Intentionally mistuned integrally bladed rotor

Fluid reaction surfaces (i.e. – impellers) – Unsymmetrical impeller or dissimilar working members

Reexamination Certificate

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Details

C416S234000, C416S500000, C415S119000

Reexamination Certificate

active

08043063

ABSTRACT:
A frequency mistuned integrally bladed rotor (IBR) for a gas turbine engine comprises a hub and a circumferential row of blades of varying frequency projecting integrally from the hub. Each blade in the row alternate with another blade having a different pressure surface definition but similar suction surface, leading edge and trailing edge definitions.

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