Patents by Inventor John Bywater
John Bywater 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: 11536192Abstract: A rotary turbine bypass valve comprises a valve chamber positioned at a junction of an inlet port, an outlet port and a bypass port, the inlet port configured for fluid communication with a flow of exhaust gas from an engine, the outlet port configured for fluid communication with an inlet of a turbine, and the bypass port configured for fluid communication with an exhaust aftertreatment device; and a valve rotor supported for rotation, about a valve axis, within the valve chamber. The valve rotor is rotatable about the valve axis between a first position in which the valve rotor permits gas flow through the bypass port and a second position in which the valve rotor blocks gas flow through the bypass port.Type: GrantFiled: August 22, 2018Date of Patent: December 27, 2022Assignee: CUMMINS LTD.Inventors: Robin Daniels, Gareth Williamson, Ross Deacon, Laith Al-Kazaz, Thomas Morton, Christopher Parry, Richard Goodyear, Mark R. Holden, Jon-Luke Keating, Waqas Ali, John Bywater, Thomas Roberts
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Patent number: 11280259Abstract: There is provided a turbine comprising: a turbine housing; a turbine wheel; an inlet upstream of the turbine wheel, the inlet defining a first inlet portion and a second inlet portion; an outlet downstream of the turbine wheel, the outlet defining a first outlet portion and a second outlet portion; and a wastegate arrangement configured to selectively vent exhaust gas from the first inlet portion to the first outlet portion via a first bypass passage, and further configured to selectively vent exhaust gas from the second inlet portion to the second outlet portion via a second bypass passage; wherein the first outlet portion and the second outlet portion are separated by a baffle of the turbine housing.Type: GrantFiled: October 17, 2018Date of Patent: March 22, 2022Assignee: CUMMINS LTDInventors: Oscar McGeehan, John Bywater, Richard Goodyear, Mark R. Holden, George E. Sandford
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Publication number: 20200370473Abstract: There is provided a turbine comprising: a turbine housing; a turbine wheel; an inlet upstream of the turbine wheel, the inlet defining a first inlet portion and a second inlet portion; an outlet downstream of the turbine wheel, the outlet defining a first outlet portion and a second outlet portion; and a wastegate arrangement configured to selectively vent exhaust gas from the first inlet portion to the first outlet portion via a first bypass passage, and further configured to selectively vent exhaust gas from the second inlet portion to the second outlet portion via a second bypass passage; wherein the first outlet portion and the second outlet portion are separated by a baffle of the turbine housing.Type: ApplicationFiled: October 17, 2018Publication date: November 26, 2020Inventors: Oscar McGeehan, John Bywater, Richard Goodyear, Mark R. Holden, George E. Sandford
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Publication number: 20200362752Abstract: A rotary turbine bypass valve comprises a valve chamber positioned at a junction of an inlet port, an outlet port and a bypass port, the inlet port configured for fluid communication with a flow of exhaust gas from an engine, the outlet port configured for fluid communication with an inlet of a turbine, and the bypass port configured for fluid communication with an exhaust aftertreatment device; and a valve rotor supported for rotation, about a valve axis, within the valve chamber. The valve rotor is rotatable about the valve axis between a first position in which the valve rotor permits gas flow through the bypass port and a second position in which the valve rotor blocks gas flow through the bypass port.Type: ApplicationFiled: August 22, 2018Publication date: November 19, 2020Inventors: Robin Daniels, Gareth Williamson, Ross Deacon, Laith Al-Kazaz, Thomas Morton, Christopher Parry, Richard Goodyear, Mark R. Holden, Jon-Luke Keating, Waqas Ali, John Bywater, Thomas Roberts
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Patent number: 10605111Abstract: A turbine generator comprises an elongate member, a support structure, a turbine wheel and an electrical generator. The support structure comprises a shaft and support the elongate member for rotation about a rotation axis. The turbine wheel is attached to the elongate member. The electrical generator comprises a rotor and a stator, the rotor being attached to the elongate member and the stator being arranged around the elongate member. The elongate member is provided with a bore and the shaft extends through an end of the elongate member into the bore so as to support it for rotation about the rotation axis.Type: GrantFiled: July 27, 2015Date of Patent: March 31, 2020Assignee: Cummins Ltd.Inventor: John Bywater
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Patent number: 10570812Abstract: A variable geometry turbine having a turbine wheel, an inlet passageway, a movable wall member being moveable axially to vary the width of the inlet passageway, an annular seal being mounted to the movable wall member or an adjacent housing member to provide a seal between adjacent surfaces of the movable wall member and housing member respectively, wherein a bypass passage is provided in the other of said movable wall member or housing member, extending from an inlet bypass port to an outlet bypass port, said ports being spaced from each other and provided in said adjacent surface of said other of the movable wall member or housing member, arranged such that as the movable wall member moves axially, the annular seal moves axially relative to the ports to vary the flow that may pass from a region of the cavity inboard of the seal, through the bypass passage.Type: GrantFiled: October 9, 2015Date of Patent: February 25, 2020Assignee: Cummins Ltd.Inventors: Lisa Jane Hill, John F. Parker, John Bywater
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Publication number: 20180252152Abstract: A variable geometry turbine having a turbine wheel, an inlet passageway, a movable wall member being moveable axially to vary the width of the inlet passageway, an annular seal being mounted to the movable wall member or an adjacent housing member to provide a seal between adjacent surfaces of the movable wall member and housing member respectively, wherein a bypass passage is provided in the other of said movable wall member or housing member, extending from an inlet bypass port to an outlet bypass port, said ports being spaced from each other and provided in said adjacent surface of said other of the movable wall member or housing member, arranged such that as the movable wall member moves axially, the annular seal moves axially relative to the ports to vary the flow that may pass from a region of the cavity inboard of the seal, through the bypass passage.Type: ApplicationFiled: October 9, 2015Publication date: September 6, 2018Inventors: Lisa Jane Hill, John F. Parker, John Bywater
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Publication number: 20170268373Abstract: A turbine generator comprises an elongate member, a support structure, a turbine wheel and an electrical generator. The support structure comprises a shaft and supports the elongate member for rotation about a rotation axis. The turbine wheel attached to the elongate member. The electrical generator comprises a rotor and a stator, the rotor being attached to the elongate member and the stator being arranged around the elongate member. The elongate member is provided with a bore and the shaft extends through an end of the elongate member into the bore so as to support it for rotation about the rotation axis.Type: ApplicationFiled: July 27, 2015Publication date: September 21, 2017Inventor: John Bywater
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Patent number: 7083379Abstract: A compressor for compressing a gas comprises an impeller wheel (1) including a plurality of vanes (4) rotatably mounted within a housing (2). The housing (2) has an inner wall defining a surface (5) located in close proximity to radially outer edges (4a) of impeller vanes (4). The compressor inlet comprises an outer tubular wall (7) extending forming a gas intake and an inner tubular wall (8) extending within the outer tubular wall (7) and defining an inducer portion (10) of the inlet. An annular gas flow passage (11) is defined between the inner and outer tubular walls. There is at least one downstream aperture (13) communicating between the annular flow passage (11) and the surface (5) of the housing (2) swept by the impeller vanes (4) and at least one upstream aperture communicating between the annular flow passage (11) and the inducer or intake portions of the inlet.Type: GrantFiled: March 23, 2004Date of Patent: August 1, 2006Assignee: Holset Engineering Company, LimitedInventors: Bahram Nikpour, Andrew Day, Roy Saxton, John Bywater
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Patent number: 6895314Abstract: One or more small self-contained reentry breakup recorders are disposed within a spacecraft and each includes a sensor suite for collecting and recording collected and recorded sensory data during reentry breakup of the spacecraft, and includes a communications system for broadcasting the collected and recorded sensory data after breakup and before impact with the surface of the earth to a remote communication system for preserving the sensory data of the breakup as well as data relating to critical events occurring prior to breakup. An internal GPS receiver provides sensory positional data of the reentry and breakup positions.Type: GrantFiled: June 11, 2003Date of Patent: May 17, 2005Assignee: The Aerospace CorporationInventors: William Henry Ailor, Ronald John Bywater, Leon Gurevich
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Publication number: 20050002782Abstract: A compressor for compressing a gas comprises an impeller wheel (1) including a plurality of vanes (4) rotatably mounted within a housing (2). The housing (2) has an inner wall defining a surface (5) located in close proximity to radially outer edges (4a) of impeller vanes (4). The compressor inlet comprises an outer tubular wall (7) extending forming a gas intake and an inner tubular wall (8) extending within the outer tubular wall (7) and defining an inducer portion (10) of the inlet. An annular gas flow passage (11) is defined between the inner and outer tubular walls. There is at least one downstream aperture (13) communicating between the annular flow passage (11) and the surface (5) of the housing (2) swept by the impeller vanes (4) and at least one upstream aperture communicating between the annular flow passage (11) and the inducer or intake portions of the inlet.Type: ApplicationFiled: March 23, 2004Publication date: January 6, 2005Inventors: Bahram Nikpour, Andrew Day, Roy Saxton, John Bywater
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Publication number: 20040254697Abstract: One or more small self-contained reentry breakup recorders are disposed within a spacecraft and each includes a sensor suite for collecting and recording collected and recorded sensory data during reentry breakup of the spacecraft, and includes a communications system for broadcasting the collected and recorded sensory data after breakup and before impact with the surface of the earth to a remote communication system for preserving the sensory data of the breakup as well as data relating to critical events occurring prior to breakup. An internal GPS receiver provides sensory positional data of the reentry and breakup positions.Type: ApplicationFiled: June 11, 2003Publication date: December 16, 2004Inventors: William Henry Ailor, Ronald John Bywater, Leon Gurevich