Patents by Inventor Shiloh Montegomery Emerson Meyers

Shiloh Montegomery Emerson Meyers 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: 11333078
    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 an output shaft, drive shaft wherein the output shaft is selectively coupled to the drive shaft. Permanent magnets are used to transmit torque from the drive shaft to the output shaft. In a backdrive event, the decoupler decouples the output shaft from the drive shaft by uncoupling the torque transfer.
    Type: Grant
    Filed: October 30, 2017
    Date of Patent: May 17, 2022
    Assignee: GE Aviation Systems LLC
    Inventors: Subrata Nayak, Pallavi Tripathi, David Raju Yamarthi, Navin Soni, Dhiraj Thakare, Shiloh Montegomery Emerson Meyers, David Allan Dranschak
  • Patent number: 11053857
    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: February 12, 2020
    Date of Patent: July 6, 2021
    Assignee: GE AVIATION SYSTEMS LLC
    Inventors: Eliel Fresco Rodriguez, David Allan Dranschak, Shiloh Montegomery Emerson Meyers, Harsha Sanjeewa Bulathsinghalage
  • Publication number: 20200182156
    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: Application
    Filed: February 12, 2020
    Publication date: June 11, 2020
    Inventors: Eliel Fresco Rodriguez, David Allan Dranschak, Shiloh Montegomery Emerson Meyers, Harsha Sanjeewa Bulathsinghalage
  • 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: 10526974
    Abstract: An air turbine starter for starting an engine, comprising a housing defining an inlet, an outlet, and a flow path extending between the inlet and the outlet for communicating a flow of gas there through. A turbine member is journaled within the housing and disposed within the flow path for rotatably extracting mechanical power from the flow of gas. A gear train is drivingly coupled with the turbine member, a drive train is operably coupled with the gear train, and an output shaft is selectively operably coupled to rotate with the engine via a decoupler.
    Type: Grant
    Filed: August 14, 2017
    Date of Patent: January 7, 2020
    Assignee: UNISON INDUSTRIES, LLC
    Inventors: Sharad Pundlik Patil, Subrata Nayak, Shiloh Montegomery Emerson Meyers, David Allan Dranschak, Eliel Fresco Rodriguez
  • Publication number: 20190331029
    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 an output shaft, drive shaft wherein the output shaft is selectively coupled to the drive shaft. Permanent magnets are used to transmit torque from the drive shaft to the output shaft. In a backdrive event, the decoupler decouples the output shaft from the drive shaft by uncoupling the torque transfer.
    Type: Application
    Filed: October 30, 2017
    Publication date: October 31, 2019
    Inventors: Subrata Nayak, Pallavi Tripathi, David Raju Yamarthi, Navin Soni, Dhiraj Thakare, Shiloh Montegomery Emerson Meyers, David Allan Dranschak
  • Publication number: 20190048800
    Abstract: An air turbine starter for starting an engine, comprising a housing defining an inlet, an outlet, and a flow path extending between the inlet and the outlet for communicating a flow of gas there through. A turbine member is journaled within the housing and disposed within the flow path for rotatably extracting mechanical power from the flow of gas. A gear train is drivingly coupled with the turbine member, a drive train is operably coupled with the gear train, and an output shaft is selectively operably coupled to rotate with the engine via a decoupler.
    Type: Application
    Filed: August 14, 2017
    Publication date: February 14, 2019
    Inventors: Sharad Pundlik Patil, Subrata Nayak, Shiloh Montegomery Emerson Meyers, David Allan Dranschak, Eliel Fresco Rodriguez
  • Publication number: 20170356345
    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: Application
    Filed: June 13, 2016
    Publication date: December 14, 2017
    Inventors: Eliel Fresco Rodriguez, David Allan Dranschak, Shiloh Montegomery Emerson Meyers