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PMSG design for usage of VTOL UAV in consideration of occurrence of heat according to the change of input current

Title
PMSG design for usage of VTOL UAV in consideration of occurrence of heat according to the change of input current
Author
이주
Keywords
Permanent Magnet Synchronous Generator ); Vertical Take-Off and Landing (VTOL); Unmanned Aerial Vehicle (UAV); Current density; PMSG
Issue Date
2016-11
Publisher
IEEE
Citation
2016 IEEE Conference on Electromagnetic Field Computation (CEFC), Page. 1-1
Abstract
This paper presents the characteristics of heat through the input current of PMSG used in Vertical Take-Off and Landing (VTOL) hybrid-electric propulsion Unmanned Aerial Vehicles (UAV). This UAV requires 10 times more output power than horizontal flight in case of vertical takeoff. So, PMSG which is the fundamental role of providing prime power of flight vehicle also needs to respond to this momentary requirement of high output power. Generally, PMSG performance is dominated by electromagnetic field and thermal design, and these two factors are closely related to each other. In the case of high input current, heat value affects the performance of PMSG, but the research on this field is yet to be flourished. Thus, this paper analyzes the thermal characteristics of PMSG in case of high input current in comparison with rated output, and designed the PMSG based on above implication.
URI
https://access.hanyang.ac.kr/link.n2s?url=http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=7816217&SID=EBSCO:edseeehttps://repository.hanyang.ac.kr/handle/20.500.11754/101025
ISBN
978-1-5090-1032-5
DOI
10.1109/CEFC.2016.7816217
Appears in Collections:
COLLEGE OF ENGINEERING[S](공과대학) > ELECTRICAL AND BIOMEDICAL ENGINEERING(전기·생체공학부) > Articles
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