Gas turbine

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Vane or deflector

Reexamination Certificate

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Reexamination Certificate

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07410343

ABSTRACT:
An outer shape of a section in the longitudinal direction at a leading edge of the strut is an aerofoil whose thickness is gradually increased along a flow direction of the combustion gas to prevent reduction of turbine efficiency caused by a shock wave generated at the strut of the exhaust diffuser.

REFERENCES:
patent: 3909156 (1975-09-01), Stahl
patent: 4044555 (1977-08-01), McLoughlin et al.
patent: 4076452 (1978-02-01), Hartmann
patent: 4989406 (1991-02-01), Vdoviak et al.
patent: 5609467 (1997-03-01), Lenhart et al.
patent: 6000906 (1999-12-01), Draskovich
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patent: 866 555 (1961-04-01), None
patent: 1 179 009 (1970-01-01), None
patent: 1 222 902 (1971-02-01), None
patent: 4-30348 (1992-07-01), None
patent: 8-100674 (1996-04-01), None
patent: 3165611 (2001-03-01), None

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