# US 8,464,538 B2 · Trapped vortex combustor and method of operating thereof > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 8,464,538 B2 - Document ID: US8464538B2 - Status: Granted - Kind: B2 - Application number: 12/971,354 - Filed: 2010-12-17 - Published: 2012-06-21 - Granted: 2013-06-18 - Earliest claimed: 2010-12-17 - Assignees: General Electric Company - Applicants: Andrei Tristan Evulet; Gustavo Adolfo Ledezma; Corey Bourassa - Inventors: Andrei Tristan Evulet; Gustavo Adolfo Ledezma; Corey Bourassa - Web page: https://patentgrep.com/patent/US8464538B2 ## CPC - F23R 3/20: incorporating fuel injection means - F23R 3/28: characterised by the fuel supply (burners F23D) - F23R 3/42: characterised by the arrangement or form of the flame tubes or combustion chambers - F23R 2900/00015: Trapped vortex combustion chambers - 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) ## Abstract A trapped vortex combustor includes a trapped vortex cavity having a first surface and a second surface. A plurality of fluidic mixers are disposed circumferentially along the first surface and the second surface of the trapped vortex cavity. At least one fluidic mixer includes a first open end receiving a first fluid stream, a coanda profile in the proximity of the first open end, a fuel plenum to discharge a fuel stream over the coanda profile, and a second open end for receiving the mixture of the first fluid stream and the fuel stream and discharging the mixture of the first fluid stream and the fuel stream in the trapped vortex cavity. The coanda profile is configured to enable attachment of the fuel stream to the coanda profile to form a boundary layer of the fuel stream and, to entrain the incoming first fluid stream to the boundary layer of the fuel stream to form a mixture of the first fluid stream and the fuel stream. ## Claims ### Claim 1 A trapped vortex combustor, comprising: a trapped vortex cavity comprising a first surface and a second surface; a plurality of fluidic mixers disposed circumferentially along the first surface and the second surface of the trapped vortex cavity, wherein at least one fluidic mixer comprises: a first open end receiving a first fluid stream; a coanda profile in the proximity of the first open end; a fuel plenum to discharge a fuel stream over the coanda profile, wherein the coanda profile is configured to enable attachment of the fuel stream to the coanda profile to form a boundary layer of the fuel stream and, to entrain the incoming first fluid stream to the boundary layer of the fuel stream to form a mixture of the first fluid stream and the fuel stream; and a second open end for receiving the mixture of the first fluid stream and the fuel stream and discharging the mixture of the first fluid stream and the fuel stream in the trapped vortex cavity. ### Claim 2 (depends on 1) The trapped vortex combustor of claim 1, further comprising a splitting device disposed at a location upstream of the trapped vortex combustor, for splitting a fluid stream entering the trapped vortex combustor into the first fluid stream and a second fluid stream, a portion of the second fluid stream being directed to the trapped vortex cavity. ### Claim 3 (depends on 2) The trapped vortex combustor of claim 2, wherein the mixture of the first fluid stream and the fuel stream and the portion of the second stream forms a vortex inside the trapped vortex cavity. ### Claim 4 (depends on 2) The trapped vortex combustor of claim 2, wherein the fluid stream comprises air. ### Claim 5 (depends on 2) The trapped vortex combustor of claim 2, wherein the fluid stream comprises an expanded combustion gas. ### Claim 6 (depends on 1) The trapped vortex combustor of claim 1, wherein the first fluid stream forms a shear layer within the boundary layer of the fuel stream to enable mixing of the fuel stream and the first fluid stream. ### Claim 7 (depends on 1) The trapped vortex combustor of claim 1, wherein the fuel plenum is configured to discharge the fuel stream over the coanda profile at a first pressure and the first open end receive the first fluid stream at a second pressure, the first pressure being higher than the second pressure. ### Claim 8 (depends on 1) The trapped vortex combustor of claim 1, wherein the coanda profile deflects the fuel stream supplied through the fuel plenum towards the coanda profile via a Coanda effect. ### Claim 9 (depends on 1) The trapped vortex combustor of claim 1, wherein the at least one fluidic mixer further comprises a diffuser portion having a divergent profile for directing the mixture of the first fluid stream and the fuel stream to the second open end. ### Claim 10 (depends on 1) The trapped vortex combustor of claim 1, wherein the trapped vortex cavity has a rectangular cross-section. ### Claim 11 (depends on 1) The trapped vortex combustor of claim 1, wherein the first surface comprises an inner end and an outer end, the at least one fluidic mixer being disposed on the inner end of the first surface. ### Claim 12 (depends on 1) The trapped vortex combustor of claim 1, wherein the second surface comprises an inner end and an outer end, the at least one fluidic mixer being disposed on the outer end of the second surface. ### Claim 13 (depends on 1) The trapped vortex combustor of claim 1, further comprising a control unit configured to control supply of fuel to the fuel plenum of the at least one fluidic mixer. ### Claim 14 (depends on 13) The trapped vortex combustor of claim 13, wherein the control unit is configured to control the supply of the fuel to the fuel plenum based on a load on the trapped vortex combustor. ### Claim 15 (depends on 1) The trapped vortex combustor of claim 1, wherein the second surface is located opposite to the first surface. ### Claim 16 A method for operating a trapped vortex combustor, the method comprising: splitting a fluid stream entering the trapped vortex combustor into a first fluid stream and a second fluid stream; directing a portion of the second fluid stream to an open end of a trapped vortex cavity in the trapped vortex combustor; diverting the first fluid stream to a plurality of fluidic mixers disposed circumferentially along a first surface and a second surface of the trapped vortex cavity; discharging a fuel stream over a coanda profile in the proximity of a first open end of at least one fluidic mixer of the plurality of fluidic mixers so to enable attachment of the fuel stream to the coanda profile to form a boundary layer of the fuel stream and to entrain the incoming first fluid stream to the boundary layer of the fuel stream to form a mixture of the first fluid stream and the fuel stream; discharging the mixture comprising the first fluid stream and the fuel stream in the trapped vortex cavity via a second open end of the at least one fluidic mixer. ### Claim 17 (depends on 16) The method of claim 16, wherein discharging the mixture comprising the first fluid stream and the fuel stream in the trapped vortex cavity comprises: discharging the mixture comprising the first fluid stream and the fuel stream in the trapped vortex cavity in the proximity of an inner end of the first surface. ### Claim 18 (depends on 16) The method of claim 16, wherein discharging the mixture comprising the first fluid stream and the fuel stream in the trapped vortex cavity comprises: discharging the mixture comprising the first fluid stream and the fuel stream in the trapped vortex cavity in the proximity of an outer end of the second surface. ### Claim 19 (depends on 16) The method of claim 16, further comprises discharging the mixture comprising the first fluid stream and the fuel stream in the trapped vortex cavity via a second open end of the at least one fluidic mixer in such a way that the portion of the second fluid stream and the mixture comprising the first fluid stream and the fuel stream forms a vortex inside the trapped vortex cavity. ### Claim 20 (depends on 16) The method of claim 16, further comprising: discharging the fuel stream over the coanda profile at a first pressure, diverting the first fluid stream to a plurality of fluidic mixers at a second pressure, the first pressure being higher than the second pressure. ### Claim 21 (depends on 16) The method of claim 16 further comprising, deflecting the fuel stream discharged over the coanda profile, towards the coanda profile via a Coanda effect.