항공우주시스템공학회지 (Journal of Aerospace System Engineering)

  • 제13권5호
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  • Pages.24-31
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  • 2019
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  • 1976-6300(pISSN)
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  • 2508-7150(eISSN)
항공우주시스템공학회 (The Society for Aerospace System Engineering)
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항공기용 전원분배장치의 전원개폐에 의한 과도전압 특성 연구

Study for Transient Voltage Characteristic by Power Switching on Aircraft Electrical Master Box

  • 투고 : 2019.06.12
  • 심사 : 2019.10.15
  • 발행 : 2019.10.31
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초록

본 연구에서는 항공기용 전원분배장치에서 발생한 소손현상의 원인을 분석하고 개선 방안을 제안하였다. 항공기용 전원분배장치는 교류와 직류로 분류하며, 두 장비 사이에 정류기가 존재한다. 전원분배 장치의 전원이 켜지고 꺼질 때 전원 보드내의 커패시터가 소손되었다. 주요 원인은 정류기에 내장되어 있는 인덕턴스로 인해 과도한 전압이 발생했기 때문이다. 고장이 발생 할 수 있는 경우를 분류하였다. 그리고 그에 따른 영향성을 분석하였으며, 실험적인 방법을 통해서 해결책을 수립하였다.

In this study, we analyzed the cause of the burn out phenomenon in the power distribution system for aircraft and proposed the improvement method. The power distribution device for aircraft has an AC and DC, and there is a rectifier between the two devices. The capacitors in the power board burn out when the power is turned on and off. The main reason for this is the excessive voltage caused by the inductance built into the rectifier. The cases that can cause a failure are classified. The impact was analyzed and the solution was established through the experimental method.

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참고문헌

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