GUIDE VANES ASSEMBLY WITH POSITION-MAINTAINING DEVICE

A turbine engine nozzle extending about an axis and including a vane assembly mounted between an outer shroud and an inner shroud; and a position retaining device configured to be placed in an elastically prestressed state between the inner shroud and an inner platform of the vane assembly to apply...

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Bibliographische Detailangaben
Hauptverfasser: JARROSSAY, Clément, GAILLARD, Aurélien, CONGRATEL, Sébastien Serge Francis, LE CAIR, David René Pierre, GIMAT, Matthieu Arnaud
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A turbine engine nozzle extending about an axis and including a vane assembly mounted between an outer shroud and an inner shroud; and a position retaining device configured to be placed in an elastically prestressed state between the inner shroud and an inner platform of the vane assembly to apply a stress on the vane assembly towards the outer shroud. The contact between the inner shroud and the inner platform is obtained by one same surface of the position retaining device.