Bifurcated outlet guide vanes

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

Reexamination Certificate

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C415S211200, C416S09700R

Reexamination Certificate

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06997676

ABSTRACT:
A turbine rear frame includes a row of outlet guide vanes extending between outer and inner bands. Each of the vanes is bifurcated into a forward prow integrally joined to an aft stern by a septum therebetween. The prow and stern collectively define the aerodynamic profile of each vane which is locally interrupted at the septum.

REFERENCES:
patent: 2759663 (1956-08-01), Stalker
patent: 2859910 (1958-11-01), Stalker
patent: 4624104 (1986-11-01), Stroem
patent: 4817378 (1989-04-01), Giffin et al.
patent: 4989406 (1991-02-01), Vdoviak et al.
patent: 5480284 (1996-01-01), Wadia et al.
patent: 6200092 (2001-03-01), Koschier
patent: 6270037 (2001-08-01), Freese et al.
patent: 2003/0059291 (2003-03-01), Koshoffer et al.

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