헬리콥터 테일팬 시험장치 개조 및 운용

Improvement and Operation of a Helicopter Tail-Fan Performance Test System

  • 이제동 (과학기술연합대학원대학교 항공기시스템) ;
  • 송근웅 (한국항공우주연구원 로터그룹) ;
  • 강희정 (한국항공우주연구원 로터그룹) ;
  • 심정욱 (한국항공우주연구원 로터그룹) ;
  • 김승범 (한국항공우주연구원 회전익기개발실)
  • 발행 : 2005.11.17

초록

This paper described improvement and operation of a 'Tail-Fan' anti-torque performance test system KARI (Korea Aerospace Research Institute) developed a 'Tail-Fan' anti-torque system of a helicopter and a performance test-rig to test the performance of the Tail-Fan. The test-rig was improved for full rotating test in 4300rpm(100%). Machinery and hydraulic parts ware changed to reduce vibration and to increase safety. To find the operation rotating speed for the performance test, vibration test were carried out rising accelerometers on tail gear box. The performance test conditions of the Tail-Fan to avoid a resonance were found from vibration test results. The Tail-Fan operation tests were performed safely frier to carry out performance test.

키워드