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Development of Test Simulator for Developing Fuel Quantity Measurement System for Supersonic Jet Trainer Conformal Fuel Tank

초음속항공기 보조연료탱크 연료량측정시스템 개발용 모사시험장치 개발

  • 김봉균 (한국항공대학교 대학원 항공우주 및 기계공학과) ;
  • 박대진 (한국항공대학교 대학원 항공우주 및 기계공학과) ;
  • 전현우 (한국항공대학교 대학원 항공우주 및 기계공학과) ;
  • 이상철 (한국항공대학교 항공우주 및 기계공학부)
  • Received : 2018.06.17
  • Accepted : 2018.06.30
  • Published : 2018.06.30

Abstract

A test simulator is needed to develop a fuel quantity measurement system that takes into account the roll and pitch motion of the aircraft. In this paper, we develop a test simulator that consists of attitude simulation equipment, fueling equipment, and data storage equipment. The attitude simulation equipment simulates the aircraft attitude. It is manufactured to operate pitch angle and roll angle movement. The fueling equipment supplies fuel to the supplementary fuel tank. The data storage equipment collects and stores the measured data. We also develop an automation software that operates the test simulator and collects data automatically. The test simulator has been automated to prevent testers from being exposed to toxic fuel. Through automation software, the collection period is reduced by one quarter compared to manual collection. The developed fuel quantity measurement system is verified through the test simulator.

Keywords

References

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