Continuous skin leading edge slats are disclosed. A disclosed example leading edge slat for use with an aircraft includes a single-piece nose skin defining upper and lower external surfaces of the leading edge slat, where the single-piece nose skin is to extend between a fore end and an aft end of the leading edge slat, and a box spar coupled to an inner surface of the single-piece nose skin. The box spar includes lateral walls extending away from the inner surface of the single-piece nose skin. The lateral walls define at least one compartment of the box spar.
CONTINUOUS SKIN LEADING EDGE SLATS
06.05.2021
Patent
Elektronische Ressource
Englisch
ACTUATING MECHANISM FOR TRAILING EDGE FLAPS AND LEADING EDGE SLATS
Europäisches Patentamt | 2019
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