Anti-vortex device for a gas turbine engine compressor

Details Anti-vortex device for a gas turbine engine compressor Anti-vortex device for a gas turbine engine compressor

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/06 (2006.01)

Patent

CA 2704595

An anti-vortex device for use in a compressor rotor assembly of a gas turbine engine is described. Spaced-apart radial passageways extend from an axially extending passage provided in a central area of the device to an outer peripheral rim surface thereof. The radial passageways channel air from the primary gaspath about the rotor assembly to the axially extending passage where the air is directed into a central axial passage of the rotor assembly.

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