군용 항공기 인터컴 성능개량의 전기시스템 설계 요소 연구
A study on the electrical system design elements for the military aircraft intercom performance improvement
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초록
본 논문에서는 군용 항공기의 노후된 인터컴을 신규 인터컴 ICS로 교체하는 성능 개량을 제안하고 기체 내부 신규 인터컴 ICS 와 연동 장비 간연결을 위한 블록도 및 전기 배선 경로 방안을 간략하게 설계하여 제시하였다. 그러나 제시된 설계에 필요한 가이드가 부재하여 본 논문에서는 군용항공기 표준감항인증 기준과 군용항공기 작업 지침서를 기준으로 QFD 기법을 적용하여 15종의 주요 설계 요소를 도출하였다. 결과적으로 본 논문에서 제안된 연동 블록도와 배선 경로, 그리고 도출된 15종의 전기 시스템 주요 설계요소는 향후 노후된 군용 인터컴 성능개량의 전기 시스템 설계가이드로서 적용 가능함에 그 의미가 있다.
Abstract
In this paper, we proposed a performance improvement to replace the aged intercom of military aircraft with anew intercom ICS, and briefly designed and presented a interface block diagram and electrical wiring path for theconnection between the new intercom ICS and the other avionics equipment. However, due to the absence of aguide necessary for the proposed design, this paper derived 15 main design elements by using the QFD techniquebased on the military aircraft airworthiness certification criteria and military aircraft work instructions. As a result,it is meaningful that the interface block diagram, wiring path diagram, and the 15 main design elements proposedin this paper can be applied as an electrical system design guide for the performance improvement of the agedmilitary intercom in the future.
참고문헌 (14)
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