Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Reexamination Certificate
2007-06-15
2010-06-29
Collins, Timothy D (Department: 3644)
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
C244S199100, C244S199200, C244S199300
Reexamination Certificate
active
07744038
ABSTRACT:
Systems and methods for providing variable geometry winglets to an aircraft are disclosed. In one embodiment, a winglet includes a base portion configured to attach to a wing. The winglet further includes a body portion. In turn, the body portion includes at least one of a deflectable control surface, a shape memory alloy (SMA) bending plate, and a SMA torque tube. The base portion is configured to attach to the wing such that the body portion projects at an upward angle from the wing.
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PCT Intl Search Report and Written Opinion for Application No. PCT/US2008/064719, dated Apr. 6, 2009, 14 pgs.
Frommer Joshua B.
Sankrithi Mithra M. K. V.
Benedik Justin
Collins Timothy D
Lee & Hayes PLLC
The Boeing Company
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