Patents by Inventor Joseph P. Nipper

Joseph P. Nipper 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).

  • Publication number: 20240022027
    Abstract: A connector is provided and includes one or more radio frequency (RF) signal pins, ground pins arranged in a ring-shape around the one or more RF signal pins, a ground pin supporting mold formed about the ground pins and defining a borehole around the one or more RF signal pins and a dielectric mold formed in the borehole about the one or more RF signal pins and about the ground pin supporting mold.
    Type: Application
    Filed: July 18, 2022
    Publication date: January 18, 2024
    Inventors: Ian E. Nord, Joseph P. Nipper, Mikel J. White
  • Patent number: 10501184
    Abstract: An aft pivot assembly can include a mount device securable to an aft portion of a payload of an aircraft for facilitating release of the payload. The aft pivot assembly can include a shaft operable with the mount device and a release component, the shaft being rotatable about multiple shaft axes relative to the mount device so as to either minimize or eliminate carriage loads about the aft portion, while reacting jettison loads during a jettison event or phase. The rotation of the shaft about its shaft axes can further be limited via a limit device. As the payload transitions from a carriage phase to a jettison phase, the shaft moves in multiple degrees of freedom and in multiple axes relative to the mount device.
    Type: Grant
    Filed: June 13, 2016
    Date of Patent: December 10, 2019
    Assignee: Raytheon Company
    Inventors: Joseph P. Nipper, Zachary Scott Zutavern, Arthur J. Mathews
  • Patent number: 9979097
    Abstract: The present disclosure is directed toward methods for forming an expanding lattice notch array antenna that includes a plurality of notch antenna elements extending from a surface of a base plate. The properties and dimensions of the notch antenna elements can be manipulated in order to provide an expanding notch array antenna whereby an area of a base portion of the array is different from an area of a top portion of the array, without increasing an overall height of the notch array antenna. The method includes coupling a first plurality of notch elements to a first surface of a base plate in a first orientation, expanding a second plurality of notch elements from a first state to a second state and coupling the second plurality of notch elements in the second state to the first surface of the base plate in a second orientation.
    Type: Grant
    Filed: March 16, 2016
    Date of Patent: May 22, 2018
    Assignee: Raytheon Company
    Inventor: Joseph P. Nipper
  • Publication number: 20170271782
    Abstract: The present disclosure is directed toward methods for forming an expanding lattice notch array antenna that includes a plurality of notch antenna elements extending from a surface of a base plate. The properties and dimensions of the notch antenna elements can be manipulated in order to provide an expanding notch array antenna whereby an area of a base portion of the array is different from an area of a top portion of the array, without increasing an overall height of the notch array antenna. The method includes coupling a first plurality of notch elements to a first surface of a base plate in a first orientation, expanding a second plurality of notch elements from a first state to a second state and coupling the second plurality of notch elements in the second state to the first surface of the base plate in a second orientation.
    Type: Application
    Filed: March 16, 2016
    Publication date: September 21, 2017
    Applicant: Raytheon Company
    Inventor: Joseph P. Nipper
  • Publication number: 20170240282
    Abstract: An aft pivot assembly can include a mount device securable to an aft portion of a payload of an aircraft for facilitating release of the payload. The aft pivot assembly can include a shaft operable with the mount device and a release component, the shaft being rotatable about multiple shaft axes relative to the mount device so as to either minimize or eliminate carriage loads about the aft portion, while reacting jettison loads during a jettison event or phase. The rotation of the shaft about its shaft axes can further be limited via a limit device. As the payload transitions from a carriage phase to a jettison phase, the shaft moves in multiple degrees of freedom and in multiple axes relative to the mount device.
    Type: Application
    Filed: June 13, 2016
    Publication date: August 24, 2017
    Inventors: Joseph P. Nipper, Zachary Scott Zutavern, Arthur J. Mathews