Abstract: Actuator assemblies are formed by at least one cylinder where each cylinder is formed by at least one piezoelectric fiber composite actuator adapted to have actuation energy applied thereto.
Type:
Application
Filed:
August 3, 2006
Publication date:
May 13, 2010
Applicant:
United States of America as represented by the Admins of the Ntl Aeronautics and Space Admins
Inventors:
Sidney G. Allison, Qamar A. Shams, Robert L. Fox, Christopher L. Fox, Melanie L. Fox Chattin