Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1991-09-20
1992-09-29
Barefoot, Galen
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
60527, 244 75R, 244 1725, 416 24, B64L 344
Patent
active
051508648
ABSTRACT:
An airfoil camber control apparatus utilizes a cable of shape memory alloy affixed at its ends to a front interior portion of the airfoil. A tensioning system is connected to a rear interior portion of the airfoil and to the cable. When electrical current is applied to the cable to heat it, it returns to its remembered, shorter length, thereby applying tension to the tensioning system to alter the position of the rear portion of the airfoil relative to the front portion.
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Hanagud Sathyanaraya
Roglin Robert L.
Barefoot Galen
Georgia Tech Research Corporation
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