항공우주시스템공학회지 (Journal of Aerospace System Engineering)
- 제4권1호
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- Pages.10-14
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- 2010
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- 1976-6300(pISSN)
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- 2508-7150(eISSN)
최신 전투기 사례를 통한 T-50 FFP 시스템 최적 설계 연구
A Study on Optimal design of T-50 Aircraft FFP system through a case of F-16 Aircraft
- 발행 : 2010.03.31
초록
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.