Safran Aircraft Engines

Dimitri Germinal Soteras

Tony Alain Roger Joël Lhommeau

Clément René Roger Sirot

Alain Laurent Christian Vitalis

A blade for a turbomachine fan, the blade being made from a composite material containing a plurality of longitudinal conductive fibres embedded in an electrically non-conductive matrix, the blade having at least one fastening region to which an identification medium for identifying the blade is fastened, the fastening region containing longitudinal fibres oriented along a preferred fibre axis, the identification medium contains an item of identification data for identifying the blade and at least one radio antenna having at least one communication lobe configured so as to receive a read request and transmit the item of identification data in return, the communication lobe being oriented along a radio axis that is angularly offset from the preferred fibre axis by less than 45°, preferably by less than 22.5°.

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Moissy-Cramayel, France

Dimitri Germinal Soteras