A variable camber Krueger flap deployment linkage mechanism is presented. A first linkage assembly couples a flap assembly and an airfoil, and comprising a first drive arm, a first drive link, and a support arm. A second linkage assembly couples the flap assembly and the first drive arm, and comprises a drive transfer arm, a middle connection segment, and a bullnose link.
High-positioned 2-position variable camber Krueger
2016-06-14
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |