Patents by Inventor John Lafergola

John Lafergola 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: 11670827
    Abstract: The present disclosure refers to a waveguide electromechanical relay switch having a rotor with transmission paths and an axis of rotation parallel to the base plane combined with an actuator adapted to the configuration. A 4-pol switch design enables compensation of fault cases in a relatively shortened length of transmission line, reducing potential RF loss. In one embodiment, a 4-pol rotor includes an offset transmission path that enables crossing of another path on the same rotor, providing increased functionality and fault-case recovery.
    Type: Grant
    Filed: May 21, 2021
    Date of Patent: June 6, 2023
    Inventors: John Lafergola, Paul Jenkins
  • Publication number: 20210367312
    Abstract: The present disclosure refers to a waveguide electromechanical relay switch having a rotor with transmission paths and an axis of rotation parallel to the base plane combined with an actuator adapted to the configuration. A 4-pol switch design enables compensation of fault cases in a relatively shortened length of transmission line, reducing potential RF loss. In one embodiment, a 4-pol rotor includes an offset transmission path that enables crossing of another path on the same rotor, providing increased functionality and fault-case recovery.
    Type: Application
    Filed: May 21, 2021
    Publication date: November 25, 2021
    Inventors: John Lafergola, Paul Jenkins
  • Patent number: 7762499
    Abstract: A satellite thermal management system for dissipating excess heat generated within a satellite. The thermal management system includes a central platform for mounting heat dissipating components. A first thermal radiator panel and a second thermal radiator panel are mounted to the central platform. The first thermal radiator panel is arranged to face East when the satellite is in orbit. The second thermal radiator panel is arranged to face West when the satellite is in orbit. The first and second thermal radiator panels are thermally coupled to the central platform and are configured to radiate heat dissipated by the heat dissipating component mounted on the central platform.
    Type: Grant
    Filed: September 28, 2006
    Date of Patent: July 27, 2010
    Assignee: Lockheed Martin Corporation
    Inventors: David J. Hentosh, John Lafergola