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양철남,김양도 한국수소및신에너지학회 2012 한국수소 및 신에너지학회논문집 Vol.23 No.4
Long endurance is a key issue in the application of unmanned aerial vehicles. This study presents feasibility test results when fuel cell system as an alternative to the conventional engine is applied for the power of the UAV after the 150W fuel cell system is developed and packaged to the 1/4 scale super cub airplane. Fuel cell system is operated by dead-end method in the anode part and periodically purged to remove the water droplet in flow field during the operation. Oxygen in the air is supplied to the stack by the two air blowers. And fuel cell stack is water cooled by cooling circuit to dissipate the heat generated during the fuel cell operation. Weight balance is considered to integrate the stack and balance of plant (BOP) in package layout. In flight performance test, we demonstrated 4 times standalone take-off and landing. In the laboratory test simulating the flight condition to quantify the energy flow, the system is analyzed in detail. Sankey diagram shows that electric efficiency of the fuel cell system is 39.2%, heat loss 50.1%, parasitic loss 8.96%, and unreacted purged gas 1.67%, respectively compared to the total hydrogen input energy. Feasibility test results show that fuel cell system is high efficient and appropriate for the power of UAV.
양철남,문성모,김양도 대한기계학회 2015 JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY Vol.29 No.8
The present study reports the system configurations of a self-operated Polymer electrolyte fuel cell (PEFC) that is specially designedfor dead-end operation of both pure hydrogen and oxygen gas lines, including its operation features and durability. The PEFC stack with16 unit cells was constructed using homemade membrane electrode assemblies with 300 cm2 of apparent active area and bipolar plates. Aself-operated PEFC system was developed using a homemade PEFC stack, balance of plant, and electric control unit for automatic fuelcell system operation. Performance parameters of the self-operated PEFC system, including fuel utilization, parasitic loss, released heat,purge loss, and efficiency of the PEMFC stack and system were evaluated during the automatic operation of the PEFC system. A Dailystart-and-stop (DSS) test was also performed for one month to check the durability of the self-operated PEFC system. Electric efficienciesof the PEFC stack and system are approximately 60% and 49%, respectively, at an operating condition of 1.1 kW electric output; noperformance degradation of the PEFC system was observed for a month during the DSS test.
전기자동차용 축전지의 발열량 측정을 위한 열용량계 개발
양철남,박성용,Yang Cheol-Nam,Park Seong-Yong 한국전기화학회 1999 한국전기화학회지 Vol.2 No.4
EV & HEV의 성능은 다수의 축전지로 구성된 축전지팩의 성능에 좌우된다. 축전지의 열적 특성도 이러한 축전지팩의 성능을 좌우하는 많은 인자중의 하나이다. 특히 축전지의 열적 특성은 차량의 주행성능 및 축전지의 수명주기에 큰 영향을 주기 때문에, 축전지에서 발생되어 나오는 열량은 차량의 주행 모드를 모사한 다양한 조건하에서 가능한 정확히 측정되어야 한다. 또한 EV & HEV용 축전지팩의 열관리 시스템을 설계하기 위해서는 축전지팩내의 축전지에 대한 정확한 열특성 데이터를 필요로 하고 있다. 그러나 기존의 열량계로서는 EV용 축전지를 수용하여 열측정 시험을 하기엔 공동(Cavity)크기가 너무 작다. 이에 EV용 축전지의 열적 특성을 시험하기 위한 열량계를 공동(Cavity)의 크기 $120mm\times75mm\times200mm$로 개발하였다. 열량계의 보정은 0-200 W의 Heat Rate를 발생시킬 수 있는 가상셀(Dummy Cell)을 주문 제작하여 행하였다. 실제 입력 열량에 대한 측정열량의 오차범위는 $2\%$ 이내였고, 측정에 따른 전위 안정성도 2.5 mV 이내였다. The performance of the Electric Vehicle and Hybrid Electric Vehicle depends on that of the battery pack composed of series connected batteries. And thermal property is one of the main factors which decide the performance of the battery pack. So heat generation rate from the battery under the various driving mode must be measured as precise as possible because thermal characteristics of the battery affect the driving performance and battery pack's life cycle. Besides, to design and develop the battery thermal management system for the EV and HEV, the measurements of the thermal properties of the batteries are needed. However, the established calorimeter is not adequate to test an EV's battery because its cavity is too small to accommodate the EV's battery. Therefore we developed the calorimeter to test the thermal property of the EV's battery. Its cavity size is 120mm long, 75mm wide and 200mm high. The calorimeter is calibrated by the dummy cell which generates the heat rate from zero to 200W. The measuring accuracy of the calorimeter is within $2\%$ and its voltage stability is 2.5mV in the constant temperature bath.
A fuel cell/battery hybrid power system for an unmanned aerial vehicle
양철남,문성모,김양도 대한기계학회 2016 JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY Vol.30 No.5
A hybrid propulsion system composed of a homemade Polymer electrolyte fuel cell (PEFC) with a Lithium polymer (LiPo) battery in parallel connection was developed for Unmanned aerial vehicles (UAVs). The characteristics and performance of the system were evaluated considering its dynamic load responding capability and energy efficiency. A homemade PEFC stack composed of 36-unit cells and Balance of plant (BOP) was used to construct the fuel cell system directly connected to the propulsion system. Ten cells of a 3300-mAh 40C LiPo battery were combined with the PEFC system in parallel, and the LiPo battery was only switched on when high power was required for takeoff, acceleration and landing. The independent use of the homemade PEFC system and battery for the UAV showed a good load responding capability and a high fuel cell system efficiency of approximately 45%, which was obtained during cruising. The parasitic loss and the amount of unreacted hydrogen gas discharged outside of PEFC were nearly 3.91% and 0.89%, respectively. Results of the field test flights confirmed that the hybrid propulsion system based on the parallel connection of a PEFC system and a battery power is extremely effective in operating a UAV.