Green carbon dioxide injection line compression system

1 . A carbon dioxide injection line compression system, comprising:

a main carbon dioxide storage line connecting a carbon dioxide source with a storage site, the storage site is one of an underground reservoir or well, a depleted oil or gas field, or a deep rock reservoir beneath the sea, such that the main carbon dioxide storage line is configured to transport a first carbon dioxide gas flow from the carbon dioxide source to the storage site, the main carbon dioxide storage line comprising a compressor, wherein the compressor is in fluid communication with, and upstream of, the storage site, and wherein the compressor is configured to compress the first carbon dioxide gas flow from the carbon dioxide source prior to storing the carbon dioxide gas at the storage site;

a turbine configured to drive the compressor; and

an oxygen combustion chamber configured to burn a fuel in an oxygen rich environment to generate energy and a gaseous mixture comprising a second carbon dioxide gas flow and steam,

wherein, at least a part of the energy generated is used to drive the turbine; and

wherein the oxygen combustion chamber is in fluid communication with, and upstream of, the storage site such that the second carbon dioxide gas flow generated in the oxygen combustion chamber is added to the main carbon dioxide storage line.

2 . The carbon dioxide injection line compression system of claim 1 , wherein, the second carbon dioxide gas flow generated in the oxygen combustion chamber is added to the main carbon dioxide storage line upstream of the compressor.

3 . The carbon dioxide injection line compression system of claim 1 , wherein the second carbon dioxide gas flow generated in the oxygen combustion chamber is added to the main carbon dioxide storage line downstream of an output of the compressor.

4 . The carbon dioxide injection line compression system of claim 1 , wherein the compressor includes a plurality of compression stages comprising a first compression stage and one or more subsequent compression stages; and

wherein the second carbon dioxide gas flow generated in the oxygen combustion chamber is added to the main carbon dioxide storage line at one of the one or more subsequent compression stages.

5 . The carbon dioxide injection line compression system of claim 1 , further comprising:

a steam reforming module configured to generate hydrogen from natural gas and steam, wherein the steam reforming module is in communication with the oxygen combustion chamber such that at least a part of the energy generated in the oxygen combustion chamber is configured to heat the steam and natural gas within the steam reforming module.

6 . The carbon dioxide injection line compression system of claim 5 , wherein the energy generated in the oxygen combustion chamber is the sole heat source used to heat the steam and natural gas within the steam reforming module, and wherein the steam and natural gas is heated to temperatures from seven-hundred degrees Celsius (700° C.) to one-thousand one-hundred degrees Celsius (1100° C.).

7 . The carbon dioxide injection line compression system of claim 5 , wherein the steam reforming module comprises:

a reactor module in communication with the oxygen combustion chamber such that heat from the oxygen combustion chamber is transferred to the reactor module, wherein the reactor module is configured to generate a synthesis gas (syngas) by heating natural gas in the presence of steam and a catalyst; and

a separation module in fluid communication with, and downstream of, the reactor module, wherein the separation module is configured to separate the syngas into a carbon-based gas stream and a hydrogen gas stream; and

wherein the separation module is configured to input the carbon-based gas stream to the oxygen combustion chamber.

8 . The carbon dioxide injection line compression system of claim 1 , wherein the oxygen combustion chamber is configured to heat a working fluid held within a closed loop system, wherein the closed loop system further comprises the turbine and a pump configured to move the working fluid around the closed loop system.

9 . The carbon dioxide injection line compression system of claim 8 , wherein the closed loop system further comprises a condenser unit configured to convert gaseous-phase working fluid, output from the turbine, into liquid-phase working fluid.

10 . The carbon dioxide injection line compression system of claim 1 , further comprising:

a purification module configured to separate the second carbon dioxide gas flow in the gaseous mixture from the water in the gaseous mixture.

11 . The carbon dioxide injection line compression system of claim 10 , wherein the purification module comprises a separation unit in fluid communication with, and upstream of, a dehydration unit, wherein the separation unit is configured to remove at least some of the water from the gaseous mixture to provide a carbon dioxide rich stream that is passed to the dehydration unit, and wherein the dehydration unit is configured to further dehydrate the carbon dioxide rich stream.

12 . The carbon dioxide injection line compression system of claim 1 , wherein the turbine is in direct communication with a shaft of the compressor, and wherein the turbine is configured to move the shaft.

13 . The carbon dioxide injection line compression system of claim 1 , wherein the turbine is coupled to a generator, wherein the generator is configured to generate electricity to power the compressor.

14 . A method for carbon dioxide injection compression comprising:

generating energy and a gaseous mixture comprising steam and a first carbon dioxide gas flow by burning fuel in an oxygen rich environment in an oxygen combustion chamber;

adding the first carbon dioxide gas flow generated in the oxygen combustion chamber to a main carbon dioxide storage line, wherein the main carbon dioxide storage line extends between a carbon dioxide source and a storage site, the carbon dioxide source supplying a second carbon dioxide gas flow to the storage site, and wherein the main carbon dioxide storage line comprises a compressor;

driving the compressor to compress the second carbon dioxide gas flow provided thereto upstream of the storage site, wherein the compressor is driven by a turbine and the turbine is driven by the energy generated in the oxygen combustion chamber; and

transporting the carbon dioxide in the main storage line to the storage site, wherein the storage site is one of an underground reservoir or well, a depleted oil or gas field, or a deep rock reservoir beneath the sea.

15 . The method of claim 14 , further comprising:

adding the first carbon dioxide gas flow generated in the oxygen combustion chamber to the main storage line upstream of the compressor such that the first carbon dioxide gas flow is compressed and pressurised upstream of the storage site.

16 . The method of claim 14 , further comprising:

adding the first carbon dioxide gas flow generated in the oxygen combustion chamber to the main storage line downstream of the compressor to provide a mixed stream of pressurised carbon dioxide; and

transporting the mixed stream of pressurised carbon dioxide to the storage site.

17 . The method of claim 14 , further comprising:

generating a synthesis gas (syngas) in a steam reforming module by heating a mixture of natural gas and steam to a temperature between seven-hundred degrees Celsius (700° C.) to one-thousand one-hundred degrees Celsius (1100° C.) in the presence of a catalyst, wherein the thermal energy generated in the oxygen combustion chamber is used as the source of heat to heat the steam reforming module.

18 . The method of claim 17 , wherein the method further comprises:

separating the syngas into a carbon-based gas stream and a hydrogen gas stream; and

passing the carbon-based gas stream into the oxygen combustion module.

19 . The method of claim 14 , further comprising:

separating, in a purification module, the first carbon dioxide gas flow in the gaseous mixture from the water in the gaseous mixture.

20 . The method of claim 19 , further comprising:

recirculating a portion of the first carbon dioxide gas flow separated in the purification module back into the oxygen combustion chamber; and

outputting a portion of the first carbon dioxide gas flow separated in the purification module to the storage site.