System and method for deflecting an aerodynamic control surface
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United States of America Patent
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Nov 19, 2002
Issued Date -
N/A
app pub date -
Mar 5, 2001
filing date -
Mar 5, 2001
priority date (Note) -
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Abstract
According to one embodiment of the invention, a system for deflecting an aerodynamic control surface includes a first piezoelectric actuator coupled to a first flexure member. The first flexure member has a first end coupled to a first surface of the aerodynamic control surface and is operable to amplify a linear motion of the first piezoelectric actuator. The system further includes a second piezoelectric actuator coupled to a second flexure member. The second flexure member has a first end coupled to a second surface of the aerodynamic control surface and is operable to amplify a linear motion of the second piezoelectric actuator.
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