본문 바로가기
KERD
논문KCI 등재

항공기용 유압작동기 수분유입 방지를 위한 품질개선 사례

A Case Study on Quality Improvement for Prevent Water Infiltration to ISA in Aircraft

0

조회

0

다운로드

1

인용

0

참고문헌

키워드

주제분류학제간연구

초록

Purpose: The purpose of this paper is to improve quality for water infiltration to FCISA during military aircraft operation. Methods: A series of troubleshooting studies were conducted to identify the root cause of the water infiltration and reproduce the defects through various simulation tests. And design improvement measures were derived, and countermeasures were taken to prevent recurrence of moisture inflow defects. Conclusion: FCISA operates a very important role in the operation of military aircraft, and defects due to water infiltration are very fatal to flight safety. In this study, the root cause was identified and the design improvement to prevent recurrence was carried out through the failure investigation performed in this study, and the FCISA was improved so that the flight safety was not affected. The results of this study will be valuable back data that can be reflected in the design process through Lessons-Learned in the design phase of the aircraft that will be developed in the future.

Abstract

Purpose: The purpose of this paper is to improve quality for water infiltration to FCISA during military aircraft operation. Methods: A series of troubleshooting studies were conducted to identify the root cause of the water infiltration and reproduce the defects through various simulation tests. And design improvement measures were derived, and countermeasures were taken to prevent recurrence of moisture inflow defects. Conclusion: FCISA operates a very important role in the operation of military aircraft, and defects due to water infiltration are very fatal to flight safety. In this study, the root cause was identified and the design improvement to prevent recurrence was carried out through the failure investigation performed in this study, and the FCISA was improved so that the flight safety was not affected. The results of this study will be valuable back data that can be reflected in the design process through Lessons-Learned in the design phase of the aircraft that will be developed in the future.

참고문헌 (7)

  1. 최재형, "한국형 기동헬기 동계운용능력 향상을 위한 플래퍼밸브 개선연구", 한국항공우주학회지, 44(1), pp.49~56 (2016), 한국항공우주학회
  2. Kim, J. H., "Analysis on Insulation Failure for Third Winding GPT of 345kV Power Transformer", Proceedings of the Korean Institute of Electrical Engineers, pp.1325~1326 (2018)
  3. 김정훈, "한국형 기동헬기 OBIGGS 경고등 이상 점등현상 설계개선", 한국항공우주학회지, 45(6), pp.473~480 (2017), 한국항공우주학회
  4. Lee, M. S., "Improvement of Structure to Prevent Water Infiltration and Oil Leakage for Reduction Units of KTX", Proceedings of the Korean Society for Railway, pp.20~25 (2007)
  5. 임현규, "회전익 항공기 MRA 조종로드 방수 및 부식 방지에 관한 연구", 한국산학기술학회논문지, 18(9), pp.92~100 (2017), 한국산학기술학회[DOI]
  6. Shin, J. H., "A History of Flight Control Integrated Servoactuator and Advanced Development Trend", Journal of the Defense Science & Technology Information, 72, pp.8~15 (2018)
  7. Yang, W. H., "A Suggesting for Development of Field Maintenance Technology to Ensure the Demonstration of Weapon System Combat Power", Journal of Defense and Technology, 477, pp.108~121 (2018)

관련 논문AI추천

이 간행물의 다른 논문 (17건)