A system for an aircraft (20) includes a vane (54) and an air system (32). The air system (32) includes a first air circuit (86A) and a first door assembly (88A). The first air circuit (86A) extends in the vane (54) to a first circuit outlet (92A) at a first side (70A) of the vane (54). The first door assembly (88A) is arranged at the first circuit outlet (92A). The air system (32) is configured to exhaust a flow of air out of the first air circuit (86A) through the first circuit outlet (92A) during a first mode and a second mode. The first door assembly (88A) is configured to direct the flow of air exhausted from the first circuit outlet (92A) longitudinally towards a leading edge (66) of the vane (54) during the first mode. The first door assembly (88A) is configured to direct the flow of air exhausted from the first circuit outlet (92A) longitudinally towards a trailing edge (68) of the vane (54) during the second mode.
AIRCRAFT AIRFRAME COMPONENT WITH AIR SYSTEM
FLUGZEUGFLUGWERKKOMPONENTE MIT LUFTSYSTEM
COMPOSANT DE CELLULE D'AÉRONEF AVEC SYSTÈME D'AIR
2025-07-02
Patent
Electronic Resource
English
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