대한기계학회논문집A (Transactions of the Korean Society of Mechanical Engineers A)

  • 제31권5호
  • /
  • Pages.625-634
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  • 2007
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  • 1226-4873(pISSN)
  • /
  • 2288-5226(eISSN)
대한기계학회 (The Korean Society of Mechanical Engineers)
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스마트무인기 틸트로터용 짐발허브 설계

Design of Gimbal Hub for Smart UAV Tilt Rotor

  • 발행 : 2007.05.01
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초록

KARI SUAV program was initiated to develop a Smart Unmanned Aerial Vehicle with innovative smart technologies. SUAV is a tilt rotor aircraft of which rotor system is 3-bladed, gimbaled hub type. Several existing concepts of gimbaled hub were analyzed and compared to investigate the applicability to SUAV rotor system design. From the result of these investigations, it was concluded that a new design concept of low cost and high reliability characteristics was necessary for the rotor hub development of SUAV. The design requirements of new gimbal hub concept and the design results were presented. Also, the analysis results to verify the satisfaction of design requirements of SUAV rotor system were presented.

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참고문헌

  1. Nixon, M. W., 1993, 'Aeroelastic Response and Stability of Tiltrotors with Elastically-Coupled Composite Rotor Blades,' PhD. Dissertation, University of Maryland
  2. Nixon, M. W., Langston, C., Singleton, J., Piatak, D., Kvaternik, R., Corso, L., and Brown, R. 2003, 'Aeroelastic Stability of a Four-Bladed Semi-Articulated Soft-Inplane Tiltrotor Model,' Procedding of American Helicopter Society 59th Forum, Phoenix, AZ
  3. Masarati, P., Piatak, D. J., Singleton, J. D., Mantegazza, P., 2004, 'An Investigation of Soft-Inplane Tiltrotor Aeromechanics Using Two Multibody Analyses,' Proceeding of the AHS 4th Decennial Specialists' Conference on Aeromechanics, San Francisco, CA
  4. Masarati, P., Piatak, D. J., Mantegazza, P., Singleton, J. D., 2004, 'Further Results of Soft-Inplane Tiltrotor Aeromechanics Investigation using Two Multibody Analyses,' Procedding of American Helicopter Society 60th Forum, Baltimore, MD
  5. Acree, C. W., Jr., 2002, 'Rotor Design Options for Improving V-22 Whirl Mode Stability,' Proceeding of American Helicopter Society 58th Forum, Quebec, CANADA
  6. Shigley, J. E., 1977, 'Mechanical Engineering Design,' 3rd edition