Oxy-fuel combustion system having monolith membrane
AssigneeKing Fahd University of Petroleum and Minerals
InventorsMedhat Ahmed NEMITALLAH, Mohamed Abdel-Aziz HABIB
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AssigneeKing Fahd University of Petroleum and Minerals
InventorsMedhat Ahmed NEMITALLAH, Mohamed Abdel-Aziz HABIB
Estimating the term…
Experimental and numerical investigations on an atmospheric diffusion oxy-combustion flame in a gas turbine model combustor are conducted. The combustor is fuelled with CH4CH4 and a mixture of CO2 and O2 as oxidizer. The stability of the oxy-combustion flame is affected when the operating percentage of oxygen in the oxidizer mixture is reduced below 25%. A new 3D reactor design is introduced for the substitution of ITM reactors into a gas turbine combustor. A new oxygen permeation equation model has been developed by fitting the experimental data available in the literature for a LSCF ion transport membrane. The monolith structure design ITM reactor is capable of delivering power ranging from 5 to 8 MWe based on cycle first law efficiency.
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An oxy-fuel combustion system comprising:
Dependencies are inferred from the claim text.