Invention Grant
US08827650B2 Seal for a platform in the rotor of a turbine engine 有权
用于涡轮发动机转子平台的密封

Seal for a platform in the rotor of a turbine engine
Abstract:
A seal for an intermediate platform provided between two adjacent blades in the rotor of a turbine engine, the seal having an elongate shape with an upstream end and a downstream end, and including transversally, in the direction of the width thereof, a contact portion, an attachment portion, and a flexible portion between the attachment portion and the contact portion. The cross section of the seal has an open-ended shape between the two ends thereof.
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