Vibration Analyses and Design of Resonance Avoidance of the Unmanned Helicopter Master

무인 헬리콥터 마스터의 진동해석 및 공진회피 설계

  • Lee, Seong-Chul (Department of Mechanical Engineering, Graduate School of Dong-eui Univ.) ;
  • Son, In-Soo (Department of Mechanical Engineering, Dong-eui Univ.) ;
  • Hur, Kwan-Do (Department of Mechanical Engineering, Dong-eui Univ.)
  • 이성철 (동의대학교 기계공학과 대학원) ;
  • 손인수 (동의대학교 기계공학과) ;
  • 허관도 (동의대학교 기계공학과)
  • Received : 2010.12.10
  • Accepted : 2011.05.03
  • Published : 2011.08.01

Abstract

In this paper, the purpose is to investigate the vibration characteristics and the design of resonance avoidance of the unmanned helicopter master. Based on the Euler-Bernoulli beam theory for helicopter master, the equation of motion is derived by using extended Hamilton's principle. It was studied about the natural frequency of helicopter master as the design variances(tip mass, length and diameter of master). Also, it was compared the theoretical results for natural frequency with the results of FE analysis. The results of this study showed the vibration characteristics of helicopter master for the design of resonance avoidance.

Keywords

References

  1. "2005 UAV Roadmap," Department of Defense, USA, 2005.
  2. Sim, H. C. and Hur, S. S., "Development of a Multipurpose Small-size Unmanned Helicopter," Proc. of KSAS Spring Conference, pp. 184-187, 2008.
  3. Hur, K. D., Kim, K. S. and Chun, S. Y., "Process Design for Yoke Forming of Unmanned Helicopter," Journal of KSMPE, Vol. 8, No. 4, pp. 28-33, 2009.
  4. Chun, J., Byun, Y., Lee, B., Song, W., Kim, J. and Kang, B., "Preliminary Study on Development of Length-variable Rotor Blade for Unmanned Helicopter," Journal of KSPE, Vol. 27, No. 3, pp. 73-79, 2010.
  5. Johnson, W., Yamauchi, G. K. and Watts, M. E., "NASA Heavy Lift Rotorcraft Systems Investigation," Society of Automotive Engineers Transaction, Vol. 114, No. 1, pp. 688-716, 2005.
  6. Igor, A. K. and Olga, I. L., "Formulas for Structural Dynamics," McGraw-Hill, 2001.