복합회전익 무인기용 하이브리드 동력시스템 개념연구
김근배, 이보화
Abstract
김근배, 이보화
Abstract
It has been carried out that a conceptual study to apply the hybrid power system for a compound rotary-wing UAV. Basically, the hybrid power system consists of engine, motor&generator, battery and controller. The hybrid system divided into two that are series-hybrid and parallel-hybrid, and the performance characteristics have been investigated along with the system configuration. In general, the series-hybrid system design is simple, but the parallel-hybrid system design is complex to fit the operation mode of the vehicle so the power can be supplied more effectively than the series-hybrid.
A significance statement is not available in the OpenAlex record.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
It has been carried out that a conceptual study to apply the hybrid power system for a compound rotary-wing UAV. Basically, the hybrid power system consists of engine, motor&generator, battery and controller. The hybrid system divided into two that are series-hybrid and parallel-hybrid, and the performance characteristics have been investigated along with the system configuration. In general, the series-hybrid system design is simple, but the parallel-hybrid system design is complex to fit the operation mode of the vehicle so the power can be supplied more effectively than the series-hybrid.
Key concepts: Hybrid system, Hybrid power, Hybrid vehicle, Series and parallel circuits, Series (stratigraphy), Controller (irrigation), Computer science, Power (physics)