Platform seal in a turbomachine rotor, method for improving the seal between a platform and a turbomachine blade
AssigneeSnecma
InventorsJean-Bernard Forgue, Patrick Jean-Louis Reghezza, Carole Stochmil
Life of this patent
Estimating the term…
Loading patent…
AssigneeSnecma
InventorsJean-Bernard Forgue, Patrick Jean-Louis Reghezza, Carole Stochmil
Estimating the term…
An elastomer material seal for an interleaved platform between two adjacent blades in a turbomachine rotor is disclosed. The seal is of elongate shape and includes transversely a contact part, an attachment part, and a flexible part between the attachment part and the contact part. The seal is noteworthy in that it further includes a local reinforcement of the flexible part, to avoid the tearing that would result from centrifugal forces on the seal. The local reinforcement of the flexible part includes at least one transverse rib on the flexible part.
An elastomer material seal for an interleaved platform between two adjacent blades in a turbomachine rotor, of elongate shape with an upstream edge and a downstream edge, the seal including an upstream zone and a downstream zone between the upstream and downstream edges, the seal comprising transversely, in the widthwise direction:
A method for improving the seal between a platform and a blade of a turbomachine rotor provided by a seal of elongate shape extending in an upstream to downstream direction so as to present an upstream zone and a downstream zone between an upstream edge and a downstream edge, and comprising transversely, in the widthwise direction, a contact portion which is circular or oval, an attachment portion, and a flexible portion between the attachment portion and the contact portion, the method comprising:
Dependencies are inferred from the claim text.