Anti-wear device for the blades of a turbine distributor in an aeronautical turbine engine

A blade sector of a turbine distributor to be carried by a turbine casing of an aeronautical turbine engine, including a front connection mechanism and a rear connection mechanism, wherein the front connection mechanism is adapted so as to bear against a holder carried by the turbine casing. The sec...

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Bibliographische Detailangaben
Hauptverfasser: DURAND DIDIER NOEL, HERZER ERIC, ROSSI PATRICK JACQUES, BAUMAS OLIVIER JEAN DANIEL
Format: Patent
Sprache:eng
Schlagworte:
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