Patents by Inventor Garry H. Boggan

Garry H. Boggan 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).

  • Galvanic isolation interface for high-speed data link for spacecraft electronics, and method of using same
    Patent number: 9385891
    Abstract: Under one aspect of the present invention, a structure for providing galvanically isolated communication between first and second spacecraft electronic components includes a semi-insulating substrate; an input port disposed on the substrate and configured to receive a signal from the first spacecraft electronic component; a coupling structure disposed on the substrate, coupled to the input port so as to receive the signal, and configured to provide an isolated replica of the received signal as an output; a signal conditioner disposed on the substrate, coupled to the coupling structure so as to receive the isolated replica of the received signal, and configured to condition the isolated replica; and an output port disposed on the substrate, coupled to the signal conditioner so as to receive the conditioned isolated replica, and configured to provide the conditioned isolated replica to the second spacecraft electronic component.
    Type: Grant
    Filed: August 13, 2015
    Date of Patent: July 5, 2016
    Assignee: The Aerospace Corporation
    Inventor: Garry H. Boggan
  • GALVANIC ISOLATION INTERFACE FOR HIGH-SPEED DATA LINK FOR SPACECRAFT ELECTRONICS, AND METHOD OF USING SAME
    Publication number: 20160013953
    Abstract: Under one aspect of the present invention, a structure for providing galvanically isolated communication between first and second spacecraft electronic components includes a semi-insulating substrate; an input port disposed on the substrate and configured to receive a signal from the first spacecraft electronic component; a coupling structure disposed on the substrate, coupled to the input port so as to receive the signal, and configured to provide an isolated replica of the received signal as an output; a signal conditioner disposed on the substrate, coupled to the coupling structure so as to receive the isolated replica of the received signal, and configured to condition the isolated replica; and an output port disposed on the substrate, coupled to the signal conditioner so as to receive the conditioned isolated replica, and configured to provide the conditioned isolated replica to the second spacecraft electronic component.
    Type: Application
    Filed: August 13, 2015
    Publication date: January 14, 2016
    Applicant: THE AEROSPACE CORPORATION
    Inventor: Garry H. Boggan
  • Galvanic isolation interface for high-speed data link for spacecraft electronics, and method of using same
    Patent number: 9143366
    Abstract: Under one aspect of the present invention, a structure for providing galvanically isolated communication between first and second spacecraft electronic components includes a semi-insulating substrate; an input port disposed on the substrate and configured to receive a signal from the first spacecraft electronic component; a coupling structure disposed on the substrate, coupled to the input port so as to receive the signal, and configured to provide an isolated replica of the received signal as an output; a signal conditioner disposed on the substrate, coupled to the coupling structure so as to receive the isolated replica of the received signal, and configured to condition the isolated replica; and an output port disposed on the substrate, coupled to the signal conditioner so as to receive the conditioned isolated replica, and configured to provide the conditioned isolated replica to the second spacecraft electronic component.
    Type: Grant
    Filed: September 7, 2012
    Date of Patent: September 22, 2015
    Assignee: The Aerospace Corporation
    Inventor: Garry H. Boggan
  • GALVANIC ISOLATION INTERFACE FOR HIGH-SPEED DATA LINK FOR SPACECRAFT ELECTRONICS, AND METHOD OF USING SAME
    Publication number: 20140070907
    Abstract: Under one aspect of the present invention, a structure for providing galvanically isolated communication between first and second spacecraft electronic components includes a semi-insulating substrate; an input port disposed on the substrate and configured to receive a signal from the first spacecraft electronic component; a coupling structure disposed on the substrate, coupled to the input port so as to receive the signal, and configured to provide an isolated replica of the received signal as an output; a signal conditioner disposed on the substrate, coupled to the coupling structure so as to receive the isolated replica of the received signal, and configured to condition the isolated replica; and an output port disposed on the substrate, coupled to the signal conditioner so as to receive the conditioned isolated replica, and configured to provide the conditioned isolated replica to the second spacecraft electronic component.
    Type: Application
    Filed: September 7, 2012
    Publication date: March 13, 2014
    Applicant: The Aerospace Corporation
    Inventor: Garry H. Boggan