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.
SLIDEABLE DIVERGENT TRAILING EDGE DEVICE
VORRICHTUNG MIT VERSCHIEBBARER DIVERGIERENDER AUSTRITTSKANTE
DISPOSITIF DE BORD DE FUITE DIVERGENT COULISSANT
2018-08-01
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |