• Title/Summary/Keyword: 동력양수효율제어

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Design of the Condenser and Automation of a Solar Powered Water Pump (태양열 물펌프의 운전 자동화 설계)

  • Kim Y. B.;Son J. G.;Lee S. K.;Kim S. T.;Lee Y. K.
    • Journal of Animal Environmental Science
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    • v.10 no.3
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    • pp.141-154
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    • 2004
  • The solar powered water pump is very ideal equipment because solar power is more intensive when the water is more needed in summer and it is very helpful in the rural area, in which the electrical power is not available. The average so]ar radiation energy is 3.488 kWh/($m^2{\cdot}day$) in Korea. In this study, the automatic control logic and system of the water pump driven by the radiation energy were studied, designed, assembled, tested and analyzed for realizing the solar powered water pump. The experimental system was operated automatically and the cycle was continued. The average quantity of the water pumped per cycle was about 5,320 cc. The cycle time was about 4.9 minutes. The thermal efficiency of the system was about $0.030\%$. The pressure level of the n-pentane vapour in flash tank was 150$\%$450 hPa(gauge) which was set by the computer program for the control of the vapour supply. The pressure in the condenser and air tank during cycles was maintained as about 600 hPa and 1,200 hPa respectively. The water could be pumped by the amount of 128kg/($m^2{\cdot}day$) with the efficiency of $0.1\%$ and the pumping head of 10 m for the average solar energy in Korea.

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Power Characteristic Variation Simulation of Hybrid Electric Propulsion System for Small UAV (소형 무인기용 하이브리드 전기추진시스템 전력 특성변화 시뮬레이션)

  • Lee, Bo-Hwa;Park, Poo-Min;Kim, Chun-Taek;Yang, Soo-Seok;Ahn, Seok-Min
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.11
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    • pp.1052-1059
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    • 2011
  • It is conducted that power characteristic variation simulation of electric propulsion system that uses fuel cells, solar cells and a battery as power sources. Combining each power source, 400W electric propulsion system have been modeled and verified. In result, without active control logic, it is confirmed that battery's power response is faster than other power sources at starting and transient condition, fuel cell and solar cell are a major electrical power during cruise condition. After completing flight, SOC is 24.2% at the winter solstice and is 93% at the summer solstice, It is revealed that active power control for sustaining proper SOC is necessary as a securing the system safety and effective power distribution.