Patents by Inventor David W. Jesse

David W. Jesse 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).

  • Window frame assembly for use in an aircraft and associated method of manufacture
    Patent number: 6689240
    Abstract: An IR window frame assembly for use within an aircraft is manufactured at a high temperature with both the window pane and the window frame of the window frame assembly having beveled surfaces. These beveled surfaces are placed in direct contact during manufacture. As a result, the window frame assembly maintains a low radar cross section (RCS) while allowing the window assembly to be small enough to conform with aerodynamic tolerances required in an aircraft.
    Type: Grant
    Filed: December 11, 2000
    Date of Patent: February 10, 2004
    Assignee: Lockheed Martin Corporation
    Inventor: David W. Jesse
  • Window frame assembly for use in an aircraft and associated method of manufacture
    Publication number: 20030034114
    Abstract: An IR window frame assembly for use within an aircraft is manufactured at a high temperature with both the window pane and the window frame of the window frame assembly having beveled surfaces. These beveled surfaces are placed in direct contact during manufacture. As a result, the window frame assembly maintains a low radar cross section (RCS) while allowing the window assembly to be small enough to conform with aerodynamic tolerances required in an aircraft.
    Type: Application
    Filed: December 11, 2000
    Publication date: February 20, 2003
    Inventor: David W. Jesse
  • Window frame assembly for use in an aircraft and associated method of manufacture
    Patent number: 6318035
    Abstract: An IR window frame assembly for use within an aircraft is manufactured at a high temperature with both the window pane and the window frame of the window frame assembly having beveled surfaces. These beveled surfaces are placed in direct contact during manufacture. As a result, the window frame assembly maintains a low radar cross section (RCS) while allowing the window assembly to be small enough to conform with aerodynamic tolerances required in an aircraft.
    Type: Grant
    Filed: June 1, 1999
    Date of Patent: November 20, 2001
    Assignee: Lockheed Martin Corporation
    Inventor: David W. Jesse