Patents Assigned to Aviation Systems, LLC
  • Patent number: 10601218
    Abstract: A power distribution system can include a controller and a set of power-using devices. Each power-using device in the set can include a sensor configured to measure a parameter and transmit a sensor signal representing the parameter to the controller, and the controller can respond to the transmitted sensor signal.
    Type: Grant
    Filed: May 25, 2017
    Date of Patent: March 24, 2020
    Assignee: GE Aviation Systems LLC
    Inventor: Arthur Vorwerk Radun
  • Patent number: 10584640
    Abstract: A method and decoupler for disengaging an output shaft from an engine in a back drive event with a backdrive decoupler. The backdrive decoupler includes a an output shaft, drive shaft, and a retention mechanism selectively coupling the output shaft to the drive shaft. In a backdrive event, the decoupler decouples the output shaft from the drive shaft.
    Type: Grant
    Filed: June 13, 2016
    Date of Patent: March 10, 2020
    Assignee: GE Aviation Systems LLC
    Inventors: Eliel Fresco Rodriguez, David Allan Dranschak, Shiloh Montegomery Emerson Meyers, Harsha Sanjeewa Bulathsinghalage
  • Patent number: 10587307
    Abstract: Systems and methods for communicating a signal over a hydraulic line in a vehicle are provided. In one embodiment, a system can include a hydraulic line. The hydraulic line can include at least one communication medium for propagating a communication signal. The system can also include at least one signal communication device configured to receive the communication signal communicated over the hydraulic line. The system can also include at least one vehicle component in communication with the at least one signal communication device.
    Type: Grant
    Filed: November 8, 2016
    Date of Patent: March 10, 2020
    Assignee: GE Aviation Systems, LLC
    Inventors: Pavlo Bobrek, Eric Rankin Gardner
  • Patent number: 10579053
    Abstract: Systems and methods for determine a cost-improved set of control commands for an aircraft based at least in part on deterioration costs are provided. One example computing device is configured to iteratively: input a candidate set of control commands for the aircraft into the deterioration cost model; receive, as an output of the deterioration cost model, an estimated deterioration cost associated with the candidate set of control commands; input the estimated deterioration cost into a cost function to obtain a total estimated cost associated with the candidate set of control commands; and determine an improved set of control commands based at least in part on the total estimated cost and the cost function.
    Type: Grant
    Filed: July 17, 2017
    Date of Patent: March 3, 2020
    Assignee: GE Aviation Systems, LLC
    Inventors: Albert Jeffrey Ellis, Mark Lawrence Darnell, David Michael Lax
  • Patent number: 10566877
    Abstract: A wet cavity electric machine includes a stator core having 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, 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 to at least one nozzle, and liquid coolant sprays from the at least one nozzle at least a portion of the stator windings.
    Type: Grant
    Filed: December 21, 2018
    Date of Patent: February 18, 2020
    Assignee: GE Aviation Systems LLC
    Inventors: Lanchao Lin, Hao Huang, Xiaochuan Jia
  • Patent number: 10560542
    Abstract: A mechanism and method for accessing message data in a shared memory by at least one client, includes an allocation of data in the shared memory, the memory configured in a plurality of buffers, and accessing the data by a client or a server without locking or restricting access to the data.
    Type: Grant
    Filed: September 15, 2014
    Date of Patent: February 11, 2020
    Assignee: GE Aviation Systems LLC
    Inventors: Christian Reynolds Decker, Troy Stephen Brown, Kevin Brett Chapman
  • Patent number: 10554088
    Abstract: A rotor assembly for an electric machine includes a core having at least one post and a cap wherein electrical windings are wound about the rotor assembly to define a pole. The rotation of the rotor and rotor pole relative to a stator generates a current supplied from the electric machine to a power consuming device.
    Type: Grant
    Filed: November 4, 2013
    Date of Patent: February 4, 2020
    Assignee: GE Aviation Systems LLC
    Inventors: Hao Huang, Xiaochuan Jia, Jan Zywot
  • Patent number: 10552206
    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: May 23, 2017
    Date of Patent: February 4, 2020
    Assignee: GE Aviation Systems LLC
    Inventors: Melanie Sue-Hanson Graffy, Colin Holmwood, Jon Marc Diekema
  • Patent number: 10535276
    Abstract: Route planning and movement of an aircraft on the ground based on a navigation model trained to improve aircraft operational efficiency is provided herein. A system comprises a memory that stores executable components and a processor, operatively coupled to the memory, that executes the executable components that comprise an assessment component, a sensor component, and a route planning component. The assessment component accesses runway data, taxiway data, and gate configuration data associated with an airport. The sensor component collects, from a plurality of sensors, sensor data related to performance data of an aircraft and respective conditions of the runway, the taxiway, and the gate configuration data. The route planning component employs a navigation model that is trained to analyze the sensor data, the runway data, the taxiway data, and the gate configuration data, and generate a taxiing protocol to navigate the aircraft to improve aircraft operational efficiency.
    Type: Grant
    Filed: December 4, 2017
    Date of Patent: January 14, 2020
    Assignee: GE Aviation Systems LLC
    Inventor: Stefan Alexander Schwindt
  • Patent number: 10530153
    Abstract: A method and apparatus for operating a power architecture for an aircraft, includes a primary variable frequency generator system having a first power output, a secondary variable frequency generator system having a second power output, a power distribution node, an essential power bus selectively connected with a set of essential aircraft electrical loads, and a controller module.
    Type: Grant
    Filed: May 23, 2017
    Date of Patent: January 7, 2020
    Assignee: GE Aviation Systems LLC
    Inventor: Hao Huang
  • Patent number: 10529150
    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 maintaining a wireless communication unit. The method includes transmitting, by one or more computing devices, an identification file to one or more second computing devices associated with a ground system. The method includes automatically retrieving, by the one or more computing devices, a loadable software aircraft part for data load from the one or more second computing devices associated with the ground system. The method includes performing, by the one or more computing devices, a data load using the loadable software aircraft part. The method includes determining, by the one or more computing devices, if the data load was successful. The method includes transmitting, by the one or more computing devices, the determination to the one or more computing devices associated with the ground system.
    Type: Grant
    Filed: June 22, 2017
    Date of Patent: January 7, 2020
    Assignee: Aviation Systems LLC
    Inventors: Michael Clay Scholten, Richard John Reiffer, Jr.
  • Patent number: 10519865
    Abstract: A method and decoupler for disengaging an output shaft from an engine in a back drive event with a backdrive decoupler. The backdrive decoupler includes a threaded shaft and a retention mechanism selectively coupling the output shaft to the threaded shaft. In a backdrive event, the decoupler decouples the output shaft from a drive shaft.
    Type: Grant
    Filed: June 17, 2016
    Date of Patent: December 31, 2019
    Assignee: GE Aviation Systems LLC
    Inventors: Eliel Fresco Rodriguez, David Allan Dranschak
  • Patent number: 10521981
    Abstract: One example aspect of the present disclosure relates to a method for scheduling a vehicle wash. The method can include receiving, at one or more computing devices, data indicative of an actual performance efficiency factor, wherein the data is collected from one or more sensors. The method can include determining, at the one or more computing devices, an expected performance efficiency factor based on a model. The method can include performing, at the one or more computing devices, a comparison of the actual performance efficiency factor with the expected performance efficiency factor. The method can include scheduling, at the one or more computing devices, the vehicle wash based on the comparison.
    Type: Grant
    Filed: June 6, 2017
    Date of Patent: December 31, 2019
    Assignee: GE Aviation Systems LLC
    Inventors: Jeffrey Russell Bult, Mark Lawrence Darnell, David Michael Lax
  • Patent number: 10523079
    Abstract: A rotor assembly (40) for an electric machine including a core (42) having at least one post (44) about which a winding may be wound, and a cap (52) coupled to the post (44) and having a portion overlying a winding (46), wherein the cap (52) comprises a plurality of laminations and the core (42) does not comprise a plurality of laminations.
    Type: Grant
    Filed: September 6, 2013
    Date of Patent: December 31, 2019
    Assignee: GE Aviation Systems LLC
    Inventors: Hao Huang, Xiaochuan Jia, Paul James Wirsch, Jr.
  • Patent number: 10523096
    Abstract: A method for manufacturing a stator assembly for an electrical machine includes printing a stator core. The method also includes printing a first part of a stator winding. In addition, the method includes coupling the first part of the stator winding to the stator core. The method also includes printing a second part of the stator winding onto the first part of the stator winding to form the stator assembly. In particular, coupling the first part of the stator winding to the stator core precedes printing the second part of the stator winding onto the first part of the stator winding.
    Type: Grant
    Filed: August 8, 2017
    Date of Patent: December 31, 2019
    Assignee: GE Aviation Systems LLC
    Inventors: Hao Huang, Xiaochuan Jia, Joshua Tyler Mook
  • Patent number: 10496351
    Abstract: Automatic display unit backup during failures of one more display units through the utilization of graphic user interface objects defined for control transfer and reversion after resolution of the failures is provided herein. A system can comprise a memory operatively coupled to a processor that executes stored executable components comprising a first controller, a second controller, and a failure indication component that provides a first notification based on a first detection of a first failure at the second controller, and a second notification based on a second detection of a second failure at the first controller. Further, the executable components can comprise a control transfer component that automatically transfers control of a second display unit from the v controller to the first controller based on the first notification, or control of a first display unit from the first controller to the second controller based on the second notification.
    Type: Grant
    Filed: June 7, 2017
    Date of Patent: December 3, 2019
    Assignee: GE Aviation Systems LLC
    Inventor: David Allen Fairchild
  • Patent number: 10485138
    Abstract: A heat sink assembly for use with at least one heat-emitting component where the heat sink assembly includes a first phase change material conductively coupled to the at least one heat-emitting component and changing phase at a first temperature and a second phase change material conductively coupled to the first phase change material and changing phase at a second temperature, which is greater than the first temperature.
    Type: Grant
    Filed: November 12, 2015
    Date of Patent: November 19, 2019
    Assignee: GE Aviation Systems LLC
    Inventors: Michel Engelhardt, Paul Otto Stehlik, Judd Everett Swanson
  • Patent number: 10480446
    Abstract: A liquid cooling circuit includes a liquid reservoir for coolant, a heat-generating module, a conduit fluidly coupling the heat-generating module with the liquid reservoir, and a pump configured to move the coolant through the conduit to cool the heat-generating module. The liquid cooling circuit is configured such that the movement of the coolant relative to the heat-generating module transfers heat from the heat-generating module to the coolant.
    Type: Grant
    Filed: July 16, 2015
    Date of Patent: November 19, 2019
    Assignee: GE Aviation Systems LLC
    Inventor: Michel Engelhardt
  • Patent number: 10461595
    Abstract: A rotor assembly for an electric machine includes a core having at least one post and a cap wherein electrical windings are wound about the rotor assembly to define a pole. The rotation of the rotor and rotor pole relative to a stator generates a current supplied from the electric machine to a power consuming device.
    Type: Grant
    Filed: November 24, 2014
    Date of Patent: October 29, 2019
    Assignee: GE Aviation Systems LLC
    Inventors: Joseph Kenneth Teter, James Patrick Mahle, Winfred Dwight Koontz, Jr., David George Kloos
  • Patent number: 10460608
    Abstract: A method for determining uncertainty in a predicted flight path for an aerial vehicle can include determining, by one or more computing devices, uncertainty in a performance model of the aerial vehicle. The method can further include determining, by one or more computing devices, uncertainty in a weather model indicative of weather conditions along the predicted flight path. In addition, the method can include determining, by the one or more computing devices, uncertainty in the predicted flight path based on the uncertainty in the performance model and the uncertainty in the weather model. The method can further include generating, by one or more computing devices, a notification indicating the uncertainty in the predicted flight path.
    Type: Grant
    Filed: May 25, 2017
    Date of Patent: October 29, 2019
    Assignee: GE Aviation Systems LLC
    Inventors: Szabolcs Andras Borgyos, Joachim Karl Ulf Hochwarth