Combustion device having a distribution plenum
View Patent ↗The combustion device includes a burner, a combustion chamber downstream of the burner, a lance projecting into the burner for fuel and air injection, and a plenum that at least partly houses the burner. The plenum is connected to the inside of the lance to supply an oxidiser to it.
1. A combustion device comprising:
a burner,
a combustion chamber downstream of the burner,
a lance projecting into the burner for fuel and air injection, and
a main distribution plenum, an inner plenum, and an outer plenum that houses the inner plenum and the burner, the inner plenum connected to the burner to supply air to the burner, the outer plenum connected to the lance to supply air to the lance, the main distribution plenum configured to supply air received from a compressor bleed to the outer plenum at a first flow rate, the inner plenum at a second flow rate that is greater than the first flow rate, a first row of turbine vanes downstream of the combustion chamber and an outlet plenum configured to supply air received from the main distribution plenum to outlet guide vanes upstream of the burner;
wherein the main distribution plenum, inner plenum and outer plenum are configured such that a pressure at which air is fed to the lance is higher than a pressure within the inner plenum.
2. The combustion device according to claim 1 , wherein the lance comprises an air duct for the air received from the outer plenum, the lance also comprising at least one fuel duct.
3. The combustion device according to claim 2 , wherein the air duct encircles the at least one fuel duct.
4. The combustion device according to claim 2 , wherein the lance has a portion housed in the inner plenum.
5. The combustion device according to claim 4 , wherein the outer plenum is connected to the inner plenum by a cooling path for the combustion chamber.
6. The combustion device according to claim 2 , wherein the air duct is connected to the outer plenum.
7. The combustion device according to claim 2 , wherein the air duct includes nozzles with sleeves protruding outwardly from the air duct.
8. The combustion device according to claim 7 , wherein the at least one fuel duct includes nozzles, the nozzles for the air duct being substantially coaxial with the nozzles of the at least one fuel duct.
9. The combustion device according to claim 8 , wherein the nozzles of the at least one fuel duct include sleeves protruding outwardly from the at least one fuel duct.
10. The combustion device of claim 1 , wherein the main distribution plenum, the outer plenum, the inner plenum, and the outlet plenum are arranged concentrically surrounding a gas path of the gas turbine.
11. The combustion device of claim 1 , wherein the main distribution plenum is arranged concentrically around the first row of turbine vanes, the outer plenum is arranged concentrically around the combustion chamber and the inner plenum, and the outlet plenum is arranged concentrically around the outlet guide vanes.
12. The combustion device of claim 1 , wherein the main distribution plenum receives air such that a flow velocity of air passing through the outer plenum is kept below 30 m/s.
13. The combustion chamber of claim 12 , wherein the combustion chamber is configured such that a cooling air flow of the air supplied from the main distribution plenum to the inner plenum is passed along a liner of the combustion chamber at a speed of greater than 50 m/s.
14. The combustion device of claim 1 , wherein the main distribution plenum receives air such that a flow velocity of air passing through the outer plenum is kept below 15 m/s.
15. The combustion chamber of claim 14 , wherein the combustion chamber is configured such that a cooling air flow of the air supplied from the main distribution plenum to the inner plenum is passed along a liner of the combustion chamber at a speed of greater than 30 m/s.