The present invention relates to an aircraft part comprising: a composite material structure comprising a fibrous reinforcement embedded in a matrix; a heating element (9) configured to heat the part, the heating element (9) being embedded in the matrix of the composite material structure.
DISPOSITIF DE DÉGIVRAGE D'AUBE
BLADE DE-ICING DEVICE
KLINGENENTEISUNGSVORRICHTUNG
2025-01-22
Patent
Electronic Resource
French
European Patent Office | 2017
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