Paper
9 July 1999 Fin-buffet alleviation via distributed piezoelectric actuators: materials qualification program
Helmut W. Zaglauer, Johannes K. Duerr, Erik Floeth, Elmar Ihler, Ursula Herold-Schmidt, Kay W. Dittrich, John Simpson, Juergen Becker
Author Affiliations +
Abstract
One of the most innovative concepts for active fin-buffet alleviation in vertical tail aircraft is the use of piezoelectric patch actuators distributed across the tail surface to actively induce a counter-strain into the structure. This concept involves the development of a novel material compound structure consisting of a fiber-composite aircraft skin, a ceramic patch actuator and the bonding layer between both components. This actively controllable structure has to provide enough authority to dampen the fin- buffet vibrations. It also has to function reliably during long-term aircraft operation under severe mechanical and environmental load conditions.
© (1999) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Helmut W. Zaglauer, Johannes K. Duerr, Erik Floeth, Elmar Ihler, Ursula Herold-Schmidt, Kay W. Dittrich, John Simpson, and Juergen Becker "Fin-buffet alleviation via distributed piezoelectric actuators: materials qualification program", Proc. SPIE 3674, Smart Structures and Materials 1999: Industrial and Commercial Applications of Smart Structures Technologies, (9 July 1999); https://doi.org/10.1117/12.351565
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CITATIONS
Cited by 3 scholarly publications.
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KEYWORDS
Actuators

Intelligence systems

Composites

Ceramics

Aircraft structures

Failure analysis

Safety

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