Catalysis

Claim 2

In a process for the reduction with a reducing fuel of an oxide of nitrogen which comprises passing the gas mixture at an elevated temperature through a supported catalyst, the improvement which comprises using as the supported catalyst, one consisting essentially of an inert rigid porous refractory honeycomb structure having a first coating thereon containing at least one oxide selected from the group constituted by the oxides of titanium, zirconium, hafnium and thorium and a second coating of a mixture or alloy of platinum, rhodium and base metal in which the rhodium constitutes from 1 to 50 weight % and the base metal constitutes from 0.01 to 25 weight % of the total metal content.

Claim 3

In a process for the reduction with a reducing fuel of an oxide of nitrogen which comprises passing the gas mixture at an elevated temperature through a supported catalyst, the improvement which comprises using as the supported catalyst, one consisting essentially of an inert rigid porous refractory ceramic honeycomb having applied thereto a first adherent catalytically active refractory metal oxide coating containing at least 50% by weight of alumina, in which one or more of the oxides titania, zirconia, hafnia and thoria constitute at least 5% by weight of the refractory metal oxide and having a second coating of an alloy containing 1 to 50 weight % rhodium, from 0.01 to 25 weight % base metal selected from the group consisting of aluminium, magnesium, chromium, molybdenum, tungsten, manganese, iron, cobalt, nickel, copper, titanium, vanadium, thorium, uranium, copper, silver, zinc, indium, cadmium, mercury, iridium, thallium, bismuth, tin, lead, antimony, the lanthanides and the actinides, and neodymium and balance platinum.

Claim 4

In a process for the reduction with a reducing fuel of an oxide of nitrogen which comprises passing the gas mixture at an elevated temperature through a supported catalyst, the improvement which comprises using as the supported catalyst, one consisting essentially of an inert rigid porous refractory ceramic honeycomb having applied thereto a first adherent catalytically active refractory metal oxide coating containing at least 50% by weight of alumina, in which one or more of the oxides titania, zirconia, hafnia and thoria constitute at least 5% by weight of the refractory metal oxide and having a second coating of an alloy containing 1 to 50 weight % rhodium, from 0.01 to 25 weight % base metal selected from the group consisting of aluminium, magnesium, chromium, molybdenum, tungsten, manganese, iron, cobalt, nickel, copper, titanium, vanadium, thorium, uranium, copper, silver, zinc, indium, cadmium, mercury, iridium, thallium, bismuth, tin, lead, antimony, the lanthanides and the actinides, and neodymium and balance platinum.

Claim 5

A process according to claim 1, wherein the base metal in the catalyst is selected from the group consisting of chromium, iron, cobalt, nickel, copper, silver, zinc, indium, tin, the lanthanides an neodymium.

Claim 6

A process according to claim 1, wherein the base metal in the catalyst is neodymium and constitutes at least 50% by weight of the total base metal component present in the said alloy.

Claim 7

A process according to claim 1, wherein the base metal in the catalyst is neodymium and constitutes at least 5% by weight of the total metal present in the said alloy.

Claim 8

In a process of catalytically reducing an oxide of nitrogen in a gas containing at least an oxide of nitrogen comprising the steps of contacting the gas together with a gaseous reducing fuel, at a temperature above the ignition temperature of the fuel, with a supported catalyst, the improvement which comprises using, as the catalyst, one consisting essentially of an inert rigid porous refractory honeycomb structure having applied thereto a first adherent catalytically active refractory metal oxide coating containing at least 50% by weight of alumina, in which one or more of the oxides titania, zirconia, hafnia, and thoria constitute at least 5% by weight of the refractory metal oxide and having a second coating of an alloy containing 1 to 50 weight % rhodium, from 0.01 to 25 weight % base metal selected from the group consisting of aluminum, magnesium, chromium, molybdenum, tungsten, manganese, iron, cobalt, nickel, copper, titanium, vanadium, thorium, uranium, copper, silver, zinc, indium, cadmium, mercury, iridium, thallium, bismuth, tin, lead, antimony, the lanthanides and the actinides, and neodymium and balance platinum.

Claim 9

In a process of catalytically reducing an oxide of nitrogen in a gas containing at least an oxide of nitrogen comprising the steps of contacting the gas together with a gaseous reducing fuel, at a temperature above the ignition temperature of the fuel, with a supported catalyst, the improvement which comprises using, as the catalyst, one consisting essentially of an inert rigid porous refractory honeycomb structure having applied thereto a first adherent catalytically active refractory metal oxide coating containing at least 50% by weight of alumina, in which one or more of the oxides titania, zirconia, hafnia, and thoria constitute at least 5% by weight of the refractory metal oxide and having a second coating of an alloy containing 1 to 50 weight % rhodium, from 0.01 to 25 weight % base metal selected from the group consisting of aluminum, magnesium, chromium, molybdenum, tungsten, manganese, iron, cobalt, nickel, copper, titanium, vanadium, thorium, uranium, copper, silver, zinc, indium, cadmium, mercury, iridium, thallium, bismuth, tin, lead, antimony, the lanthanides and the actinides, and neodymium and balance platinum.

Claim 10

A process according to claim 6, wherein the base metal in the catalyst is selected from the group consisting of chromium, iron, cobalt, nickel, copper, silver, zinc, indium, tin, the lanthanides and neodymium.

Claim 11

A process according to claim 6, wherein the base metal in the catalyst is neodymium and constitutes at least 50% by weight of the total base metal component present in the said alloy.

Claim 12

A process according to claim 6, wherein the base metal in the catalyst is neodymium and comprises at least 5% by weight of the total metal present in the said alloy.

Claim 13

In a process for the oxidation of an organic compound in a gas containing oxygen comprising passing the gas at an elevated temperature through a supported catalyst, the improvement which comprises using, as the catalyst, one consisting essentially of an inert rigid porous refractory honeycomb structure having applied thereto a first adherent catalytically active refractory metal oxide coating containing at least 50% by weight of alumina, in which one or more of the oxides titania, zirconia, hafnia, and thoria constitute at least 5% by weight of the refractory metal oxide and having a second coating of an alloy containing 1 to 50 weight % rhodium, from 0.01 to 25 weight % base metal selected from the group consisting of aluminum, magnesium, chromium, molybdenum, tungsten, manganese, iron, cobalt, nickel, copper, titanium, vandaium, thorium, uranium, copper, silver, zinc, indium, cadmium, mercury, iridium, thallium, bismuth, tin, lead, antimony, the lanthanides and the actinides, and neodymium and balance platinum.

Claim 14

In a process for the oxidation of an organic compound in a gas containing oxygen comprising passing the gas at an elevated temperature through a supported catalyst, the improvement which comprises using, as the catalyst, one consisting essentially of an inert rigid porous refractory honeycomb structure having applied thereto a first adherent catalytically active refractory metal oxide coating containing at least 50% by weight of alumina, in which one or more of the oxides titania, zirconia, hafnia, and thoria constitute at least 5% by weight of the refractory metal oxide and having a second coating of an alloy containing 1 to 50 weight % rhodium, from 0.01 to 25 weight % base metal selected from the group consisting of aluminum, magnesium, chromium, molybdenum, tungsten, manganese, iron, cobalt, nickel, copper, titanium, vandaium, thorium, uranium, copper, silver, zinc, indium, cadmium, mercury, iridium, thallium, bismuth, tin, lead, antimony, the lanthanides and the actinides, and neodymium and balance platinum.

Claim 15

A process according to claim 10, wherein the base metal in the catalyst is selected from the group consisting of chromium, iron, cobalt, nickel, copper, silver, zinc, indium, tin, the lanthanides and neodymium.

Claim 16

A process according to claim 10, wherein the base metal in the catalyst is neodymium and constitutes at least 50% by weight of the total base metal component present in the said alloy.

Claim 17

A process according to claim 10, wherein the base metal in the catalyst is neodymium and constitutes at least 5% by weight of the total metal present in the said alloy.