Abstract
This paper describes a piezoelectric microvalve for attitude control of micro-satellite with a mass in the range of 20–100kg. 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 0.6ms. A maximum flow rate of 3100mL/min is achieved at an inlet pressure of 0.6MPa while applied with a maximum voltage of 200V. The static power consumption is 48mW with a driving voltage of 200V, and the dynamic power consumption is approximately 0.9W at 100Hz.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
