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NASA NTRS · 20170008517

Self-Latching Piezocomposite Actuator

Abstract

A self-latching piezocomposite actuator includes a plurality of shape memory ceramic fibers. The actuator can be latched by applying an electrical field to the shape memory ceramic fibers. The actuator remains in a latched state/shape after the electrical field is no longer present. A reverse polarity electric field may be applied to reset the actuator to its unlatched state/shape. Applied electric fields may be utilized to provide a plurality of latch states between the latched and unlatched states of the actuator. The self-latching piezocomposite actuator can be used for active/adaptive airfoils having variable camber, trim tabs, active/deformable engine inlets, adaptive or adjustable vortex generators, active optical components such as mirrors that change shapes, and other morphing structures.

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BibTeXRIS

Wilkie, William K., Bryant, Robert G., Lynch, Christopher S.. 2017-08-22. Self-Latching Piezocomposite Actuator. https://ntrs.nasa.gov/citations/20170008517

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