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The Evaluation of an Electric Hybrid Power System for the High Endurance Drone

장기체공 드론용 하이브리드 전기 추진시스템 성능 평가

  • Gang, Byeong Gyu (Aeronautics Research Directorate, Korea Aerospace Research Institute) ;
  • Kim, Keun-Bae (Aeronautics Research Directorate, Korea Aerospace Research Institute)
  • 강병규 (한국항공우주연구원 항공연구소) ;
  • 김근배 (한국항공우주연구원 항공연구소)
  • Received : 2022.01.10
  • Accepted : 2022.09.20
  • Published : 2022.10.05

Abstract

This research shows the test performance of a 6 kW-scale hybrid electric power system for the high endurance drone. The power system is composed of a two-stroke reciprocal engine, starter-generator and battery, and they are integrated as one power unit. The engine is designed to provide the house for holding the starter-generator at the end of a crankshaft in turn the engine and starter-generator can maintain the same speed during the operational period. In this way, the generated power is readily controlled by just manipulating an engine throttle movement. Moreover, the starter-generator can initiate an engine operation with an aid of battery power until the combustion process becomes stabilized. In consequence, integration mechanism between an engine and generator is simplified, which results in weight reduction achieved. The duty of back-up battery is to provide a starting power to generator via a system controller in addition to covering momentarily power shortage. Therefore, the electric power system is vindicated to provide 6 kW power through a ground test.

Keywords

Acknowledgement

본 과제는 'GR22260 탑재장비 10 kg 및 2시간 비행이 가능한 복합임무용 하이브리드 드론 개발' 과제지원으로 수행 되었습니다.

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