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Trend Monitoring of A Turbofan Engine for Long Endurance UAV Using Fuzzy Logic
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  • Trend Monitoring of A Turbofan Engine for Long Endurance UAV Using Fuzzy Logic
  • Trend Monitoring of A Turbofan Engine for Long Endurance UAV Using Fuzzy Logic
저자명
Kong. Chang-Duk,Ki. Ja-Young,Oh. Seong-Hwan,Kim. Ji-Hyun
간행물명
KSAS international journal
권/호정보
2008년|9권 2호|pp.64-70 (7 pages)
발행정보
한국항공우주학회
파일정보
정기간행물|ENG|
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이 논문은 한국과학기술정보연구원과 논문 연계를 통해 무료로 제공되는 원문입니다.
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기타언어초록

The UAV propulsion system that will be operated for long time at more than 40,000ft altitude should have not only fuel flow minimization but also high reliability and durability. If this UAV propulsion system may have faults, it is not easy to recover the system from the abnormal, and hence an accurate diagnostic technology must be needed to keep the operational reliability. For this purpose, the development of the health monitoring system which can monitor remotely the engine condition should be required. In this study, a fuzzy trend monitoring method for detecting the engine faults including mechanical faults was proposed through analyzing performance trends of measurement data. The trend monitoring is an engine conditioning method which can find engine faults by monitoring important measuring parameters such as fuel flow, exhaust gas temperatures, rotational speeds, vibration and etc. Using engine condition database as an input to be generated by linear regression analysis of real engine instrument data, an application of the fuzzy logic in diagnostics estimated the cause of fault in each component. According to study results. it was confirmed that the proposed trend monitoring method can improve reliability and durability of the propulsion system for a long endurance UAV to be operated at medium altitude