Patents by Inventor Jeremy Kevin Payne

Jeremy Kevin Payne 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: 11149692
    Abstract: A combustion section for a gas turbine engine including an inner casing comprising a first material defining an inner diameter of a pressure vessel and a first heat transfer coefficient. A second material is extended at least partially over an outer diameter of the first material. The second material is disposed radially between the first material and a combustor liner. The second material defines a second heat transfer coefficient less than the first heat transfer coefficient.
    Type: Grant
    Filed: June 12, 2018
    Date of Patent: October 19, 2021
    Assignee: General Electric Company
    Inventors: Anthony Joseph Venzon, Jeremy Kevin Payne, Narendra Kumar Patel
  • Patent number: 10697372
    Abstract: An apparatus and method for a turbine engine having an engine core. A casing can contain a compressor section, a combustor section and a turbine section in axial flow arrangement. An air conduit can extend at least partially between the compressor section and the turbine section. A compliant interface can include a nut and a biasing device mount the air conduit to the casing.
    Type: Grant
    Filed: April 5, 2017
    Date of Patent: June 30, 2020
    Assignee: General Electric Company
    Inventors: Jeremy Kevin Payne, John Wilbur Acree, Anthony James Bailey, Satyambabu Kalyani, Thomas Alan Wall, Michael Alan Zupancic, Jonathan Russell Ratzlaff, Anthony Paul Greenwood, Kevin William Caldwell, Christophe Jude Day
  • Publication number: 20190376471
    Abstract: A combustion section for a gas turbine engine including an inner casing comprising a first material defining an inner diameter of a pressure vessel and a first heat transfer coefficient. A second material is extended at least partially over an outer diameter of the first material. The second material is disposed radially between the first material and a combustor liner. The second material defines a second heat transfer coefficient less than the first heat transfer coefficient.
    Type: Application
    Filed: June 12, 2018
    Publication date: December 12, 2019
    Inventors: Anthony Joseph Venzon, Jeremy Kevin Payne, Narendra Kumar Patel
  • Publication number: 20190368381
    Abstract: A turbine engine including a first outer casing and a second outer casing coupled together at a flange. The first outer casing and the second outer casing are together disposed around a core engine. An inner casing assembly is extended from the flange between the first outer casing and the second outer casing. A flow circuit is defined between the first outer casing, the inner casing assembly, and the second outer casing.
    Type: Application
    Filed: May 30, 2018
    Publication date: December 5, 2019
    Inventors: Anthony Paul Greenwood, Brian Michael Dixon, Nestor Martinez Toro, David Fasig, Kimbra Chaplin, Ashish Narayan, Jeremy Kevin Payne
  • Publication number: 20180291812
    Abstract: An apparatus and method for a turbine engine having an engine core. A casing can contain a compressor section, a combustor section and a turbine section in axial flow arrangement. An air conduit can extend at least partially between the compressor section and the turbine section. A compliant interface can include a nut and a biasing device mount the air conduit to the casing.
    Type: Application
    Filed: April 5, 2017
    Publication date: October 11, 2018
    Inventors: Jeremy Kevin Payne, John Wilbur Acree, Anthony James Bailey, Satyambabu Kalyani, Thomas Alan Wall, Michael Alan Zupancic, Jonathan Russell Ratzlaff, Anthony Paul Greenwood, Kevin William Caldwell, Christophe Jude Day