Safran Aircraft Engines

Safran

Lola Auliac

Thibaut Dominique Augustin Girard

Jérémy Guivarc'h

Pierre Jean Faivre D'arcier

Jérémy Philippe Pierre Edynak

Jeremy Guivarc'h

Pierre Faivre D'Arcier

Jeremy Philippe Pierre Edynak

The invention relates to a fan rotor for a turbomachine, including a fan disk, fan blades with a leading edge and a trailing edge, platforms inserted between the blades and fixed to the periphery of the disk, each including an aerodynamic surface extending from the leading edges to the trailing edges of the blades. The aerodynamic surface includes an upstream longitudinal portion on the side of the leading edges and a downstream longitudinal portion on the side of the trailing edges, the upstream longitudinal portion being supported by a first member of the platform fixed to the disk in a pivotable manner, and the downstream longitudinal portion being independent of the upstream longitudinal portion and supported by a second member of the platform which is independent of the first member and fixed to the disk in a pivotable manner.

Turbomachine fan rotor

Seal () for an inter-blade platform intended to extend circumferentially about an axis and to be mounted between two axial ends of the inter-blade platform, including a first part () in contact with a first blade adjacent to a first circumferential end of the platform, and a second part () in contact with a second blade adjacent to a second circumferential end of the platform, the first part () and the second part () of the seal () being fixed to each other such that a displacement in the circumferential direction of one of the two parts () of the seal () causes a displacement of the other part () of the seal () in the same direction, when the two parts () of the seal () are fixed to each other.

Inter-blade platform seal

Growing community of inventors

Moissy-Cramayel, France

Lola Auliac