Honeycomb catalyst structure and SCR device
12025044 ยท 2024-07-02
Assignee
Inventors
Cpc classification
F01N3/206
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/0814
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/2066
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2370/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/281
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/0871
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01J35/56
PERFORMING OPERATIONS; TRANSPORTING
B01J29/085
PERFORMING OPERATIONS; TRANSPORTING
B01J21/06
PERFORMING OPERATIONS; TRANSPORTING
F01N2590/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/2828
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01N3/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01J21/06
PERFORMING OPERATIONS; TRANSPORTING
B01J29/08
PERFORMING OPERATIONS; TRANSPORTING
B01J35/56
PERFORMING OPERATIONS; TRANSPORTING
F01N3/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The honeycomb catalyst structure to be used for exhaust gas of a marine engine includes an SCR catalyst supported on a metal honeycomb unit having a shape divided by cell walls into a plurality of cells extending from one end face to the other end face. The SCR catalyst contains TiO2 alone, or contains TiO2 as a principal component and any one type or two or more types of V2O5, WO3, MoO3, SiO2, and Al2O3 in combination. The cell density of the plurality cells is 100 to 500 cpsi, and the slope of a straight line represented by a relationship between the flow velocity and the pressure loss of the exhaust gas passing through the cells is 30 or more and 180 or less.
Claims
1. A honeycomb catalyst structure to be used for exhaust gas of a marine engine, comprising a selective catalytic reduction (SCR) catalyst supported on a metal honeycomb unit having a shape divided by cell walls into a plurality of cells extending from one end face to the other end face along a longitudinal direction, wherein: the SCR catalyst supported on the metal honeycomb unit contains TiO.sub.2 alone, or contains TiO.sub.2 as a principal component and any one type or two or more types of V.sub.2O.sub.5, WO.sub.3, MoO.sub.3, SiO.sub.2, and Al.sub.2O.sub.3 in combination, a cell density of the plurality of cells is 100 to 500 cpsi, and a slope of a straight line represented by a relationship between a flow velocity of the exhaust gas passing through the plurality of cells and a pressure loss is 30 or more and 180 or less.
2. A honeycomb catalyst structure to be used for exhaust gas of a marine engine, comprising a selective catalytic reduction (SCR) catalyst supported on a metal honeycomb unit having shape divided by cell walls into a plurality of cells extending from one end face to the other end face along a longitudinal direction, wherein: a material of the metal honeycomb unit is an alloy containing Fe as a principal component, Cr at 15 to 20 wt %, and Al at 2 to 5 wt %, the SCR catalyst supported on the metal honeycomb unit contains TiO.sub.2 alone, or contains TiO.sub.2 as a principal component and any one type or two or more types of V.sub.2O.sub.5, WO.sub.3, MoO.sub.3, SiO.sub.2 or Al.sub.2O.sub.3 in combination, a cell density of the plurality of cells is 100 to 500 cpsi, and a slope of a straight line represented by a relationship between a flow velocity and a pressure loss of the exhaust gas passing through the plurality of cells is 30 or more and 180 or less.
3. An SCR device comprising the honeycomb catalyst structure of claim 2, wherein the honeycomb catalyst structure is integrated into the marine engine.
4. An SCR device comprising the honeycomb catalyst structure of claim 1, wherein the honeycomb catalyst structure is integrated into the marine engine.
Description
BRIEF DESCRIPTION OF DRAWINGS
(1)
(2)
(3)
(4)
(5)
(6)
(7)
DESCRIPTION OF THE PREFERRED EMBODIMENTS
(8) An embodiment of the present invention will now be described with reference to the drawings.
(9) An SCR device of the present invention includes a honeycomb catalyst structure having a unique configuration of the present invention, in which an SCR catalyst is supported on a metal honeycomb unit having a shape divided by cell walls into a plurality of cells extending from one end face to the other end face along a longitudinal direction.
(10) A conventional ceramic-type monolithic honeycomb catalyst described in Patent Document 2 has a problem of being damaged by vibrations when being in direct contact with a marine diesel engine. However, in the SCR device of the present invention, even if it is disposed so as to be in direct contact with a marine diesel engine, the honeycomb catalyst structure having the unique configuration of the present invention can continuously perform denitration without being damaged by vibrations of the marine diesel engine.
(11) Types of the SCR device disposed so as to be in direct contact with the marine diesel engine are illustrated in
(12)
(13) In
(14) The numeral 2 denotes a receiver tank that receives and stores exhaust gas sent from the diesel engine body 1, and serves as a buffer tank that absorbs a fluctuation in the amount of exhaust gas sent from the diesel engine body 1, for example. The receiver tank 2 also serves as piping 2 for exhaust gas.
(15) The diesel engine illustrated in
(16) Into the receiver tank 2, a urea-solution supply pipe 3 for supplying pressurized air (compressed air) and a urea solution is disposed, and a urea-solution spray nozzle 4 is provided near a tip of the urea-solution supply pipe 3. The urea-solution spray nozzle 4 is configured to be able to spray the urea solution into the receiver tank 2.
(17) In the receiver tank 2, downstream of the urea-solution spray nozzle 4, a urea-solution hydrolysis unit (not illustrated) may be provided.
(18) The hydrolysis unit is preferably provided with a hydrolysis catalyst. The hydrolysis catalyst can promote hydrolysis of urea and decrease the amount of urea to be sent to the SCR catalyst described later, thereby decreasing formation of urea-derived solids in the SCR honeycomb catalyst.
(19) The urea solution sprayed by the urea-solution spray nozzle 4 and/or the NH 3 produced by hydrolysis in the hydrolysis unit is sent with the exhaust gas to the denitration unit 5.
(20) The denitration unit 5 is provided with an SCR catalyst supported on a metal honeycomb serving as a support. In the denitration unit 5, when exhaust gas containing NH 3 and NOx produced by the hydrolysis of urea has been introduced, the NOx is reduced by the action of the SCR catalyst to produce nitrogen gas (N 2), whereby denitration treatment is performed.
(21) The treated gas thus denitrated is returned for reuse to a turbocharger 7 through treated-gas piping 6.
(22)
(23) In
(24) The diesel engine illustrated in
(25) In
(26) The following describes an example of the honeycomb catalyst structure of the denitration unit 5 used in the SCR device with reference to
(27) The numeral 10 in
(28) The metal corrugated plate 11 and the metal flat plate 12 are brazed together to form a honeycomb substrate (not illustrated). The honeycomb substrate is then spirally wound to form the metal honeycomb unit 10.
(29) The diameter of the metal honeycomb unit 10 can be adjusted appropriately in accordance with the number of windings of the honeycomb substrate, as long as the metal honeycomb unit 10 can be attached to the piping 2 for exhaust gas.
(30)
(31) The metal honeycomb unit 10 has a configuration including cells extending from one end face to the other end face along the longitudinal direction (left-and-right direction in
(32) As illustrated in
(33) The cells 13 each having a triangular cross-section extend and penetrate from one end to the other end along the longitudinal direction (left-and-right direction in
(34) In the above example, the shape of each cell is triangular in cross section, but is not limited to a particular one. The cell may have any of a semicircular cross-section, an elliptical cross-section, a quadrangular cross-section, and a polygonal cross-section, for example.
(35) The materials of the metal corrugated plate 11 and the metal flat plate 12, which constitute the metal honeycomb unit 10, are preferably made of an alloy containing Fe as a main component, Cr at 15 to 20 wt %, and Al at 2 to 5 wt % (an alloy containing Cr at 15 to 20 wt % and Al at 2 to 5 wt % with a remainder of Fe and unavoidable impurities). With this composition, the metal honeycomb unit 10 constituted by the metal corrugated plate 11 and the metal flat plate 12 is excellent in strength, vibration resistance, and heat resistance.
(36) In particular, during brazing of the honeycomb unit 10 or during firing of SCR, a temperature reaches about 1000? C. In this case, the Cr content of 15 to 20 wt % allows formation of the honeycomb unit 10 having excellent heat resistance.
(37) The presence of Al provides excellent corrosion resistance because aluminum oxide is formed on an outermost surface of the honeycomb unit when heated at high temperature. For example, because exhaust gas from marine engines has a higher sulfur (S) content in the fuel and chlorine (Cl) is easily mixed thereinto, a higher Al content tends to make the honeycomb unit less likely to corrode. Thus, for the honeycomb unit, the content of Al is preferably within a range of 2 to 5 wt % when balance is considered in terms of strength, vibration resistance, heat resistance, and corrosion resistance.
(38) In the present invention, the cell density is 50 to 500 cpsi, preferably 80 to 500 cpsi, more preferably 100 to 500 cpsi, and even more preferably 100 to 400 cpsi. A cell density within this range has such effects that the honeycomb catalyst structure can be made compact and the pressure loss can be kept within a range that does not impair the performance of an engine including a turbocharger.
(39) In the present embodiment, a relationship between linear velocity LV and pressure loss, which was determined in examples described later, is illustrated in
(40) When the slope of the straight line represented by the relationship between the flow velocity (linear velocity LV) and the pressure loss of exhaust gas passing through the cells is 30 or more and 180 or less, an optimal cell density based on the pressure loss in the cells can be set in consideration of the performance of the engine with the turbocharger, as well as the honeycomb catalyst structure can be made compact as described above.
(41) In the present invention, the SCR catalyst, which is a carrier, is supported on the support forming the metal honeycomb unit 10 provided to the denitration unit 5.
(42) The SCR catalyst contains TiO.sub.2 as a principal component. The content of TiO.sub.2 is preferably 50 vol % or more. This is because it is excellent in functionality as an SCR catalyst.
(43) The SCR catalyst preferably contains, in addition to TiO.sub.2, any one type or two or more types of V.sub.2O.sub.5, WO.sub.3, MoO.sub.3, SiO.sub.2, and Al.sub.2O.sub.3 in combination.
(44) The method of supporting the SCR catalyst on the support is not limited to a particular one, but the impregnation method is preferred.
EXAMPLES
(45) The following describes Examples of the present invention. However, the present invention is not limited to the Examples.
Example 1
(46) The SCR device illustrated in
(47) The cross-sectional shape of each of the cells is an isosceles triangle.
(48) The following four honeycomb catalyst structures were prepared. Honeycomb catalyst structure A: cell density 80 cpsi Honeycomb catalyst structure B: cell density 130 cpsi Honeycomb catalyst structure C: cell density 300 cpsi Honeycomb catalyst structure D: cell density 400 cpsi
(49) Exhaust gas at 350? C. was fed to the SCR device, and denitration experiments were conducted with the respective honeycomb catalyst structures A to D listed above.
(50) In each experiment, the relationship between the maximum SV (h.sup.?1) and the cell density was determined. The results are illustrated in
(51) From the results of the experiments, it is found that a cell density of 100 cpsi or more improves denitration performance and enables the SCR device to be made compact.
Example 2
(52) The following four honeycomb catalyst structures were prepared such that a cell density is less than 500 cpsi, and denitration experiments were conducted. Honeycomb catalyst structure E: cell density 78 cpsi Honeycomb catalyst structure F: cell density 100 cpsi Honeycomb catalyst structure G: cell density 200 cpsi Honeycomb catalyst structure H: cell density 400 cpsi
(53) In each experiment, the relationship between the linear velocity LV and the pressure loss was determined. Each relationship is illustrated in
(54) The linear velocity LV is a gas flow velocity (m/sec) measured as (the flow rate of exhaust gas flowing through each cell)/(cell cross-sectional area).
(55) The pressure loss was calculated from the gas pressures at the inlet and the outlet of the honeycomb catalyst structure. The unit of the result thus determined is the pascal (Pa).
(56) From the results of the experiments, it is found that the pressure loss increases as the number of cells increases. It is found that a cell density of 500 cpsi or less is appropriate to prevent the engine performance from being impaired.
EXPLANATIONS OF LETTERS OR NUMERALS
(57) 1 diesel engine body 2 receiver tank (piping for exhaust gas) 3 urea-solution supply pipe 4 urea-solution spray nozzle 5 denitration unit 6 treated-gas piping 7 turbocharger 8 SCR device 10 metal honeycomb unit 11 metal corrugated plate 12 metal flat plate 13 cell