Patents by Inventor David L. Hunn

David L. Hunn 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: 6843179
    Abstract: A penetrator includes a fore body comprising a pin and having a center of aerodynamic pressure forward of a center of gravity and a stabilizing portion comprising a material of lower density than that of the fore body and a plurality of outwardly extending fins for improving an aerodynamic stability of the projectile and defining a bore in which the pin is received for removably attaching the fore body thereto such that, when attached to the fore body, a center of gravity for the penetrator is forward of a center of aerodynamic pressure for the penetrator.
    Type: Grant
    Filed: September 20, 2002
    Date of Patent: January 18, 2005
    Assignee: Lockheed Martin Corporation
    Inventors: David L. Hunn, Johnny E. Banks, Carlton B. Cowan
  • Publication number: 20040055502
    Abstract: A penetrator includes a fore body comprising a pin and having a center of aerodynamic pressure forward of a center of gravity and a stabilizing portion comprising a material of lower density than that of the fore body and a plurality of outwardly extending fins for improving an aerodynamic stability of the projectile and defining a bore in which the pin is received for removably attaching the fore body thereto such that, when attached to the fore body, a center of gravity for the penetrator is forward of a center of aerodynamic pressure for the penetrator.
    Type: Application
    Filed: September 20, 2002
    Publication date: March 25, 2004
    Applicant: Lockheed Martin Corporation
    Inventors: David L. Hunn, Johnny E. Banks, Carlton B. Cowan
  • Publication number: 20040055501
    Abstract: A penetrator includes a fore body having a center of aerodynamic pressure forward of a center of gravity and a stabilizing portion removably attached to the fore body such that, when attached to the fore body, a center of gravity for the penetrator is forward of a center of aerodynamic pressure for the penetrator. A method of using a penetrator includes propelling the penetrator toward a first target, penetrating the first target with a fore body of the penetrator, and detaching a stabilizing portion of the penetrator from the fore body. The method further includes impacting the second target with the fore body.
    Type: Application
    Filed: September 20, 2002
    Publication date: March 25, 2004
    Inventors: David L. Hunn, Johnny E. Banks, Carlton B. Cowan
  • Publication number: 20030064606
    Abstract: A low-density electrically-conductive thermal insulator is a coupling of a polymer-based thermally-insulating material with an open-celled electrically-conductive base material defining a plurality of interconnected cells throughout. The open-celled, electrically-conductive base material is preferably an open-celled metallic foam material formed by an interconnected plurality of electrically-conductive ligaments. The electrically-conductive base material may be first formed into a desired shape or structure, coated such that cells in the electrically-conductive base structure are substantially filled with the insulating material, and then cured to solidify the insulating material. The electrically-conductive thermal insulator provides thermal protection while providing electrical conductivity.
    Type: Application
    Filed: September 28, 2001
    Publication date: April 3, 2003
    Applicant: LOCKHEED MARTIN CORPORATION
    Inventor: David L. Hunn
  • Patent number: 6472601
    Abstract: An electrically-conductive, thermally-insulating structure includes a thermally-insulating layer having a thermal conductivity of no more than about 3.5×10−3 W/hr·cm·°K and an electrically-conductive layer, applied to the thermally-insulating layer, which has an electrical resistivity of no more than about five ohms at 700° C. The thermally-insulating layer can include a plurality of microballoons to decrease the density of the thermally-insulating layer.
    Type: Grant
    Filed: January 30, 2001
    Date of Patent: October 29, 2002
    Assignee: Lockheed Martin Corporation
    Inventors: David L. Hunn, Barry W. Bartos
  • Publication number: 20020144836
    Abstract: An electrically-conductive, thermally-insulating structure includes a thermally-insulating layer having a thermal conductivity of no more than about 3.5×10−3 W/hr·cm·° K and an electrically-conductive layer, applied to the thermally-insulating layer, which has an electrical resistivity of no more than about five ohms at 700° C. The thermally-insulating layer can comprise a plurality of microballoons to decrease the density of the thermally-insulating layer.
    Type: Application
    Filed: January 15, 2002
    Publication date: October 10, 2002
    Applicant: LOCKHEED MARTIN CORPORATION
    Inventors: David L. Hunn, Barry W. Bartos
  • Publication number: 20020129964
    Abstract: An electrically-conductive, thermally-insulating structure includes a thermally-insulating layer having a thermal conductivity of no more than about 3.5×10−3 W/hr·cm·°K. and an electrically-conductive layer, applied to the thermally-insulating layer, which has an electrical resistivity of no more than about five ohms at 700° C. The thermally-insulating layer can comprise a plurality of microballoons to decrease the density of the thermally-insulating layer.
    Type: Application
    Filed: January 30, 2001
    Publication date: September 19, 2002
    Applicant: LOCKHEED MARTIN CORPORATION
    Inventors: David L. Hunn, Barry W. Bartos