Harvest IP Law, LLP
Combustor and gas turbine including the same
A combustor and a gas turbine capable of stably supporting a fuel peg and guiding the flow of air are provided. The combustor may include: a plurality of nozzles configured to eject fuel and air; a flow passage configured to guide a flow of air to be drawn into the nozzles; a plurality of fuel pegs configured to protrude into the flow passage, each of the plurality of fuel pegs including an injection hole through which fuel is discharged; and a peg support configured to be coupled to the fuel pegs to support the fuel pegs.
F F F F F F F
F05D F23R F05D F23R F02C F23R F02C
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Heonseop
Jin