F - Mech Eng,Light,Heat,Weapons – 23 – R
Patent
F - Mech Eng,Light,Heat,Weapons
23
R
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.
Brooks Robert T.
Harris Meggan H.
Muldoon Marc J.
Sherwood Tor W.
Ogilvy Renault Llp/s.e.n.c.r.l.,s.r.l.
United Technologies Corporation
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