능동 비틀림 제어에 용이한 블레이드의 스파형상 선정

  • 배재성 (건국대학교 항공우주정보시스템공학과) ;
  • 신명승 (건국대학교 항공우주정보시스템공학과)
  • Published : 2015.03.19

Abstract

On wide variety of fields, studies on active twist control are becoming more active. For effective twist control, blades have to have low torsional stresses with high torsional deformations to the same magnitude of torque acting on its cross-section. In this study, 2D sectional analysis and 3D finite element analysis were made for 5 different blades with each having different cross - sections which have different spars. The results from 2D sectional analysis, were then put into 3D blade deformation and stress calculations which lead to analysis. Outcomes from 2D and 3D analysis, showed that on the same torque and concentrated load conditions, the blade with 'C' shaped spar was the best of all the blades which were used in this study.

Keywords

Acknowledgement

Supported by : 한국연구재단