항공우주시스템공학회지 (Journal of Aerospace System Engineering)

  • 제9권3호
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  • Pages.1-7
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  • 2015
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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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중소형 무인기 브레이크 시스템용 복합형 지능재료펌프 설계

Design of the Compound Smart Material Pump for Brake System of Small·Medium Size UAV

  • 이종훈 (한국항공대학교 항공우주 및 기계공학과) ;
  • 황재혁 (한국항공대학교 항공우주 및 기계공학과) ;
  • 양지연 (한국항공대학교 항공우주 및 기계공학과) ;
  • 주용휘 (한국항공대학교 항공우주 및 기계공학과) ;
  • 배재성 (한국항공대학교 항공우주 및 기계공학과) ;
  • 권준용 (국방과학연구소 제7기술연구본부)
  • Lee, Jonghoon (Department of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Hwang, Jaihyuk (Department of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Yang, Jiyoun (Department of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Joo, Yonghwi (Department of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Bae, Jaesung (Department of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Kwon, Junyong (The 7th Research and Development Institute, Agency for Defense Development)
  • 투고 : 2015.07.09
  • 심사 : 2015.09.01
  • 발행 : 2015.09.30
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초록

In this study, the design of compound smart materials hydraulic pump that can be applied to a small-medium size UAV having a limited space envelope and weight has been conducted. Compound Smart Material Pump(CSMP) proposed in this paper is composed of a pressurize pump and a flow pump for supplying the high pressure and fluid displacement to overcome the disadvantages of the piezoelectric actuator which has a small strain. Though this compound smart material pump has been designed as small size and lightweight as possible, it can sequentially supply the sufficient large flow rate and pressure required for the brake operation. For the design of CSMP, about 2,700 kg (6,000 lb) class fixed wing manned aircraft was selected. Based on the established requirements, the design of the CSMP have been done by strength, vibration, and fluid flow analysis.

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