Patents by Inventor Kalyani G MENON
Kalyani G MENON 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: 11542021Abstract: An aircraft propulsion system includes at least first and second electrical generators, each being configured to provide electrical power to a respective first and second AC electrical network. The system further comprises at least first and second AC electrical motors directly electrically coupled to a respective AC network and coupled to a respective propulsor, and a DC electrical network electrically coupled to the first and second AC networks via respective first and second AC to DC converters, and to a further electrical motor, the further electrical motor being coupled to a propulsor.Type: GrantFiled: March 10, 2021Date of Patent: January 3, 2023Assignee: ROLLS-ROYCE plcInventors: Richard Harwood, Kalyani G. Menon, Joseph Palmer, Ivan Popovic
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Publication number: 20210214094Abstract: An aircraft propulsion system includes at least first and second electrical generators, each being configured to provide electrical power to a respective first and second AC electrical network. The system further comprises at least first and second AC electrical motors directly electrically coupled to a respective AC network and coupled to a respective propulsor, and a DC electrical network electrically coupled to the first and second AC networks via respective first and second AC to DC converters, and to a further electrical motor, the further electrical motor being coupled to a propulsor.Type: ApplicationFiled: March 10, 2021Publication date: July 15, 2021Applicant: ROLLS-ROYCE PLCInventors: Richard HARWOOD, Kalyani G. MENON, Joseph PALMER, Ivan POPOVIC
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Patent number: 10974836Abstract: An aircraft propulsion system (10) comprises at least first and second electrical generators (15a, 15b), each being configured to provide electrical power to a respective first and second AC electrical network (16a, 16b). The system (10) further comprises at least first and second AC electrical motors (19a, 19b) directly electrically coupled to a respective AC network (16a, 16b) and coupled to a respective propulsor (4), and a DC electrical network electrically coupled to the first and second AC networks (16a, 16b) via respective first and second AC to DC converters (17a, 17b), and to a further electrical motor 19c), the further electrical motor (19c) being coupled to a propulsor (4).Type: GrantFiled: August 23, 2017Date of Patent: April 13, 2021Assignee: ROLLS-ROYCE plcInventors: Richard Harwood, Kalyani G Menon, Chloe Jo Palmer, Ivan Popovic
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Patent number: 10971973Abstract: Energy conversion apparatus comprising: an electrical machine including a rotor arranged to rotate about an axis, the rotor defining a first cavity therein; power electronic circuitry arranged at least partially around the axis and defining a second cavity therein, the power electronic circuitry being positioned adjacent to the electrical machine; a heat pipe positioned within the first cavity of the rotor and within the second cavity defined by the power electronic circuitry, the heat pipe being arranged to receive thermal energy from the rotor; and a cooling arrangement positioned at least partially within the second cavity and arranged to receive thermal energy from the power electronic circuitry and from the heat pipe.Type: GrantFiled: January 5, 2017Date of Patent: April 6, 2021Assignee: ROLLS-ROYCE plcInventors: Kalyani G Menon, Richard Harwood
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Patent number: 10049963Abstract: A power electronics module is provided having one or more power converter semiconductor components. The power electronics module further has a substrate having a first surface to which the one or more components are mounted, and having an opposing second surface from which project a plurality of heat transfer formations for enhancing heat transfer from the substrate. The power electronics module further has a coolant housing which sealingly connects to the substrate to form a void over the heat transfer formations of the second surface. The coolant housing has an inlet for directing a flow of an electrically insulating coolant into the void and an outlet for removing the coolant flow from the void, whereby heat generated during operation of the one or more components is transferred into the coolant flow via the substrate.Type: GrantFiled: March 21, 2017Date of Patent: August 14, 2018Assignee: ROLLS-ROYCE plcInventors: Kalyani G Menon, Richard Harwood
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Publication number: 20180079515Abstract: An aircraft propulsion system (10) comprises at least first and second electrical generators (15a, 15b), each being configured to provide electrical power to a respective first and second AC electrical network (16a, 16b). The system (10) further comprises at least first and second AC electrical motors (19a, 19b) directly electrically coupled to a respective AC network (16a, 16b) and coupled to a respective propulsor (4), and a DC electrical network electrically coupled to the first and second AC networks (16a, 16b) via respective first and second AC to DC converters (17a, 17b), and to a further electrical motor 19c), the further electrical motor (19c) being coupled to a propulsor (4).Type: ApplicationFiled: August 23, 2017Publication date: March 22, 2018Applicant: ROLLS-ROYCE PLCInventors: Richard HARWOOD, Kalyani G. MENON, Joseph PALMER, Ivan POPOVIC
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Publication number: 20170301609Abstract: A power electronics module is provided having one or more power converter semiconductor components. The power electronics module further has a substrate having a first surface to which the one or more components are mounted, and having an opposing second surface from which project a plurality of heat transfer formations for enhancing heat transfer from the substrate. The power electronics module further has a coolant housing which sealingly connects to the substrate to form a void over the heat transfer formations of the second surface. The coolant housing has an inlet for directing a flow of an electrically insulating coolant into the void and an outlet for removing the coolant flow from the void, whereby heat generated during operation of the one or more components is transferred into the coolant flow via the substrate.Type: ApplicationFiled: March 21, 2017Publication date: October 19, 2017Applicant: ROLLS-ROYCE plcInventors: Kalyani G. MENON, Richard HARWOOD
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Publication number: 20170214294Abstract: Energy conversion apparatus comprising: an electrical machine including a rotor arranged to rotate about an axis, the rotor defining a first cavity therein; power electronic circuitry arranged at least partially around the axis and defining a second cavity therein, the power electronic circuitry being positioned adjacent to the electrical machine; a heat pipe positioned within the first cavity of the rotor and within the second cavity defined by the power electronic circuitry, the heat pipe being arranged to receive thermal energy from the rotor; and a cooling arrangement positioned at least partially within the second cavity and arranged to receive thermal energy from the power electronic circuitry and from the heat pipe.Type: ApplicationFiled: January 5, 2017Publication date: July 27, 2017Applicant: ROLLS-ROYCE PLCInventors: Kalyani G MENON, Richard HARWOOD