Sistema y método para mejorar el rendimiento de aleta

A winglet system for an aircraft wing may include an upper winglet and a lower winglet mounted to a wing tip. The lower winglet may have a static position when the wing is subject to a ground static loading. The lower winglet may be configured such that upward deflection of the wing under an approxi...

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Bibliographic Details
Main Authors Roman, Dino L, Vassberg, John Charles, Malachowski, Adam P, Vegter, Christopher A, Friedman, Douglas M
Format Patent
LanguageSpanish
Published 18.05.2022
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:A winglet system for an aircraft wing may include an upper winglet and a lower winglet mounted to a wing tip. The lower winglet may have a static position when the wing is subject to a ground static loading. The lower winglet may be configured such that upward deflection of the wing under an approximate 1-g flight loading causes the lower winglet to move from the static position to an in-flight position and resulting in a relative span increase of the wing.
Bibliography:Application Number: ES20130161307T