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.
Sistema y método para mejorar el rendimiento de aleta
2022-05-18
Patent
Electronic Resource
Spanish
IPC: | B64C AEROPLANES , Flugzeuge |
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