An aircraft wing is disclosed having a wing tip device configurable between a flight configuration for use during flight and a ground configuration for use during ground-based operations to reduce the span. The wing includes an actuator and an actuation assembly having an articulation mechanism having a master bell crank connected to the actuator and a slave link connecting the master bell crank with the wing tip device. The slave link is pivoted, at one end, to the master bell crank about a first pivot, and at the other end, to the wing tip device about a second pivot. The master bell crank being pivotably mounted, at its base, about a third pivot.
ARTICULATION MECHANISM FOR FORMING A LOCK TO HOLD A WING TIP DEVICE IN A GROUND CONFIGURATION
2017-05-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Articulation mechanism for forming a lock to hold a wing tip device in a ground configuration
European Patent Office | 2019
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