CPC F23R 3/28 (2013.01) [F23R 3/002 (2013.01)] | 18 Claims |
1. An assembly for a gas turbine engine, comprising:
a combustor comprising a combustor wall that forms a peripheral boundary of a combustion chamber within the combustor;
a fuel conduit extending along and formed integral with the combustor wall, the fuel conduit disposed outside of the combustion chamber;
a turbine engine case with a plenum formed by and disposed between the turbine engine case and the combustor wall; and
a fuel manifold extending along and formed integral with the turbine engine case, the fuel manifold fluidly coupled with the fuel conduit.
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