Patents by Inventor Xiaochuan Jia

Xiaochuan Jia 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).

  • Patent number: 11757421
    Abstract: An electrical filter circuit is disclosed. The circuit includes a first input line and a second input line. A first transmission line is coupled electrically in series at a first node with a first output line, and an inductor is coupled electrically in series between the first input line and the first transmission line. The filter also includes a second transmission line having a first impedance coupled to the first node. The second input line is coupled electrically in series at a second node with a second output line. A third transmission line is coupled to the second node, and a capacitor is coupled electrically in series between the second transmission line and the third transmission line. The first output line has a second impedance that is greater than the first impedance.
    Type: Grant
    Filed: September 1, 2021
    Date of Patent: September 12, 2023
    Assignee: GE Aviation Systems LLC
    Inventors: Cong Li, Han Xiong, Xiaochuan Jia, David Dimitri Karipides, Ren Xie
  • Publication number: 20230246500
    Abstract: A rotor assembly comprises a rotor core comprising a first end and an opposing second end, and an outwardly facing peripheral surface having a set of rotor teeth projecting outwardly therefrom to define a set of rotor slots therebetween. Each rotor tooth can comprise a first rotor tooth wall, an opposing second rotor tooth wall, and a distal tip between the first rotor tooth wall and second rotor tooth wall. Each respective rotor slot can be defined by a respective first rotor tooth wall of a first rotor tooth, and a respective second rotor tooth wall of a second rotor tooth, and includes a first rotor core conduit extending axially along a length of the first rotor tooth. The first rotor core conduit can comprise a first rotor core conduit inlet at the rotor core first end and a first rotor core conduit inlet at the rotor core second end, the rotor core conduit defining a first taper that is narrower at first rotor core conduit inlet than the first rotor core conduit outlet.
    Type: Application
    Filed: January 28, 2022
    Publication date: August 3, 2023
    Inventors: Xiaochuan Jia, Balamurugan Sridharan, Ami Hatim, Anirban Chatterjee
  • Patent number: 11682947
    Abstract: A method and apparatus for a rotor assembly. The rotor assembly includes a rotor core having a rotatable shaft and defining at least one rotor post, a winding wound around the post that defines an end turn, and at least one coolant conduit defined in part by an end support and in a thermally conductive relationship with a portion of the winding.
    Type: Grant
    Filed: January 27, 2021
    Date of Patent: June 20, 2023
    Assignee: GE Aviation Systems LLC
    Inventors: Anirban Chatterjee, Mamatha Ramakrishnaiah, Samir Dey, Mohammad Khaja Mohiddin Shaik, Balamurugan Sridharan, Rajendra Vishwanath Pawar, Xiaochuan Jia
  • Publication number: 20230061575
    Abstract: An electrical filter circuit is disclosed. The circuit includes a first input line and a second input line. A first transmission line is coupled electrically in series at a first node with a first output line, and an inductor is coupled electrically in series between the first input line and the first transmission line. The filter also includes a second transmission line having a first impedance coupled to the first node. The second input line is coupled electrically in series at a second node with a second output line. A third transmission line is coupled to the second node, and a capacitor is coupled electrically in series between the second transmission line and the third transmission line. The first output line has a second impedance that is greater than the first impedance.
    Type: Application
    Filed: September 1, 2021
    Publication date: March 2, 2023
    Inventors: Cong Li, Han Xiong, Xiaochuan Jia, David Dimitri Karipides, Ren Xie
  • Publication number: 20230043602
    Abstract: A method for manufacturing a main rotor for a generator is provided. The method includes printing at least part of a rotor shaft by a three-dimensional printing process. The step of printing at least part of the rotor shaft includes printing a plurality of closed outlets and a plurality of open outlets. A rotor core is printed by the three-dimensional printing process. The step of printing the rotor core includes printing a plurality of liquid coolant conduits that extend through the rotor core and fluidly connecting the plurality of liquid coolant conduits to the plurality of closed openings.
    Type: Application
    Filed: October 6, 2022
    Publication date: February 9, 2023
    Applicant: GE Aviation Systems LLC
    Inventors: Hao Huang, James Mahle, Xiaochuan Jia
  • Patent number: 11552539
    Abstract: Disclosed within are a structure and method for forming a component for a rotor to be used in an electric machine. The formed rotor components can include a rotor assembly or rotor shaft. The rotor assembly can include a plurality of poles spaced about a rotor core. The plurality of poles can include a pole shoe or pole body. Quasi-laminations that can result in a unitary structure that includes support structures can be used to form all or a portion of the pole shoe or pole body.
    Type: Grant
    Filed: July 16, 2021
    Date of Patent: January 10, 2023
    Assignee: GE Aviation Systems LLC
    Inventors: Hao Huang, James Patrick Mahle, Sudeep Pradhan Sadananda Rao, Xiaochuan Jia
  • Patent number: 11542029
    Abstract: A method for manufacturing a dual-structured aircraft engine starting and generating apparatus is provided. The method includes printing a housing using a three-dimensional printing process including a main machine portion and an exciter portion for receiving at least part of a generator system. Printing the housing includes printing a cooling jacket portion comprising one or more cooling passages that is a monolithic part of a sidewall of the housing.
    Type: Grant
    Filed: August 31, 2020
    Date of Patent: January 3, 2023
    Assignee: General Electric Company
    Inventors: Hao Huang, Xiaochuan Jia, Jan Zywot
  • Patent number: 11489386
    Abstract: A method for manufacturing a main rotor for a generator is provided. The method includes printing at least part of a rotor shaft by a three-dimensional printing process. The step of printing at least part of the rotor shaft includes printing a plurality of closed outlets and a plurality of open outlets. A rotor core is printed by the three-dimensional printing process. The step of printing the rotor core includes printing a plurality of liquid coolant conduits that extend through the rotor core and fluidly connecting the plurality of liquid coolant conduits to the plurality of closed openings.
    Type: Grant
    Filed: December 18, 2019
    Date of Patent: November 1, 2022
    Assignee: GE Aviation Systems LLC
    Inventors: Hao Huang, James Mahle, Xiaochuan Jia
  • Patent number: 11476728
    Abstract: A rotor assembly comprising rotatable element defining a periphery, a first set of elements defining magnetic pole regions and a second set of elements defining interpolar regions that alternately placed about the periphery. The rotor assembly further comprising a containment band circumscribing the first set of elements and the second set of elements. The containment band defining a first set of material and a second set of material, with each overlying at least a portion of the first set of elements or the second set of elements.
    Type: Grant
    Filed: January 15, 2021
    Date of Patent: October 18, 2022
    Assignee: GE Aviation Systems LLC
    Inventors: Jason Randall Gulley, Xiaochuan Jia
  • Patent number: 11437970
    Abstract: A common-mode voltage cancellation (CMVC) circuit, is disclosed. The circuit includes a set of input lines arranged to receive a respective phase voltage, and a set of output lines arranged to provide a respective output phase voltage. The circuit further includes a set of coupled inductors, each having a respective primary winding and secondary winding coupled in signal communication at a respective upstream end to a respective input line to receive a respective phase voltage therefrom, each respective phase voltage having a common-mode voltage component. Each primary winding being coupled at a respective downstream end to ground, and each secondary winding being coupled in series between the respective input line and a respective output line. The circuit includes a set of capacitors, each capacitor being electrically coupled to a respective input line and in series with a respective primary winding of the set of coupled inductors.
    Type: Grant
    Filed: January 12, 2021
    Date of Patent: September 6, 2022
    Assignee: GE Aviation Systems LLC
    Inventors: Cong Li, Xiaochuan Jia
  • Publication number: 20220231556
    Abstract: A rotor assembly comprising rotatable element defining a periphery, a first set of elements defining magnetic pole regions and a second set of elements defining interpolar regions that alternately placed about the periphery. The rotor assembly further comprising a containment band circumscribing the first set of elements and the second set of elements. The containment band defining a first set of material and a second set of material, with each overlying at least a portion of the first set of elements or the second set of elements.
    Type: Application
    Filed: January 15, 2021
    Publication date: July 21, 2022
    Inventors: Jason Randall Gulley, Xiaochuan Jia
  • Publication number: 20220224301
    Abstract: A common-mode voltage cancellation (CMVC) circuit, is disclosed. The circuit includes a set of input lines arranged to receive a respective phase voltage, and a set of output lines arranged to provide a respective output phase voltage. The circuit further includes a set of coupled inductors, each having a respective primary winding and secondary winding coupled in signal communication at a respective upstream end to a respective input line to receive a respective phase voltage therefrom, each respective phase voltage having a common-mode voltage component. Each primary winding being coupled at a respective downstream end to ground, and each secondary winding being coupled in series between the respective input line and a respective output line. The circuit includes a set of capacitors, each capacitor being electrically coupled to a respective input line and in series with a respective primary winding of the set of coupled inductors.
    Type: Application
    Filed: January 12, 2021
    Publication date: July 14, 2022
    Inventors: Cong Li, Xiaochuan Jia
  • Patent number: 11271456
    Abstract: An electric machine assembly having a main machine stator core having at least one stator post, a set of stator windings wound about the at least one stator post and having a first end and an opposing second end, a coolant inlet housing defining an inlet passage, a coolant outlet housing defining an outlet passage, proximate to the coolant inlet housing, and wherein the coolant inlet passage and the coolant outlet passage define a coolant circuit configured to receive a supply of coolant to remove heat generated in the set of stator windings.
    Type: Grant
    Filed: August 12, 2019
    Date of Patent: March 8, 2022
    Assignee: GE Aviation Systems LLC
    Inventors: Hao Huang, Xiaochuan Jia
  • Publication number: 20220069673
    Abstract: A rotating rectifier associated with an electric machine is provided. In one example aspect, a rotating rectifier includes a diode. The diode can be one diode of a stage of diodes. The rotating rectifier can also include a connection lead, such an exciter connection lead. The connection lead has a diode contact segment in contact with the diode and a first spring segment and a second spring segment positioned on opposite sides of the diode contact segment. The first spring segment and the second spring segment can be positioned adjacent to the diode contact segment. The first spring segment and the second spring segment each have one or more spring laps. The spring laps can be non-planar spring laps, such as undulating spring laps.
    Type: Application
    Filed: August 18, 2021
    Publication date: March 3, 2022
    Inventors: Balamurugan Sridharan, Mamatha Ramakrishnaiah, Mohammad Khaja Mohiddin Shaik, Xiaochuan Jia, Hao Huang
  • Publication number: 20220063829
    Abstract: A method for manufacturing a dual-structured aircraft engine starting and generating apparatus is provided. The method includes printing a housing using a three-dimensional printing process including a main machine portion and an exciter portion for receiving at least part of a generator system. Printing the housing includes printing a cooling jacket portion comprising one or more cooling passages that is a monolithic part of a sidewall of the housing.
    Type: Application
    Filed: August 31, 2020
    Publication date: March 3, 2022
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: Hao Huang, Xiaochuan Jia, Jan Zywot
  • Patent number: 11211836
    Abstract: A permanent magnet generator, includes a cylindrical rotor assembly having a set of circumferentially-spaced permanent magnets arranged at an outer radius of the rotor assembly, and spaced from one another by non-magnetic spacing element, and a stator assembly configured to coaxially receive the rotor assembly. The stator assembly includes a cylindrical stator core, a circumferentially spaced set of posts extending from the stator core and defining a set of stator slots between adjacent posts, and a set of conductive windings wound about the stator slots.
    Type: Grant
    Filed: May 3, 2019
    Date of Patent: December 28, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Hao Huang, Xiaochuan Jia
  • Patent number: 11211848
    Abstract: A method and assembly of a dry cavity oil cooled electric machine includes a housing, a shaft configured to operably couple with a source of rotational force and rotate about a rotational axis, and an exciter rotor and a permanent magnet generator rotor carried by the shaft, wherein the exciter rotor and the permanent magnet generator rotor rotate relative to the housing, which provides such a construction of dry cavity generators that have high efficiency and high power density.
    Type: Grant
    Filed: August 2, 2019
    Date of Patent: December 28, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Hao Huang, Xiaochuan Jia
  • Publication number: 20210384853
    Abstract: An aircraft starting and generating system includes a starter/generator and an inverter/converter/controller that is connected to the starter/generator and that generates AC power to drive the starter/generator in a start mode for starting a prime mover of the aircraft, and that converts AC power, obtained from the starter/generator after the prime mover have been started, to DC power in a generate mode of the starter/generator. A four leg inverter is coupled with the DC power output and has an inverter/converter/controller (ICC) with a four leg MOSFET-based bridge configuration that drives the starter/generator in a start mode for starting a prime mover of the aircraft, and converts DC power to AC power in a generate mode of the starter/generator. A four leg bridge gate driver is configured to drive the four leg MOSFET-based bridge using pulse width modulation (PWM) during start and generate mode.
    Type: Application
    Filed: June 5, 2020
    Publication date: December 9, 2021
    Inventors: Hao Huang, Xiaochuan Jia, Manish Ashvinkumar Dalal
  • Patent number: 11177708
    Abstract: A method for integrally manufacturing a stator core and a housing for an electrical machine includes printing, by a three-dimensional (3D) printing process, the stator core. In addition, the method includes printing, by the 3D printing process, the housing. In particular, printing the housing occurs contemporaneously with printing the stator core. The method also includes printing, by the 3D printing process, at least one end cap and coupling the at least one end cap to the housing to enclose a cavity defined by the housing.
    Type: Grant
    Filed: August 8, 2017
    Date of Patent: November 16, 2021
    Assignee: GE AVIATION SYSTEMS LLC
    Inventors: Hao Huang, Xiaochuan Jia, Joshua Tyler Mook
  • Publication number: 20210344263
    Abstract: Disclosed within are a structure and method for forming a component for a rotor to be used in an electric machine. The formed rotor components can include a rotor assembly or rotor shaft. The rotor assembly can include a plurality of poles spaced about a rotor core. The plurality of poles can include a pole shoe or pole body. Quasi-laminations that can result in a unitary structure that includes support structures can be used to form all or a portion of the pole shoe or pole body.
    Type: Application
    Filed: July 16, 2021
    Publication date: November 4, 2021
    Inventors: Hao Huang, James Patrick Mahle, Sudeep Pradhan Sadananda Rao, Xiaochuan Jia