Claims
- 1. A method of generating a H2 rich gas from a fuel, comprising: supplying a mixture of molecular oxygen, fuel, and water to a fuel processor; and converting the mixture of molecular oxygen, fuel, and water in the fuel processor to the H2 rich gas, wherein the fuel has the formula CnHmOp where n has a value ranging from 1 to 20 and is the average number of carbon atoms per molecule of the fuel, m has a value ranging from 2 to 42 and is the average number of hydrogen atoms per molecule of the fuel, p has a value ranging from 0 to 12 and is the average number of oxygen atoms per molecule of the fuel, and further wherein the molar ratio of molecular oxygen supplied to the fuel processor per mole of fuel is represented by the symbol x and has a value ranging from about 0.5x0 to about 1.5x0, wherein x0 is equal to 0.3 12n−0.5p+0.5(ΔHf, fuel/ΔHf, water) where n and p have the values described above, ΔHf, fuel is the heat of formation of the fuel, and ΔHf, water is the heat of formation of water.
- 2. The method of claim 1, wherein converting the mixture of molecular oxygen, fuel, and water in the fuel processor to produce the H2 rich gas further comprises contacting the mixture of molecular oxygen, fuel, and water with a catalyst in the fuel processor to produce the H2 rich gas.
- 3. The method of claim 1, wherein the molar ratio of molecular oxygen supplied to the fuel processor per mole of fuel is x and has a value ranging from about x0 to about 1.5x0.
- 4. The method of claim 1, wherein the molar ratio of molecular oxygen supplied to the fuel processor per mole of fuel is x and the molar ratio of water supplied to the fuel processor per mole of fuel is a value ranging from about 0.8(2n-2x-p) to about 2.0(2n-2x-p).
- 5. The method of claim 4, wherein the molar ratio of water supplied to the fuel processor per mole of fuel is a value ranging from about 0.9(2n-2x-p) to about 1.5(2n-2x-p).
- 6. The method of claim 5, wherein the molar ratio of water supplied to the fuel processor per mole of fuel is a value ranging from about 0.95(2n-2x-p) to about 1.2(2n-2x-p).
- 7. The method of claim 6, wherein the molar ratio of water supplied to the fuel processor per mole of fuel is a value ranging from about 1.0(2n-2x-p) to about 1.1(2n-2x-p).
- 8. The method of claim 1, wherein the molecular oxygen is supplied to the fuel processor in a mixture of gases comprising N2 and molecular oxygen.
- 9. The method of claim 1, wherein the mixture of gases comprising N2 and molecular oxygen is air.
- 10. The method of claim 1, wherein the fuel is selected from the group consisting of methane, methanol, ethane, ethylene, ethanol, propane, propene, i-propanol, n-propanol, butane, butene, butanol, pentane, pentene, hexane cyclohexane, cyclopentane, benzene, toluene, xylene, natural gas, liquefied petroleum gas, iso-octane, gasoline, kerosene, and diesel.
- 11. The method of claim 10, wherein the fuel is selected from the group consisting of methane, natural gas, propane, methanol, ethanol, liquefied petroleum gas, gasoline, kerosene, and diesel.
- 12. The method of claim 1, wherein the fuel processor comprises a reforming portion and the H2 rich gas exiting the reforming portion is maintained at a temperature of from about 100° C. to about 900° C.
- 13. The method of claim 1 wherein the fuel processor comprises a reforming portion and the H2 rich gas exiting the reforming portion is maintained at a temperature of from about 400° C. to about 700° C.
- 14. The method of claim 1, wherein the molar ratio of molecular oxygen supplied to the fuel processor per mole of fuel is x and has a value ranging from about 0.8x0 to about 1.4x0.
- 15. The method of claim 14, wherein the molar ratio of molecular oxygen supplied to the fuel processor per mole of fuel is x and has a value ranging from about 0.9x0 to about 1.3x0.
- 16. The method of claim 15, wherein the molar ratio of molecular oxygen supplied to the fuel processor per mole of fuel is x and has a value ranging from about 0.95x0 to about 1.2x0.
- 17. The method of claim 16, wherein the molar ratio of molecular oxygen supplied to the fuel processor per mole of fuel is x and the molar ratio of water supplied to the fuel processor per mole of fuel is a value ranging from about 1.0(2n-2x-p) to about 1.1(2n-2x-p).
- 18. The method of claim 2, wherein the catalyst comprises a two part catalyst comprising a transition metal and an oxide-ion conducting portion, and the mixture of molecular oxygen, fuel, and water is contacted with the catalyst at a temperature of 400° C. or greater.
- 19. The method of claim 18, wherein the transition metal is selected from the group consisting of platinum, palladium, ruthenium, rhodium, iridium, iron, cobalt, nickel, copper, silver, gold, and mixtures thereof, and the oxide-ion conducting portion of the catalyst is selected from a ceramic oxide from the group crystallizing in the fluorite structure or LaGaO3 or mixtures thereof.
- 20. The method of claim 2, wherein the catalyst is selected from the group of autothermally reforming catalysts that operate at a temperature ranging from about 100° C. to about 700° C.
- 21. The method of claim 2, wherein the H2 rich gas comprises carbon monoxide and carbon dioxide, and the method further comprises contacting the H2 rich gas with a second catalyst effective at converting carbon monoxide and water into carbon dioxide and H2 to produce a second gas further enriched in H2 and with a reduced level of carbon monoxide.
- 22. The method of claim 21, wherein the second catalyst comprises a transition metal on cerium oxide or on ceria doped with a rare earth or an alkaline earth element, further wherein the transition metal is selected from the group consisting of platinum, palladium, nickel, iridium, rhodium, cobalt, copper, gold, ruthenium, iron, silver, and combinations thereof, the rare earth element is selected from the group consisting of gadolinium, samarium, yttrium, lanthanum, praseodymium, and combinations thereof, and the alkaline earth element is selected from the group consisting of magnesium, calcium, strontium, barium, and combinations thereof.
Government Interests
[0001] The United States government has rights in this invention pursuant to Contract No. W-31-108-ENG-38 between the United States Department of Energy and the University of Chicago representing Argonne National Laboratory.