Control surface for an aircraft
The present invention relates generally to the field of aircraft and more particularly to a control surface for an aircraft. A control surface () for an aircraft has a reinforced elastomer surface () on a surface of the aircraft and has a perimeter () attached to the aircraft. An actuation mechanism...
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| Format: | Patent |
| Sprache: | eng |
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| Zusammenfassung: | The present invention relates generally to the field of aircraft and more particularly to a control surface for an aircraft.
A control surface () for an aircraft has a reinforced elastomer surface () on a surface of the aircraft and has a perimeter () attached to the aircraft. An actuation mechanism () moves the reinforced elastomer surface () 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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