Gas turbine combustor
View Patent ↗A gas turbine combustor includes a burner disposed upstream of the combustion chamber for supplying a gas and air to an interior of the combustion chamber to hold a flame. The burner is provided with a first swirler in which a gas hole and an air hole are alternately formed in a circumferential direction. A first gas is supplied to the gas hole in the first swirler and air is supplied to the air hole. A swiveling flow path is formed in the gas hole and the air hole in the burner to swivel the gas and the air and supply the gas and the air to the interior of the combustion chamber, a second gas hole is formed in the swiveling flow path in at least one of the air hole and the gas hole, and a second gas is supplied through the second gas hole.
1. A gas turbine combustor having a combustion chamber for mixing a gas and air together to burn the gas, and a burner disposed upstream of the combustion chamber for supplying a gas and air to an interior of the combustion chamber to hold a flame, wherein:
the burner is provided with a first swirler comprising a gas hole and an air hole alternately formed in a circumferential direction thereof;
a first gas from a first gas source is supplied to the gas hole in the first swirler and air is supplied to the air hole; and
a swiveling flow path is formed in the gas hole and the air hole in the burner to swivel the gas and the air and supply the gas and the air to the interior of the combustion chamber, a second gas hole is formed in the swiveling flow path in at least one of the air hole and the gas hole, and a second gas from a second gas source is supplied through the second gas hole.
2. The gas turbine combustor according to claim 1 , wherein:
the first gas is a low BTU gas and the second gas is a high BTU gas.
3. The gas turbine combustor according to claim 1 , wherein:
the burner is provided with a plurality of gas holes in an end surface on an inner circumferential side of the first swirler in a radial direction, and the second gas is supplied to the interior of the combustion chamber through the plurality of gas holes.
4. The gas turbine combustor according to claim 1 , wherein:
the burner is provided with a second swirler in which a gas hole is formed, the second swirler is disposed on an outer circumferential side of the first swirler in a radial direction, the first gas is supplied to the gas hole in the second swirler,
another swiveling flow path is formed in the gas hole in the second swirler, the another swiveling flow path being used to swivel the first gas and supply the first gas to the interior of the combustion chamber.
5. The gas turbine combustor according to claim 4 , wherein:
a third gas hole is formed on an upstream side of the swiveling flow path formed in the gas hole in the second swirler, the third gas hole being used to supply the second gas.
6. The gas turbine combustor according to claim 1 , wherein:
the first gas is a low BTU gas selected from the group consisting of a blast furnace gas, a coal gas, and a biogas; and
the second gas is a high BTU gas selected from the group consisting of an LNG, an LPG, and a butane gas.
7. A gas turbine combustor comprising:
a combustion chamber; and
a burner disposed upstream of the combustion chamber,
wherein the burner comprises a first swirler, the first swirler comprises at least one gas hole and at least one air hole alternately formed in a circumferential direction of the first swirler;
a first gas from a first gas source is supplied to the at least one gas hole in the first swirler and air is supplied to the at least one air hole; and
a swiveling flow path is formed in the at least one gas hole and the at least one air hole in the first swirler to swivel the gas and the air and to supply the gas and the air to the interior of the combustion chamber, a second gas hole is formed in the swiveling flow path in at least one of the at least one air hole and the at least one gas hole, and a second gas from a second gas source is supplied through the second gas hole.
8. The gas turbine combustor according to claim 7 , wherein:
the first gas is a low BTU gas and the second gas is a high BTU gas.
9. The gas turbine combustor according to claim 7 , wherein:
the burner is provided with a plurality of gas holes in an end surface on an inner circumferential side of the first swirler in a radial direction, and the second gas is supplied to the interior of the combustion chamber through the plurality of gas holes.
10. The gas turbine combustor according to claim 7 , wherein:
the burner is provided with a second swirler in which a gas hole is formed, the second swirler is disposed on an outer circumferential side of the first swirler in a radial direction, the first gas is supplied to the gas hole in the second swirler,
another swiveling flow path is formed in the gas hole in the second swirler, and the another swiveling flow path is used to swivel the first gas and to supply the first gas to the interior of the combustion chamber.
11. The gas turbine combustor according to claim 10 , wherein:
a third gas hole is formed on an upstream side of the another swiveling flow path formed in the gas hole in the second swirler, the third gas hole being used to supply the second gas.
12. The gas turbine combustor according to claim 7 , wherein:
the first gas is a low BTU gas selected from the group consisting of a blast furnace gas, a coal gas, and a biogas; and
the second gas is a high BTU gas selected from the group consisting of an LNG, an LPG, and a butane gas.