Gas turbine compressor

Rotary kinetic fluid motors or pumps – Selectively adjustable vane or working fluid control means – Upstream of runner

Reexamination Certificate

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Details

C415S013000, C415S017000, C415S118000, C415S148000

Reexamination Certificate

active

08075253

ABSTRACT:
A gas turbine compressor presents a first fixed stage having a plurality of first adjustable vanes and a further fixed stage, which has an inner ring extending about a first axis; an outer ring arranged about the inner ring and coaxial with the inner ring; and a plurality of second adjustable vanes, each of which extends along a second axis in an essentially radial direction with respect to the first axis between the inner ring and the outer ring; and it is adjustable about the corresponding second axis independently from the first adjustable vanes.

REFERENCES:
patent: 5165845 (1992-11-01), Khalid
patent: 2005/0079046 (2005-04-01), Jolibois et al.
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patent: 2 294 094 (1996-04-01), None
patent: 2 399 865 (2005-05-01), None
patent: 2 410 530 (2005-08-01), None

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