Journal of the Korean Society for Aeronautical & Space Sciences (한국항공우주학회지)

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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On the Performance Test of the Piezoelectric-Hydraulic Pump

압전유압펌프 성능실험에 대한 연구

  • Joo, Yong-Hwi (Department of Aerospace and Mechanical Engineering, Graduate School at KAU) ;
  • Hwang, Jai-Hyuk (Department of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Yang, Ji-Youn (Department of Aerospace and Mechanical Engineering, Graduate School at KAU) ;
  • Bae, Jae-Sung (Department of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Lee, Jong-Hoon (The 7th Research and Development Institute, Agency for Defense Development) ;
  • Kwon, Jun-Yong (The 7th Research and Development Institute, Agency for Defense Development)
  • Received : 2015.08.06
  • Accepted : 2015.08.18
  • Published : 2015.09.01
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Abstract

In this paper, the piezoelectric-hydraulic pump with a piezostack actuator as a driving source has been designed, fabricated, and evaluated for its application to UAV's brake system. The performance requirements of the piezoelectric-hydraulic pump were decided based on the requirements analysis of the target aircraft brake system. The geometric design of the piezoelectric-hydraulic pump to meet the performance requirements of the pump was conducted, and all components of the pump including the spring sheet type check valves were machined with close tolerance. By constructing a test apparatus for the performance check of the piezoelectric-hydraulic pump, the performance characteristics of the pump, such as the outlet flow rate for load-free condition and the outlet oil pressure for closed loop condition, have been evaluated. It has been found by the performance test result that the developed piezoelectric-hydraulic pump satisfies the design requirements effectively.

본 논문에서는 압전재료를 이용하여 중소형 무인기 브레이크 시스템에 적용 가능한 압전유압펌프를 설계 및 제작하고, 제작된 압전유압펌프의 성능검증 실험을 수행하였다. 중소형 무인기급 목표 항공기를 선정하여 브레이크 시스템의 요구조건을 분석하였으며, 이를 바탕으로 압전유압펌프의 성능 요구조건을 선정하였다. 요구조건을 만족하는 압전유압펌프의 형상설계를 수행하였으며, 고속 동작 조건에서도 유체의 역류를 효과적으로 차단시킬 수 있는 체크밸브를 비롯한 모든 구성품을 제작하였다. 제작된 압전유압펌프의 성능검증을 위해 실험장치를 구성하여 무부하 토출특성, 부하 시 압력형성 특성실험을 수행하였다. 실험결과, 무부하 최대 토출유량은 80 Hz에서 120.04 cc/min이고, 부하 시 최대 토출압력은 140 Hz에서 783.17 psi이고, 압력형성 반응속도는 약 30 ms 이내임을 확인하였다. 이는 설계 제작된 압전유압펌프가 펌프성능 요구조건을 충족하고 있다고 판단된다.

Keywords

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