An arrangement for avoiding clashing on a folding wing tip
AssigneeAirbus Operations GmbH
InventorsJack HORWOOD, Paul MORRELL, Matt HARDING
Life of this patent
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AssigneeAirbus Operations GmbH
InventorsJack HORWOOD, Paul MORRELL, Matt HARDING
Estimating the term…
An aircraft wing including a fixed wing and a wing tip device rotatable about a hinge at the tip of the fixed wing is disclosed. The wing further includes a hinged panel at the boundary between the wing tip device and the fixed wing. In the flight configuration the panel is closed such that the panel is substantially flush with the upper surface of the wing, and the hinged panel is located in the path of a moveable element (for example part of an actuation mechanism, such as a curved rack). In the ground configuration the panel is hinged open to a position outside the path of the moveable element such that clashing of the moveable element with the stationary structure at the tip of the fixed wing is avoided.
An aircraft wing, the aircraft wing comprising a fixed wing and a wing tip device rotatable about a hinge at the tip of the fixed wing,
A method of moving a wing tip device from a flight configuration for use during flight, to a ground configuration for use during ground-based operations, in which ground configuration the wing tip device is moved away from the flight configuration such that the span of the aircraft wing is reduced,
A method of moving a wing tip device from a ground configuration for use during ground-based operations, to a flight configuration for use during flight in which flight configuration the wing tip device is moved away from the ground configuration such that the span of the aircraft wing is increased,
A folding wing tip arrangement for an aircraft wing, the arrangement comprising a fixed wing and a rotatable wing tip device at the tip thereof, the wing tip device being configurable by a wing tip actuator between:
Dependencies are inferred from the claim text.