Control surface for an aircraft
Number of patents in Portfolio can not be more than 2000
United States of America Patent
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-
Apr 3, 2001
Grant Date -
N/A
app pub date -
Mar 2, 2000
filing date -
Sep 17, 1997
priority date (Note) -
In Force
status (Latency Note)
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Abstract
A control surface (152) for an aircraft has a reinforced elastomer surface (154) on a surface of the aircraft and has a perimeter (156) attached to the aircraft. An actuation mechanism (160) moves the reinforced elastomer surface (154) from a first position, substantially conforming to a moldline of the aircraft, to a second position, protruding from the moldline of the aircraft.
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