무인기 구동을 위한 PEM 연료전지 스택의 초경량 바이폴라 플레이트Light Bipolar Plate of the PEM Fuel Cell Stack for UAV Application

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dc.contributor.author김, 기인-
dc.contributor.author이, 종광-
dc.contributor.author김, 태규-
dc.contributor.author권, 세진-
dc.contributor.authorKim, Kiin-
dc.contributor.authorLee, Jongkwang-
dc.contributor.authorKim, Taegyu-
dc.contributor.authorKwon, Sejin-
dc.date.accessioned2011-03-08T08:20:57Z-
dc.date.available2011-03-08T08:20:57Z-
dc.date.issued2011-03-08-
dc.identifier.urihttp://hdl.handle.net/10203/22530-
dc.description.abstractPEM(Proton Exchange Membrane) fuel cell was selected as a power plant of a UAV as it delivers power output higher than other types of fuel cell. PEM fuel cell consists of four main parts; membrane, electrode, GDL(Gas Diffusion Layer) and bipolar plate. This paper presented the fabrication process of the photosensitive glass bipolar plate for a compactness and a light weight that are necessaries for UAV systems. The glass bipolar plate is made of an anode layer, a cathode layer, a separation layer and an electrode. The fabrication methods on photosensitive glass for each parts were developed. Thermal bonding technique was used in assembly procedure. Aluminum insert was used to improve an electric conductivity.en
dc.description.sponsorship이 연구는′08년도 정부(교육과학기술부)의 재원으로 한국과학재단의 지원을 받아 수행되었으며, 이에 관계자 여러분께 감사드립니다.(No. R0A-2007-000-20065-0)en
dc.language.isokoen
dc.title무인기 구동을 위한 PEM 연료전지 스택의 초경량 바이폴라 플레이트en
dc.title.alternativeLight Bipolar Plate of the PEM Fuel Cell Stack for UAV Applicationen
dc.typeArticleen

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