This study indirectly measures the vibration value corresponding to the abnormal vibration generated by the small engine for light aircraft to which the dual carburetor is applied by the pressure difference from each carburetor. It relates to a system for outputting a warning to a pilot, comprising two pressure gauges for measuring the pressure from each carburetor and a warning signal output unit for outputting a warning signal corresponding to the pressure difference measured by the two pressure gauges do.
목차
ABSTRACT 1. 서론 1.1 연구배경 1.2 연구목적 및 범위 2. 본론 2.1 항공용 카브레이터 이론 2.2 실험대상 엔진 2.3 진동측정방법 4. 결론 후기 References