Self-Latching Piezocomposite Actuator
AssigneeU.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
InventorsWILLIAM K. WILKIE, ROBERT G. BRYANT, CHRISTOPHER S. LYNCH
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AssigneeU.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
InventorsWILLIAM K. WILKIE, ROBERT G. BRYANT, CHRISTOPHER S. LYNCH
Estimating the term…
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.
A method of controlling a self-latching piezocomposite actuator having a layer of shape memory ceramic fibers and first and second layers including conductive patterns disposed on opposite sides of the layer of shape memory ceramic fibers, the method comprising:
A method of controlling the shape of a structure capable of defining at least first and second shapes, the method comprising:
A method of controlling a self-latching piezocomposite actuator, the method comprising:
Dependencies are inferred from the claim text.