NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Thin-Layer Composite Unimorph Ferroelectric Driver Sensor PropertiesTests were conducted on 13 different configurations of a new class of piezoelectric devices called THUNDER (thin layer composite unimorph ferroelectric driver and sensor). These configurations consisted of a combination of 1, 3, 5, 7, and 9 layers of 25.4 micron thick aluminium as a backing material, with and without a top layer of 25.4 micrometer aluminum. All of these configurations used the same piezoelectric ceramic wafer (PZT-5A) with dimensions of 5.08 x 3.81 x 0.018 cm. The above configurations were tested at two stages of the manufacturing process: before and after repoling. The parameters measured included frequency, driving voltage. displacement, capacitance, and radius of curvature. An optic sensor recorded the displacement at a fixed voltage(100 - 400 V peak to peak) over a predetermined frequency range (1 - 1000 Hz). These displacement measurements were performed using a computer that controlled the process of activating and measuring the displacement of the device. A parameter alpha was defined which can be used to predict the which configuration will produce the most displacement for a free standing device.
Document ID
19990017742
Acquisition Source
Langley Research Center
Document Type
Reprint (Version printed in journal)
Authors
Mossi, Karla M.
(FACE International Corp. Norfolk, VA United States)
Selby, Gregory V.
(Old Dominion Univ. Norfolk, VA United States)
Bryant, Robert G.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1998
Publication Information
Publication: Materials Letters
Publisher: Elsevier Science Publishers
Volume: 35
ISSN: 0167-577X
Subject Category
Composite Materials
Funding Number(s)
CONTRACT_GRANT: NCA1-326
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available