A flap and spoiler system (300) of an aircraft wing including a spoiler (304) having a spoiler leading edge and a spoiler trailing edge (310). The flap and spoiler system (300) also includes a flap (306) having a flap leading edge (314) and a flap trailing edge (312), an axis of rotation (322) through the flap, and a top surface portion (332) above the axis of rotation (322). The top surface portion (332) has a first semi-circular shape (334) such that, when the flap (306) rotates about the axis of rotation (322), the spoiler trailing edge (310) remains substantially stationary. When the spoiler trailing edge (310) remains substantially stationary the spoiler is not driven by a spoiler drive.
VARIABLE CAMBER SYSTEM
SYSTEM MIT VARIABLER WÖLBUNG
SYSTÈME DE CAMBRAGE VARIABLE
2019-12-25
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |