Patents Assigned to GE Aviations Systems LLC
  • Publication number: 20210327284
    Abstract: Methods, apparatus, and articles of manufacture to provide improved engine load models are disclosed. An example apparatus includes a model generator to generate an engine load model for an engine using flight information, weather information, and manifest information to predict a load on the engine from an engine subsystem utilization modeled for a flight. The example model generator is to incorporate the engine load model into an engine model, the engine model representing engine behavior for the flight. The example model generator is to determine a first measure of thrust from the engine and a second measure of fuel flow to the engine using the engine model with the engine load model, the engine load model to modify engine behavior by the predicted load on the engine from the engine subsystem utilization.
    Type: Application
    Filed: May 3, 2021
    Publication date: October 21, 2021
    Applicant: GE Aviation Systems, LLC
    Inventors: David Michael Lax, Mark Darnell
  • Patent number: 11128201
    Abstract: A stator sleeve assembly for an electric machine includes a first cylindrical housing portion defining an inner radial cavity defined by at least one circumferential wall and an outer radial cavity, and a set of radial passages fluidly connecting the inner radial cavity with the outer radial cavity, and a second cylindrical housing portion defining a third cavity, the second housing portion axially spaced from the first housing portion.
    Type: Grant
    Filed: September 6, 2017
    Date of Patent: September 21, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Pradeep Hemant Sangli, Santosh Kumar Prasad, Todd Eric Rook
  • Patent number: 11119818
    Abstract: Contextual awareness associated with resources can be employed to facilitate controlling access to resources of a system, including function blocks. A resource manager component (RMC) can pre-load a defined number of respective versions of configuration parameter data associated with respective applications in each resource. With regard to each application, the RMC can associate a context value, unique for each application, with the respective versions of configuration parameter data associated with that application. When a current application is being changed to a next application, the RMC can write the context value associated with the next application to a context select component (CSC). Each resource can read the context value in the CSC, identify and retrieve the version of configuration parameter data associated with the next application based on the context value, and configure the function block based on the version of configuration parameter data.
    Type: Grant
    Filed: December 31, 2019
    Date of Patent: September 14, 2021
    Assignee: GE Aviation Systems, LLC
    Inventors: Melanie Sue-Hanson Graffy, Colin Holmwood, Jon Marc Diekema
  • Patent number: 11114932
    Abstract: A ripple current reduction circuit is disclosed. The circuit includes a set of first coupled inductors, each comprising a primary winding configured to receive at a first end a respective phase voltage, and a secondary winding. The circuit also includes a set of second coupled inductors and a set of first capacitors, each first capacitor having an upstream end and a downstream end, wherein the set of first capacitors are coupled together at the downstream end to define a first node. The circuit further includes a set of auxiliary circuits each corresponding to a respective phase voltage, and coupled between the second end of the primary winding of a respective first inductor and the first node, wherein each auxiliary circuit comprises a respective second coupled inductor, a respective first capacitor, and the secondary winding of a respective first coupled inductor coupled in series.
    Type: Grant
    Filed: June 18, 2020
    Date of Patent: September 7, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Slobodan Gataric, Predrag Hadzibabic
  • Patent number: 11095202
    Abstract: A common-mode voltage cancellation (CMVC) circuit, is disclosed. The circuit includes a first set of coupled inductors, each having a primary winding defining a first polarity, and a secondary winding. The secondary windings are electrically coupled in series. Each primary winding receives a phase voltage having a common mode voltage component from a respective input line. The circuit includes a second set of coupled inductors comprising at least one primary winding and at least one secondary winding The at least one primary winding receives a second voltage from the series connected secondary windings of the first set of coupled inductors. Each at least one secondary winding is coupled in series with a respective input line such that the common mode voltage component received on input lines will be reduced at an output of the set of secondary windings.
    Type: Grant
    Filed: June 16, 2020
    Date of Patent: August 17, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Cong Li, Michael J. Schutten, Di Pan, Ren Xie
  • Patent number: 11079425
    Abstract: An electrical fault detecting system (10) for a circuit includes a conductor (20) delivering an electrical signal from a source (12) to a destination (14), a sheath (22) encircling the conductor, and a fault detection circuit (18). The sheath further includes an electrical insulator layer (24) and a conductive shield (26) encircling the conductor. The fault detection circuit is configured to detect a change in the electrical characteristics of the conductor and/or conductor sheath.
    Type: Grant
    Filed: February 23, 2015
    Date of Patent: August 3, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Arthur Vorwerk Radun, Adrian Shipley
  • Patent number: 11081936
    Abstract: A wet cavity electric machine includes a stator core having two stator poles formed by a post and a wire wound about the post to form a stator winding, with the stator winding having end turns, and a rotor having two rotor poles and configured to rotate relative to the stator and a channel for liquid coolant to flow through the rotor, and at least one fluid port in fluid communication with the channel and the stator winding end turns wherein the end turns will be exposed to liquid coolant passing through the channel.
    Type: Grant
    Filed: April 10, 2015
    Date of Patent: August 3, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Hao Huang, Jan Zywot, Xiaochuan Jia
  • Patent number: 11061394
    Abstract: Systems and methods for recording and communicating engine data are provided. One example aspect of the present disclosure is directed to a method for monitoring performance. The method includes receiving, by one or more computing devices, a measurement from a sensor. The method includes assigning, by the one or more computing devices, a time to the measurement. The method includes storing, by the one or more computing devices, the received measurement and the assigned time to a file. The method includes transmitting, by the one or more computing devices, the file to a remove computing device associated with a ground system.
    Type: Grant
    Filed: September 4, 2019
    Date of Patent: July 13, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Keith Richard Feenstra, Michael Clay Scholten, Hilbrand Harlan-Jacob Sybesma, Michael James Dusseau
  • Patent number: 11058979
    Abstract: An air-oil separator assembly can include an air-oil mixture inlet, an air outlet, and an oil outlet, a housing defining a cylindrical separating cavity, and an outlet conduit disposed within the separating cavity, wherein, outlet conduit is adapted to receive oil removed by the air-oil separator assembly from a flow containing an air-oil mixture fluid received by the air-oil mixture inlet.
    Type: Grant
    Filed: January 19, 2018
    Date of Patent: July 13, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Lanchao Lin, Richard Louis Heil, Jan Zywot
  • Publication number: 20210194305
    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: December 18, 2019
    Publication date: June 24, 2021
    Applicant: GE Aviation Systems LLC
    Inventors: Hao Huang, James Mahle, Xiaochuan Jia
  • Patent number: 11038394
    Abstract: A rotor assembly includes a rotor core having winding slots, and one or more coils, which have slot-inserted segments included in the winding slots, and first and second end-turn segments external to the winding slots and located around opposite axial ends of the rotor core, respectively. The rotor assembly further includes a first containment band located around at least a portion of the first end-turn segments and configured to prevent the first end-turn segments from moving away from the rotor core radially, a second containment band located around at least a portion of the second end-turn segments and configured to prevent the second end-turn segments from moving away from the rotor core radially, and one or more sticks mounted in one or more of the winding slots, respectively. The first and second containment bands are retained via the sticks against moving away axially.
    Type: Grant
    Filed: January 25, 2018
    Date of Patent: June 15, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Parmeet Singh Chhabra, David Raju Yamarthi, Navin Soni, Mamatha Ramakrishnaiah, Balamurugan Sridharan
  • Patent number: 11035621
    Abstract: One example aspect of the present disclosure is directed to a system for cooling a surface. The system can include a housing. The housing can include an evaporator portion. The housing can include at least one trifurcated heat exchange portion. The at least one trifurcated heat exchange portion can include a condenser portion coupled to the evaporator portion. The at least one trifurcated heat exchange portion can include a coolant portion substantially surrounded by the condenser portion. The at least one trifurcated heat exchange portion can include a phase change material portion substantially surrounding the condenser portion.
    Type: Grant
    Filed: June 5, 2019
    Date of Patent: June 15, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Stefano Lassini, Brian Rush, Daniel Erno, William Dwight Gerstler
  • Patent number: 11032919
    Abstract: A control box includes a housing defining an interior, the housing including a cover and a stiffener, the stiffener removably connected in contact with the cover, the stiffener including an outer frame and at least one cross-member. The control box further includes a heat sink removably connected in contact with the stiffener. The control box further includes a first circuit board disposed within the interior, the first circuit board positioned between the stiffener and the heat sink, and a second circuit board disposed within the interior, the second circuit board positioned between the cover and the stiffener. The cover, stiffener, and heat sink are stacked along a transverse direction.
    Type: Grant
    Filed: January 19, 2018
    Date of Patent: June 8, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Randall Lee Neuman, Stefano Angelo Mario Lassini, Jason Eggiman
  • Patent number: 11029985
    Abstract: A processing system for an unmanned vehicle (UV) such as an unmanned aerial vehicle (UAV) is provided. The processing system comprises a first processing unit of an integrated circuit and a second processing unit of the integrated circuit. The processing system comprises a first operating system provisioned using the first processing unit. The first operating system is configured to execute a first vehicle control process. The processing system comprises a virtualization layer configured using at least the second processing unit, and a second operating system provisioned using the virtualization layer. The second operating system is configured to execute a second vehicle control process.
    Type: Grant
    Filed: January 19, 2018
    Date of Patent: June 8, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Braeton Taylor, Stefano Angelo Mario Lassini, Brent Dale Hooker
  • Patent number: 11025114
    Abstract: A rotor for an electric machine includes a core having circumferentially-spaced, axially-extending posts, and defining an axial passage, a winding carried by each of the posts and comprising an electrically-conductive wire repeatedly wound around the post such that a portion of the winding extends axially beyond the post to define an overhang with upper and lower surfaces connected by an end, and a hollow shaft defining a rotor inner surface and a rotor outer surface.
    Type: Grant
    Filed: December 27, 2018
    Date of Patent: June 1, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Balamurugan Sridharan, Rajendra Vishwanath Pawar, Mamatha Ramakrishnaiah, Xiaochuan Jia, Samir Dey, Hao Huang, Dhiraj Khushal Thakare, Pankaj Kumar Morya
  • Patent number: 11003603
    Abstract: Systems and methods for recording and communicating engine data are provided. One example aspect of the present disclosure is directed to a method for communicating engine data. The method includes receiving data. The method includes separating the data into categories. For one or more categories, the method includes creating a file including the separated data. For one or more categories, the method includes naming the file, at least in part, based on the category and based on a file naming convention. The method includes prioritizing the created files. The method includes transmitting an identification file comprising identification information for a wireless communication unit and the file naming convention. The method includes transmitting the created files based on the priority.
    Type: Grant
    Filed: April 24, 2019
    Date of Patent: May 11, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Michael Clay Scholten, Richard John Reiffer, Jr., Lambros Lambrou, Robert Alan Meneghini, Jr.
  • Patent number: 10984995
    Abstract: A solar generator can include a photon-enhanced thermionic emission generator with a cathode to receive solar radiation. The photon-enhanced thermionic emission generator can include an anode that in conjunction with the cathode generates a first current and waste heat from the solar radiation. A thermoelectric generator can be thermally coupled to the anode and can convert the waste heat from the anode into a second current. A circuit can connect to the photon-enhanced thermionic emission generator and to the thermoelectric generator and can combine the first and the second currents into an output current.
    Type: Grant
    Filed: March 4, 2020
    Date of Patent: April 20, 2021
    Assignee: GE Aviation Systems LLC
    Inventor: John Xiaozhong Wang
  • Patent number: 10986028
    Abstract: Systems and methods for managing aircraft messages are provided. In one embodiment, the method can include receiving a message from an onboard system of an aircraft. The method can include determining a priority associated with the message based, at least in part, on data associated with the message. The data can be indicative of at least a content of the message. The method can include determining data indicative of availability for each of a plurality of communications networks based, at least in part, on one or more first parameters associated with the aircraft. The method can include selecting a network based, at least in part, on message priority, the data indicative of availability, and one or more second parameters associated with each of the networks. The method can include sending the message via the selected network when the network is available, or storing the message when the network is unavailable.
    Type: Grant
    Filed: February 22, 2017
    Date of Patent: April 20, 2021
    Assignee: GE Aviation Systems, LLC
    Inventors: Randy E. Bolling, Joseph Bernard Steffler, Michael Francis Guidoboni, Venkat Sankar, Eric Rankin Gardner
  • Patent number: 10985537
    Abstract: A modular power overlay architecture includes at least two sets of power overlay tiles arranged to provide for or meet a desired power overlay architecture demand. The power overlay assembly can include a base having seats to receive the power overlay tiles. The power overlay tiles can include power switching components arranged relative to a conductive surface commonly arranged relative to each of the at least two sets of power overlay tiles.
    Type: Grant
    Filed: May 3, 2019
    Date of Patent: April 20, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Liqiang Yang, Richard Anthony Eddins, Robert Lloyd George, Darrell Lee Grimes
  • Patent number: 10980153
    Abstract: A heat exchanger for cooling a component includes a heat transfer chamber containing a heated substance having a first density and a liquid coolant having a second density. The heat exchanger can also include a circulation circuit that recirculates the heated substance through the heat transfer chamber for mixing with the liquid coolant.
    Type: Grant
    Filed: June 7, 2019
    Date of Patent: April 13, 2021
    Assignee: GE Aviation Systems LLC
    Inventors: Nader Dariavach, Michel Engelhardt