An aircraft structural component having an upwardly- or downwardly-extending portion, such as a wing tip or tail fin, comprising one or more outlets for the delivery of anti-icing fluid to a first surface of the aircraft structural component. Anti-icing fluid is delivered through an outlet located at or near the tip of the upwardly-extending portion, or the base of the downwardly-extending portion. The anti-icing fluid thus delivered may, under the influence of gravity, run down the surface of the component, thereby providing the surface of the component with anti-icing fluid.
AIRCRAFT WING OR TAIL ARRANGEMENTS
2025-04-03
Patent
Electronic Resource
English