# US 2021/0340913 A1 · Fuel oxygen reduction unit with bleed driven boost impeller > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 2021/0340913 A1 - Document ID: US20210340913A1 - Status: Published application - Kind: A1 - Application number: 16/864,349 - Filed: 2020-05-01 - Published: 2021-11-04 - Earliest claimed: 2020-05-01 - Assignees: General Electric Company - Applicants: General Electric Company - Inventors: Peter Allen Andrews, JR.; Ethan Patrick O'Connor; David Vickery Parker; Brandon Wayne Miller; Richard Alan Wesling; Christian Xavier Stevenson - Web page: https://patentgrep.com/patent/US20210340913A1 ## CPC - F02C 7/22: Fuel supply systems - C10G 29/00: Refining of hydrocarbon oils, in the absence of hydrogen, with other chemicals - F02C 3/00: Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C5/00) - 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 - Y02T 50/60: Efficient propulsion technologies, e.g. for aircraft - 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) - C10G: CRACKING HYDROCARBON OILS; PRODUCTION OF LIQUID HYDROCARBON MIXTURES, e.g. BY DESTRUCTIVE HYDROGENATION, OLIGOMERISATION, POLYMERISATION (cracking to hydrogen or synthesis gas C01B; cracking or pyrolysis of hydrocarbon gases to individual hydrocarbons or mixtures thereof of definite or specified constitution C07C; cracking to cokes C10B); RECOVERY OF HYDROCARBON OILS FROM OIL-SHALE, OIL-SAND, OR GASES; REFINING MIXTURES MAINLY CONSISTING OF HYDROCARBONS; REFORMING OF NAPHTHA; MINERAL WAXES - Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION ## Abstract A fuel delivery system for a gas turbine engine including a fuel oxygen reduction unit is provided. The fuel oxygen reduction unit defines a liquid fuel flowpath and a stripping gas flowpath and is configured to transfer an oxygen content of a fuel flow through the liquid fuel flowpath to a stripping gas flow through the stripping gas flowpath. The fuel oxygen reduction unit includes an impeller in airflow communication with the stripping gas flowpath for circulating the stripping gas flow through the stripping gas flowpath; and a turbine coupled to the impeller. ## Claims ### Claim 1 A fuel delivery system for a gas turbine engine comprising: a fuel oxygen reduction unit defining a liquid fuel flowpath and a stripping gas flowpath and configured to transfer an oxygen content of a fuel flow through the liquid fuel flowpath to a stripping gas flow through the stripping gas flowpath, the fuel oxygen conversion unit comprising: an impeller in airflow communication with the stripping gas flowpath for circulating the stripping gas flow through the stripping gas flowpath; and a turbine coupled to the impeller. ### Claim 2 (depends on 1) The fuel delivery system of claim 1, wherein the turbine is powered by a bleed air through a bleed air conduit, and wherein the stripping gas flowpath of the fuel oxygen reduction unit is in airflow communication with the bleed air conduit. ### Claim 3 (depends on 1) The fuel delivery system of claim 1, wherein the turbine is powered by a bleed air, and wherein the impeller is coupled to, and driven by, the turbine. ### Claim 4 (depends on 3) The fuel delivery system of claim 3, wherein the turbine is powered by a main engine bleed air. ### Claim 5 (depends on 4) The fuel delivery system of claim 4, further comprising: a first valve downstream of the turbine, wherein the first valve modulates the main engine bleed air downstream of the turbine to control a speed of rotation of the impeller. ### Claim 6 (depends on 5) The fuel delivery system of claim 5, further comprising: a second valve upstream of the turbine, wherein the second valve modulates the main engine bleed air upstream of the turbine to control the speed of rotation of the impeller. ### Claim 7 (depends on 1) The fuel delivery system of claim 1, wherein the fuel oxygen conversion unit comprises: a contactor including a fuel inlet that receives the fuel flow from the liquid fuel flowpath and a stripping gas inlet that receives the stripping gas flow from the stripping gas flowpath, the contactor configured to form a fuel/gas mixture; and a separator including an inlet in fluid communication with the contactor that receives the fuel/gas mixture, a fuel outlet, and a stripping gas outlet, wherein the separator is configured to separate the fuel/gas mixture into an outlet stripping gas flow and an outlet fuel flow and provide the outlet stripping gas flow through the stripping gas outlet back to the stripping gas flowpath and the outlet fuel flow through the fuel outlet back to the liquid fuel flowpath. ### Claim 8 (depends on 7) The fuel delivery system of claim 7, wherein the separator is coupled to a second power source that is separate from the turbine. ### Claim 9 (depends on 7) The fuel delivery system of claim 7, further comprising: a catalyst disposed downstream of the separator, the catalyst receives and treats the outlet stripping gas flow, wherein an inlet stripping gas flow exits the catalyst; wherein the impeller is disposed between the catalyst and the contactor. ### Claim 10 A fuel delivery system for a gas turbine engine comprising: a fuel source; a draw pump downstream of the fuel source for generating a liquid fuel flow from the fuel source; a main fuel pump downstream of the draw pump; and a fuel oxygen reduction unit downstream of the draw pump and upstream of the main fuel pump, the fuel oxygen reduction unit comprising: a stripping gas line; a contactor in fluid communication with the stripping gas line and the draw pump for forming a fuel/gas mixture, wherein the contactor receives an inlet fuel flow from the draw pump; a separator in fluid communication with the contactor, the separator receives the fuel/gas mixture and separates the fuel/gas mixture into an outlet stripping gas flow and an outlet fuel flow at a location upstream of the main fuel pump; an impeller disposed downstream of the separator and upstream of the contactor, wherein the impeller circulates a stripping gas to the contactor; and a turbine coupled to the impeller. ### Claim 11 (depends on 10) The fuel delivery system of claim 10, wherein the turbine is powered by a bleed air, and wherein the impeller is coupled to, and driven by, the turbine. ### Claim 12 (depends on 11) The fuel delivery system of claim 11, wherein the turbine is powered by a main engine bleed air. ### Claim 13 (depends on 12) The fuel delivery system of claim 12, further comprising: a first valve downstream of the turbine, wherein the first valve modulates the main engine bleed air downstream of the turbine to control a speed of rotation of the impeller. ### Claim 14 (depends on 13) The fuel delivery system of claim 13, further comprising: a second valve upstream of the turbine, wherein the second valve modulates the main engine bleed air upstream of the turbine to control the speed of rotation of the impeller. ### Claim 15 (depends on 10) The fuel delivery system of claim 10, wherein the separator is coupled to a second power source that is separate from the turbine. ### Claim 16 (depends on 15) The fuel delivery system of claim 15, wherein an input shaft of the separator is coupled to, and driven by, an accessory gearbox. ### Claim 17 (depends on 10) The fuel delivery system of claim 10, further comprising: a catalyst disposed downstream of the separator, the catalyst receives and treats the outlet stripping gas flow, wherein an inlet stripping gas flow exits the catalyst; wherein the impeller is disposed between the catalyst and the contactor. ### Claim 18 (depends on 11) The fuel delivery system of claim 11, wherein the turbine comprises a bleed gas recovery turbine. ### Claim 19 (depends on 12) The fuel delivery system of claim 12, wherein the main engine bleed air comprises a high pressure compressor bleed air, and wherein the fuel oxygen reduction unit recirculates the high pressure compressor bleed air back to a high pressure compressor of a main engine. ### Claim 20 A method for operating a fuel delivery system comprising: using a fuel oxygen reduction unit to reduce an oxygen content of a fuel flow through the fuel delivery system, wherein using the fuel oxygen reduction unit comprises operating a gas pump in fluid communication with a stripping gas flowpath of the fuel oxygen reduction unit at a first speed; and operating a separator in fluid communication with the stripping gas flowpath of the fuel oxygen reduction unit and a fuel flowpath of the fuel delivery system at a second speed that is different than the first speed.