A thermally activated paraffin-based actuator for gas-flow control in a satellite electrical propulsion system

摘要

Microstructured silicon devices consisting of three inflatable paraffin-filled, corrugated caddies suspended in springs to minimize thermal losses have been fabricated and evaluated with a valve application in mind. The large volume expansion associated with the thermally induced solid-to-liquid phase transition of paraffin is used to activate the caddies' diaphragms. Theses components all with a thickness of 600 mum and a diameter of 39 mm, but with three different corrugations, have been fabricated with deep reactive etching (DRIE). Whereas the corrugated diaphragms could endure a deflection larger than 50 mum, only strokes of 15 mum on each side were attained when the components were activated. Together with the valve seats proposed, the investigated devices have a potential in electrical propulsion systems for satellites. (C) 2003 Elsevier B.V All rights reserved. [References: 14]