METHOD AND SYSTEM FOR THE REMOVAL OF PARTICULATE MATTER AND HEAVY METALS FROM ENGINE EXHAUST GAS
20170211441 · 2017-07-27
Assignee
Inventors
Cpc classification
B01D53/944
PERFORMING OPERATIONS; TRANSPORTING
F01N2340/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01D53/9418
PERFORMING OPERATIONS; TRANSPORTING
F01N2550/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2590/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2550/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2410/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/0093
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01D53/501
PERFORMING OPERATIONS; TRANSPORTING
F01N3/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N9/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01J35/56
PERFORMING OPERATIONS; TRANSPORTING
Y02T10/40
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B01J21/063
PERFORMING OPERATIONS; TRANSPORTING
B01D2257/60
PERFORMING OPERATIONS; TRANSPORTING
Y02A50/20
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B01D53/9495
PERFORMING OPERATIONS; TRANSPORTING
F01N3/032
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/0233
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2590/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01D53/9477
PERFORMING OPERATIONS; TRANSPORTING
F01N2370/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/106
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/017
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/12
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B01D53/9459
PERFORMING OPERATIONS; TRANSPORTING
F01N13/087
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01D46/71
PERFORMING OPERATIONS; TRANSPORTING
F01N3/2066
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01D2257/404
PERFORMING OPERATIONS; TRANSPORTING
F01N5/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01J35/19
PERFORMING OPERATIONS; TRANSPORTING
F01N13/009
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2570/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01N3/023
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/032
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01J35/00
PERFORMING OPERATIONS; TRANSPORTING
B01J23/652
PERFORMING OPERATIONS; TRANSPORTING
B01D46/00
PERFORMING OPERATIONS; TRANSPORTING
F01N9/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Method and system for removal of soot, ash and heavy metals, and optionally additionally NOx and SOx being present in exhaust gas from an engine operated on heavy fuel oil.
Claims
1. A method for removal particulate matter, hydrocarbons, and heavy metals being present in exhaust gas from an engine operated on heavy fuel oil, comprising the steps of operating the engine at a load to obtain an exhaust temperature of the exhaust gas of at least 325 C.; passing the exhaust gas at exhaust gas temperatures of 325 C. to 550 C. through the at least one filter unit each comprising at least one particulate filter and capturing the particulate matter and heavy metals contained in the exhaust gas; continuously burning the captured soot and adhered hydrocarbons off the at least one particulate filter by contact with a catalyst being arranged on the particulate filter; periodically disconnecting the at least one filter unit from flow of the exhaust gas; applying a pneumatic pulse at the outlet of the at least one particulate filter by pulse injecting air into the outlet in reverse to the previous flow of the exhaust gas and blowing off the captured particulate matter together with the heavy metals from the at least one particulate filter; applying suction at inlet of the at least one particulate filter; and conveying the blown off particulate matter and heavy metals from the at least one particulate filter, optionally through an external auxiliary filter unit, to a container.
2. The method of claim 1, wherein the at least one particulate filter is in form of a wall flow filter.
3. The method of claim 2, wherein the catalyst is coated on or inside the walls of the at least one particulate filter.
4. The method of claim 1, wherein the catalyst comprises of titanium dioxide, oxides of vanadium and tungsten and metallic palladium.
5. The method of claim 1, wherein body of the at least one particulate filter is prepared from silicon carbide, cordierite, mullite, aluminium titanate or sintered metal.
6. The method of claim 1, wherein the air is pulse injected with injection pulse duration of between 10 and 600 msec, preferably 300 msec.
7. The method of claim 1, wherein the air for pulse injection is withdrawn from an accumulator tank with compressed air at a pressure 4 to 10 bar abs, preferably 6.5 bar abs.
8. The method of claim 1, wherein the at least one filter unit is arranged in a pressure vessel upstream an engine turbocharger.
9. The method of claim 8, wherein the exhaust gas is passed through the at least one filter unit at a pressure of between 0 and 3 bar abs.
10. The method according to claim 1, comprising the further step of selective catalytic reduction of nitrogen oxides in the exhaust gas prior to the gas is passed through the at least one filter unit or after the gas has passed through the at least one filter unit.
11. The method according to claim 1, comprising the further step of reducing amounts of sulphur oxides contained in the exhaust gas by scrubbing the gas with an alkaline solution or sea water in an open or closed loop, downstream of the at least one filter unit.
12. A system for removal of particulate matter comprising soot, ash and heavy metals being present in exhaust gas from an engine operated on heavy fuel oil comprising one or more exhaust gas inlet pipes connecting each the engine with inlet of each of one or more filtration units; one or more exhaust gas outlet pipes connected to outlet of each of the one or more filtration units; arranged within the one or more filtration units at least one particulate filter catalyzed with a catalyst for effectuating burning off of soot and hydrocarbons; an air pulse jet arrangement mounted at the outlet of the at least one particulate filter for blowing off the particulate matter collected at the at least one particulate filter; and the air pulse jet arrangement comprises one or more air blow pipes connected to an air supply, nozzles in the air blow pipes and an eductor arranged at the outlet of the at least one particulate filter for pulse injection of air into the at least one particulate filter; and a suction pipe installed close to the inlet of the least one particulate filter, the suction pipe being connected to a suction source.
13. The system of claim 12, wherein the at least one particulate filter is in form of a wall flow filter.
14. The system of claim 13, the at least one particulate filter is coated on walls or inside walls with a catalyst catalysing burning of captured soot of the filters.
15. The system of claim 12, wherein the catalyst consists of titanium dioxide, oxides of vanadium and tungsten and metallic palladium.
16. The system according to claim 12, wherein body of the at least one particulate filter is prepared from silicon carbide, cordierite, or mullite or aluminium titanate or sintered metal.
17. The system of claim 12, wherein the one or more air blow pipes are connected to an accumulator tank with compressed air.
18. The system of claim 12, wherein the one or more filtration units are arranged in a pressure vessel upstream an engine turbocharger.
19. The system of claim 12, wherein the one or more filtration units are arranged downstream an engine turbocharger.
20. The system of claim 12, wherein the one or more exhaust gas outlet pipes connect the one or more filtration units to a downstream selective catalytic reduction unit comprising a denitrification catalyst.
21. The system of claim 12, wherein the one or more exhaust gas inlet pipes connect the one or more filtration units to an upstream selective catalytic reduction unit comprising a denitrification catalyst.
22. The system of claim 12, wherein the one or more exhaust gas outlet pipes connect the one or more filtration units to a scrubber unit.
23. The system of claim 12, wherein a selective catalytic reduction unit comprising a denitrification catalyst unit is connected upstream to the one or more filtration units and downstream to a scrubbing unit.
24. The system of claim 20, wherein the selective catalytic reduction unit is arranged upstream or downstream an engine turbocharger
25. The system of claim 12, further comprising a by-pass pipe by-passing the exhaust gas at least one of the one or more filtration units.
26. The system of claim 12, further comprising one or more auxiliary filter units connected to the suction pipe.
27. The system of claim 12, wherein the air pulse jet arrangement further comprises an isolation valve at outlet of the at least one particulate filter.
28. The system of claim 12, wherein the suction pipe connects an exhaust gas inlet side of the filter unit/s or the particulate filter/s with an exhaust gas outlet side from the filter unit/s or the particulate filter/s.
Description
[0068] A more detailed description of the method and system is apparent from the following description of a specific embodiment with reference to the drawings in which
[0069]
[0070]
[0071] Referring now to
[0072] The filtration unit 4 is divided by a wall 14 into an exhaust gas inlet section 4a and a filtrated exhaust gas outlet section 4b. The unit 4 comprises three particulate filters 16 a,b,c.
[0073] The particulate filters are modular and spaced apart arranged in unit 4, which allows individual regeneration or replacing of spent filters as described below.
[0074] Outlets 18 a, b, c of the particulate filters are lockable and connected to pulse jet cleaning valves 20 a, b, c. The cleaning valves can lock the outlet of the filters sequentially or all at once after a predetermined time on stream or otherwise determined, e.g. by the pressure drop created over the filters. The jet cleaning valves may be connected to an accumulator tank with compressed air (not shown)and provide a pressurized and pulsed air stream with a duration as disclosed above in reverse flow to the previous exhaust gas flow through filters 16a,b,c. By these means, ash and remaining amount of soot together with heavy metals accumulated in the filters are blown off to a discharge sluice 22. During regeneration of filters 4 a,b,c, exhaust gas flow to the actual filtration units, unit 4 in
[0075] The filtration unit 4 is connected to a downstream air compressor 24 of a turbocharger 10 via the engine 2 by an exhaust gas pipe 26. The advantage of such a configuration is described hereinbefore.
[0076] When connected upstream of turbocharger air compressor 24, it is preferred to arrange the filtration unit 4 within a pressure vessel 28 in order to allow the filtration unit to better utilize the pressure drop gain with the same soot load obtained by the pressurized engine exhaust gas. The soot combustion increases with higher temperature that is always present upstream a turbocharger and may eliminate support heating.
[0077] The filtrated exhaust gas is passed from filtration unit 4 in line 32 via exhaust turbine 12 of turbocharger 10 to SCR catalyst unit 6. Prior to be introduced into unit 6, urea is injected into the gas as reductant for the SCR of nitrogen oxides. The SCR reaction and catalysts for use in the reaction are widely disclosed and known in the art and need no further description.
[0078] Finally, the SCR treated exhaust gas in pipe 34 is passed to scrubber unit 8 for the removal of SO.sub.x. In unit 8 the exhaust gas is scrubbed with a diluted alkaline solution, e.g. an aqueous solution of sodium hydroxide wherein the SO.sub.x are converted to sodium sulphite and/or sodium sulphate dissolved in the scrubber solution. The pH value of spent scrubber solution can easily be adjusted to a value around 7 and because heavy metals, soot and ash have been removed from the exhaust gas prior to scrubbing it is possible to distribute spent scrubber solution into the environment with negligible risk thus fulfilling foreseen IMO regulations.
[0079] The thus cleaned exhaust gas is withdrawn from scrubber unit 8 and passed in pipe 36 to an exhaust stack (not shown).
[0080]
[0081] The air pulse jet valve arrangement 20 according to an embodiment of the invention comprises air blow pipes 21a and 21b with air nozzles (not shown) at outlet of the pipes. The air blow pipes are connected through pipe 23 to a pressurized air supply from a compressed air tank (not shown). Valve arrangement 20 comprises further an isolation valve 25 at outlet 18 of a filtration unit 4. The filtration unit 4 is provided with two filters 16a and 16b with outlet pipes 19a and 19b, respectively. The outlet pipes are in form of eductors.
[0082] During filtration operation, the outlet 18 is open and filtered exhaust gas leaving filters 16a and 16b from outlet pipes 19a and 19b is withdrawn through outlet 18.
[0083] In regeneration mode as shown in
[0084] In