The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 22, 2017

Filed:

Dec. 16, 2014
Applicant:

The United States of America As Represented BY the Administrator of the National Aeronautics and Space Administration, Washington, DC (US);

Inventors:

William K. Wilkie, Williamsburg, VA (US);

Robert G. Bryant, Williamsburg, VA (US);

Christopher S. Lynch, Sherman Oaks, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
H01L 41/09 (2006.01); H01L 41/08 (2006.01); B64C 3/48 (2006.01); B64C 27/72 (2006.01); F02C 7/042 (2006.01); G02B 26/08 (2006.01);
U.S. Cl.
CPC ...
H01L 41/09 (2013.01); B64C 3/48 (2013.01); B64C 27/72 (2013.01); F02C 7/042 (2013.01); G02B 26/0858 (2013.01); H01L 41/082 (2013.01); B64C 2027/7211 (2013.01); F05D 2260/407 (2013.01); F05D 2300/603 (2013.01); Y02T 50/672 (2013.01);
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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