# US 11,441,485 B2 · Electric motor control for demand fuel pumping system > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 11,441,485 B2 - Document ID: US11441485B2 - Status: Granted - Kind: B2 - Application number: 16/815,802 - Filed: 2020-03-11 - Published: 2021-06-17 - Granted: 2022-09-13 - Earliest claimed: 2019-03-20 - Assignees: Raytheon Technologies Corporation - Applicants: United Technologies Corporation - Inventors: Neal R. Herring - Web page: https://patentgrep.com/patent/US11441485B2 ## CPC - F02C 7/22: Fuel supply systems - F02C 7/236: Fuel delivery systems comprising two or more pumps - F02C 7/224: Heating fuel before feeding to the burner - F02C 9/26: Control of fuel supply (F02C9/48 takes precedence; fuel valves F02C7/232) - F02C 9/46: Emergency fuel control - F05D 2260/213: by the provision of a heat exchanger within the cooling circuit - F05D 2260/84: Redundancy - F05D 2270/46: redundant, i.e. failsafe operation - 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) - F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS - Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION ## Abstract A fuel system for a gas turbine engine includes a first electric motor, a main fuel pump driven by the first electric motor to provide a fuel flow, and an actuator operable by a second electric motor. A first motor controller governs operation of the first electric motor. A second motor controller governs operation of the second electric motor. The second motor controller is operable to control operation of the first electric motor in response the first motor controller being incapable of governing operation of the first electric motor. ## Claims ### Claim 1 A fuel system for a gas turbine engine comprising: a first electric motor; a main fuel pump driven by the first electric motor to provide a fuel flow; an actuator operable by a second electric motor wherein the actuator comprises a control surface system for moving a surface; a first motor controller governing operation of the first electric motor; a second motor controller governing operation of the second electric motor, wherein the second motor controller is operable to control operation of the first electric motor in response to the first motor controller being incapable of governing operation of the first electric motor; and a default mechanical device for moving the surface to a default position in response to the second motor controller being utilized to control the first electric motor. ### Claim 2 (depends on 1) The fuel system as recited in claim 1, including a control system controlling operation of the first motor controller and the second motor controller and switching of the second motor controller to control operation of the first electric motor. ### Claim 3 (depends on 1) The fuel system as recited in claim 1, wherein the control surface system includes a default motor control that is operable to control the second electric motor in response to the second motor controller being utilized for the first electric motor. ### Claim 4 (depends on 3) The fuel system as recited in claim 3, wherein the default motor control is positioned with the actuator. ### Claim 5 (depends on 1) The fuel system as recited in claim 1, including a heat exchanger receiving at least a portion of the fuel flow from the main fuel pump for cooling a flow from another system of the gas turbine engine. ### Claim 6 (depends on 1) The fuel system as recited in claim 1, wherein the first electric motor drives the main fuel pump at a speed that varies to tailor the fuel flow to an engine operating condition. ### Claim 7 (depends on 1) The fuel system as recited in claim 1, wherein the actuator comprises a component operable independent of the first electric motor. ### Claim 8 A gas turbine engine comprising: a fan rotatable within a fan nacelle; a core engine including a compressor communicating compressed air to a combustor where the compressed air is mixed with fuel and ignited to generate a high-energy gas flow expanded through a turbine; a fuel system including a main fuel pump driven by a first electric motor to provide a fuel flow, wherein the first electric motor drives the main fuel pump at a speed that varies to tailor the fuel flow to an engine operating condition; an actuator operable by a second electric motor, wherein the actuator is part of a control surface system; a control system including a first motor controller governing operation of the first electric motor and a second motor controller governing operation of the second electric motor, wherein the second motor controller is operable to control operation of the first electric motor in response the first motor controller being incapable of governing operation of the first electric motor; and a default mechanical device for moving a surface of the control surface system to a default position in response to the second motor controller being utilized to control the first electric motor. ### Claim 9 (depends on 8) The gas turbine engine as recited in claim 8, wherein the control system controls operation of the first motor controller and the second motor controller and switching of the second motor controller to control operation of the first electric motor. ### Claim 10 (depends on 8) The gas turbine engine as recited in claim 8, wherein the control surface system includes a default motor control that is operable to control the second electric motor in response to the second motor controller being utilized for the first electric motor. ### Claim 11 (depends on 8) The gas turbine engine as recited in claim 8, including a heat exchanger receiving at least a portion of the fuel flow from the main fuel pump for cooling a flow from another system of the gas turbine engine. ### Claim 12 A method of controlling a fuel pump for a gas turbine engine comprising: generating a fuel flow with the fuel pump driven by a first electric motor, wherein operation of the first electric motor is governed by a first motor controller; and switching control of the first electric motor from the first motor controller to a second motor controller in response to the first motor controller being incapable of controlling the first electric motor, wherein the second motor controller governs operation of a second electric motor that is part of an electromagnetic actuator prior to taking control of the first electric motor; and engaging a default system of the electromagnetic actuator in response to the second motor controller being switched to control the first electric motor, wherein the default system is a mechanical device for moving a portion of the electromagnetic actuator to a default position. ### Claim 13 (depends on 12) The method as recited in claim 12, wherein the fuel pump is driven by the first electric motor to vary the fuel flow to minimize excess fuel flow. ### Claim 14 (depends on 12) The method as recited in claim 12, including cooling a flow from another engine system with the fuel flow. ### Claim 15 (depends on 12) The method as recited in claim 12, wherein the default system is a default motor control disposed at the second electric motor for moving the second electric motor in a predefined default manner.