비행시험을 통한 엔진의 혼합기레버 위치 설정에 관한 연구

A Study on Determination for Mixture Lever's Position by Flight Test

  • 김진곤 (한국항공대학교 기계설계학과) ;
  • 김칠영 (한국항공대학교 항공운항학과) ;
  • 이정모 (한국항공대학교 항공운항학과) ;
  • 이정훈 ((주) 대한항공)
  • 발행 : 1995.12.08

초록

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.

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