COOLING FOR THE RETAINING DOVETAIL OF A TURBOMACHINE BLADE

A turbomachine assembly in which a foil is configured to cover mainly one of bulbs of a disc and to be held, radially with respect to the disc, by the bulb of the disc and a pocket for a blade that can collaborate therewith, when these two are effectively collaborating, and the bulb of the disc incl...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: GENDRAUD ALAIN DOMINIQUE, VARIN BRUNO ANDRE, JEAN, SICARD JOSSELIN, DA COSTA EMMANUEL, MARTET RENAUD
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:A turbomachine assembly in which a foil is configured to cover mainly one of bulbs of a disc and to be held, radially with respect to the disc, by the bulb of the disc and a pocket for a blade that can collaborate therewith, when these two are effectively collaborating, and the bulb of the disc includes at least one longitudinal cavity configured to form, with the foil, when the foil is covering the bulb of the disc, a secondary passage through which a secondary cooling air flow can pass.