Journal of the Korean Society for Aviation and Aeronautics (한국항공운항학회지)

The Korean Society for Aviation and Aeronautics (한국항공운항학회)
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Design Modification of Airframe Shape for Ultra Light Quad-Rotor Development

초소형 쿼드로터 개발을 위한 기체형상 설계변경

  • 박대진 (한국항공대학교 대학원 항공우주 및 기계공학과) ;
  • 이상철 (한국항공대학교 항공우주 및 기계공학부) ;
  • 박생진 (인터켐) ;
  • 송태훈 ((주) 휴인스)
  • Received : 2017.11.30
  • Accepted : 2017.12.28
  • Published : 2017.12.31
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Abstract

An ultra light quad-rotor is utilized in various areas for military and commercial purpose. Especially, the airframe shape is designed with various airframe size, weight and purpose. In this paper, the initial airframe shape of the quad-rotor was designed and manufactured. Flight test was conducted for the quad-rotor. The design modification of airframe shape was conducted to meet design requirement. By changing design, weight of airframe structure was reduced and payloads were placed to the best position. By reinforcing ribs and reducing vehicle's legs, the durability of airframe structure was enhanced.

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References

  1. Kim, J., Ryu, D., Cho, D., Moon, S., "Spherical Flying Machine Control Study", The Korean Society For Aeronautical And Space Sciences, 2012 KSAS Fall Conference, Nov. 2012, pp. 1949-1954
  2. Yang, H., "Status of Industrial Rundon for Private Use and Technology Trends", Korea Multimedia Society, Vol. 20, No. 1-2, Jun. 2016, pp. 1-5
  3. Byun, Y., Lee, J., Lee, K., Gu, T., Song, W., Kang, B., "Re-design of the Coaxial UAV's Platform for an Improvement in Performance", The Korean Society For Aeronautical And Space Sciences, 2007 KSAS Fall Conference, Nov. 2007, pp. 221-224.
  4. Cho, I., "A Case Study for Improving the Manufacturing Process of Composite Main Wing for Small Aircraft", Journal of the Korean Society for Aviation and Aeronautics, Vol. 23, No. 1, Mar. 31. 2015, pp. 96-102 https://doi.org/10.12985/ksaa.2015.23.1.096
  5. Park, D., Lee, S., Park, S., Song, T., "Airframe Structure Design to comply with Design Requirement of Ultra Light Quad-Rotor", The Korean Society for Aviation and Aeronautics, 2017 KSAA Fall Conference, Nov. 24. 2017, pp. 17-19