Patents by Inventor Joshua V. Wood

Joshua V. Wood 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: 10295420
    Abstract: A deflection measurement assembly according to an example of the present disclosure includes, among other things, a nacelle arranged about an axis to define a flow path, a cable assembly arranged at least partially about the axis, and a transducer coupled to the cable assembly.
    Type: Grant
    Filed: April 11, 2016
    Date of Patent: May 21, 2019
    Assignee: UNITED TECHNOLOGIES CORPORATION
    Inventors: Joshua V. Wood, Michael Joseph Murphy, Justin R. Urban, Robert E. Malecki, William W. Rice, David W. Lamarre
  • Publication number: 20170292882
    Abstract: A deflection measurement assembly according to an example of the present disclosure includes, among other things, a nacelle arranged about an axis to define a flow path, a cable assembly arranged at least partially about the axis, and a transducer coupled to the cable assembly.
    Type: Application
    Filed: April 11, 2016
    Publication date: October 12, 2017
    Inventors: Joshua V. Wood, Michael Joseph Murphy, Justin R. Urban, Robert E. Malecki, William W. Rice, David W. Lamarre
  • Patent number: 9194330
    Abstract: A gas turbine engine includes a fan nacelle and a core nacelle spaced radially inwardly of the fan nacelle to define a bypass flowpath. The engine includes a scoop to direct air from the bypass flowpath into an engine core. The scoop is comprised of a first piece extending outwardly of an outer surface the core nacelle to define an air inlet and a second piece extending inwardly of the core nacelle to define an air outlet.
    Type: Grant
    Filed: July 31, 2012
    Date of Patent: November 24, 2015
    Assignee: United Technologies Corporation
    Inventors: Joshua V. Wood, Michael Joseph Murphy
  • Publication number: 20140037437
    Abstract: A gas turbine engine includes a fan nacelle and a core nacelle spaced radially inwardly of the fan nacelle to define a bypass flowpath. The engine includes a scoop to direct air from the bypass flowpath into an engine core. The scoop is comprised of a first piece extending outwardly of an outer surface the core nacelle to define an air inlet and a second piece extending inwardly of the core nacelle to define an air outlet.
    Type: Application
    Filed: July 31, 2012
    Publication date: February 6, 2014
    Inventors: Joshua V. Wood, Michael Joseph Murphy