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

The invention relates to a blade sector of a turbine distributor to be carried by a turbine casing (7) of an aeronautical turbine engine, comprising a front connection means (9) and a rear connection means (10), wherein said front connection means (9) is adapted so as to bear against a holder (8) ca...

Ausführliche Beschreibung

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