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Hingeless Blade Flexure Bending Stiffness Reinforcement for Whirl Tower Test

훨타워 시험 수행을 위한 무힌지 블레이드 플렉셔 굽힘 강성 보강

  • Received : 2014.02.18
  • Accepted : 2014.04.25
  • Published : 2014.05.01

Abstract

BO-105 helicopter applies hingeless rotor hub system and blade root uses a flexure of hingeless rotor hub system. So bending stiffness reinforcement for flexure was conducted for preparation of whirl tower test using BO-105 blade. Bending moment of flexure area was calculated with FE modeling of section shape for stiffness reinforcement of flexure and thickness of composite material for reinforcement was chosen. Flexure bending stiffness reinforcement was conducted and bending stiffness measurement test was performed before and after bending stiffness reinforcement. And the test data are compared with analysis results.

Acknowledgement

Supported by : 한국항공우주연구원

References

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Cited by

  1. Dynamic Characteristics of Helicopter Bearingless Main Rotor vol.44, pp.5, 2016, https://doi.org/10.5139/JKSAS.2016.44.5.439