항공우주시스템공학회지 (Journal of Aerospace System Engineering)

  • 제10권4호
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  • Pages.75-83
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  • 2016
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  • 1976-6300(pISSN)
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  • 2508-7150(eISSN)
항공우주시스템공학회 (The Society for Aerospace System Engineering)
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복합형 무인 회전익기 로터드라이브시스템 개념 연구를 위한 특허 조사 및 분석

Patents Survey and Analysis on a Conceptual Study of Rotor Drive Systems of Combined Unmanned Rotorcraft

  • 투고 : 2016.07.05
  • 심사 : 2016.09.23
  • 발행 : 2016.12.31
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초록

본 연구에서는 복합형 무인 회전익기의 로터드라이브시스템 개발 개념을 정립하기 위해 관련 특허를 조사하고 분석하였다. 특허를 로터드라이브시스템 개발의 관점에서 10개의 유사한 그룹별로 나누어 세부적인 검토 및 분석을 수행하였다. 결과적으로, 특허 분석 결과를 통해 비행체의 로터드라이브시스템 개발 개념을 제안한다.

This paper presents a survey of patents and an analysis of a conceptual study for the development of rotor drive systems in combined unmanned rotorcraft in. The patents were classified into 10 cases with respect to the rotor drive system development, and these are reviewed and analyzed in detail. The results describe development concepts for rotor drive systems for vehicles obtained through the patent analysis.

키워드

참고문헌

  1. Korea Aerospace Research Institute, 2016 Project Plan - Core Technology Study on the Advanced Aircraft, 2016.
  2. Taejin Chang, "Regulatory Environment and Structural Change of UAV Industry," Jouranl of Aerospace System Engineering, Vol. 9, No. 3, pp.17-22, 2015.
  3. Jung-Hoon Lee, "Trade-Off Study of Propulsion Systems Weight Estimation for Tilt-Rotor Personal Air Vehicle," Jouranl of Aerospace System Engineering, Vol. 8, No. 4, pp.1-6, 2014.
  4. Korea Aerospace Research Institute, Development of Personal Air Vehicles (PAV) for Future Aircraft - Advanced Research Report, 2010.
  5. US3722830A, Helicopter Type Vehicle, 1973.
  6. US5791592A, Helicopter with Coaxial Counter-Rotating Dual Rotors and No Tail Rotor, 1998.
  7. US2002/0109044A1, Coaxial Helicopter, 2002.
  8. US6886777B2, Coaxial Helicopter, 2005.
  9. WO2002/064425A2, Coaxial Helicopter with One Cyclic Pitch Control Rotor, 2002.
  10. WO2002/064425A3, Coaxial Helicopter with One Cyclic Pitch Control Rotor, 2003.
  11. WO2002/064425A9, Coaxial Helicopter with One Cyclic Pitch Control Rotor, 2004.
  12. US2006/0102777A1, Coaxial Rotorcraft Control System, 2006.
  13. US2002/0125368A1, Ultralight Coaxial Rotor Aircraft, 2002.
  14. WO2002/064426A1, Ultralight Coaxial Rotor Aircraft, 2002.
  15. WO2003/091099A2, Rotorcraft, 2003.
  16. US2004/0007644A1, Rotor Craft, 2004.
  17. WO2003/091099A3, Rotorcraft, 2004.
  18. US7198223B2, Ultralight Coaxial Rotor Aircraft, 2007.
  19. US2007/0262197A1, Ultralight Coaxial Rotor Aircraft, 2007.
  20. US6460802B1, Helicopter Propulsion and Control System, 2002.
  21. US6540570B1, Counter-Rotating Transmission, 2003.
  22. CA2416479A1, Counter-Rotating Transmission, 2003.
  23. CA2416479C, Counter-Rotating Transmission, 2004.
  24. CA2547534A1, Helicopter, 2005.
  25. WO2005/054053A1, Helicopter, 2005.
  26. US2005/0151005A1, Helicopter, 2005.
  27. US7128293B2, Helicopter, 2006.
  28. CA2547534C, Helicopter, 2013.
  29. US2461348A, Helicopter of the Coaxial Wing Type, 1949.
  30. WO2002/062661A1, A Light Weight Helicopter, 2002.
  31. US2005/0098682A1, Light Weight Helicopter, 2005.
  32. US2005/0211826A1, Lightweight Helicopter, 2005.
  33. US7168656B2, Lightweight Helicopter, 2007.
  34. US2009/0159740A1, Coaxial Rotor Aircraft, 2009.
  35. WO2009/108178A2, Coaxial Rotor Aircraft, 2009.
  36. WO2009/108178A3, Coaxial Rotor Aircraft, 2009.
  37. WO2009/108178A9, Coaxial Rotor Aircraft, 2009.
  38. EP2265495A2, Coaxial Rotor Aircraft, 2010.
  39. US8167233B2, Coaxial Rotor Aircraft, 2012.
  40. EP2265495A4, Coaxial Rotor Aircraft, 2013.
  41. US2006/0231677A1, Rotary-Wing Vehicle System, 2006.
  42. CA2544980A1, Rotary-Wing Vehicle System, 2007.
  43. WO2007/052246A1, Rotary-Wing Vehicle System, 2007.
  44. CN2910313Y, Rotary-Wing Vehicle System, 2007.
  45. CN101007218A, Rotary-Wing Apparatus, 2007.
  46. EP1943001A1, Rotary-Wing Vehicle System, 2008.
  47. CA254480C, Rotary-Wing Vehicle System, 2009.
  48. EP1943001B1, Rotary-Wing Vehicle System, 2010.
  49. DE602006014182D1, Rotary-Wing Vehicle System, 2010.
  50. US7946526B2, Rotary-Wing Vehicle System, 2011.
  51. CN101007218B, Rotary-Wing Apparatus, 2012.