Method for cleaning process off- or engine exhaust gas
10286360 ยท 2019-05-14
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
F01N3/0232
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01N3/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01D46/00
PERFORMING OPERATIONS; TRANSPORTING
F01N13/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N5/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N9/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/023
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/032
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01J23/652
PERFORMING OPERATIONS; TRANSPORTING
B01J35/00
PERFORMING OPERATIONS; TRANSPORTING
B01J21/06
PERFORMING OPERATIONS; TRANSPORTING
Abstract
Method for removal of soot, ash and metals or metal compounds, together with removal of NOx and SOx being present in process off-gasses or engine exhaust gasses.
Claims
1. A method for the removal of particulate matter in the form of soot, ash, metals and metal compounds, together with hydrocarbons and nitrogen oxides being present in process off-gas or engine exhaust gas, comprising the steps of: providing a process off-gas or engine exhaust gas containing a nitrogenous reductant or adding the nitrogenous reductant to the off- or exhaust gas; passing the off-gas or the exhaust gas at a gas temperature of 225 C. to 550 C. through at least one filter unit each comprising at least one particulate filter and capturing the particulate matter; reducing amounts of soot captured on the at least one particulate filter and reducing amounts of nitrogen oxides and hydrocarbons in the off- or exhaust gas by selective catalytic reduction (SCR) with the nitrogenous reductant and by oxidation in contact with at least a first combined SCR and oxidation catalyst being coated on or inside walls at a gas inlet side of the particulate filter; periodically disconnecting the at least one filter unit from flow of the off- or exhaust gas; applying a pneumatic pulse at an 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 and metal compounds from the at least one particulate filter; and applying suction at the gas inlet side of the at least one particulate filter, and conveying the blown off particulate matter and heavy metals and metal compounds from the at least one particulate filter, optionally through an external auxiliary filter unit, to a container, wherein the at least first combined SCR and oxidation catalyst consists of titanium dioxide, oxides of vanadium and oxides of tungsten, and wherein a second oxidation catalyst is coated at a gas outlet side of the particulate filter, consisting of vanadium oxide and palladium in at least one of metallic form and oxide form, and titania, or consisting of vanadium oxide, tungsten oxide and palladium in at least one of metallic form and oxide form, and titania.
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 1, wherein a body of the at least one particulate filter is prepared from silicon carbide, cordierite, mullite, aluminium titanate or sintered metal.
4. The method of claim 1, wherein the air is pulse injected with an injection pulse duration of between 10 and 600 msec.
5. The method of claim 1, wherein the air for pulse injection is withdrawn from an accumulator tank with compressed air at a pressure of 4 to 10 bar abs.
6. The method of claim 1, wherein the at least one filter unit is arranged in a pressure vessel upstream an engine turbocharger.
7. The method of claim 1, wherein the exhaust gas is passed through the at least one filter unit at a pressure of between 0 and 3 bar abs.
8. The method according to claim 1, comprising the further step of an additional selective catalytic reduction of nitrogen oxides in the off- or exhaust gas downstream of the at least one filter unit.
9. 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 water in an open or closed loop, downstream of the at least one filter unit.
Description
(1) In further an embodiment the V/W/Ti SCR catalyst is coated on the gas inlet side and within the walls of a wall flow filter, while a further catalyst composition consisting of vanadium oxide and palladium in metallic and/or oxidic form and titania or vanadium oxide, tungsten oxide and palladium in metallic and/or oxidic form and titania is coated at the gas outlet side of the wall flow filter.
(2) The advantage of providing the outlet side of the filter with a V/W/Ti/Pd or a V/Ti/Pd catalyst is a lower slip of ammonia and carbon monoxide from the filter.
(3) As mentioned above a further essential feature of invention is removal of trapped particulate matter formed during combustion of the heavy fuel oil. The particulate filters must be cleaned periodically by shutting off the filters from exhaust gas flow.
(4) Preferably, the off- or exhaust gas is passed through more than one filter units. All filter units can then be cleaned in a cyclic cleaning loop by the method according to the invention as described in more detail in the following. The engine can remain in continuous operation because at least one filter unit remains in filtration mode.
(5) During cleaning of the particulate filters, air is injected in reverse to the previous flow of the exhaust gas at an injection pulse duration of between 10 and 600 msec, preferably 300 msec.
(6) In the cleaning cycle, a particulate filter or a section of a filter unit (5-50% of the entire filtering surface) can be closed at the outlet and the air is injected into the outlet by a valve or nozzle e.g. mounted on or near a closing valve. Thereby blowing off particulate matter comprising ash, uncombusted soot and heavy metals, metals, metal compounds trapped in the particulate filter is even more efficiently because of the lower volume the air pulse injected into the particulate filter compared to a manner, where the outlet is open. In the latter case, the air pulse propagates throughout the whole filter unit encasing the particulate filter/s and thus limit cleaning effect.
(7) Alternatively, the outlet of each particulate filter can be open during the cleaning cycle using a more powerful air injection pulse. The advantage of this embodiment is simplicity and a more compact filter arrangement.
(8) During the pneumatic injection pulse into the particulate filter to be cleaned, a cleaning air stream with high concentration of particulate matter exits from the inlet side of the particulate filter and the air stream is captured by a proper suction system. The air stream containing the blown off particulate matter is then conveyed away from the inlet of the particulate filter through a suction pipe, optionally provided with a perforated grid installed at or close to the inlet of the particulate filter. The suction pipe is connected to a suction source e.g. a suction pump, which is activated during or after the air pulse is injected into outlet of the particulate filter.
(9) The particulate matter may be sucked in the suction pipe through an external auxiliary low temperature filter or an auxiliary high temperature filter or both, optionally catalysed with a soot combustion catalyst as described above. Thereby, particulate matter removed from the main particulate filters and contained in the cleaning air stream is separated from the stream in the auxiliary filter/s and then discharged into a storage container for future disposal.
(10) The suction source can be made alternatively by an external suction pump provided with a small auxiliary filter. The auxiliary filter collects the particle carried in the air stream in the suction gas flow line.
(11) Alternatively the suction stream can be also created by utilizing the pressure drop across the particulate filter/s. In this embodiment the suction pipe connects the exhaust gas inlet side of the filter unit/s or the particulate filter/s with the exhaust gas outlet side from the filter unit/s or the particulate filter/s and the particulate matter blown off the particulate filter/s is sucked through an auxiliary filter installed in the suction pipe. When the cleaning cycle is in pause, captured particulate matter can be removed from the auxiliary filter.
(12) The pressure applied in the suction pipe must be low enough to ensure an efficient transport of particulate matter in the suction pipe.
(13) Preferably the pressure in the suction pipe is in the range of 30-300 mbar below the pressure inside the particulate filters.
(14) In further an embodiment of the invention, 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.
(15) In still an embodiment, the unit/s are arranged in a pressure vessel upstream an engine turbocharger. The exhaust gas may then be passed through the filter unit/s at a pressure of between 0 and 3 bar abs.
(16) The soot combustion temperature can in this embodiment be kept at a more optimal level about 400 C. without additional exhaust gas heating. As further an advantage, pressure drop over the particulate filter(s) is decreased when increasing the pressure of the exhaust gas and the temperature. This results advantageously in a diminished particulate filter volume required for effective filtration and facilitates e.g. retrofit installation on ships with limited space for exhaust gas treatment.
(17) A further feature of the invention as disclosed above is the possibility to remove sulphur oxides being formed in process off-gasses and when burning heavy fuel oil in an engine. The upstream SCR and oxidation catalyst in the filters is resistant to sulphur compounds and has a limited SO.sub.2 to SO.sub.3 oxidation potential that therefore facilitates use of a SOX scrubber for SO.sub.2 and SO.sub.3 removal.
(18) Thus, in a further embodiment the method comprises the additional step of reducing amounts of sulphur oxides contained in the gas by scrubbing the gas in an open or closed loop, downstream of the at least one filter unit with a scrubbing liquid comprising an aqueous alkaline solution or an alkaline solution in sea water. In the alkaline scrubbing liquid the sulphur oxides are converted to harmless alkaline metal sulphates or sulphites. The sulphur oxides are thereby almost completely removed from the off gases without any sulphuric acid mist and a clear low turbidity spent solution is stored for later disposal.