Turbomachine blade fitted with an elastomer gasket
AssigneeSafran Aircraft Engines
InventorsGilles Pierre-Marie NOTARIANNI, Audrey LAGUERRE, Stephane Roger MAHIAS
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Abstract
A turbomachine blade (10) comprising a body (11) and an elastomer gasket (12) fastened to said body (11).
Claims8
A rotor wheel having at least one turbomachine blade, said blade comprising a body and an elastomer gasket fastened to said body, an inter-blade platform adjacent to said blade, the platform presenting a plate that extends circumferentially, whereas, considered in a radial direction, the gasket extends under said plate, the inter-blade platform having a second gasket fastened to the plate, said second gasket being configured to co-operate with said blade, and when considered in the radial direction, the second gasket extends between the gasket of the blade and the plate.
Dependencies are inferred from the claim text.