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US 2026/0258736 A1Published application
Blade de-icing device
AssigneeSafran Aircraft Engines
InventorsHugo CARTRON, Julien David Alexandre TREBAOL, Henri OUTTRABADY
Life of this patent
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Abstract
An aircraft part includes a composite material structure including a fibrous reinforcement and matrix, the fibrous reinforcement being embedded into the matrix, and heating elements that heat the aircraft part, each of the heating elements being embedded into the matrix of the composite material structure and being distributed across the aircraft part with a density depending on a position in the aircraft part.
Claims12
1-11. (canceled)
An aircraft part comprising:
- a composite material structure comprising a fibrous reinforcement and a matrix, the fibrous reinforcement being embedded into the matrix;
- and
- a plurality of heating elements configured to heat the aircraft part, each of the plurality of heating elements being embedded into the matrix of the composite material structure, the plurality of heating elements being distributed across the aircraft part with a density depending on a position in the aircraft part.
Dependencies are inferred from the claim text.