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公开(公告)号：US11101688B2
公开(公告)日：2021-08-24
申请号：US16434289
申请日：2019-06-07
Applicant: GE Aviation Systems Limited
Inventor： Colin John Halsey
Abstract: 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.
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公开(公告)号：US10913543B2
公开(公告)日：2021-02-09
申请号：US15791475
申请日：2017-10-24
Applicant: GE Aviation Systems Limited
Inventor： Michael David Bailey , Colin John Halsey
IPC: H02J7/00 , H01M10/44 , H01M10/46 , B64D41/00 , H01M8/0612 , H01M8/0656 , H01M8/04082 , H01M8/04828 , H01M16/00 , H01M8/086 , H01M8/1018 , H01M8/124 , H01M8/083 , H01M8/14 , H01M8/18
Abstract: 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.
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公开(公告)号：US11040875B2
公开(公告)日：2021-06-22
申请号：US15778977
申请日：2015-11-24
Applicant: GE Aviation Systems Limited
Inventor： Colin John Halsey , Michael David Bailey , Ross Jonathan Williams
IPC: C01B3/06 , C01B3/00 , C01B3/04 , B01J7/02 , H01M8/0606
Abstract: 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.
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公开(公告)号：US20210155477A1
公开(公告)日：2021-05-27
申请号：US17161081
申请日：2021-01-28
Applicant: GE AVIATION SYSTEMS LIMITED
Inventor： Colin John Halsey , Alexander James Rainbow
IPC: C01B3/06 , C01B3/00 , C01B3/04 , H01M8/0612 , H01M8/065
Abstract: 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.
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公开(公告)号：US10958075B2
公开(公告)日：2021-03-23
申请号：US16282790
申请日：2019-02-22
Applicant: GE Aviation Systems Limited
Inventor： John Oliver Collins , Colin John Halsey , Russell Mark Compton
IPC: H02J3/38 , B60R16/03 , H02J9/04 , H02J3/14 , H02J4/00 , H02J9/06 , H02J7/00 , G01R31/42 , G05B19/04
Abstract: 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.
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Patent Agency Ranking
公开(公告)号：US20200017232A1
公开(公告)日：2020-01-16
申请号：US16509666
申请日：2019-07-12
Applicant: GE Aviation Systems Limited
Inventor： Russell Mark Compton , Colin John Halsey
Abstract: 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.
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公开(公告)号：US11269392B2
公开(公告)日：2022-03-08
申请号：US16589732
申请日：2019-10-01
Applicant: GE Aviation Systems Limited
Inventor： Colin John Halsey
Abstract: 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.
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公开(公告)号：US20210359539A1
公开(公告)日：2021-11-18
申请号：US17387600
申请日：2021-07-28
Applicant: GE Aviation Systems Limited
Inventor： Colin John Halsey
Abstract: 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.
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公开(公告)号：US10926870B2
公开(公告)日：2021-02-23
申请号：US15824528
申请日：2017-11-28
Applicant: GE Aviation Systems Limited
Inventor： Colin John Halsey , Michael David Bailey
Abstract: 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.
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公开(公告)号：US20190386510A1
公开(公告)日：2019-12-19
申请号：US16434289
申请日：2019-06-07
Applicant: GE Aviation Systems Limited
Inventor： Colin John Halsey
Abstract: 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.
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