Compressor rotor blade having a tip with asymmetric lips

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Tined or irregular periphery

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416224, F04D 2938

Patent

active

048758310

ABSTRACT:
A blade of a compressor rotor has its tip provided with at least one discontinuous sealing lip formed by two half lips arranged on opposite sides of the blade asymmetrically with respect to a transverse sectional plane of the blade tip, either with or without overlap of the half lips in the direction of the chord of the blade.

REFERENCES:
patent: 2459850 (1949-01-01), Stine

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