METHOD FOR TREATING A SUPPORTED CATALYST
A method for treating a supported catalyst includes establishing shell-removal conditions for a supported catalyst that includes nanoparticles of a catalyst material on a carbon support. The nanoparticles each include a platinum alloy core capped in an organic shell. The shell-removal conditions include an elevated temperature and an inert gas atmosphere that is substantially free of oxygen. The organic shell is then removed from the platinum alloy core in the shell-removal conditions.
1 . A method for treating a supported catalyst, comprising:
establishing shell-removal conditions for a supported catalyst that includes nanoparticles of a catalyst material on a carbon support, the nanoparticles each comprise a platinum alloy core capped in an organic shell, and the shell-removal conditions include an elevated temperature and an inert gas atmosphere that is substantially free of oxygen; and
removing the organic shell from the platinum alloy core in the shell-removal conditions.
2 . The method as recited in claim 1 , wherein the elevated temperature of the shell-removal conditions is 220° C.-600° C.
3 . The method as recited in claim 1 , wherein the elevated temperature of the shell-removal conditions is about 270° C.
4 . The method as recited in claim 1 , wherein the inert gas is selected from a group consisting of nitrogen, argon, and combinations thereof.
5 . The method as recited in claim 1 , wherein the removing of the organic shell includes thermal decomposition of the organic shell.
6 . The method as recited in claim 1 , wherein the inert gas atmosphere is a mixture of at least two different kinds of inert gases and hydrogen.
7 . The method as recited in claim 6 , wherein the mixture includes nitrogen, argon, and the hydrogen, and the hydrogen is present in an amount no greater than about 10 vol %.
8 . The method as recited in claim 1 , further comprising, after removing the organic shell, annealing the supported catalyst at an annealing temperature of 400° C.-1200° C.
9 . The method as recited in claim 8 , wherein the annealing temperature is 700° C.-1000° C.
10 . The method as recited in claim 8 , wherein the annealing temperature is 800° C.-1000° C.
11 . The method as recited in claim 1 , wherein the platinum alloy catalyst consists of platinum and at least one alloy metal selected from a group consisting of iron, nickel, cobalt, iridium, chromium, molybdenum, palladium, rhodium, gold, copper and vanadium.
12 . The method as recited in claim 1 , further comprising, prior to establishing the shell-removal conditions, forming the organic shells of the nanoparticles using a polyol process.
13 . The method as recited in claim 1 , wherein the support is carbon black, carbides, oxides, boron doped diamond, and combination thereof.
14 . The method as recited in claim 1 , wherein the support is unmodified carbon black, modified carbon black, graphitized carbon black, carbon nanotube, carbon nanowire, carbon fiber, and combination thereof.
15 . The method as recited in claim 1 , wherein the organic shell is selected from a group consisting of oleylamine, oleic acid, thiol, polyacrylic acid, trimethylaluminum, tetraoctylammonium bromide, sodium dodecyl sulfate, acetic acid, cetryltrimethylammonium chloride, and combinations thereof.
16 . A method for treating a supported catalyst, comprising:
establishing shell-removal conditions for a supported catalyst that includes nanoparticles of a catalyst material on a carbon black support, the nanoparticles each comprise a platinum alloy core capped in an organic shell selected from a group consisting of oleylamine, oleic acid, and combinations thereof, the platinum alloy core includes platinum and at least one alloy metal selected from a group consisting of nickel, iron, cobalt, iridium, chromium, molybdenum, palladium, rhodium, gold, copper and vanadium, and the shell-removal conditions include an elevated temperature of higher than 220° C., and an inert gas atmosphere that is substantially free of oxygen;
removing the organic shell from the platinum alloy core in the shell-removal conditions; and
annealing the platinum alloy cores that remain after the removing of the organic shells at an annealing temperature of 400° C.-1200° C.
17 . The method as recited in claim 14 , further comprising, prior to establishing the shell-removal conditions, forming the organic shells of the nanoparticles using a polyol process.
18 . A method for treating a supported catalyst, comprising:
establishing shell-removal conditions for a supported catalyst that includes nanoparticles of a catalyst material on a carbon support, the nanoparticles each comprise a platinum alloy core capped in an organic shell, and the shell-removal conditions include an elevated temperature and an atmosphere that is substantially free of oxygen and is substantially inert with respect to the carbon support;
removing the organic shell from the platinum alloy core in the shell-removal conditions; and
annealing the platinum alloy core, after shell-removal, at a temperature of at least 400° C.
19 . A method for treating a supported catalyst, comprising:
establishing shell-removal conditions for a supported catalyst that includes nanoparticles of a catalyst material on a carbon black support, the nanoparticles each comprise a platinum alloy core capped in an organic shell selected from a group consisting of oleylamine, oleic acid, and combinations thereof, the platinum alloy core includes platinum and at least one alloy metal selected from a group consisting of nickel, iron, cobalt, iridium, chromium, molybdenum, palladium, rhodium, gold, copper and vanadium, and the shell-removal conditions include an elevated temperature of higher than 220° C., and an atmosphere that is substantially free of oxygen such that the atmosphere does not substantially decompose the carbon black support under the shell removal conditions;
removing the organic shell from the platinum alloy core in the shell-removal conditions; and
annealing the platinum alloy cores that remain after the removing of the organic shells at an annealing temperature of 400° C.-1200° C.