• 한국전자통신학회논문지
• /
• 제15권6호
• /
• pp.1175-1186
• /
• 2020

본 논문은 전력발전용 가스터빈에 사용하는 내구성이 개선된 Exhaust Gas Temperature(EGT)센서에 관한 연구이다. 가스 터빈에 적용된 EGT 센서는 고온으로 인하여 EGT 센서의 커넥터가 손상되는 문제가 있고 회전 날개의 회전으로 인해 발생하는 심각한 진동 조건에서 센서의 물리적으로 약한 부분이 진동으로 인하여 손상이 야기되기도 한다. 이러한 문제들은 잦은 센서 교체를 유발하고, 발전 효율을 감소시킨다. 본 논문에서는 이러한 문제점들을 분석하고 개선방법을 제시하였고, 제안된 EGT 센서의 성능을 평가하기 위해서, 고온과 진동조건을 동시에 시험할 수 있는 복합 환경 테스트 장비를 개발하였다. EGT센서의 정확도와 응답시간을 평가하고 열과 진동의 복합환경 시험 장비로 비교시험한 결과 기존 센서는 탄화문제가 발생하였지만, 제안된 센서는 이러한 문제가 해결된 것을 확인하였다.

• 한국항공운항학회지
• /
• 제3권1호
• /
• pp.37-47
• /
• 1995

It is very important to determine the performance and operating envelope of engine for aircraft's flight. The basic performance is provided by manufacturer, but installed engine's operating envelop is only determined by flight test. First, this study was measured cylinder head temperature(CHT), exhaust gas temperature(EGT) and oil temperature. At pre-determined altitude and power rate, these temperatures were measured by change of mixture ratio and mixture ratio condition for economic operation and max. power were found. And secondly, with the measured temperatures, possible positions of mixture lever were determined by flight test for stable flight Chang-91 and Lycoming IO-360-A series four cylinders engine with 200 hp was used for this study.

• 한국항공운항학회지
• /
• 제27권4호
• /
• pp.21-26
• /
• 2019

The purpose of this study is to suggest a method for the efficient preventive maintenance of aircraft gas turbine engine turbine blades. For this study, the types and characteristics of gas turbine engines and its turbine blades were studied, the turbine blade defect types that caused an In-Flight Shut Down(IFSD) were analyzed, the blade failure rate according to the blade life cycle was analyzed through the Weibull distribution, one of the statistical techniques. Through these research results, it is possible to supplement the problems of the life cycle management and maintenance method of the turbine blade, and to suggest the measures to strengthen the preventive maintenance of the turbine blade. In this analysis, when total cycle of turbine blade exceeds 18,000 cycles, the failure rate is over 98%, and then the special management measures are required.