Control surface for an aircraft
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United States of America Patent
Stats
-
Feb 26, 2002
Grant Date -
Jul 5, 2001
app pub date -
Feb 15, 2001
filing date -
Sep 17, 1997
priority date (Note) -
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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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