摘要
This paper describes a piezoelectric microvalve for attitude control of micro-satellite with a mass in the range of 20-100 kg. The microvalve comprises of a driving mechanism with a flexure-hinged frame and a valve body with a silicon sealing pair. The silicon valve core with sealing rings can achieve a low leak rate with a small structural deformation. The driving mechanism using a flexure-hinged frame and piezoelectric actuators assures the microvalve normally closed and leads to a fast response of the microvalve. The response time of the driving mechanism is characterized to be as small as 0.6 ms. A maximum flow rate of 3100 mL/min is achieved at an inlet pressure of 0.6 MPa while applied with a maximum voltage of 200 V. The static power consumption is 48 mW with a driving voltage of 200 V, and the dynamic power consumption is approximately 0.9 W at 100 Hz.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 511-518 |
| 页数 | 8 |
| 期刊 | Mechatronics |
| 卷 | 24 |
| 期 | 5 |
| DOI | |
| 出版状态 | 已出版 - 8月 2014 |
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