Title :
An electrohydrodynamically driven microfabricated actuator for the study of miniature ion propulsion engine and electric wind devices
Author :
Chua, B.L. ; Logeeswaran, V.J. ; Chan, M.L. ; Park, H.K. ; Horsley, D.A. ; Tien, N.C.
Author_Institution :
Dept. of Electr. & Comput. Eng., California Univ., Davis, CA, USA
Abstract :
For the study of miniature ion propulsion engine and electric wind devices, we have developed an electrohydrodynamically (EHD) driven microfabricated actuator. It consumes a maximum power of 100 mW and has a maximum resultant driving force of 0.45 μN in the first observed driving mode. The actuator consists of a mass/spring configuration fabricated with dual ion drives for propulsion. DC partial electrical discharge produces and accelerates the ions. Electric wind is generated by the momentum transfer from the ions to the air. Momentum is also transferred by virtue of the formation of intermittent space charge near the ionization zone. A selection between single and dual ion drives allows observation of various oscillation modes beginning at 896 Hz. The maximum out-of-plane oscillation amplitude measured was approximately 2 μm.
Keywords :
electrohydrodynamics; ion engines; microactuators; momentum; partial discharges; space charge; 100 mW; 2 micron; 896 Hz; DC partial electrical discharge; EHD; dual ion drives; electric wind devices; electrohydrodynamic propulsion; electrohydrodynamically driven actuator; engine oscillation modes; ion/air momentum transfer; ionization zone intermittent space charge; maximum driving force; microfabricated actuator; microfabricated suspended mass/spring system; miniature ion propulsion engine; Acceleration; Actuators; Aerospace engineering; Corona; Electrodes; Electrohydrodynamics; Engines; Micromotors; Propulsion; Space charge;
Conference_Titel :
Solid-State Sensors, Actuators and Microsystems, 2005. Digest of Technical Papers. TRANSDUCERS '05. The 13th International Conference on
Print_ISBN :
0-7803-8994-8
DOI :
10.1109/SENSOR.2005.1496392
