An aircraft wing 200 comprises a Krueger flap 215 with an anti-icing system. The anti-icing system comprises a conduit 201 that is configured to provide hot air to an interior surface of the leading edge of the wing 200. The conduit 201 of the anti-icing system structurally supports at least part of the weight of the Krueger flap 215 by means of a support bracket 230. The flap is actuated by a drive shaft 223.
Aircraft wing with anti-icing system and Krueger flap
2021-05-19
Patent
Elektronische Ressource
Englisch
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