전기전자학회논문지 (Journal of IKEEE)

  • 제28권3호
  • /
  • Pages.243-252
  • /
  • 2024
  • /
  • 1226-7244(pISSN)
  • /
  • 2288-243X(eISSN)
한국전기전자학회 (Institute of Korean Electrical and Electronics Engineers)
권호 표지
DOI QR코드

DOI QR Code

군용 항공기 인터컴 성능개량의 전기시스템 설계 요소 연구

A study on the electrical system design elements for the military aircraft intercom performance improvement

  • 윤인복
  • In-Bok Yoon (Avionics R&D center, Hanwha systems)
  • 투고 : 2024.07.08
  • 심사 : 2024.07.29
  • 발행 : 2024.09.30
PDF 다운로드
⟨ 이전 논문 다음 논문 ⟩

초록

본 논문에서는 군용 항공기의 노후된 인터컴을 신규 인터컴 ICS로 교체하는 성능 개량을 제안하고 기체 내부 신규 인터컴 ICS와 연동 장비 간 연결을 위한 블록도 및 전기 배선 경로 방안을 간략하게 설계하여 제시하였다. 그러나 제시된 설계에 필요한 가이드가 부재하여 본 논문에서는 군용 항공기 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 설계 가이드로서 적용 가능함에 그 의미가 있다.

In this paper, we proposed a performance improvement to replace the aged intercom of military aircraft with a new intercom ICS, and briefly designed and presented a interface block diagram and electrical wiring path for the connection between the new intercom ICS and the other avionics equipment. However, due to the absence of a guide necessary for the proposed design, this paper derived 15 main design elements by using the QFD technique based 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 proposed in this paper can be applied as an electrical system design guide for the performance improvement of the aged military intercom in the future.

키워드

참고문헌

  1. Head quarters, Department of the ARMY, Technical Manual, DS, GS, And Depot Maintenance Manual, Control, Intercommunication Set C-1611D /AIC and Discriminator Discrete signal MD-736 /A, TM 11-5831-201-35, January. 1970. 
  2. Ramjyu, Kim, "A Study on measures to maximize military strength operation in the air force weapon system - focusing on the air force's aging aircraft availability," Master thesis, Kyonggi University, 2014. 
  3. Jae-Won Lee, Yong-Soo Kwon, Nam- Kyoung Ko, "Derivation of Critical Functions of the Future Attack Helicopter Using QFD," Journal of the Korea Institute of Military Science and Technology, vol.16, no.3, pp.348-357, 2013. DOI: 10.9766/KIMST.2013.16.3.348 
  4. Emersys Co.,LTD, A development of the 3D audio module and software to be applied on aircraft intercom(10060483), Korea Ministry of Trade Industry and Energy, January. 2017. 
  5. Jay Paul Wihelm, "Aircraft Intercom System Design for Project Oculus", Master Theses, West Virginia University, 2005. 
  6. ebay, "Control Intercommunication Set C-16 11D/AIC F-4 Phantom, AH-1G Cobra" https://www.ebay.at/itm/Control-Intercommunication-Set-C-1611D-AIC-F-4-Phantom-AH-1G-Cobra/263022921328 
  7. Head quarters, Department of the ARMY, Operator's Manual, Army Model UH-1H/V Helicopters, TM 55-1520-210-10, 15 February. 1988. 
  8. The JoongAng, Politics:Military, "The Korean Army's UH-1H helicopter, after flying a distance equivalent to circling the Earth more than 3,500 times, is entering retirement, 27 July. 2020". https://www.joongang.co.kr/article/23834221#home 
  9. Department of Defense USA, Department of Defense Interface Standard, Digital Time Division Command/Response Multiplex Data Bus, MIL-STD-1553C(Superseding MIL-STD-1553B, 21 September 1978), 28 February. 2018. 
  10. PartTarget, "5831-00-933-9822(C-1611D/AIC) Data-5831-00-933-9822 Features", https://www.parttarget.com/5831-00-933-9822_5831009339822_C-1611D-AIC.html 
  11. DAPA, Airworthiness Certification Criteria (Part 1), 29 April. 2021. 
  12. Direction of the Commander, Naval air system Command, Technical Manual, Installation and Repair practices, Volume 1 Aircraft Electric and Electronic Wiring, NAVAIR 01-1A-505-1, TO 1-1A-14, TM 1-1500-323-24-1, 15 September. 2009. 
  13. Min Joon Seok, Yong Seok Nam, "A Research on the Application of Single Point Ground for Intercom of T-50 Advanced Trainer", J. of The Korean Society for Aeronautical and Space Sciences, vol.42, no.9, pp.773-778, September. 2014. DOI: 10.5139/JKSAS.2014.42.9.773 
  14. Naval Air Engineering Center, Military Specification, Electric load and power source capacity aircraft, analysis of, MIL-E-7016F, 20 July 1976.