Bifurcated outlet guide vanes

Details Bifurcated outlet guide vanes Bifurcated outlet guide vanes

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 9/02 (2006.01) F01D 5/14 (2006.01)

Patent

CA 2491619

A turbine rear frame (34) includes a row of outlet guide vanes (36) extending between outer and inner bands (38,40). Each of the vanes (36) is bifurcated into a forward prow (44) integrally joined to an aft stern (46) by a septum (48) therebetween. The prow (44) and stern (46) collectively define the aerodynamic profile of each vane which is locally interrupted at the septum (48).

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