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...
Gespeichert in:
Hauptverfasser: | , , , |
---|---|
Format: | Patent |
Sprache: | eng ; fre |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Zusammenfassung: | 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 external face presenting a groove, where the external face presents inclination angle with a longitudinal axis of the blade ranging between 20 and 45 degree. The hooks comprise a trapezoidal shaped section. An independent claim is also included for a method for manufacturing a blade.
L'invention concerne une aube (1) de turbine comprenant une pale (2) se terminant par un pied (3), le pied (3) comprenant : - un becquet amont (4) et un becquet aval (5), - chaque becquet (4, 5) comprenant un crochet (7, 8) en saillie apte à former une butée axiale pour des anneaux (22) de la turbine, caractérisée en ce qu'au moins l'un des crochets (7, 8) comprend une face (16) externe présentant une rainure (17). |
---|