DOI QR코드

DOI QR Code

An Empirical Study on the Quality Reliability of the Start-up performance of the Fixed Wing Aircraft at low temperature

고정익 항공기 저온 시동 성능의 품질 신뢰성 향상에 관한 실증적 연구

  • Kim, DW (Defence Agency for Technology and Quality) ;
  • Jeong, SH (Defence Agency for Technology and Quality)
  • Received : 2018.02.12
  • Accepted : 2018.03.05
  • Published : 2018.03.31

Abstract

Purpose: The purpose of this study is to analyze low-temperature starting performance of the light attacker and to search and improve the aircraft system including battery and Battery Charge and Control Unit(BCCU). Methods: In order to improve the starting up performance of the light attacker at low-temp, various deficiency cause were derived and analyzed using Fault Tree Analysis method. As a result, it was confirmed there were drawbacks in the charging and discharging mechanism of the battery. The inactivation of the battery's electrolyte at low-temp and the premature termination of the battery charge were the main cause. After long error and trial, we improved these problems by improving performance of battery and optimizing the charging algorithm of BCCU. Results: It was confirmed that the problems of starting up failures were solved through the combined performance test of the battery and BCCU, the ground test using the aircraft system and the operation test conducted by Korea Airforce operating unit for 3 months in winter. Conclusion: This study showed that the improvement of quality reliability was achieved and thus the start-up performance issue of the light attacker has been resolved at low temperature. And it is expected that the design methodologies of temperature-affected electrical system of aircraft will contribute to the development of the aircraft industry in the future.

Keywords

References

  1. J.E. Melton. 1993. "3D Euler Flow Solutions using Unstructured Cartesian and Prismatic Grids." 31st Aerospace Sciences Meeting & Exhibit(Jan):11-14.
  2. DAPA(Defense Acquisition Program Administration). 2013. "Specification for Airplane, Attack(FA-50)." KDS 1510-4004.
  3. DAPA(Defense Acquisition Program Administration). 2013. "Specification for Battery Charger- control Unit & Tray, Battery." KDS 6110-4010-3.
  4. DoD(Department of Defense). 1999. "Electronic Equipment, Airborne, General Specification For." MIL-STD-5400.
  5. DoD(Department of Defense). 2000. "Environmental Engineering Considerations And Laboratory Tests." MIL-STD-810F.
  6. DoD(Department of Defense). 1991. "Aircraft Electric Power Character." MIL-STD-704F.
  7. DTaQ(Agency for Technology and Quality). 2013. "Qualification Assurance Requiements for Battery, Charging Type." QAR85032340.
  8. Jung-Kyun Kim et al. 2009. Estimation of thermal parameters of the enclosed electronic package system by using thermal network model, Mechatronics 19(6):1034-1040. https://doi.org/10.1016/j.mechatronics.2009.06.013
  9. Jung-Kyun Kim et al. 2011. Compact Thermal Network Model of the Thermal Interface Material Measurement Apparatus with Multi-Dimensional Heat Flow. IEEE CPMT 1(8):1186-1194.
  10. Kim, D., Jeong, S., 2016. "A Study on the quality improvement of aircraft battery at low temperature based on the heat transfer analysis." Kerea Quality Congress, Fall Conference, 179-180.
  11. Su-Heon Jeong et al. 2013. New design of a liquid bridge heat switch to ensure repetitive operation during changes in thermal conditions. Applied thermal engineering 59:283-289. https://doi.org/10.1016/j.applthermaleng.2013.05.027