Gas turbine integrated with fuel catalytic partial oxidation

1. A gas turbine engine comprising:

a compressor;

a plenum that receives a source of air from the compressor, the plenum having an air collection device capable of diverting a portion of the air source from the plenum;

a premixer in fluid communication with the plenum and capable of mixing the portion of the air source with a supply of natural gas to form a fuel/air mixture, wherein mixing is performed via a molecular diffusion process to ensure a minimum pressure drop;

a catalytic partial oxidation (CPOX) reactor in fluid communication with the premixer;

a shift reactor in fluid communication with the CPOX reactor, wherein the shift reactor is capable of selectively injecting steam from an external steam source into the fuel/air mixture via a steam inlet, wherein the steam inlet selectively injects the steam using a variable valve within the steam inlet that is controlled by a control system;

a separator capable of removing carbon dioxide from the fuel/air mixture; and

one or more combustion systems in fluid communication with the plenum and the separator, the one or more combustion systems having a plurality of fuel injectors,

wherein the fuel/air mixture is directed from the premixer to a catalyst in the CPOX reactor that initiates a partial oxidation of hydrocarbons to carbon monoxide and hydrogen, and

wherein the carbon monoxide and hydrogen are then directed to the shift reactor that injects the steam for converting the carbon monoxide into carbon dioxide.

2. The gas turbine engine of claim 1 , wherein the air source is supplied to the plenum by the compressor.

3. The gas turbine engine of claim 2 , wherein a variable valve is located between the plenum and the premixer for adjusting the portion of the air source drawn from the plenum.

4. The gas turbine engine of claim 1 , wherein the premixer has a low pressure drop.

5. The gas turbine engine of claim 1 , wherein the supply of natural gas is metered between 0% and 100% of a total fuel supply to the one or more combustion systems, as determined by availability and requirements of a carbon storage process.

6. The gas turbine engine of claim 1 , wherein the carbon dioxide is removed prior to a hydrogen/nitrogen mixture being directed to the plurality of fuel injectors.

7. The gas turbine engine of claim 1 , wherein a hydrogen level of the hydrogen/nitrogen mixture is increased by the shift reactor.

8. The gas turbine engine of claim 1 , wherein the CPOX reactor comprises a monolith, fixed bed, or fluid bed having a precious metal such as platinum, palladium, or rhodium, or any combination thereof.

9. The gas turbine engine of claim 1 , wherein a temperature of the fuel/air mixture rises during the partial oxidation of the fuel/air mixture.

10. The gas turbine engine of claim 1 , wherein the carbon dioxide is removed by a chemical and/or physical absorption unit or membrane of the separator.

11. A method of removing carbon dioxide from a fuel/air mixture prior to entry of the fuel/air mixture into a combustion system, the method comprising:

directing a supply of compressed air from a plenum into a premixer;

mixing a supply of natural gas with the supply of compressed air to produce the fuel/air mixture;

directing the fuel/air mixture into a catalytic partial oxidation (CPOX) reactor;

partially-oxidizing hydrocarbons in the fuel/air mixture to form carbon monoxide and hydrogen;

mixing the fuel/air mixture with a supply of steam in a shift reactor, wherein the shift reactor mixes via a first step that selectively injects high-pressure steam and a second step that selectively injects low-pressure steam;

directing the fuel/air mixture into a separator;

removing at least carbon dioxide from the fuel/air mixture, resulting in mostly hydrogen and nitrogen components; and

directing the mostly hydrogen and nitrogen components into a combustion system.

12. The method of claim 11 , wherein the supply of compressed air is directed into the plenum by a ram scoop.

13. The method of claim 11 , wherein the natural gas is mixed with the compressed air in a low pressure drop premixer, external to the plenum.

14. The method of claim 13 , wherein the mixing with steam increases hydrogen yield and converts the carbon monoxide into carbon dioxide.

15. The method of claim 11 , wherein the CPOX reactor comprises a monolith, fixed bed, or fluid bed and having a precious metal such as platinum, palladium, or rhodium.

16. A system capable of removing carbon dioxide from a fuel/air mixture comprising:

a plenum that receives a supply of air from a compressor, the plenum having an air collection device capable of diverting a portion of the air supply from the plenum, wherein the air collection device includes a ram scoop that captures the portion of the air supply at a pressure generated by the compressor, wherein the pressure is adequate to move the portion of the air supply through the system without an additional compressor;

a premixer for receiving the variable air supply from the engine compressor and injecting natural gas into the air supply to form the fuel/air mixture;

a catalytic partial oxidation (CPOX) reactor in fluid communication with the premixer;

a shift reactor having a steam inlet through which steam may be injected into the mixture, where the steam converts the carbon monoxide into carbon dioxide; and,

a separator capable of removing at least carbon from the fuel/air mixture;

wherein a catalyst in the CPOX reactor initiates a partial oxidation of methane components of the fuel/air mixture into carbon monoxide and hydrogen.

17. The system of claim 16 , wherein the premixer receives the air source from a compressor plenum.

18. The system of claim 16 , wherein the CPOX reactor comprises a monolith, fixed bed, or fluid bed having a precious metal such as platinum, palladium, or rhodium, or a combination thereof.

19. The system of claim 16 , further comprising a combustion system having one or more fuel injectors for receiving an output of mostly hydrogen and nitrogen from the separator.

20. The system of claim 19 , wherein the combustion system also receives a supply of natural gas to the one or more fuel injectors.