초록 ▼

The invention concerns a method of operating a combustion plant comprising at least a first gas turbine (26), a second turbine (34, 50) and a membrane reactor device (16) which comprises a membrane filter device (18) for separating oxygen from a gas mixture and a combustion space (19). A gas mixture

The invention concerns a method of operating a combustion plant comprising at least a first gas turbine (26), a second turbine (34, 50) and a membrane reactor device (16) which comprises a membrane filter device (18) for separating oxygen from a gas mixture and a combustion space (19). A gas mixture containing oxygen is supplied to the membrane reactor device (16). At least some oxygen is separated from the gas mixture with the help of the membrane filter device (18). The separated oxygen is used at the combustion in the combustion space (19). The oxygen-depleted gas that is obtained after the separation of oxygen and which has not gone through a combustion process is used to run the first gas turbine (26). Combustion gases run the second turbine (34, 50). The invention also concerns a combustion plant for carrying out the method.

대표청구항 ▼

1. A method of operating a combustion plant comprising at least a first gas turbine, a second turbine and a membrane reactor device which comprises a membrane filter device for separating oxygen from a gas mixture and a combustion space for the combustion of a fuel, which method comprises:that a gas

1. A method of operating a combustion plant comprising at least a first gas turbine, a second turbine and a membrane reactor device which comprises a membrane filter device for separating oxygen from a gas mixture and a combustion space for the combustion of a fuel, which method comprises:that a gas mixture containing oxygen is supplied to the membrane reactor device and there goes through a separation in the membrane filter device, such that at least some oxygen is separated from the gas mixture such that an oxygen-depleted gas is obtained, that at least a part of said oxygen which has been separated from the gas mixture is used at said combustion in the combustion space, that said gas mixture is heated with the help of heat generated through said combustion in the combustion space, that at least a part of said heated oxygen-depleted gas, which has not gone through a combustion process, is used to run said first gas turbine, and that at least a part of the combustion gases which emanate from said combustion is used to run said second turbine. 2. A method according to claim 1, wherein said gas mixture which is supplied to the membrane reactor device consists of air.3. A method according to claim 1, wherein the gas which leaves said first gas turbine is used for heating in a heat exchanger.4. A method according to claim 3, wherein said heat exchanger is used to evaporate a medium that runs a steam turbine.5. A method according to claim 3, wherein also the gas which leaves the second turbine is used for heating in said heat exchanger.6. A method according to claim 5, wherein said gas which leaves the second turbine comprises at least the substances CO2 and H2O and wherein, after passing through said heat exchanger, at least some H2O is conducted back to the membrane reactor device.7. A method according to claim 5, wherein said gas which leaves the second turbine comprises at least the substances CO2 and H2O, wherein, after passing through said heat exchanger, CO2 is completely or partly taken care of for use or storage.8. A method according to claim 4, wherein said second turbine constitutes said steam turbine, wherein the steam turbine is fed with a turbine medium which is conducted in a conduit member and heated in said heat exchanger, and wherein at least a part of said combustion gases from the combustion in the membrane reactor device is conducted to said conduit member for being supplied to said steam turbine.9. A method according to claim 8, wherein said combustion gases which are conducted to said conduit member comprises at least the substances CO2 and H2O, wherein, after passing through said steam turbine, at least some CO2 is drained off from the conduit member for use or storage.10. A method according to claim 8, wherein after passing through said steam turbine, at least some H2O is drained off from the conduit member and brought back to said membrane reactor device.11. A method according to claim 1, wherein said gas mixture is compressed with the help of a compressor before it is supplied to the membrane reactor device.12. A method according to claim 11, wherein said compressor is run by said first and/or second turbine.13. A method according to claim 1, wherein electric energy is derived from the membrane reactor device.14. A method according to claim 13, wherein the membrane filter device comprises both MCM-material and a fuel cell material and wherein said fuel cell material is used for deriving said electric energy.15. A combustion plant comprising: a first gas turbine, a second turbine, a membrane reactor device which comprises a membrane filter device for separating oxygen from a gas mixture and a combustion space for the combustion of a fuel, first conduit means arranged to conduct a gas mixture containing oxygen to said membrane reactor device, wherein the membrane reactor device is arranged such that said gas mixture goes through a separation in the membrane filter device, such that at least some oxygen is separated from the gas mixture such that an oxygen-depleted gas is obtained and such that at least a part of said oxygen which has been separated from the gas mixture is used at said combustion in the combustion space, wherein the membrane reactor device is arranged such that said gas mixture is heated with the help of heat generated through said combustion in the combustion space, a second conduit means arranged for conducting at least a part of said heated oxygen-depleted gas, which has not gone through a combustion process, to said first gas turbine for running the same, and third conduit means arranged for conducting at least a part of the combustion gases which emanate from said combustion to said second turbine for running the same.