Blade for turbine of turboshaft engine, has upstream spoiler and downstream spoiler including hooks, where hooks are projected to generate axial thrust and include oblique external face presenting groove

The blade has a vane (2) for terminating in a foot (3), where the foot includes an upstream spoiler (4) and a downstream spoiler (5). The upstream spoiler and the downstream spoiler include hooks (7, 8) that are projected to generate axial thrust for rings of a turbine. The hooks include an oblique...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: BASSERY JOSSERAND, DOREMUS SIBYLLE, DUPEYRE RAPHAEL, BOULAY VINCENT
Format: Patent
Sprache:eng ; fre
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