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Development of a Peristaltic Micropump with Lightweight Piezo-Composite Actuator Membrane Valves
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  • Development of a Peristaltic Micropump with Lightweight Piezo-Composite Actuator Membrane Valves
  • Development of a Peristaltic Micropump with Lightweight Piezo-Composite Actuator Membrane Valves
저자명
Pham. My,Goo. Nam-Seo
간행물명
International journal of aeronautical and space sciences
권/호정보
2011년|12권 1호|pp.69-77 (9 pages)
발행정보
한국항공우주학회
파일정보
정기간행물|ENG|
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이 논문은 한국과학기술정보연구원과 논문 연계를 통해 무료로 제공되는 원문입니다.
서지반출

기타언어초록

A peristaltic micropump with lightweight piezo-composite actuator (LIPCA) membrane valves is presented. The micropump contained three cylinder chambers that were connected by microchannels and two active membrane valves. A circular miniature LIPCA was developed and manufactured to be used as actuating diaphragms. The LIPCA diaphragm acted as an active membrane valve that alternate between open and closed positions at the inlet and outlet in order to produce high pumping pressure. In this LIPCA, a lead zirconium titanate ceramic with a thickness of 0.1 mm was used as an active layer. The results confirmed that the actuator produced a large out-of-plane deflection. During the design process, a coupled field analysis was conducted in order to predict the actuating behavior of the LIPCA diaphragm; the behavior of the actuator was investigated from both a theoretical and experimental perspective. The active membrane valve concept was introduced as a means for increasing pumping pressure, and microelectromechanical system techniques were used to fabricate the peristaltic micropump. The pumping performance was analyzed experimentally in terms of the flow rate, pumping pressure and power consumption.