VANE FOR AN AIRCRAFT TURBINE ENGINE

A rotor vane for an aircraft turbine engine, the vane having an axis of rotation once it has been rigidly connected to a rotor and a stacking axis. The vane includes a blade extending between an internal platform and an external platform bearing at least one projecting lip. The external platform is...

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Bibliographische Detailangaben
Hauptverfasser: PERSON, Laëtitia, Nicole, LOISEL, Bruno, Marc-Etienne, DELCOIGNE, Eric, Jacques, LIMOUSIN, Franck, Denis, Daniel, DEFLANDRE, Stéphanie, Aline, Marie
Format: Patent
Sprache:eng ; fre ; ger
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