Patents by Inventor Jon Champion

Jon Champion 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: 10300740
    Abstract: In some examples, an aircraft wheel assembly includes an axle, a bearing assembly, and a hub defining a bearing bore. The bearing bore may be configured such that the dynamic radial and axial thrust bearing reactions between the axle and the hub results in a first reaction force FR applied to the hub, the first reaction force FR having a radial component, and a second reaction force FN applied to the hub, the second reaction force FN having both a radial and an axial component.
    Type: Grant
    Filed: June 26, 2015
    Date of Patent: May 28, 2019
    Assignee: Honeywell International Inc.
    Inventor: Jon Champion
  • Patent number: 10226962
    Abstract: A vehicle wheel includes a first annular component, a second annular component configured to be separable from the first annular component and mechanically connected to and aligned with the first annular component about an axis of rotation of the wheel, and a plate. In some examples, when the first and second annular components are mechanically connected, the first and second annular components are configured to receive a tire and define a recess along an annular surface of the first and second annular components, the recess being configured to receive the plate. In addition, in some examples, when the plate is received in the recess, the plate inhibits relative rotation between the first annular component and the second annular component about the axis of rotation of the wheel.
    Type: Grant
    Filed: December 5, 2016
    Date of Patent: March 12, 2019
    Assignee: Honeywelll International Inc.
    Inventors: Jon Champion, Elliot Conrad, Jonathan T. Beehler, Thomas Regnier
  • Publication number: 20180154689
    Abstract: A vehicle wheel includes a first annular component, a second annular component configured to be separable from the first annular component and mechanically connected to and aligned with the first annular component about an axis of rotation of the wheel, and a plate. In some examples, when the first and second annular components are mechanically connected, the first and second annular components are configured to receive a tire and define a recess along an annular surface of the first and second annular components, the recess being configured to receive the plate. In addition, in some examples, when the plate is received in the recess, the plate inhibits relative rotation between the first annular component and the second annular component about the axis of rotation of the wheel.
    Type: Application
    Filed: December 5, 2016
    Publication date: June 7, 2018
    Inventors: Jon Champion, Elliot Conrad, Jonathan T. Beehler, Thomas Regnier
  • Publication number: 20160031259
    Abstract: In some examples, an aircraft wheel assembly includes an axle, a bearing assembly, and a hub defining a bearing bore. The bearing bore may be configured such that the dynamic radial and axial thrust bearing reactions between the axle and the hub results in a first reaction force FR applied to the hub, the first reaction force FR having a radial component, and a second reaction force FN applied to the hub, the second reaction force FN having both a radial and an axial component.
    Type: Application
    Filed: June 26, 2015
    Publication date: February 4, 2016
    Inventor: Jon Champion