A wing 130 includes a trailing edge 210, and a divergent trailing edge device 240 slideable along an aft surface of the trailing edge 210 between a stowed position and a fully deployed position. The divergent trailing edge device 240 is located entirely within the trailing edge 210 when stowed, and it increases lift over drag of the wing 130 when deployed.
SLIDABLE DIVERGENT TRAILING EDGE DEVICE
VORRICHTUNG MIT VERSCHIEBBARER DIVERGIERENDER AUSTRITTSKANTE
DISPOSITIF DE BORD DE FUITE DIVERGENT COULISSANT
04.12.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |