Exhaust duct for a fossil fuel powered engine comprising a dilution selective catalytic reduction system
An exhaust duct for a fossil fuel powered engine includes an exhaust gas passage, a cooling fluid passage, a mixing device for mixing cooling fluid with the hot exhaust gas and a selective catalytic reduction catalyst for removing nitrogen oxides arranged in the exhaust gas passage. The mixing device has a mixing chamber with a first wall and an opposed second wall, the first and second wall arranged upstream of the selective catalytic reduction catalyst in the exhaust gas passage and extending over the cross-sectional area of the exhaust gas passage, both walls perforated by through holes, wherein through holes of the first wall are connected with through holes of the second wall in pairs by pipes extending through the mixing chamber, the pipes perforated by at least one hole into the mixing chamber and the cooling fluid passage ending into the mixing chamber.
1. An exhaust duct, for an engine, the exhaust duct comprising:
an exhaust gas passage carrying exhaust gas,
a cooling fluid passage carrying a cooling fluid,
a mixing device for mixing the cooling fluid with the exhaust gas,
at least a selective catalytic reduction catalyst arranged in the exhaust gas passage for removing nitrogen oxides, and
at least one injection nozzle to supply a reducing agent,
wherein the mixing device comprises a mixing chamber with a first wall and an opposed second wall, the first and second wall arranged upstream of the selective catalytic reduction catalyst in the exhaust gas passage and extending over an entire cross-sectional area of the exhaust gas passage, both walls perforated by through holes, wherein the through holes of the first wall are connected with the through holes of the second wall in pairs by pipes extending through the mixing chamber, the pipes are each perforated by at least one hole into the mixing chamber and the cooling fluid passage ending into the mixing chamber.
2. The exhaust duct according to claim 1 , wherein the at least one injection nozzle to supply the reducing agent are arranged such that the reducing agent is supplied into the exhaust duct.
3. The exhaust duct according to claim 2 , wherein the at least one injection nozzle to supply the reducing agent is adapted for supplying the reducing agent comprising a urea component and/or an ammonia component.
4. The exhaust duct according to claim 1 , wherein the at least one injection nozzle to supply the reducing agent further comprises several injection nozzles to supply the reducing agent.
5. The exhaust duct according to claim 1 , wherein the pipes of the mixing chamber each comprise inside at least one turbulator for increasing the turbulence of the exhaust gas flowing through the pipes.
6. The exhaust duct according to claim 1 , wherein the sum of a cross-sectional area of the through holes in the first and second wall are adapted to keep a pressure drop between an inlet of the exhaust gas passage and a downstream exit of the exhaust gas passage less or equal than 25 mbar.
7. The exhaust duct according to claim 6 , wherein the sum of the cross-sectional area of the through holes is 25% of a surface area of the first and second wall.
8. The exhaust duct according to claim 1 , wherein openings of the through holes through the first and second wall are uniformly distributed on a surface of the first and second wall.
9. The exhaust duct according to claim 1 , wherein the first wall guides the exhaust gas upstream thereof into the pipes, and wherein in the pipes the exhaust gas mixes with the cooling fluid that enters each pipe via a respective hole of the at least one hole.
10. The exhaust duct according to claim 9 , wherein the first wall directs all of the exhaust gas in the exhaust gas passage into the pipes.
11. The exhaust duct according to claim 9 , wherein the first wall fluidically separates the exhaust gas in the exhaust gas passage from the cooling air in the mixing chamber.
12. The exhaust duct according to claim 11 , wherein the first wall and the second wall define a volume therebetween and within the exhaust gas passage, wherein the pipes are disposed within the volume, and wherein the volume provides fluid communication between the cooling fluid passage and the pipes.
13. The exhaust duct according to claim 1 , wherein during operation a static pressure in the pipes is less than a static pressure in the mixing device which thereby causes the cooling fluid to be sucked from the mixing chamber into the pipes.
14. The exhaust duct according to claim 13 , wherein an amount of the cooling fluid sucked into the pipes varies according to a velocity of the exhaust gas in the pipes.
15. The exhaust duct according to claim 1 , wherein the at least one injection nozzle to supply the reducing agent is adapted to spray the reducing agent.
16. The exhaust duct according to claim 15 , wherein the at least one injection nozzle to supply the reducing agent is adapted to spray the reducing agent as a liquid.
17. The exhaust duct according to claim 15 , wherein the at least one injection nozzle to supply the reducing agent is adapted to spray the reducing agent as a vapor.
18. The exhaust duct according to claim 1 , wherein the engine is a fossil fuel powered engine.
19. A power plant comprising:
a gas turbine, and
an exhaust duct for an engine, the exhaust duct comprising
an exhaust gas passage carrying exhaust gas,
a cooling fluid passage carrying a cooling fluid,
a mixing device for mixing the cooling fluid with the exhaust gas,
at least a selective catalytic reduction catalyst arranged in the exhaust gas passage for removing nitrogen oxides, and
at least one injection nozzle to supply a reducing agent,
wherein the mixing device comprises a mixing chamber with a first wall and an opposed second wall, the first and second wall arranged upstream of the selective catalytic reduction catalyst in the exhaust gas passage and extending over an entire cross-sectional area of the exhaust gas passage, both walls perforated by through holes, wherein the through holes of the first wall are connected with the through holes of the second wall in pairs by pipes extending through the mixing chamber, the pipes are each perforated by at least one hole into the mixing chamber and the cooling fluid passage ending into the mixing chamber.
20. The power plant according to claim 19 , wherein the gas turbine comprises a simple cycle gas turbine.
21. A mixing chamber for an exhaust duct of an engine for mixing cooling fluid with exhaust gas, the mixing chamber comprising:
a first wall and an opposed second wall and at least one entrance for a cooling fluid passage of the exhaust duct,
the first wall and second wall arranged in an exhaust gas passage of the exhaust duct and extending over an entire cross-sectional area of the exhaust gas passage,
the first and second wall both perforated by through holes, wherein the through holes of the first wall are connected with the through holes of the second wall in pairs by pipes extending through the mixing chamber, the pipes are each perforated by at least one hole into the mixing chamber.
22. The exhaust duct according to claim 21 , wherein the engine is a fossil fuel powered engine.