Rotor for a contrarotating turbine of a turbine engine
AssigneeSafran Aircraft Engines
InventorsPatrick Jean Laurent Sultana, Olivier Renon, Laurent Cédric Zamai, Clément Charles Jérémy Coiffier
Life of this patent
Estimating the term…
Loading patent…
AssigneeSafran Aircraft Engines
InventorsPatrick Jean Laurent Sultana, Olivier Renon, Laurent Cédric Zamai, Clément Charles Jérémy Coiffier
Estimating the term…
A rotor for a contrarotating turbine comprising a drum and a blading mounted inside, the drum comprising a hook delimiting a housing having an outer wall and an inner wall, the blading comprising a blade and an outer platform provided with spoiler placed inside the housing, wherein the rotor comprises a foil comprising an elastic inner wing and an outer wing, the outer wing being arranged radially between the spoiler and the outer wall, the inner wing having a first support with the inner wall and a second support with the spoiler, the inner wing being arranged in the housing so as to exert a force on the spoiler so as to press the spoiler against the outer wall via the outer wing.
A rotor for a contrarotating turbine of a turbine engine, comprising:
Dependencies are inferred from the claim text.