# US 10,480,403 B2 · Combustor with adjustable swirler and a combustion system > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,480,403 B2 - Document ID: US10480403B2 - Status: Granted - Kind: B2 - Application number: 15/364,299 - Filed: 2016-11-30 - Published: 2017-08-24 - Granted: 2019-11-19 - Earliest claimed: 2016-02-22 - Assignees: King Fahd University of Petroleum and Minerals - Applicants: King Fahd University of Petroleum and Minerals - Inventors: Esmail M. A. Mokheimer; Yinka S. Sanusi - Web page: https://patentgrep.com/patent/US10480403B2 ## CPC - F02C 3/22: the fuel or oxidant being gaseous at standard temperature and pressure (F02C3/28 takes precedence) - F02C 7/224: Heating fuel before feeding to the burner - F23C 7/002: {the air being submitted to a rotary or spinning motion (cyclonic combustion chamber F23C3/006)} - F23C 7/006: {adjustable} - F23L 7/007: {Supplying oxygen or oxygen-enriched air} - F23N 5/003: {using detectors sensitive to combustion gas properties (F23N5/02, F23N5/18 - F23N5/26 take precedence)} - F23R 3/14: by using swirl vanes - F23R 3/28: characterised by the fuel supply (burners F23D) - F23R 3/286: {having fuel-air premixing devices (F23R3/30 takes precedence)} - F23C 2900/07001: Air swirling vanes incorporating fuel injectors - F23D 2900/14701: Swirling means inside the mixing tube or chamber to improve premixing - Y02E 20/34: Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery - F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00) - F23C: METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN {A CARRIER GAS OR} AIR (burners F23D) - F23L: SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ({air-supply arrangements for fluent fuels F23C;} firebridges with means for feeding air or steam F23M3/04; baffles or shields with air supply passages F23M9/04); VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS {(dampers and throat restrictors for open fire-places F24; air inlet valves for open fire fronts F24)}; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES - F23N: REGULATING OR CONTROLLING COMBUSTION (control devices specially adapted for combustion apparatus in which combustion takes place in a fluidised bed of fuel or other particles F23C10/28; condition responsive controls for regulating combustion in domestic stoves with open fires for solid fuel F24B1/187) - F23R: GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS (fluidised bed combustion apparatus specially adapted for operation at superatmospheric pressures F23C10/16) - F23D: BURNERS - Y02E: REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION ## Abstract A combustor having an ion transport membrane therein and an adjustable swirler, which is mechanically connected at an inlet of a combustion zone of the combustor; a combustion system comprising the combustor, a feedback control system adapted to adjust swirler blades of the combustor based on a compositional variation of a fuel stream, and a plurality of feedback control systems to control operational variables within the combustor for an efficient oxy-combustion; and a process for combusting a fuel stream via the combustion system. Various embodiments of the combustor, the combustion system, and the process for combusting the fuel stream are disclosed. ## Claims ### Claim 1 A combustion system, comprising: a combustor comprising: a cylindrical vessel with an internal cavity, an ion transport membrane that divides the internal cavity of said cylindrical vessel into a first and a second concentric cylindrical zone, wherein the first concentric cylindrical zone is a feed zone and the second concentric cylindrical zone is a combustion one, a first inlet and a first outlet located in the feed zone, and a second inlet and a second outlet located in the combustion zone, and a swirler that is connected to the second inlet, wherein the swirler has adjustable blades with adjustable angles: an oxygen supplier located upstream of and fluidly connected to the first inlet via a feed line for supplying an oxygen-containing stream; a fuel supplier located upstream of and fluidly connected to the second inlet via a fuel line for supplying a fuel stream; an expander located downstream of and fluidly connected to the second outlet via an exhaust line for expanding an exhaust stream to generate power; a recycle line that fluidly connects the exhaust line to the fuel line; a mixer located upstream of the combustor and fluidly connected to the fuel line and the recycle line configured to mix the fuel stream with the exhaust stream; an oxygen-depleted line fluidly connected to the first outlet; and a primary heat exchanger disposed on the recycle line and fluidly connected to the oxygen-depleted line, wherein the primary beat exchanger is located downstream of the first outlet and upstream of the mixer, and is configured to heat exchange the exhaust stream with an oxygen-depleted stream that egresses the first outlet to raise a temperature of the exhaust stream. ### Claim 2 (depends on 1) The combustion system of claim 1, further comprising: a swirler control unit comprising a first gas analyzer disposed on the fuel line configured to determine a composition of the fuel stream, a second gas analyzer disposed on the exhaust line configured to determine a composition of the exhaust stream, an actuator connected to the adjustable blades of the swirler configured to adjust an angle of the adjustable blades, and a processor that is configured to receive a first signal from the first gas analyzer and a second signal from the second gas analyzer, and to transmit a first output signal to the actuator, wherein the swirler control unit is configured to adjust an angle of the adjustable blades based on the composition of the fuel stream and the exhaust stream. ### Claim 3 (depends on 2) The combustion system of claim 2, further comprising: a flow control unit comprising: the first gas analyzer disposed on the fuel line configured to determine the composition of the fuel stream, a flowmeter disposed on the fuel line configured to determine a volumetric flow rate of the fuel stream, a first control valve disposed on the feed line configured to control a volumetric flow rate of the oxygen-containing stream, a flow controller that is configured to receive the first signal from the first gas analyzer and a flow rate signal from the flowmeter, and to transmit a second output signal to the first control valve, wherein the flow control unit is configured to control the volumetric flow rate of the oxygen-containing stream based on the composition and volumetric flow rate of the fuel stream. ### Claim 4 (depends on 3) The combustion system of claim 3, further comprising: a temperature control unit comprising: a temperature sensor disposed on the exhaust line configured to determine the temperature of the exhaust stream, a second control valve disposed on the recycle line configured to control a volumetric flow rate of the exhaust stream, a temperature controller configured to receive a temperature signal from the temperature sensor, and to transmit a third output signal to the second control valve, wherein the temperature control unit is configured to control a temperature of the fuel stream based on the temperature of the exhaust stream. ### Claim 5 (depends on 1) The combustion system of claim 1, further comprising: a secondary heat exchanger disposed on the feed line and fluidly connected to the oxygen-depleted line, wherein the secondary heat exchanger is located upstream of the first inlet and downstream of the first outlet, and is configured to heat exchange the oxygen-containing stream with the oxygen-depleted stream that egresses the first outlet. ### Claim 6 (depends on 1) The combustion system of claim 1, further comprising: a condenser located downstream of and fluidly connected to the expander via the exhaust line configured to separate a liquid phase from the exhaust stream. ### Claim 7 (depends on 1) The combustion system of claim 1, wherein the combustor further comprises: a third concentric cylindrical zone sandwiched between the first and the second concentric cylindrical zones, defining a sweep zone; and a third inlet and a third outlet located in the sweep zone. ### Claim 8 (depends on 7) The combustion system of claim 7, wherein the recycle line fluidly connects the exhaust line to the third inlet. ### Claim 9 (depends on 1) The combustion system of claim 1, wherein the swirler comprises a plurality of the adjustable blades extending radially from a shaft, wherein each blade of the plurality of the adjustable blades has a longitudinal axis and an angle of the longitudinal axis of said each blade is adjustable relative to a longitudinal axis of the shaft. ### Claim 10 (depends on 9) The combustion system of claim 9, wherein the angle of the longitudinal axis of said each blade is adjustable in the range of 0 to 85 degrees relative to the longitudinal axis of the shaft. ### Claim 11 (depends on 1) The combustion system of claim 1, wherein the combustor further comprises a third concentric cylindrical zone which is sandwiched between the first and the second concentric cylindrical zones, defining a sweep zone, and a third inlet and a third outlet located in the sweep zone. ### Claim 12 A process for combusting a fuel stream with a combustor comprising: a cylindrical vessel with an internal cavity; an ion transport membrane that divides the internal cavity of said cylindrical vessel into a first and a second concentric cylindrical tone, wherein the first concentric cylindrical zone is a feed zone and the second concentric cylindrical zone is a combustion zone; a first inlet and a first outlet located in the feed zone, and a second inlet and a second outlet located in the combustion zone; a swirler that is connected to the second inlet, wherein the swirler has adjustable blades with adjustable angles; a third concentric cylindrical zone which is sandwiched between the first and the second concentric cylindrical zones, defining a sweep zone; and a third inlet and a third outlet located in the sweep zone, the process comprising: combusting the fuel stream with molecular oxygen in the combustion zone to form an exhaust stream comprising water vapor and carbon dioxide; delivering an oxygen-containing stream to the first inlet of the combustor, wherein molecular oxygen present in the oxygen-containing stream is transported to the sweep zone through the ion transport membrane; flowing a portion of the exhaust stream into the third inlet of the combustor to sweep the molecular oxygen away from the sweep zone and to form an oxygen-enriched stream; mixing the oxygen-enriched stream with the fuel stream in a mixer to form a combustion mixture; and delivering the combustion mixture to the second inlet of the combustor, wherein the combustion mixture is expanded and/or agitated in the combustion zone via the swirler and is combusted to form the exhaust stream; and repeating the flowing, the mixing, and the delivering. ### Claim 13 (depends on 12) The process of claim 12, wherein the fuel stream is a syngas stream. ### Claim 14 (depends on 12) The process of claim 12, further comprising: expanding the exhaust stream in an expander to generate power. ### Claim 15 (depends on 12) The process of claim 12, further comprising: adjusting the adjustable angles of the adjustable blades of the swirler based on a composition of the combustion mixture.