Patents by Inventor COLIN JOHN HALSEY
COLIN JOHN HALSEY has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 11718520Abstract: A hydrogen storage system includes a pressure-sealed sleeve defining an interior and having an outlet, a shaft extending through the interior of the sleeve, a set of porous chambers arranged axially along and concentric to the shaft, and a hydrogen storage, wherein at least some hydrogen gas is supplied to the outlet.Type: GrantFiled: January 28, 2021Date of Patent: August 8, 2023Assignee: GE Aviation Systems LimitedInventors: Colin John Halsey, Alexander James Rainbow
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Patent number: 11462937Abstract: A method and apparatus for no-break power transfer in a power distribution system, including providing, from a first power source, a first power supply to a power bus, disabling the first power supply from the power bus, and providing, from a second power source, a second power supply to the power bus, the second power supply having the second set of electrical characteristics.Type: GrantFiled: July 28, 2021Date of Patent: October 4, 2022Assignee: GE Aviation Systems LimitedInventor: Colin John Halsey
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Patent number: 11269392Abstract: A method for maintaining a power source can include selecting, by a controller module, a rechargeable power storage device from a set of power storage devices arranged to selectively provide a summated output of the power source, and selectively enabling the selected power storage device to discharge its stored power at the output of the power source. The controller module can compare a sensed voltage of the selected power storage device with a minimum voltage threshold.Type: GrantFiled: October 1, 2019Date of Patent: March 8, 2022Assignee: GE Aviation Systems LimitedInventor: Colin John Halsey
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Publication number: 20210359539Abstract: A method and apparatus for no-break power transfer in a power distribution system, including providing, from a first power source, a first power supply to a power bus, disabling the first power supply from the power bus, and providing, from a second power source, a second power supply to the power bus, the second power supply having the second set of electrical characteristics.Type: ApplicationFiled: July 28, 2021Publication date: November 18, 2021Inventor: Colin John Halsey
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Patent number: 11142332Abstract: A method and apparatus for a power distribution system, includes providing, from a power source having a set of dischargeable power storage devices connected by way of selectable connections, a power supply to a voltage output, and switchably connecting the voltage output to a set of power outputs having different electrical characteristics.Type: GrantFiled: July 12, 2019Date of Patent: October 12, 2021Assignee: GE Aviation Systems LimitedInventors: Russell Mark Compton, Colin John Halsey
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Publication number: 20210309514Abstract: A solid state storage system includes a pressure-sealed storage unit defining an interior and having an outlet, an upper manifold and a lower manifold separated by a dividing plane having a set of ports, a set of chambers, and a solid state storage, wherein at least some gas is supplied to the outlet.Type: ApplicationFiled: June 21, 2021Publication date: October 7, 2021Inventors: Colin John HALSEY, Michael David BAILEY, Ross Jonathan WILLIAMS
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Patent number: 11101688Abstract: A method and apparatus for no-break power transfer in a power distribution system, including providing, from a first power source, a first power supply to a power bus, disabling the first power supply from the power bus, and providing, from a second power source, a second power supply to the power bus, the second power supply having the second set of electrical characteristics.Type: GrantFiled: June 7, 2019Date of Patent: August 24, 2021Assignee: GE Aviation Systems LimitedInventor: Colin John Halsey
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Patent number: 11040875Abstract: A hydrogen storage system includes a pressure-sealed storage unit defining an interior and having an outlet, an upper manifold and a lower manifold separated by a dividing plane having a set of ports, a set of chambers, and a hydrogen storage, wherein at least some hydrogen gas is supplied to the outlet.Type: GrantFiled: November 24, 2015Date of Patent: June 22, 2021Assignee: GE Aviation Systems LimitedInventors: Colin John Halsey, Michael David Bailey, Ross Jonathan Williams
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Publication number: 20210155477Abstract: A hydrogen storage system includes a pressure-sealed sleeve defining an interior and having an outlet, a shaft extending through the interior of the sleeve, a set of porous chambers arranged axially along and concentric to the shaft, and a hydrogen storage, wherein at least some hydrogen gas is supplied to the outlet.Type: ApplicationFiled: January 28, 2021Publication date: May 27, 2021Inventors: Colin John Halsey, Alexander James Rainbow
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Patent number: 10958083Abstract: In one aspect, there is disclosed a cell stack which can include cell modules connected in series to generate a stack operating voltage. The cell modules can include a battery cell in series with a series switch and include a shunt switch connected in parallel to the battery cell and the series switch. A stack monitor circuit can have a series control coupled to the series switch, a shunt control coupled to the shunt switch, and a battery cell monitor coupled to the battery cell for measuring a cell parameter from each cell module. Based on the measured cell parameter, the stack monitor circuit can select at least one cell module either to contribute to the stack operating voltage by closing the series switch and opening the shunt switch or to bypass the stack operating voltage by the opening the series switch and closing the shunt switch.Type: GrantFiled: February 16, 2018Date of Patent: March 23, 2021Assignee: GE Aviation Systems LimitedInventor: Colin John Halsey
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Patent number: 10958075Abstract: An alternating-current power source can include a set of power storage units arranged in series and defining a power output. Each power storage unit can include a power storage device, a first connection configured to enable a voltage output of the power storage device, and a second connection configured to enable bypassing the voltage output of the power storage device.Type: GrantFiled: February 22, 2019Date of Patent: March 23, 2021Assignee: GE Aviation Systems LimitedInventors: John Oliver Collins, Colin John Halsey, Russell Mark Compton
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Patent number: 10934165Abstract: A hydrogen storage system includes a pressure-sealed sleeve defining an interior and having an outlet, a shaft extending through the interior of the sleeve, a set of porous chambers arranged axially along and concentric to the shaft, and a hydrogen storage, wherein at least some hydrogen gas is supplied to the outlet.Type: GrantFiled: August 20, 2015Date of Patent: March 2, 2021Assignee: GE AVIATION SYSTEMS LIMITEDInventors: Colin John Halsey, Alexander James Rainbow
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Patent number: 10926870Abstract: A method and apparatus for operating a power system architecture including an electrical power storage system, a power distribution bus selectively connected with the electrical power storage device, a hydraulic pump selectively connected with the electrical power storage device and a controller module communicatively connected with the electrical power storage system and the hydraulic pump.Type: GrantFiled: November 28, 2017Date of Patent: February 23, 2021Assignee: GE Aviation Systems LimitedInventors: Colin John Halsey, Michael David Bailey
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Patent number: 10913543Abstract: Systems and methods for providing power to one or more loads on an aircraft are provided. A power system for an aircraft can include a first fuel cell configured to provide base power to one or more loads on the aircraft. The power system can further include a second fuel cell configured to provide peak power to the one or more loads on the aircraft. The peak power can be a power exceeding the base power. The power system can further include an energy storage device configured to provide transient power to the one or more loads on the aircraft. The transient power can be a power exceeding the peak power. The power system can further include a controller configured to control delivery of power from the first fuel cell, the second fuel cell, and the energy storage device to the one or more loads on the aircraft.Type: GrantFiled: October 24, 2017Date of Patent: February 9, 2021Assignee: GE Aviation Systems LimitedInventors: Michael David Bailey, Colin John Halsey
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Patent number: 10822232Abstract: A solid hydrogen reaction system and method of liberating hydrogen gas includes the utilization of a reactor having a body that defines a reaction chamber, having a first narrow end and a second wider end such that the reactor has an increasing cross-sectional area from the first end toward the second end, for facilitating a reaction to liberate hydrogen gas stored in a hydrogen storage solid located within the reaction chamber.Type: GrantFiled: January 10, 2019Date of Patent: November 3, 2020Assignee: GE Aviation Systems LLCInventor: Colin John Halsey
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Patent number: 10814992Abstract: A power source for an aircraft including a solid oxide fuel cell and a proton exchange membrane fuel cell along with a solid oxide fuel cell multi-power source. At least one battery is electrically coupled to the solid oxide fuel cell, the proton exchange membrane fuel cell, and an aircraft distribution network to supply electricity to the aircraft and also for becoming recharged by the solid oxide fuel cell and the proton exchange membrane fuel cell.Type: GrantFiled: November 16, 2017Date of Patent: October 27, 2020Assignee: GE Aviation Systems LimitedInventors: Colin John Halsey, Michael David Bailey
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Patent number: 10777861Abstract: A battery pack for carrying one or more battery cells in the battery pack can include a chassis defining a body for holding the battery cells. The chassis can include a set of vertical battery cell holders adapted to hold the battery cells. A set of horizontal passages can be provided in the chassis between the set of vertical battery cell holders. A cap assembly can be provided at one end of the battery cells and within the body providing venting for the battery cells through the battery cell holders.Type: GrantFiled: May 10, 2018Date of Patent: September 15, 2020Assignee: GE Aviation Systems LimitedInventors: Colin John Halsey, Michael James Smith
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Publication number: 20200103950Abstract: A method for maintaining a power source can include selecting, by a controller module, a rechargeable power storage device from a set of power storage devices arranged to selectively provide a summated output of the power source, and selectively enabling the selected power storage device to discharge its stored power at the output of the power source. The controller module can compare a sensed voltage of the selected power storage device with a minimum voltage threshold.Type: ApplicationFiled: October 1, 2019Publication date: April 2, 2020Inventor: Colin John Halsey
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Patent number: 10569904Abstract: In one aspect, there is disclosed a taxi vehicle comprising a chassis having a coupler to connect to a coupling location of a craft and a set of wheels with at least one electric motor coupled to the set of wheels. The taxi vehicle can include a fuel cell coupled to the at least one electric motor and a battery coupled to the fuel cell. The battery can be configured to supply peak power demand to the at least one electric motor to start moving the craft. The battery can receive charging from the fuel cell when not supplying peak power demand while the fuel cell supplies power to the at least one electric motor to continue moving the craft.Type: GrantFiled: November 7, 2017Date of Patent: February 25, 2020Assignee: GE Aviation Systems LimitedInventors: Colin John Halsey, Michael David Bailey
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Patent number: 10547183Abstract: A high voltage battery pack includes a set of battery bricks, wherein the battery bricks each have a positive and a negative terminal. Each battery brick is connected in series or in parallel to an adjacent battery brick to generate a total voltage of the battery pack. A battery pack lower assembly holds the battery bricks. A battery pack upper assembly includes a battery pack upper housing and a circuit board connected to the battery pack upper housing, the circuit board having brick connectors attached thereto. The brick connectors are positioned to come into physical contact with the positive and negative terminals of the battery bricks to generate the total voltage of the battery pack, and the battery pack upper housing defines a physical separation distance between the brick connectors and an exterior of the battery pack upper housing.Type: GrantFiled: May 24, 2018Date of Patent: January 28, 2020Assignee: GE Aviation Systems LimitedInventor: Colin John Halsey