Morphing airfoil leading edge

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United States of America Patent

PATENT NO 9598167
SERIAL NO

14196461

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Abstract

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An airfoil may include a leading edge and a shape control mechanism. The leading edge may include a flexible leading edge skin having a first end, a second end, and an arc length defined therebetween. The shape control mechanism may be attached to the flexible leading edge skin at a plurality of support locations and may transition the flexible leading edge skin from a first shape having a first curvature profile to a second shape having a second curvature profile different than the first curvature profile without a change in the arc length.

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Patent Owner(s)

  • THE BOEING COMPANY

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Brown, John J Costa Mesa, US 40 306
Grip, Robert E Rancho Palos Verdes, US 22 175
Harrison, Neal A San Clemente, US 12 66
Rawdon, Blaine K San Pedro, US 32 667
Vassberg, John C Long Beach, US 26 272

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