Journal of Aerospace System Engineering (항공우주시스템공학회지)

The Society for Aerospace System Engineering (항공우주시스템공학회)
권호 표지

A Study on Optimal design of T-50 Aircraft FFP system through a case of F-16 Aircraft

최신 전투기 사례를 통한 T-50 FFP 시스템 최적 설계 연구

  • 남용석 (국방기술품질원 항공센터) ;
  • 김태환 (국방기술품질원 항공센터) ;
  • 정년수 (한국항공우주산업(주))
  • Published : 2010.03.31
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Abstract

The Fuel system of T-50 Advanced Trainer is equipped with two boost pump and fuel flow proportioner for feeding fuel to turbo jet engine. when an unexpected failure occurs, they can feed the fuel to turbo jet engine which fuel quantity required. fuel quantity control method is applied for minimizing the center of gravity change. and fuel quantity control method is controlled by FQMS(Fuel Quantity Measuring System) and FFP(Fuel Flow Proportioner). This paper presents life cycle extension plans of FFP hydraulic motor by design improvements of connecting and arrangement of pipe comparing with KF-16.

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