Method for securing a stator assembly

Rotary kinetic fluid motors or pumps – With shaft connected fluid force subjected thrust balancing...

Reexamination Certificate

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C415S136000, C415S137000, C415S207000, C415S209200, C415S211200

Reexamination Certificate

active

07819622

ABSTRACT:
An example exit guide vane for a gas turbine engine is mounted adjacent to a diffuser case defining an air flow path. A thrust balance seal is attached to the diffuser and the exit guide vane is mounted adjacent the diffuser case for guiding air flow into the air flow path. The exit guide vane is mounted adjacent to the diffuser without interfering with the air flow path or restricting thermal expansion.

REFERENCES:
patent: 3067983 (1962-12-01), Koziura
patent: 6517313 (2003-02-01), Rogers
patent: 6916154 (2005-07-01), Synnott
patent: 7121791 (2006-10-01), Friedl et al.
patent: 7300246 (2007-11-01), Durocher et al.
patent: 7329096 (2008-02-01), Tomko et al.

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