Augmentor fuel conduit bushing

F - Mech Eng,Light,Heat,Weapons – 23 – R

Patent

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Details

F23R 3/20 (2006.01) F02C 7/32 (2006.01) F02K 3/10 (2006.01) F16C 33/16 (2006.01)

Patent

CA 2545113

A gas turbine engine augmentor has a centerbody within a gas flowpath from upstream to downstream. A plurality of vanes are positioned in the gas flowpath outboard of the centerbody. An augmentor fuel conduit extends through a first of the vanes to deliver fuel to the centerbody. An electrographitic carbon bushing guides and supports the augmentor fuel conduit.

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