Safran Aircraft Engines

Francois Pierre Georges Maurice Ribassin

Romain Nicolas Lunel

Christophe Pieussergues

Haris Musaefendic

Guillaume Aurelien Godel

An air intake swirler for a turbomachine injection system includes an upstream wall and a downstream wall, both of revolution about an axis of the air intake swirler, and fins distributed about the axis and connecting the upstream wall to the downstream wall so as to delimit, between the upstream wall and the downstream wall, air inlet channels each having an inlet and an outlet. The swirler includes two aerodynamic deflectors that respectively extend the downstream walls radially outward and that have a concavity oriented upstream. The aerodynamic deflectors extend radially facing the respective inlets of the air inlet channels and thus make it possible to limit the loss of pressure of the air supplied to the air inlet channels.

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Mennecy, France

Francois Pierre Georges Maurice Ribassin