한국수소및신에너지학회논문집 (Transactions of the Korean hydrogen and new energy society)

  • 제32권6호
  • /
  • Pages.542-550
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  • 2021
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  • 1738-7264(pISSN)
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  • 2288-7407(eISSN)
한국수소및신에너지학회 (The Korean Hydrogen and New Energy Society)
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연료전지 추진 멀티콥터의 사이징 계산 방법에 관한 연구

Study on Sizing Calculation Method of Fuel Cell Propulsion Multirotor

  • 이동근 (한국기계연구원 청정연료발전연구실) ;
  • 안국영 (한국기계연구원 청정연료발전연구실) ;
  • 김영상 (한국기계연구원 청정연료발전연구실)
  • LEE, DONGKEUN (Department of Clean Fuel and Power Generation, Korea Institute of Machinery & Materials (KIMM)) ;
  • AHN, KOOKYOUNG (Department of Clean Fuel and Power Generation, Korea Institute of Machinery & Materials (KIMM)) ;
  • KIM, YOUNGSANG (Department of Clean Fuel and Power Generation, Korea Institute of Machinery & Materials (KIMM))
  • 투고 : 2021.11.15
  • 심사 : 2021.12.16
  • 발행 : 2021.12.30
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초록

As the application of multirotor grows, the demands for multirotor that can fly longer and load more are increasing. Hydrogen has a high energy density, so it can satisfy these demands when used in multirotor. In order to design hydrogen fueled multirotor that satisfies the desired flight time and payload, it is important to calculate the specifications of a fuel cell, battery, and hydrogen storage system. This paper contains detailed information on various energy systems used in multirotor and fuel cell powered multirotor research trends. This study proposed a sizing calculation method that meets the target flight time and payload using thrust and power equations. It has been explained how the two equations derive the particular specifications. The specifications of the multirotor were derived by assuming a payload of 50 kg and a flight time of 1 hour. In addition, the effects of the values of the fuel cell, hydrogen storage system, and motor propeller were analyzed.

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과제정보

본 연구는 산업통상자원부(MOTIE)와 한국에너지기술평가원(KETEP)의 지원을 받아 수행되었다(No. 2019281010007A, No. 20203020040010).

참고문헌

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