveform Received Signal and Target Tracking Information on a Ground Radar)

  • 오현석;김수근
    • 한국전자파학회논문지
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    • 제28권2호
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    • pp.129-138
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    • 2017
  • 본 논문에서는 지상레이다가 추적 중인 항공기로부터 획득한 수신신호를 이용하여 도플러 형상(signature)을 추출하였다. 이를 위해 펄스열(pulse train) 파형의 수학적 모델로부터 레이다의 도플러 해상도를 검증하고, 비행 중인 항공기 도플러 형상이 엔진에 대한 레이다 측각(aspect angle)과 엔진의 제원에 따라 결정됨을 보였다. 이를 확인하기 위해 비행 중인 항공기에서 반사된 레이다 수신신호를 레이다 수신신호 저장장치를 이용하여 획득하고, 수신신호로부터 도플러 형상을 추출한 후, 항공기 추적 정보로부터 엔진에 대한 레이다 측각을 추정하였다. 이들 결과를 조합하여 측각에 대한 상대 도플러 형상 차이를 확인하고, 레이다에 사용가능한 표적인식용 도플러 프로파일을 제안하였다.

항문호흡 수련 및 항문호흡의 한의학적 고찰 (Anal breathing training and oriental medical study of the anal breathing)

  • 송정민;강한주;김정환
    • 대한의료기공학회지
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    • 제11권1호
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    • pp.262-283
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    • 2009
  • 1. Anus is one of the nine holes, a soul store and on the lungs and the lungs, so the soulgate is said to meet. In addition, weight 450g, length 14.31inch, horizontal, and the 2.74inch, hit the road, the lungs and the reaction of the colon was found to represent the five viscera were dirty. 2. Spirit directly to the anus of the five viscera and the traffic outside and pass the information where I can get, and a close relation to the breathing, and each groups' je-hang-suk-sin-gong, je-hang-gong, anal breathing, jwa-sik training, jung-gi-dan-beop, martial arts method, Kegel exercises, breathing training, such as the anus is the name. 3.Anal way of breathing while breathing naturally slow down when you inhale air, tighten the anus and rectum to release when you breathe out, give way (or vice versa), the number of 5-20, he'll make you build up gradually. 4.Associated with respiratory training in Oriental medicine perspective, it is a Mac gi-gyeong eight vessel. In addition, out of gi-gyeong eight vessel in breathing training and more closely related to the Conception Vessel, Governor Vessel. 5.Governor Vessel, Conception Vessel and connect the energy up, down, left and right to communicate is the so-ju-cheon. To complete the Governor Vessel instantly without the energy leak from the Mir-yeo(尾閭) to reach the anus should be breathing. 6.Start the Conception Vessel Through fare Vessel hoeǔm, hoeǔm important acupuncture point can be activated by itself does not have the muscle to the hoeǔm around the anus energy and blood breathing helps circulation.

Nonlinear Adaptive Velocity Controller Design for an Air-breathing Supersonic Engine

  • Park, Jung-Woo;Park, Ik-Soo;Tahk, Min-Jea
    • International Journal of Aeronautical and Space Sciences
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    • 제13권3호
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    • pp.361-368
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    • 2012
  • This paper presents an approach on the design of a nonlinear controller to track a reference velocity for an air-breathing supersonic vehicle. The nonlinear control scheme involves an adaptation of propulsive and aerodynamic characteristics in the equations of motion. In this paper, the coefficients of given thrust and drag functions are estimated and they are used to approximate the equations of motion under varying flight conditions. The form of the function of propulsive thrust is extracted from a thrust database which is given by preliminary engine input/output performance analysis. The aerodynamic drag is approximated as a function of angle of attack and fin deflection. The nonlinear controller, designed by using the approximated nonlinear control model equations, provides engine fuel supply command to follow the desired velocity varying with time. On the other hand, the stabilization of altitude, separated from the velocity control scheme, is done by a classical altitude hold autopilot design. Finally, several simulations are performed in order to demonstrate the relevance of the controller design regarding the vehicle.

압축 충격파를 이용한 평판형상 세라믹의 파괴거동 (Fracture Behavior of Plate Shape Ceramic using Compressive Shock Wave)

  • 황권태;김재훈;이영신;박종호;송기혁;윤수진
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 춘계학술대회 논문집
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    • pp.103-106
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    • 2009
  • Fracture characteristics of plate shape using shock tube for glass filled ceramics was carried out. Glass filled ceramics have been considered as a promising candidate material for the dome port cover of air breathing engine. This part of the air breathing engine has an important role separating solid and liquid fuel, and needs the frangible characteristics that the fracture of a part should not affect the internal components of combustion. The objectives of this study are to evaluate the fracture pressures for various thicknesses and diameters of shock impact area. Also fracture phenomena of separated membrane using a shock tube are observed. The experimental apparatus of shock tube consists of a driver, a driven section and a dump tank. The used material is glass filled ceramic made from Corning company. Specimens are used 3, 4.5 and 6mm thickness. Also diameters of shock wave area are chosen 70, 60 and 50 mm. It is expected that the results obtained from this study can be used in the basic data for the dome port cover design of an air breathing engine.

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압축 충격파를 이용한 세라믹의 파괴특성에 관한 연구 (A Study on the Fracture Characteristics of Ceramics Using Compressed Shock Wave)

  • 황권태;김재훈;이영신;박종호;송기혁;윤수진
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회A
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    • pp.338-343
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    • 2008
  • Fracture characteristics of plates and dome shapes for machinable glass ceramics using compressed shock wave. Machinable glass ceramics have been considered as a promising candidate material for the dome port cover of air breathing engine. This part of the air breathing engine has an important role separating solid and liquid fuel, and needs the frangible characteristics whereby the fracture of a part should not affect the internal components of combustion. The objective of this study are to evaluate the fracture pressure and phenomena of separated membrane using a shock tunnel. The experimental apparatus consists of driver, a driven section and a dump tank. The used material is machinable glass ceramic from Corning company. Specimens are used 3, 4.5 and 6mm thickness with plates and dome shapes. It is expected that the results obtained from this study can be used in the basic data for the dome port cover design of an air breathing engine.

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환기량 변화에 따른 실내공기질과 국소급기지수 특성 (Characteristics of Indoor Air Quality and Local Supply Index with a Variation of Supply ${\cdot}$ Exhaust Airflow rate)

  • 한창우;노광철;오명도
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2005년도 동계학술발표대회 논문집
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    • pp.21-26
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    • 2005
  • We performed the numerical analysis on the characteristics of indoor air quality and local supply index with a variation of supply · exhaust airflow rate. We analyzed the local supply index and carbon dioxide concentration at the room and breathing zone with respect to the variation of the supply · exhaust airflow rate. From the numerical results, we found that local supply index was affected but carbon dioxide concentration was hardly affected by the variation of the airflow rate in the room. And we also knew that carbon dioxide concentration was raised in despite of the increment of the supply airflow rate in the breathing zone. After this study it is necessary to analyze the local exhaust index when we evaluate the state of the ventilation in the room.

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고에너지 금속 연료를 이용한 Fuel-Rich 추진제 개발 (Development of Fuel-Rich Propellant Using High Energy Metal Fuel)

  • 김혜림;신경훈;최성한;이원복;김준형;고승원
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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    • pp.424-428
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    • 2012
  • 공기흡입형 추진기관은 운용의 단순함, 저비용, 저장의 용이성 등의 장점으로 각광받고 있는 추진 기관이다. 본 논문에서는 Boron을 이용한 공기흡입형 추진기관의 가스발생기에 사용될 추진제 연구를 수행하였다. 이를 위하여, Amorphous Boron Powder를 적용한 추진제에 다양한 첨가제를 사용하여 연소특성을 파악하였고, Boron bead를 제조하여 추진제에 적용하여 Amorphous Boron Power를 적용한 추진제와의 차이점을 비교 분석 하였다.

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