Combustor and gas turbine including the same
A combustor includes: a casing having an air chamber filled with air; at least one mixing passage forming member forming at least one mixing passage which is connected at an inlet side to the air chamber and at an outlet side to a combustion chamber and having an inlet at the inlet side of the at least one mixing passage so as to communicate with the air chamber; and at least one fuel nozzle disposed inside the air chamber and having a fuel injection hole, positioned upstream of the inlet of the at least one mixing passage forming member, for injecting fuel downstream.
1. A combustor, comprising:
a casing having an air chamber filled with air inside the casing;
a plurality of mixing passage forming members defining a plurality of mixing passages, respectively, each of the plurality of mixing passages being connected at an inlet side to the air chamber and at an outlet side to a combustion chamber, and each of the plurality of mixing passage forming members having an inlet formed at the inlet side of a corresponding mixing passage of the plurality of mixing passages so as to communicate with the air chamber;
a plurality of fuel nozzles disposed inside the air chamber, each of the plurality of fuel nozzles having a fuel injection hole, positioned upstream of the inlet of a corresponding mixing passage forming member of the plurality of mixing passage forming members, for injecting fuel downstream; and
a porous plate separating the air chamber from a fuel chamber, the porous plate having a first opening connecting the air chamber and the fuel chamber, and a second opening, forming the inlet of one of the plurality of mixing passages, connecting the air chamber and the one of the plurality of mixing passages,
wherein:
the casing has the fuel chamber for storing the fuel inside the casing, the fuel chamber being formed between the air chamber and the combustion chamber;
a first fuel nozzle of the plurality of fuel nozzles is adjacent to a second fuel nozzle of the plurality of fuel nozzles;
the fuel injection hole of the first fuel nozzle and the fuel injection hole of the second fuel nozzle are directed to a common inlet of the inlets when viewed from upstream to downstream along an axial direction of the casing,
one of the plurality of fuel nozzles has a bottomed cylindrical shape with a closed terminal end and an open terminal end;
the open terminal end of the one of the plurality of fuel nozzles is connected to the first opening of the porous plate; and
the fuel is to flow from the fuel chamber to the one of the plurality of fuel nozzles via the open terminal end of the one of the plurality of fuel nozzles.
2. The combustor according to claim 1 ,
wherein the fuel injection holes of the plurality of fuel nozzles are arranged at even intervals in a circumferential direction of the common inlet.
3. A gas turbine, comprising:
a combustor;
a compressor for compressing air to be supplied to the combustor; and
a turbine configured to be driven by a combustion gas discharged from a combustion chamber of the combustor,
wherein the combustor comprises:
a casing having an air chamber filled with the air inside the casing;
a plurality of mixing passage forming members defining a plurality of mixing passages, respectively, each of the plurality of mixing passages being connected at an inlet side to the air chamber and at an outlet side to the combustion chamber, and each of the plurality of mixing passage forming members having an inlet formed at the inlet side of a corresponding mixing passage of the plurality of mixing passages so as to communicate with the air chamber;
a plurality of fuel nozzles disposed inside the air chamber, each of the plurality of fuel nozzles having a fuel injection hole, positioned upstream of the inlet of a corresponding mixing passage forming member of the plurality of mixing passage forming members, for injecting fuel downstream; and
a porous plate separating the air chamber from a fuel chamber, the porous plate having a first opening connecting the air chamber and the fuel chamber, and a second opening, forming the inlet of one of the plurality of mixing passages, connecting the air chamber and the one of the plurality of mixing passages,
wherein:
the casing has the fuel chamber for storing the fuel inside the casing, the fuel chamber being formed between the air chamber and the combustion chamber;
a first fuel nozzle of the plurality of fuel nozzles is adjacent to a second fuel nozzle of the plurality of fuel nozzles;
the fuel injection hole of the first fuel nozzle and the fuel injection hole of the second fuel nozzle are directed to a common inlet of the inlets when viewed from upstream to downstream along an axial direction of the casing;
one of the plurality of fuel nozzles has a bottomed cylindrical shape with a closed terminal end and an open terminal end;
the open terminal end of the one of the plurality of fuel nozzles is connected to the first opening of the porous plate; and
the fuel is to flow from the fuel chamber to the one of the plurality of fuel nozzles via the open terminal end of the one of the plurality of fuel nozzles.